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@AIRBUSA330
AIRPLANE CHARACTERISTICSFOR AIRPORT PLANNING
AC
The content of this document is the property of Airbus.It is supplied in confidence and commercial security on its contents must be maintained.It must not be used for any purpose other than that for which it is supplied, nor mayinformation contained in it be disclosed to unauthorized persons.It must not be reproduced in whole or in part without permission in writing from the owners ofthe copyright. Requests for reproduction of any data in this document and the media authorizedfor it must be addressed to Airbus.
© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.Customer Services
Technical Data Support and Services31707 Blagnac Cedex
FRANCE
Issue: Jan 01/93 Rev: Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
HIGHLIGHTS
Revision No. 19 - Jan 01/11
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 2
Section 2-1
Subject 2-1-1
General Airplane Characteristics Data R PART EFFECTIVITYADDED/REVISED/DELETED
General Airplane Characteristics Data R
CHAPTER 4
Section 4-2
Subject 4-2-0
FIGURE Turning Radii - All Models R ILLUSTRATION REVISEDILLUSTRATION REVISED
FIGURE Turning Radii - Steady StateTurning Radii
R ILLUSTRATION REVISED ANDCOMPLETEDILLUSTRATION REVISED
FIGURE Turning Radii - Steady StateTurning Radii
R ILLUSTRATION REVISED ANDCOMPLETEDILLUSTRATION REVISED
Section 4-3
Subject 4-3-0
Minimum Turning Radii R
FIGURE Minimum Turning Radii -Minimum Turning Radii
R ILLUSTRATION REVISED ANDCOMPLETEDILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Minimum Turning Radii -Minimum Turning Radii
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
Section 4-5
Subject 4-5-1
135˚ Turn - Runway to Taxiway R
HIGHLIGHTSPage 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE 135˚ Turn - Runway to Taxiway- Judgemental Oversteer Method
R ILLUSTRATION REVISED
FIGURE 135˚ Turn - Runway to Taxiway- Cockpit Over Centerline Method
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
FIGURE 135˚ Turn - Runway to Taxiway- Judgemental Oversteer Method
R ILLUSTRATION REVISED
FIGURE 135˚ Turn - Runway to Taxiway- Cockpit Over Centerline Method
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
Subject 4-5-2
90˚ Turn - Runway to Taxiway R DESCRIPTION TITLE UPDATED
FIGURE 90˚ Turn - Runway to Taxiway -Judgemental Oversteer Method
R ILLUSTRATION REVISEDILLUSTRATION REVISED
FIGURE 90˚ Turn - Runway to Taxiway -Cockpit Over Centerline Method
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
FIGURE 90˚ Turn - Runway to Taxiway -Judgemental Oversteer Method
R ILLUSTRATION REVISEDILLUSTRATION REVISED
FIGURE 90˚ Turn - Runway to Taxiway -Cockpit Over Centerline Method
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
Subject 4-5-3
180˚ Turn on a Runway N
FIGURE 180˚ Turn on a Runway - 180˚Turn on a Runway
N ILLUSTRATION ADDED
FIGURE 180˚ Turn on a Runway - 180˚Turn on a Runway
N ILLUSTRATION ADDED
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway R
FIGURE 135˚ Turn - Taxiway to Taxiway- Judgemental Oversteer Method
R ILLUSTRATION REVISED
FIGURE 135˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
FIGURE 135˚ Turn - Taxiway to Taxiway- Judgemental Oversteer Method
R ILLUSTRATION REVISED
FIGURE 135˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
HIGHLIGHTSPage 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway R
FIGURE 90˚ Turn - Taxiway to Taxiway- Judgemental Oversteer Method
R ILLUSTRATION REVISED
FIGURE 90˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
FIGURE 90˚ Turn - Taxiway to Taxiway- Judgemental Oversteer Method
R ILLUSTRATION REVISED
FIGURE 90˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
Section 4-6
Subject 4-6-0
Runway Holding Bay (Apron) R
FIGURE Runway Holding Bay (Apron) -Runway Holding Bay (Apron)
R ILLUSTRATION REVISEDILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
CHAPTER 5
Section 5-4
Subject 5-4-6
Fuel System R
Section 5-8
Subject 5-8-0
Ground Towing Requirements R
FIGURE Ground Towing Requirements -Ground Towing Requirements
R ILLUSTRATION REVISED
CHAPTER 7
Section 7-1
Subject 7-1-0
General Information R
Section 7-2
Subject 7-2-0
HIGHLIGHTSPage 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Landing Gear Footprint R NOTE AMENDED
FIGURE Landing Gear Footprint - MTOW192 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW202 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW210 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW220 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW230 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW233 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW227 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW233 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW184 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW205 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW205 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW205 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW212 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW212 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW212 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW215 000 kg
R TABLE REVISED
HIGHLIGHTSPage 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Landing Gear Footprint - MTOW217 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW217 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW218 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW230 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW230 000 kg
R TABLE REVISED
FIGURE Landing Gear Footprint - MTOW233 000 kg
R TABLE REVISED
Section 7-4 R
Subject 7-4-0
Landing Gear Loading on Pavement R
Subject 7-4-1
FIGURE Landing Gear Loading onPavement - MTOW 192 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 210 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 233 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 233 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 227 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 233 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 184 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 212 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 215 000 kg
R GRAPHIC REVISED
HIGHLIGHTSPage 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Landing Gear Loading onPavement - MTOW 215 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 217 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 217 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 218 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 230 000 kg
R GRAPHIC REVISED
FIGURE Landing Gear Loading onPavement - MTOW 233 000 kg
R GRAPHIC REVISED
Subject 07-04-02 D
Subject 07-04-03 D
Section 7-5
Subject 7-5-0
Flexible Pavement Requirements - USArmy Corps of Engineers Design Method
R
Subject 7-5-1
FIGURE Flexible Pavement Requirements- MTOW 233 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 233 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 212 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 218 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 230 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 233 000 kg
R
Section 7-6
Subject 7-6-0
HIGHLIGHTSPage 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Flexible Pavement Requirements - LCNConversion
R
Subject 7-6-1
FIGURE Flexible Pavement Requirements- MTOW 233 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 233 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 212 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 218 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 230 000 kg
R
FIGURE Flexible Pavement Requirements- MTOW 233 000 kg
R
Section 7-7
Subject 7-7-0
Rigid Pavement Requirements - PortlandCement Association Design Method
R
Subject 7-7-1
FIGURE Rigid Pavement Requirements -MTOW 233 000 kg
R
FIGURE Rigid Pavement Requirements -MTOW 233 000 kg
R
FIGURE Rigid Pavement Requirements -MTOW 212 000 kg
R
FIGURE Rigid Pavement Requirements -MTOW 218 000 kg
R
FIGURE Rigid Pavement Requirements -MTOW 230 000 kg
R
FIGURE Rigid Pavement Requirements -MTOW 233 000 kg
R
Section 7-8
Subject 7-8-0
HIGHLIGHTSPage 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Rigid Pavement Requirements - LCNConversion
R
Subject 7-8-2
FIGURE Rigid Pavement RequirementsLCN - MTOW 233 000 kg
R
FIGURE Rigid Pavement RequirementsLCN - MTOW 233 000 kg
R
FIGURE Rigid Pavement RequirementsLCN - MTOW 212 000 kg
R
FIGURE Rigid Pavement RequirementsLCN - MTOW 218 000 kg
R
FIGURE Rigid Pavement RequirementsLCN - MTOW 230 000 kg
R
FIGURE Rigid Pavement RequirementsLCN - MTOW 233 000 kg
R
Subject 7-8-3
Radius of Relative Stiffness (Other valuesof ”E” and ”µ”)
R
Section 7-9
Subject 7-9-0
ACN/PCN Reporting System - Flexibleand Rigid Pavements
R
Subject 7-9-1
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 192 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 202 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 210 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 220 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 230 000 kg
R TEXT OF ILLUSTRATION REVISED
HIGHLIGHTSPage 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 233 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 227 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 233 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 184 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 205 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 212 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 215 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 217 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 218 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 230 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Flexible Pavement - MTOW 233 000 kg
R TEXT OF ILLUSTRATION REVISED
Subject 7-9-2
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 192 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 202 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 210 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 220 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 230 000 kg
R TEXT OF ILLUSTRATION REVISED
HIGHLIGHTSPage 9
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 233 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 227 000 kg
R TEXT OF ILLUSTRATION REVISED,GRAPHIC REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 233 000 kg
R TEXT OF ILLUSTRATION REVISED,GRAPHIC REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 184 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 205 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 212 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 215 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 217 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 218 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 230 000 kg
R TEXT OF ILLUSTRATION REVISED
FIGURE Aircraft Classification Number --Rigid Pavement - MTOW 233 000 kg
R TEXT OF ILLUSTRATION REVISED
HIGHLIGHTSPage 10
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 19 - Jan 01/11
CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 1
Subject 1-1-0
Purpose Feb 01/09
Subject 1-2-0
Introduction Jan 01/10
CHAPTER 2
Subject 2-1-0
General Airplane Characteristics Feb 01/09
Subject 2-1-1
General Airplane Characteristics Data R Jan 01/11
General Airplane Characteristics Data R Jan 01/11
Subject 2-2-0
General Airplane Dimensions May 01/07
FIGURE General Airplane Dimensions - General Airplane Dimensions Feb 01/09
FIGURE General Airplane Dimensions - General Airplane Dimensions Feb 01/09
General Airplane Dimensions Feb 01/09
FIGURE General Airplane Dimensions - General Airplane Dimensions Feb 01/09
Subject 2-3-0
Ground Clearances Feb 01/09
FIGURE Ground Clearances - Ground Clearances May 01/07
FIGURE Ground Clearances - Ground Clearances May 01/07
Ground Clearances Feb 01/09
FIGURE Ground Clearances - Ground Clearances MRW 227 900 kg Jan 01/10
FIGURE Ground Clearances - Ground Clearances MRW 233 900 kg Jan 01/10
Subject 2-4-0
Interior Arrangements Jan 01/10
L.E.C.Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Subject 2-4-1
Typical Configuration May 01/07
FIGURE Typical Configuration - Typical Configuration May 01/07
FIGURE Typical Configuration - Typical Configuration May 01/07
Subject 2-5-0
Passenger Compartment Cross-section May 01/07
FIGURE Passenger Compartment Cross-section - PassengerCompartment Cross-section
May 01/07
Subject 2-6-0
Cargo Compartment Jan 01/10
Subject 2-6-1
Lower Deck Cargo Compartments Jan 01/10
FIGURE Lower Deck Cargo Compartments - Lower Deck CargoCompartments
Feb 01/09
FIGURE Loading Combinations - Loading Combinations Feb 01/09
Subject 2-6-2
Main Deck Cargo Compartments (Loading combinations) Feb 01/09
FIGURE Main Deck Cargo Compartments - Loading combinations Feb 01/09
FIGURE Main Deck Cargo Compartments - Loading combinations Feb 01/09
FIGURE Main Deck Cargo Compartments - Loading combinations Feb 01/09
Subject 2-6-3
Main and Lower Deck Cross-sections Feb 01/09
FIGURE Main and Lower Deck Cross-sections - Main and Lower DeckCross-sections
Feb 01/09
Subject 2-7-0
Doors Clearances Feb 01/09
Subject 2-7-1
Forward Passenger / Crew Door Feb 01/09
FIGURE Forward Passenger / Crew Doors - Forward Passenger /Crew Doors
May 01/07
L.E.C.Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Forward Passenger / Crew Doors - Forward Passenger /Crew Doors
Feb 01/09
Subject 2-7-2
Mid Passenger / Crew Door May 01/07
FIGURE Mid Passenger / Crew Door - Mid Passenger / Crew Door May 01/07
Subject 2-7-3
Emergency Exits May 01/07
FIGURE Emergency Exits - Emergency Exits May 01/07
Subject 2-7-4
Aft Passenger / Crew Doors May 01/07
FIGURE Aft Passenger / Crew Doors - Aft Passenger / Crew Doors May 01/07
Subject 2-7-5
Forward Cargo Compartment Doors May 01/07
FIGURE Forward Cargo Compartment Doors - Forward CargoCompartment Doors
May 01/07
Forward Cargo Compartment Doors Feb 01/09
FIGURE Forward Cargo Compartment Doors - Forward CargoCompartment Doors
Feb 01/09
FIGURE Forward Cargo Compartment Doors - Forward CargoCompartment Doors
Feb 01/09
Subject 2-7-6
Aft Cargo Compartment Doors Feb 01/09
FIGURE Aft Cargo Compartment Doors - Aft Cargo CompartmentDoors
Feb 01/09
FIGURE Aft Cargo Compartment Doors - Aft Cargo CompartmentDoors
Feb 01/09
FIGURE Aft Cargo Compartment Doors - Aft Cargo CompartmentDoors
Feb 01/09
Subject 2-7-7
Bulk Cargo Compartment Doors May 01/07
FIGURE Bulk Cargo Compartment Doors - Bulk Cargo CompartmentDoors
May 01/07
L.E.C.Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Bulk Cargo Compartment Doors Feb 01/09
FIGURE Bulk Cargo Compartment Doors - Bulk Cargo CompartmentDoors
Feb 01/09
Subject 2-7-8
Main Landing Gear Doors May 01/07
FIGURE Main Landing Gear Doors - Main Landing Gear Doors May 01/07
Main Landing Gear Doors Feb 01/09
FIGURE Main Landing Gear Doors - Main Landing Gear Doors Feb 01/09
Subject 2-7-9
Radome Feb 01/09
FIGURE Radome - Radome Feb 01/09
Subject 2-7-10
APU and Nose Landing Gear Doors May 01/07
FIGURE APU and Nose Landing Gear Doors - APU and Nose LandingGear Doors
May 01/07
APU and Nose Landing Gear Doors Feb 01/09
FIGURE APU and Nose Landing Gear Doors - APU and Nose LandingGear Doors
Feb 01/09
CHAPTER 3
Subject 3-1-0
General Information Jan 01/10
Subject 3-2-0
Payload / Range Feb 01/09
Subject 3-2-1
ISA Conditions May 01/07
FIGURE PAYLOAD / RANGE - PW 4000 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - RR TRENT 700 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - GE CF6-80E1 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - PW 4000 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - RR TRENT 700 Series Engine Feb 01/09
L.E.C.Page 4
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE PAYLOAD / RANGE - GE CF6-80E1 Series Engine Feb 01/09
ISA Conditions Feb 01/09
FIGURE PAYLOAD / RANGE - RR TRENT 700 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - RR TRENT 700 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - PW 4000 Series Engine Feb 01/09
FIGURE PAYLOAD / RANGE - PW 4000 Series Engine Feb 01/09
Subject 3-3-0
FAR / JAR Takeoff Weight Limitation Feb 01/09
Subject 3-3-1
FAR / JAR Takeoff Weight Limitation Feb 01/09
FIGURE Takeoff Weight Limitation - ISA Conditions - PW 4000Series Engine
Feb 01/09
FIGURE Takeoff Weight Limitation - ISA Conditions - RR TRENT700 Series Engine
Feb 01/09
FIGURE Takeoff Weight Limitation - ISA Conditions - GE CF6-80E1Series Engine
Feb 01/09
Subject 3-3-2
ISA +15 ˚C (ISA +27 ˚F) Conditions Jan 01/10
FIGURE FAR / JAR Takeoff Weight Limitation - ISA +15˚C (ISA+27˚F) Conditions - PW 4000 Series Engine
Jan 01/10
FIGURE FAR / JAR Takeoff Weight Limitation - ISA +15˚C (ISA+27˚F) Conditions - RR TRENT 700 Series Engine
Jan 01/10
FIGURE FAR / JAR Takeoff Weight Limitation - ISA +15˚C (ISA+27˚F) Conditions - GE CF6-80E1 Series Engine
Jan 01/10
Subject 3-4-0
Landing Field Length Feb 01/09
Subject 3-4-1
ISA Conditions All series engine Jan 01/10
FIGURE FAR / JAR Landing Field Length - ISA Conditions - PW4000 Series Engine
Jan 01/10
L.E.C.Page 5
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE FAR / JAR Landing Field Length - ISA Conditions - RRTRENT 700 Series Engine
Jan 01/10
FIGURE FAR / JAR Landing Field Length - ISA Conditions - GECF6-80E1 Series Engine
Jan 01/10
Subject 3-5-0
Final Approach Speed Feb 01/09
Subject 3-5-1
Final Approach Speed Feb 01/09
FIGURE Final Approach Speed - PW 4000 Series Engine Feb 01/09
FIGURE Final Approach Speed - RR TRENT 700 Series Engine Feb 01/09
FIGURE Final Approach Speed - GE CF6-80E1 Series Engine Feb 01/09
CHAPTER 4
Subject 4-1-0
General Information Feb 01/09
Subject 4-2-0
Turning Radii Feb 01/09
FIGURE Turning Radii - All Models R Jan 01/11
FIGURE Turning Radii - Steady State Turning Radii R Jan 01/11
FIGURE Turning Radii - Steady State Turning Radii R Jan 01/11
Subject 4-3-0
Minimum Turning Radii R Jan 01/11
FIGURE Minimum Turning Radii - Minimum Turning Radii R Jan 01/11
FIGURE Minimum Turning Radii - Minimum Turning Radii N Jan 01/11
Subject 4-4-0
Visibility from Cockpit in Static Position. Feb 01/09
FIGURE Visibility from Cockpit in Static Position - Visibility fromCockpit in Static Position
May 01/07
FIGURE Visibility from Cockpit in Static Position - Visibility fromCockpit in Static Position
Feb 01/09
Subject 4-5-0
L.E.C.Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Runway and Taxiway Turn Paths Jan 01/10
Subject 4-5-1
135˚ Turn - Runway to Taxiway R Jan 01/11
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteerMethod
R Jan 01/11
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
N Jan 01/11
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteerMethod
R Jan 01/11
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
N Jan 01/11
Subject 4-5-2
90˚ Turn - Runway to Taxiway R Jan 01/11
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental OversteerMethod
R Jan 01/11
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
N Jan 01/11
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental OversteerMethod
R Jan 01/11
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
N Jan 01/11
Subject 4-5-3
180˚ Turn on a Runway N Jan 01/11
FIGURE 180˚ Turn on a Runway - 180˚ Turn on a Runway N Jan 01/11
FIGURE 180˚ Turn on a Runway - 180˚ Turn on a Runway N Jan 01/11
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway R Jan 01/11
FIGURE 135˚ Turn - Taxiway to Taxiway - Judgemental OversteerMethod
R Jan 01/11
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
N Jan 01/11
FIGURE 135˚ Turn - Taxiway to Taxiway - Judgemental OversteerMethod
R Jan 01/11
L.E.C.Page 7
Jan 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
N Jan 01/11
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway R Jan 01/11
FIGURE 90˚ Turn - Taxiway to Taxiway - Judgemental OversteerMethod
R Jan 01/11
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
N Jan 01/11
FIGURE 90˚ Turn - Taxiway to Taxiway - Judgemental OversteerMethod
R Jan 01/11
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
N Jan 01/11
Subject 4-6-0
Runway Holding Bay (Apron) R Jan 01/11
FIGURE Runway Holding Bay (Apron) - Runway Holding Bay(Apron)
R Jan 01/11
Subject 4-7-0
Airplane Parking Feb 01/09
FIGURE Airplane Parking - Steering Geometry May 01/07
FIGURE Airplane Parking - Steering Geometry May 01/07
FIGURE Airplane Parking - Minimum Parking Space Requirements May 01/07
FIGURE Airplane Parking - Steering Geometry Feb 01/09
FIGURE Airplane Parking - Steering Geometry Feb 01/09
FIGURE Airplane Parking - Minimum Parking Space Requirements Feb 01/09
CHAPTER 5
Subject 5-0-0
TERMINAL SERVICING Jan 01/10
Subject 5-1-0
Airplane Servicing Arrangements Jan 01/10
Airplane Servicing Arrangements Jan 01/10
Subject 5-1-1
L.E.C.Page 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Symbols Used on Servicing Diagrams Jan 01/10
Subject 5-1-2
Loading (Open Apron) Jan 01/10
FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(Open Apron)
Jan 01/10
FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(Open Apron)
Jan 01/10
Loading (Open Apron) Jan 01/10
FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(Open Apron)
Jan 01/10
Subject 5-1-3
Loading (Passenger Bridge) Jan 01/10
FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(gate area)
Jan 01/10
FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(gate area)
Jan 01/10
Subject 5-2-0
Terminal Operations - Full Servicing Turn Round Charts Jan 01/10
Subject 5-2-1
Full Servicing Turn Round Charts Jan 01/10
FIGURE Full Servicing Turn Round Charts - Turn Round Time 60min.
Jan 01/10
FIGURE Full Servicing Turn Round Charts - Turn Round Time 64min.
Jan 01/10
Full Servicing Turn Round Charts Jan 01/10
FIGURE Full Servicing Turn Round Charts - Turn Round Time 62min.
Jan 01/10
Subject 5-3-0
Terminal Operations - Transit Turn Round Charts Jan 01/10
Subject 5-3-1
Transit Turn Round Charts Jan 01/10
FIGURE Transit Turn Round Charts - Turn Round Time 44 min. Jan 01/10
L.E.C.Page 9
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Transit Turn Round Charts - Turn Round Time 48 min. Jan 01/10
Subject 5-4-0
Ground Service Connections Jan 01/10
Subject 5-4-1
Ground Service Connections Layout May 01/07
FIGURE Ground Service Connections - Ground Service Connections May 01/07
Ground Service Connections Layout Feb 01/09
FIGURE Ground Service Connections - Ground Service Connections Feb 01/09
Subject 5-4-2
Grounding Points Feb 01/09
FIGURE Ground Service Connections - Grounding Points Feb 01/09
FIGURE Ground Service Connections - Grounding Points Feb 01/09
Subject 5-4-3
Hydraulic System Jan 01/10
Subject 5-4-4
Electrical System Jan 01/10
Subject 5-4-5
Oxygen System Feb 01/09
Subject 5-4-6
Fuel System R Jan 01/11
Subject 5-4-7
Pneumatic System Feb 01/09
Subject 5-4-8
Potable Water System Jan 01/10
Subject 5-4-9
Oil System Feb 01/09
FIGURE Ground Service Connections - Engine Oil Tank - PW 4000series engine
Feb 01/09
FIGURE Ground Service Connections - Engine Oil Tank - RR Trent700 series engine
Feb 01/09
L.E.C.Page 10
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Ground Service Connections - Engine Oil Tank - GECF6-80E1 series engine
May 01/07
FIGURE Ground Service Connections - IDG Oil Tank - PW 4000series engine
Feb 01/09
FIGURE Ground Service Connections - IDG Oil Tank - RR Trent 700series engine
Feb 01/09
FIGURE Ground Service Connections - IDG Oil Tank - GE CF6-80E1series engine
May 01/07
APU Oil System Jan 01/10
FIGURE Ground Service Connections - APU Oil Tank Jan 01/10
Subject 5-4-10
Vacuum Toilet System Jan 01/10
Subject 5-5-0
Engine Starting Pneumatic Requirements Jan 01/10
Subject 5-5-1
Ambient Temperature - 40˚C (- 40˚F) and - 55˚C (- 67˚F) Feb 01/09
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature - 40˚C (- 40˚F) -- PW 4000 series engine
Feb 01/09
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature - 55˚C (- 67˚F) -- RR Trent 700 series engine
Feb 01/09
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature - 40˚C (- 40˚F) -- GE CF6-80E1 series engine
May 01/07
Subject 5-5-2
Ambient Temperature +0˚C (+32˚F) and +15˚C (+59˚F) Jan 01/10
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature +15˚C (+59˚F) -- PW 4000 series engine
Jan 01/10
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature 0˚C (+32˚F) -- RR Trent 700 series engine
Jan 01/10
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature +15˚C (+59˚F) -- GE CF6-80E1 series engine
Jan 01/10
Subject 5-5-3
Ambient Temperature Upper +38˚C (+100˚F) Feb 01/09
L.E.C.Page 11
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature +55˚C (+131˚F) -- PW 4000 series engine
Jan 01/10
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature +40˚C (+104˚F) -- RR Trent 700 series engine
Jan 01/10
FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature +50˚C (122˚F) -- GE CF6-80E1 series engine
Jan 01/10
Subject 5-6-0
Ground Pneumatic Power Requirements Jan 01/10
Subject 5-6-1
Heating Feb 01/09
FIGURE Ground Pneumatic Power Requirements - Heating Feb 01/09
Subject 5-6-2
Cooling Feb 01/09
FIGURE Ground Pneumatic Power Requirements - Cooling Feb 01/09
Subject 5-7-0
Preconditioned Airflow Requirements Jan 01/10
FIGURE Preconditioned Airflow Requirements - PreconditionedAirflow Requirements
Feb 01/09
FIGURE Preconditioned Airflow Requirements - PreconditionedAirflow Requirements
Feb 01/09
Subject 5-8-0
Ground Towing Requirements R Jan 01/11
FIGURE Ground Towing Requirements - Ground TowingRequirements
R Jan 01/11
FIGURE Ground Towing Requirements - Typical tow barconfiguration 1
Jan 01/10
FIGURE Ground Towing Requirements - Typical tow barconfiguration 2
Jan 01/10
FIGURE Ground Towing Requirements - Maximum Extension of theNLG Shock Absorber
Jan 01/10
CHAPTER 6
L.E.C.Page 12
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Subject 6-1-0
Engine Exhaust Velocities and Temperatures Jan 01/10
Subject 6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power Feb 01/09
FIGURE Engine Exhaust Velocities - Ground Idle Power - PW 4000series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Ground Idle Power - RR Trent700 series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Ground Idle Power - GECF6-80E1 series engine
Jan 01/10
Subject 6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power Jan 01/10
FIGURE Engine Exhaust Temperatures - Ground Idle Power - PW4000 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Ground Idle Power - RRTrent 700 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Ground Idle Power - GECF6-80E1 series engine
Jan 01/10
Subject 6-1-3
Engine Exhaust Velocities Contours - Breakaway Power Feb 01/09
FIGURE Engine Exhaust Velocities - Breakaway Power - PW 4000series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Breakaway Power - RR Trent700 series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Breakaway Power - GECF6-80E1 series engine
Jan 01/10
Subject 6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power Jan 01/10
FIGURE Engine Exhaust Temperatures - Breakaway Power - PW4000 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Breakaway Power - RRTrent 700 series engine
Feb 01/09
L.E.C.Page 13
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Exhaust Temperatures - Breakaway Power - GECF6-80E1 series engine
Jan 01/10
Subject 6-1-5
Engine Exhaust Velocities Contours - Takeoff Power Feb 01/09
FIGURE Engine Exhaust Velocities - Takeoff Power - PW 4000 seriesengine
Feb 01/09
FIGURE Engine Exhaust Velocities - Takeoff Power - RR Trent 700series engine
Feb 01/09
FIGURE Engine Exhaust Velocities - Takeoff Power - GE CF6-80E1series engine
May 01/07
Subject 6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power Feb 01/09
FIGURE Engine Exhaust Temperatures - Takeoff Power - PW 4000series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Takeoff Power - RR Trent700 series engine
Feb 01/09
FIGURE Engine Exhaust Temperatures - Takeoff Power - GECF6-80E1 series engine
May 01/07
Subject 6-2-0
Airport and Community Noise Data Feb 01/09
Subject 6-2-1
Noise Data Feb 01/09
FIGURE Airport and Community Noise - PW 4000 series engine Feb 01/09
FIGURE Airport and Community Noise - RR Trent 700 series engine Feb 01/09
FIGURE Airport and Community Noise - GE CF6-80E1 series engine May 01/07
Subject 6-3-0
Danger Areas of Engines Jan 01/10
Subject 6-3-1
Ground Idle Power Feb 01/09
FIGURE Danger Areas of Engines - PW 4000 series engine Feb 01/09
FIGURE Danger Areas of Engines - RR Trent 700 series engine Feb 01/09
L.E.C.Page 14
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Danger Areas of Engines - GE CF6-80E1 series engine May 01/07
Subject 6-3-2
Breakaway Power Feb 01/09
FIGURE Danger Areas of Engines - PW 4000 series engine Feb 01/09
FIGURE Danger Areas of Engines - RR Trent 700 series engine Feb 01/09
FIGURE Danger Areas of Engines - GE CF6-80E1 series engine May 01/07
Subject 6-3-3
Takeoff Power Feb 01/09
FIGURE Danger Areas of Engines - PW 4000 series engine Feb 01/09
FIGURE Danger Areas of Engines - RR Trent 700 series engine Feb 01/09
FIGURE Danger Areas of Engines - GE CF6-80E1 series engine May 01/07
Subject 6-4-0
APU Exhaust Velocities and Temperatures Jan 01/10
Subject 6-4-1
APU - GARRETT Feb 01/09
FIGURE Exhaust Velocities and Temperatures - APU -- GARRETTGTCP 331-350
Feb 01/09
CHAPTER 7
Subject 7-1-0
General Information R Jan 01/11
Subject 7-2-0
Landing Gear Footprint R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 192 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 202 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 210 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 220 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 230 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 233 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 227 000 kg R Jan 01/11
L.E.C.Page 15
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Landing Gear Footprint - MTOW 233 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 184 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 205 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 205 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 205 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 212 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 212 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 212 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 215 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 217 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 217 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 218 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 230 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 230 000 kg R Jan 01/11
FIGURE Landing Gear Footprint - MTOW 233 000 kg R Jan 01/11
Subject 7-3-0
Maximum Pavement Loads Feb 01/09
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/07
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/07
FIGURE Maximum Pavement Loads - Maximum Pavement Loads Feb 01/09
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/07
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/07
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/07
Subject 7-4-0
Landing Gear Loading on Pavement R Jan 01/11
Subject 7-4-1
Landing Gear Loading on Pavement Feb 01/09
FIGURE Landing Gear Loading on Pavement - MTOW 192 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 210 000 kg R Jan 01/11
L.E.C.Page 16
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Landing Gear Loading on Pavement - MTOW 233 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 233 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 227 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 233 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 184 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 212 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 215 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 215 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 217 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 217 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 218 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 230 000 kg R Jan 01/11
FIGURE Landing Gear Loading on Pavement - MTOW 233 000 kg R Jan 01/11
Subject 7-5-0
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method
R Jan 01/11
Subject 7-5-1
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method
Jan 01/10
FIGURE Flexible Pavement Requirements - MTOW 233 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 233 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 212 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 218 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 230 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 233 000 kg R Jan 01/11
Subject 7-6-0
Flexible Pavement Requirements - LCN Conversion R Jan 01/11
Subject 7-6-1
Flexible Pavement Requirements - LCN Conversion Feb 01/09
L.E.C.Page 17
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flexible Pavement Requirements - MTOW 233 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 233 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 212 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 218 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 230 000 kg R Jan 01/11
FIGURE Flexible Pavement Requirements - MTOW 233 000 kg R Jan 01/11
Subject 7-7-0
Rigid Pavement Requirements - Portland Cement Association DesignMethod
R Jan 01/11
Subject 7-7-1
Rigid Pavement Requirements - Portland Cement Association DesignMethod
Feb 01/09
FIGURE Rigid Pavement Requirements - MTOW 233 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements - MTOW 233 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements - MTOW 212 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements - MTOW 218 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements - MTOW 230 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements - MTOW 233 000 kg R Jan 01/11
Subject 7-8-0
Rigid Pavement Requirements - LCN Conversion R Jan 01/11
Subject 7-8-1
Radius of Relative Stiffness Feb 01/09
FIGURE Radius of relative stiffness - (Reference : Portland CementAssociation)
Feb 01/09
Subject 7-8-2
Rigid Pavement Requirements - LCN Conversion Feb 01/09
FIGURE Rigid Pavement Requirements LCN - MTOW 233 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements LCN - MTOW 233 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements LCN - MTOW 212 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements LCN - MTOW 218 000 kg R Jan 01/11
L.E.C.Page 18
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Rigid Pavement Requirements LCN - MTOW 230 000 kg R Jan 01/11
FIGURE Rigid Pavement Requirements LCN - MTOW 233 000 kg R Jan 01/11
Subject 7-8-3
Radius of Relative Stiffness (Other values of ”E” and ”µ”) R Jan 01/11
Subject 7-8-4
Radius of Relative Stiffness Feb 01/09
FIGURE Radius of Relative Stiffness - (Effect E and µ ON ”L”values)
Feb 01/09
Subject 7-9-0
ACN/PCN Reporting System - Flexible and Rigid Pavements R Jan 01/11
Subject 7-9-1
Aircraft Classification Number - Flexible Pavement Feb 01/09
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW192 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW202 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW210 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW220 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW230 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW233 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW227 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW233 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW184 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW205 000 kg
R Jan 01/11
L.E.C.Page 19
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW212 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW215 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW217 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW218 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW230 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - MTOW233 000 kg
R Jan 01/11
Subject 7-9-2
Aircraft Classification Number - Rigid Pavement Feb 01/09
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW192 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW202 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW210 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW220 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW230 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW233 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW227 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW233 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW184 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW205 000 kg
R Jan 01/11
L.E.C.Page 20
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW212 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW215 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW217 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW218 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW230 000 kg
R Jan 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - MTOW233 000 kg
R Jan 01/11
CHAPTER 8
Subject 8-1-0
Possible Future Derivative Airplane Feb 01/09
CHAPTER 9
Subject 9-1-0
Scaled Drawing 1 in. = 50 ft. Jan 01/10
FIGURE Scaled Drawing - 1 in. = 50 ft. Jan 01/10
FIGURE Scaled Drawing - 1 in. = 50 ft. Jan 01/10
FIGURE Scaled Drawing - 1 in. = 50 ft. Jan 01/10
FIGURE Scaled Drawing - 1 in. = 50 ft. Jan 01/10
FIGURE Scaled Drawing - 1 in. = 50 ft. Jan 01/10
FIGURE Scaled Drawing - 1 in. = 50 ft. Jan 01/10
Subject 9-2-0
Scaled Drawing 1 cm. = 500 cm. Feb 01/09
FIGURE Scaled Drawing - 1 cm. = 500 cm. Feb 01/09
FIGURE Scaled Drawing - 1 cm. = 500 cm. Feb 01/09
FIGURE Scaled Drawing - 1 cm. = 500 cm. Feb 01/09
FIGURE Scaled Drawing - 1 cm. = 500 cm. Feb 01/09
L.E.C.Page 21
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Scaled Drawing - 1 cm. = 500 cm. Feb 01/09
FIGURE Scaled Drawing - 1 cm. = 500 cm. Feb 01/09
L.E.C.Page 22
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
TABLE OF CONTENTS
1 SCOPE
1-1-0 Purpose
1-2-0 Introduction
2 AIRPLANE DESCRIPTION
2-1-0 General Airplane Characteristics
2-1-1 General Airplane Characteristics Data
2-2-0 General Airplane Dimensions
2-3-0 Ground Clearances
2-4-0 Interior Arrangements
2-4-1 Typical Configuration
2-5-0 Passenger Compartment Cross Section
2-6-0 Cargo Compartments
2-6-1 Lower Deck Cargo Compartments (Loading combinations)
2-6-2 Main Deck Cargo Compartments (Loading combinations)
2-6-3 Main and Lower Deck Cross-sections
2-7-0 Door Clearances
2-7-1 Forward Passenger / Crew Doors
2-7-2 Mid Passenger / Crew Doors
2-7-3 Emergency Exits
2-7-4 Aft Passenger / Crew Doors
2-7-5 Forward Cargo Compartment Doors
2-7-6 Aft Cargo Compartment Doors
2-7-7 Bulk Cargo Compartment Doors
2-7-8 Main and Center Landing Gear Doors
2-7-9 Radome
2-7-10 APU and Nose Landing Gear Doors
3 AIRPLANE PERFORMANCE
3-1-0 General Information
3-2-0 Payload / Range
3-2-1 ISA Conditions
3-3-0 FAR / JAR Takeoff Weight Limitation
3-3-1 ISA Conditions
3-3-2 ISA +15˚C (ISA +27˚F) Conditions
T.O.C.Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-4-0 FAR / JAR Landing Field Length
3-4-1 ISA Conditions All series engines
3-5-0 Final Approach Speed
3-5-1 Final Approach Speed
4 GROUND MANEUVERING
4-1-0 General Information
4-2-0 Turning Radii
4-3-0 Minimum Turning Radii
4-4-0 Visibility from Cockpit in Static Position
4-5-0 Runway and Taxiway Turn Paths
4-5-1 135˚ Turn - Runway to Taxiway
4-5-2 90˚ Turn - Runway to Taxiway
4-5-3 180˚ Turn on a Runway
4-5-4 135˚ Turn - Taxiway to Taxiway
4-5-5 90˚ Turn - Taxiway to Taxiway
4-6-0 Runway Holding Bay (Apron)
4-7-0 Airplane Parking
5 TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
5-1-0 Airplane Servicing Arrangements
5-1-1 Symbols Used on Servicing Diagrams
5-1-2 Loading (Open Apron)
5-1-3 Loading (Passenger Bridge)
5-2-0 Terminal Operations - Full Servicing Turn Round Charts
5-2-1 Full Servicing Turn Round Charts
5-3-0 Terminal Operations - Transit Turn Round Charts
5-3-1 Transit Turn Round Charts
5-4-0 Ground Service Connections
5-4-1 Ground Service Connections Layout
5-4-2 Grounding Points
5-4-3 Hydraulic System
5-4-4 Electrical System
5-4-5 Oxygen System
5-4-6 Fuel System
5-4-7 Pneumatic System
5-4-8 Potable Water System
T.O.C.Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-9 Oil System
5-4-10 Vacuum Toilet System
5-5-0 Engine Starting Pneumatic Requirements
5-5-1 Low Temperatures
5-5-2 Ambient Temperatures
5-5-3 High Temperatures
5-6-0 Ground Pneumatic Power Requirements
5-6-1 Heating
5-6-2 Cooling
5-7-0 Preconditioned Airflow Requirements
5-8-0 Ground Towing Requirements
6 OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
6-2-0 Airport and Community Noise
6-2-1 Noise Data
6-3-0 Danger Areas of Engines
6-3-1 Ground Idle Power
6-3-2 Breakaway Power
6-3-3 Takeoff Power
6-4-0 APU Exhaust Velocities and Temperatures
6-4-1 APU
7 PAVEMENT DATA
7-1-0 General Information
7-2-0 Landing Gear Footprint
7-3-0 Maximum Pavement Loads
7-4-0 Landing Gear Loading on Pavement
7-4-1 Landing Gear Loading on Pavement
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method S-77-1
7-6-0 Flexible Pavement Requirements - LCN Conversion
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7-6-1 Flexible Pavement Requirements - LCN Conversion
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
7-8-0 Rigid Pavement Requirements - LCN Conversion
7-8-1 Radius of Relative Stiffness
7-8-2 Rigid Pavement Requirements - LCN Conversion
7-8-3 Radius of Relative Stiffness (Other values of E and L)
7-8-4 Radius of Relative Stiffness
7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements
7-9-1 Aircraft Classification Number - Flexible Pavement
7-9-2 Aircraft Classification Number - Rigid Pavement
8 DERIVATIVE AIRPLANES
8-1-0 Possible Future Derivative Airplane
9 SCALED DRAWINGS
9-1-0 Scaled Drawing 1 in. = 500 ft.
9-2-0 Scaled Drawing 1 cm. = 500 cm.
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
SCOPE
1-1-0 Purpose
**ON A/C A330-200 A330-200F A330-300
Purpose
1. GeneralThe A330 AIRPLANE CHARACTERISTICS (AC) manual is issued for the A330-200, A330-200F,A330-300 basic versions to provide the necessary data needed by airport operators and airlines for theplanning of airport facilities.
This document conforms to NAS 3601.
CORRESPONDENCECorrespondence concerning this publication should be directed to :
AIRBUS S.A.S.Customer ServicesTechnical Data Support and Services1 Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
1-2-0 Introduction
**ON A/C A330-200 A330-200F A330-300
Introduction
1. General
This manual comprises 9 chapters with a List of Effective Pages (LEP) and a Table Of Content(TOC) at the beginning of the manual.
Chapter 1 : SCOPE
Chapter 2 : AIRPLANE DESCRIPTION
This chapter contains general dimensional and other basic aircraft data.
It covers :- aircraft dimensions and ground clearances,- passenger and cargo compartments arrangement.
Chapter 3 : AIRPLANE PERFORMANCE
This chapter indicates the aircraft performance.
It covers :- payload range,- takeoff and landing runway requirements,- landing approach speed.
Chapter 4 : GROUND MANEUVERING
This chapter provides the aircraft turning capability and maneuvering characteristics on the ground.
It includes :- turning radii and visibility from the cockpit,- runway and taxiway turn path.
Chapter 5 : TERMINAL SERVICING
This chapter provides information for the arrangement of ground handling and servicing equipment.
It covers :- location and connections of ground servicing equipment,
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
- engines starting pneumatic and preconditioned airflow requirements.
Chapter 6 : OPERATING CONDITIONS
This chapter contains data and safety/environmental precautions related to engine and APUoperation on the ground.
It covers :- contour size and shape of the jet engine exhaust velocities and temperatures,- noise data.
Chapter 7 : PAVEMENT DATA
This chapter contains the pavement data helpful for airport planning.
It gives :- landing gear foot print and static load,- charts for flexible pavements with Load Classification Number (LCN),- charts for rigid pavements with LCN,- Aircraft Classification Number (ACN), Pavement Classification Number (PCN), reporting system
for flexible and rigid pavements.
Chapter 8 : DERIVATIVE AIRPLANES
This chapter gives relevant data of possible new version with the associated size change.
Chapter 9 : SCALED DRAWINGS
This chapter contains different airplane scaled drawings.
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
AIRPLANE DESCRIPTION
2-1-0 General Airplane Characteristics
**ON A/C A330-200 A330-200F A330-300
General Airplane Characteristics
1. General Airplane CharacteristicsThe weight terms used throughout this manual are given below together with their respectivedefinitions.
Maximum Taxi Weight (MTW) :Maximum weight for ground maneuver as limited by aircraft strength and airworthiness requirements.(It includes weight of run-up and taxi fuel). It is also called Maximum Ramp Weight (MRW).
Maximum Landing Weight (MLW) :Maximum weight for landing as limited by aircraft strength and airworthiness requirements.
Maximum Takeoff Weight (MTOW) :Maximum weight for takeoff as limited by aircraft strength and airworthiness requirements. (This isthe maximum weight at start of the takeoff run).
Maximum Zero Fuel Weight (MZFW) :Maximum operational weight of the aircraft without usable fuel.
Operational Empty Weight (OEW) :Weight of structure, powerplant, furnishings, systems, and other items of equipment that are anintegral part of a particular aircraft configuration plus the operator’s items. The operator’s items arethe flight and cabin crew and their baggage, unusable fuel, engine oil, emergency equipment, toiletchemical and fluids, galley structure, catering equipment, passenger seats and life vests, documents,etc.
Maximum Payload :Maximum Zero Fuel Weight (MZFW) minus Operational Empty Weight (OEW).
Maximum Seating Capacity :Maximum number of passengers specifically certified or anticipated for certification.
Maximum Cargo Volume :Maximum usable volume available for cargo.
Usable Fuel :Fuel available for aircraft propulsion.
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2-1-1 General Airplane Characteristics Data
**ON A/C A330-200 A330-300
General Airplane Characteristics Data
**ON A/C A330-300
1. The following table provides characteristics of A330-300 Models,these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
212 900 kg(469 363
lb)
184 900 kg(407 634
lb)
212 900 kg(469 363
lb)
215 900 kg(475 977
lb)
209 900 kg(462 749
lb)
Maximum Takeoff Weight (MTOW)212 000 kg(467 379
lb)
184 000 kg(405 650
lb)
212 000 kg(467 379
lb)
215 000 kg(473 993
lb)
209 000 kg(460 765
lb)
Maximum Landing Weight (MLW)174 000 kg(383 603
lb)
174 000 kg(383 603
lb)
177 000 kg(390 217
lb)
177 000 kg(390 217
lb)
182 000 kg(401 240
lb)
Maximum Zero Fuel Weight (MZFW)164 000 kg(361 557
lb)
164 000 kg(361 557
lb)
167 000 kg(368 171
lb)
167 000 kg(368 171
lb)
172 000 kg(379 194
lb)
CF6 Engines 119 831 kg (264 182 lb)
PW Engines 120 132 kg (264 845 lb)Estimated OperationalEmpty Weight (OEW)
Trent Engines 119 931 kg (264 402 lb)
Estimated Maximum Payload CF6-80E144 169 kg(97 375 lb)
47 169 kg(103 989 lb)
52 169 kg(115 012
lb)
Estimated Maximum Payload PW 400043 868 kg(96 712 lb)
48 868 kg(107 735 lb)
51 868 kg(114 349
lb)
Estimated Maximum Payload TRENT700
44 069 kg(97 155 lb)
47 069 kg(103 769 lb)
52 069 kg(114 792
lb)
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft CharacteristicsWV010 WV011 WV012 WV013 WV014
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
217 900 kg(480 386
lb)
212 900 kg(469 363
lb)
218 900kg
(482 591lb)
215 900 kg(475 977
lb)
205 900 kg(453 931
lb)
Maximum Takeoff Weight (MTOW)217 000 kg(478 402
lb)
212 000 kg(467 379
lb)
218 000kg
(480 607lb)
215 000 kg(473 993
lb)
205 000 kg(451 947
lb)
Maximum Landing Weight (MLW)179 000 kg(394 627
lb)
177 000 kg(390 217
lb)
182 000kg
(401 240lb)
177 000 kg(390 217
lb)
182 000 kg(401 240
Maximum Zero Fuel Weight (MZFW)169 000 kg(372 580
lb)
167 000 kg(368 171
lb)
172 000kg
(379 194lb)
167 000 kg(368 171
lb)
172 000 kg(379 194
lb)
CF6 Engines 119 831 kg (264 182 lb)
PW Engines 120 132 kg (264 845 lb)Estimated OperationalEmpty Weight (OEW)
Trent Engines 119 931 kg (264 402 lb)
Estimated Maximum Payload CF6-80E149 169 kg(110 052
lb)
47 169 kg(103 989
lb)
52 169 kg(115 012
lb)
47 169 kg(103 989
lb)
52 169 kg(115 012
lb)
Estimated Maximum Payload PW 400048 868 kg(107 735
lb)
46 868 kg(103 326
lb)
51 868 kg(114 349
lb)
46 868 kg(103 326
lb)
51 868 kg(114 349
lb)
Estimated Maximum Payload TRENT700
49 069 kg(108 178
lb)
47 069 kg(103 769
lb)
52 069 kg(114 792
lb)
47 069 kg(103 769
lb)
52 069 kg(114 792
lb)
Aircraft CharacteristicsWV020 WV022 WV024 WV025
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
230 900 kg(509 046 lb)
233 900 kg(515 660 lb)
205 900 kg(453 931 lb)
217 900 kg(480 386 lb)
Maximum Takeoff Weight (MTOW)230 000 kg(507 062 lb)
233 000 kg(513 676 lb)
205 000 kg(451 947 lb)
217 000 kg(478 000 lb)
Maximum Landing Weight (MLW)185 000 kg(407 854 lb)
187 000 kg(412 263 lb)
185 000 kg(407 854 lb)
179 000 kg(394 627 lb)
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft CharacteristicsWV020 WV022 WV024 WV025
Maximum Zero Fuel Weight (MZFW)173 000 kg(381 399 lb)
175 000 kg(385 808 lb)
173 000 kg(381 399 lb)
169 000 kg(372 580 lb)
CF6 Engines 119 831 kg (264 182 lb)
PW Engines 120 132 kg (264 845 lb)Estimated OperationalEmpty Weight (OEW)
Trent Engines 119 931 kg (264 402 lb)
Estimated Maximum Payload CF6-80E153 169 kg
(117 217 lb)55 169 kg
(121 626 lb)53 169 kg
(117 217 lb)49 169 kg
(110 052 lb)
Estimated Maximum Payload PW 400052 868 kg
(116 554 lb)54 868 kg
(120 963 lb)52 868 kg
(116 554 lb)48 868 kg
(107 735 lb)
Estimated Maximum Payload TRENT700
53 069 kg(116 997 lb)
55 069 kg(121 406 lb)
53 069 kg(116 997 lb)
49 069 kg(108 178 lb)
Aircraft CharacteristicsWV050 WV051 WV052 WV053
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
230 900 kg(509 046 lb)
212 900 kg(469 363 lb)
233 900 kg(515 660 lb)
205 900 kg(453 931 lb)
Maximum Takeoff Weight (MTOW)230 000 kg(507 062 lb)
212 000 kg(467 379 lb)
233 000 kg(513 676
205 000 kg(451 947 lb)
Maximum Landing Weight (MLW)185 000 kg(407 854 lb)
187 000 kg(412 263 lb)
187 000 kg(412 263 lb)
185 000 kg(407 854 lb)
Maximum Zero Fuel Weight (MZFW)173 000 kg(381 399 lb)
175 000 kg(385 808 lb)
175 000 kg(385 808 lb)
173 000 kg(381 399 lb)
CF6 Engines 119 831 kg (264 182 lb)
PW Engines 120 132 kg (264 845 lb)Estimated OperationalEmpty Weight (OEW)
Trent Engines 119 931 kg (264 402 lb)
Estimated Maximum Payload CF6-80E153 169 kg
(117 217 lb)55 169 kg
(121 626 lb)53 169 kg
(117 217 lb)
Estimated Maximum Payload PW 400052 868 kg
(116 554 lb)54 868 kg
(120 963 lb)52 868 kg
(116 554 lb)
Estimated Maximum Payload TRENT700
53 069 kg(116 997 lb)
55 069 kg(121 406 lb)
53 069 kg(116 997 lb)
2. The following table provides characteristics of A330-300 Models, these data are common to eachWeight Variant:
Aircraft Characteristics
Standard Seating Capacity (Single-class) 335
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft Characteristics97 530 l
(25 765 US gal)Usable Fuel Capacity(density = 0.785 kg/l) 76 561 kg
(168 787 lb)
Pressurized Fuselage Volume (A/C nonequipped)
1 056 m3
(37 292 ft3)
Passenger Compartment Volume372 m3
(13 137 ft3)
Cockpit Volume12 m3
(424 ft3)
Usable Volume, FWD CC(Based on LD3)
80.5 m3
(2 844 ft3)
Usable Volume, AFT CC(Based on LD3)
62.6 m3
(2 212 ft3)
Usable Volume, Bulk CC19.7 m3
(695 ft3)
Water Volume, FWD CC107 m3
(3 789ft3)
Water Volume, AFT CC85.7 m3
(3 026ft3)
Water Volume, Bulk CC22.7 m3
(802 ft3)
**ON A/C A330-200
3. The following table provides characteristics of A330-200 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV020 WV021 WV022 WV023 WV024
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
230 900 kg(509 046
lb)
230 900 kg(509 046
lb)
233 900 kg(515 660
lb)
233 900 kg(515 660
lb)
202 900 kg(447 317
lb)
Maximum Takeoff Weight (MTOW)230 000 kg(507 062
lb)
230 000 kg(507 062
lb)
233 000 kg(513 676
lb)
233 000 kg(513 676
lb)
202 000 kg(445 333
lb)
Maximum Landing Weight (MLW)180 000 kg(396 831
lb)
182 000 kg(401 240
lb)
182 000 kg(401 240
lb)
180 000 kg(396 831
lb)
180 000 kg(396 831
lb)
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft CharacteristicsWV020 WV021 WV022 WV023 WV024
Maximum Zero Fuel Weight (MZFW)168 000 kg(370 376
lb)
170 000 kg(374 785
lb)
170 000 kg(374 785
lb)
168 000 kg(370 376
lb)
168 000 kg(370 376
lb)
CF6 Engines 116 740 kg (257 368 lb)
PW Engines 117 041 kg (258 031 lb)Estimated OperationalEmpty Weight (OEW)
Trent Engines 116 840 kg (257 588 lb)
Estimated Maximum Payload CF6-80E151 260 kg(133 009
lb)
53 260 kg(117 418 lb)
51 260 kg(133 009 lb)
Estimated Maximum Payload PW 400050 959 kg(112 345
lb)
52 959 kg(116 754 lb)
50 959 kg(112 345 lb)
Estimated Maximum Payload TRENT700
51 160 kg(112 788
lb)
53 160 kg(117 197 lb)
51 160 kg(112 788 lb)
Aircraft CharacteristicsWV025 WV026 WV027 WV050 WV051
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
220 900 kg(487 000
lb)
192 900 kg(425 271
lb)
220 900 kg(487 000
lb)
230 900 kg(509 046
lb)
192 900 kg(425 271
lb)
Maximum Takeoff Weight (MTOW)220 000 kg(485 016
lb)
192 000 kg(423 287
lb)
220 000 kg(485 016
lb)
230 000 kg(507 062
lb)
192 000 kg(423 287
lb)
Maximum Landing Weight (MLW)182 000 kg(401 240
lb)
180 000 kg(396 831
lb)
180 000 kg(396 831
lb)
180 000 kg(396 831
lb)
180 000 kg(396 831
lb)
Maximum Zero FuelWeight (MZFW)
170 000 kg(374 785
lb)
168 000 kg(370 376
lb)
168 000 kg(370 376
lb)
168 000 kg(370 376
lb)
168 000 kg(370 376
lb)
CF6 Engines 116 740 kg (257 368 lb)
PW Engines 117 041 kg (258 031 lb)Estimated OperationalEmpty Weight (OEW)
Trent Engines 116 840 kg (257 588 lb)
Estimated Maximum Payload CF6-80E153 260 kg(117 418
lb)
51 260 kg(133 009 lb)
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft CharacteristicsWV025 WV026 WV027 WV050 WV051
Estimated Maximum Payload PW 400052 959 kg(116 754
lb)
50 959 kg(112 345 lb)
Estimated Maximum Payload TRENT700
53 160 kg(117 197
lb)
51 160 kg(112 788 lb)
Aircraft CharacteristicsWV052 WV053 WV054 WV055 WV056
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
233 900 kg(515 660
lb)
210 900 kg(464 954
lb)
230 900 kg(509 046
lb)
192 900 kg(425 271
lb)
233 900 kg(515 660
lb)
Maximum Takeoff Weight (MTOW)233 000 kg(513 676
lb)
210 000 kg(462 970
lb)
230 000 kg(507 062
lb)
192 000 kg(423 287
lb)
233 000 kg(513 676
lb)
Maximum Landing Weight (MLW)182 000 kg(401 240
lb)
180 000 kg(396 831
lb)
182 000 kg(401 240
lb)
182 000 kg(401 240
lb)
180 000 kg(396 831
lb)
Maximum Zero Fuel Weight (MZFW)170 000 kg(374 785
lb)
168 000 kg(370 376
lb)
170 000 kg(374 785
lb)
170 000 kg(374 785
lb)
168 000 kg(370 376
lb)
CF6 Engines 116 740 kg (257 368 lb)
PW Engines 117 041 kg (258 031 lb)Estimated OperationalEmpty Weight (OEW)
Trent Engines 116 840 kg (257 588 lb)
Estimated Maximum Payload CF6-80E153 260 kg(117 418
lb)
51 260 kg(133 009
lb)
53 260 kg(117 418 lb)
51 260 kg(133 009
lb)
Estimated Maximum Payload PW 400052 959 kg(116 754
50 959 kg(112 345
lb)
52 959 kg(116 754
50 959 kg(112 345
lb)
Estimated Maximum Payload TRENT 70053 160 kg(117 197
lb)
51 160 kg(112 788
lb)
53 160 kg(117 197 lb)
51 160 kg(112 788
lb)
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft CharacteristicsWV057 WV058 WV059 WV060 WV061
Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)
236 900 kg(522 276
lb)
238 900 kg(526 684 lb)
202 900 kg(447 317 lb)
220 900 kg(487 001 lb)
230 900 kg(509 047 lb)
Maximum Takeoff Weight (MTOW)236 000 kg(520 291
lb)
238 000 kg(524 700 lb)
202 000 kg(445 333 lb)
220 000 kg(485 017 lb)
230 000 kg(507 063 lb)
Maximum Landing Weight (MLW)182 000 kg(401 240
lb)
182 000 kg(401 240 lb)
182 000 kg(401 240 lb)
182 000 kg(401 240 lb)
182 000 kg(401 240 lb)
Maximum Zero Fuel Weight(MZFW)
170 000 kg(374 785
lb)
168 000 kg(370 376 lb)
170 000 kg(374 785 lb)
170 000 kg(374 785 lb)
168 000 kg(370 376 lb)
CF6 Engines 116 740 kg (257 368 lb)
PW Engines 117 041 kg (258 031 lb)EstimatedOperational EmptyWeight (OEW) Trent
Engines116 840 kg (257 588 lb)
Estimated Maximum PayloadCF6-80E1
53 260 kg(117 418
lb)
51 260 kg(133 009 lb)
53 260 kg(117 418 lb)
51 260 kg(133 009 lb)
Estimated Maximum Payload PW4000
52 959 kg(116 754
lb)
50 959 kg(112 345 lb)
52 959 kg(116 754 lb)
50 959 kg(112 345 lb)
Estimated Maximum PayloadTRENT 700
53 160 kg(117 197
lb)
51 160 kg(112 788 lb)
53 160 kg(117 197 lb)
51 160 kg(112 788 lb)
4. The following table provides characteristics of A330-200 Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsStandard Seating Capacity 303
139 090 l(36 744 US gal)Usable Fuel Capacity
(density = 0.785 kg/l) 109 185 kg(240 711 lb)
Pressurized Fuselage Volume (A/C nonequipped)
950 m3
(33 548 ft3)
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft Characteristics
Passenger Compartment Volume335 m3
(11 830 ft3)
Cockpit Volume12 m3
(424 ft3)
Usable Volume, FWD CC(Based on LD3)
62.6 m3
(2 212 ft3)
Usable Volume, AFT CC(Based on LD3)
53.6 m3
(1 896 ft3)
Usable Volume, Bulk CC19.7 m3
(695 ft3)
Water Volume, FWD CC84.6 m3
(2 988 ft3)
Water Volume, AFT CC71.1 m3
(2 511 ft3)
Water Volume, Bulk CC22.7 m3
(802 ft3)
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
General Airplane Characteristics Data
1. The following table provides characteristics of A330-200F Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001
Maximum Taxi Weight (MTW)Maximum Rampi Weight (MRW)
233 900 kg(515 660 lb)
227 900 kg(502 432 lb)
Maximum Takeoff Weight (MTOW)233 000 kg(513 676 lb)
227 000 kg(500 448 lb)
Maximum Landing Weight (MLW)182 000 kg(401 240 lb)
187 000 kg(412 263 lb)
Maximum Zero Fuel Weight (MZFW)173 000 kg(381 399 lb)
178 000 kg(392 422 lb)
PW Engines 109 358 kg (241 093 lb)EstimatedOperational EmptyWeight (OEW)
Trent Engines 109 100 kg (240 524 lb)
Estimated Maximum Payload PW4000
63 642 kg(140 306 lb)
68 642 kg(151 329 lb)
Estimated Maximum Payload TRENT700
63 900 kg(140 875 lb)
68 900 kg(151 898 lb)
2. The following table provides characteristics of A330-200F Models, these data are common to eachWeight Variant:
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picard_c
Typewritten Text
picard_c
Typewritten Text
picard_c
Text Box
64 742 kg (142 733 lb)
picard_c
Text Box
65 000 kg (143 302 lb)
picard_c
Text Box
69 738 kg (153 746 lb)
picard_c
Text Box
70 000 kg (154 324 lb)
picard_c
Text Box
108 261 kg (238 675 lb)
picard_c
Text Box
108 000 kg (238 100 lb)
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft CharacteristicsSupernumerary area 6
Usable Fuel Capacity(density = 0.785 kg/l)
139 090 l(36 755 US gal)
Pressurized Fuselage Volume (A/C nonequipped)
900 m3
(31 783 ft3)
Cockpit Volume12 m3
(424 ft3)
Main Deck Cargo Compartment UsableVolume(Based on 96”x125” pallet)
336.8 m3
(11 894ft3)
Main Deck Cargo Compartment WaterVolume
466.5 m3
(16 474 ft3)
Usable Volume, FWD CC(Based on LD3)
62.6 m3
(2 212 ft3)
Usable Volume, AFT CC(Based on LD3)
53.6 m3
(1 896 ft3)
Usable Volume, Bulk CC19.7 m3
(695 ft3)
Water Volume, FWD CC84.6 m3
(2 988 ft3)
Water Volume, AFT CC71.1 m3
(2 511 ft3)
Water Volume, Bulk CC22.7 m3
(802 ft3)
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picard_c
Text Box
97 530 l (25 764 US gal)
picard_c
Text Box
328.2 m3 (11 592ft3)
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-2-0 General Airplane Dimensions
**ON A/C A330-200 A330-300
General Airplane Dimensions
1. This section provides General Airplane Dimensions for pax version.
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
SCALE METER960 3 3020100
SEECHAPTER
60.304 m
(35 ft 0.6 in)
(83 ft 3 in)
(197 ft 10 in)
FOR DOOR SIZESEE CHAPTER 2−7
25.37 m
10.684 m
SCALE FEET
RR=21.275m (69 ft 9 in)
GE=21.136 m (69 ft 3 in)PW=21.447 m (70 ft 4 in)
(63 ft 6 in)19.404 m
NOTE:
(30 ft 9 in)9.37 m
(208 ft 11.5 in)
63.689 m
6.671 m
(21 ft 10.7 in)
F_AC_020200_1_0010101_01_01
2−3
General Airplane DimensionsFIGURE 1
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
0SCALE METER
300 10 20SCALE FEET
SEE CHAPTER 2−7FOR DOOR SIZE
(35 ft 0.6 in)
(197 ft 10 in)
(21 ft 10.7 in) (72 ft 9.2 in)
3 6 9
(191 ft 5.5 in)
58.372 m
10.684 m
60.304 m
22.18 m6.671 m
GE=17.942 m (58 ft 10 in)
RR=18.081 m (59 ft 3 in)PW=18.253 m (59 ft 10 in)
CHAPTER2−3
SEE
(63 ft 6 in)19.404 m
NOTE:
(30 ft 9 in)9.37 m
F_AC_020200_1_0020101_01_01
General Airplane DimensionsFIGURE 2
2-2-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
General Airplane Dimensions
1. This section provides General Airplane Dimensions for cargo version.
2-2-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
0SCALE METER
300 10 20SCALE FEET
(35 ft 0.6 in)
(197 ft 10 in)
(72 ft 9.2 in)
3 6 9
60.304 m
6.671 m
(191 ft 5.7 in)
58.362 m
(63 ft 7.9 in)19.404 m
SEECHAPTER
2−3
SEE CHAPTER 2−7FOR DOOR SIZENOTE:
10.684 m
(30 ft 9 in)9.37 m
RR=18.081 m (59 ft 3 in)PW=18.253 m (59 ft. 10 in)
22.18 m
(21 ft 10.6 in)
F_AC_020200_1_0030101_01_01
General Airplane DimensionsFIGURE 3
2-2-0Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-3-0 Ground Clearances
**ON A/C A330-200 A330-300
Ground Clearances
1. This section gives the height of various points of the aircraft, above the ground, for different aircraftpax configurations.Dimensions in the tables are approximate and will vary with tire type and conditions.
NOTE : The distances given in the Ground Clearances charts are reference distances calculated forA/C weight and CG conditions.The conditions used in the calculations are maximum A/C weight (minimum groundclearances) and a typical A/C maintenance weight (typical ground clearances formaintenance).
2-3-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
X L C2 Y K E3 H E2 D C1 B E1 AM
P N V U T S R O
J
MRW212 900 kg469 360 lb
Am ftm ftm ftm
EMPTY CG 26.8%
BC1C2D
FR 26FR 72
FR 20FR 37FR 56FR 45
GE = RPW = RRR = R
YXVUTS
PONMLKJH
E3E2E1
3.687.484.974.644.333.870.870.900.948.058.336.4617.185.773.435.342.042.742.282.104.838.537.742.704.55
12.0724.54
15.2214.2012.702.852.953.0826.4127.3221.2056.3618.9311.2517.56.7
8.997.486.89
15.8428
25.48.85
14.92
16.30
3.467.244.724.414.133.680.690.720.767.708.096.13
16.945.553.225.311.862.542.101.954.678.317.582.554.41
11.3523.7615.4814.4613.5512.072.262.362.49
25.2626.5420.1155.5818.2010.5617.46.108.336.886.39
15.3227.2624.868.36
14.46
3.357.034.674.374.11
0.720.750.797.617.886.0616.725.413.135.201.852.452.142.034.738.197.672.664.55
3.64
1123.0615.3214.3313.4811.942.362.462.59
24.9625.8519.8854.8517.7510.2717.066.078.037.026.6615.5126.8725.16
8.7214.92
4.398.106.306.005.705.252.212.292.348.969.237.55
17.626.534.246.433.263.683.683.686.329.329.324.146.32
14.426.520.619.618.717.27.257.517.6729.430.224.757.821.4
21.110.7121212
20.730.530.513.520.7
13.9
ft
*
* NOTE:
OPERATING WEIGHT MAXIMUM RAMPWEIGHT CG 36.5%
MAXIMUM RAMPWEIGHT CG 15%
AIRCRAFTON JACKS
THESE FIGURES WILL GIVE AN AIRCRAFT FUSELAGE DATUM (FD) AT 6500 MM.F_AC_020300_1_0010101_01_00
Ground ClearancesFIGURE 1
2-3-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
L C2 Y K E3 H E2 D C1 B E1 AM
P N V U T S R O
ZJ
Am ftm m ftm
BC1C2D
FR 26FR 72
FR 20FR 37FR 56FR 45
GE =PW =RR =
VUTS
PON
MLKJHE3E2E1
3.683.68
6.32
20.619.618.717.27.257.517.6729.430.224.7
21.4
10.712.12.12.20.730.5
20.7
OPERATING WEIGHTEMPTY CG 27.9%
MAXIMUM RAMPWEIGHT CG 37.5%
5.413.667.474.954.634.353.890.870.900.948.088.306.48
5.743.505.36
2.702.232.044.868.547.75
2.02
YZ
2.784.63
12.01
16.2415.1914.2712.762.852.953.0826.5127.2321.26
18.8311.4817.66.638.867.31
28.02
17.75
24.51
25.429.1215.19
3.437.234.734.424.133.670.670.700.747.718.056.14
5.513.275.151.812.482.031.844.668.317.56
4.442.58
17.1211.2523.7215.52
13.5512.042.192.292.4225.2926.4120.14
18.0710.73
5.938.136.666.03
27.2624.80
14.568.46
5.433.306.974.674.374.113.640.720.750.797.617.776.05
5.353.165.101.832.402.122.014.78
4.632.74
17.8110.8222.8615.3214.3313.4811.942.362.462.5924.9625.4919.85
17.5510.3616.76.007.876.956.5915.7
25.2326.77
8.99
ft15.19
7.104.398.106.306.005.705.252.212.292.348.969.237.55
6.534.246.463.26
3.686.369.329.324.14 13.5
30.5
21.213.9
14.423.30
MRW230 900 kg509 042 lb
14.50
8.167.69
ft
MAXIMUM RAMPWEIGHT CG 21%
15.96.7
15.3
16.9
5.22
25.5
V U
V U
M1 18.1261.0959.45
18.23 59.858.17
17.9817.48
58.9957.35
17.7117.21
58.1 18.6256.4617.73
AIRCRAFTON JACKS *
M1 = POST MOD 48979 (SHORTER FIN INSTALLATION)* NOTE: THESE FIGURES WILL GIVE AN AIRCRAFT FUSELAGE DATUM (FD) AT 6500 MM.
RRR
F_AC_020300_1_0030101_01_00
Ground ClearancesFIGURE 2
2-3-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
Ground Clearances
1. This section gives the height of various points of the aircraft, above the ground, for different aircraftcargo configurations.Dimensions in the tables are approximate and will vary with tire type and conditions.
NOTE : The distances given in the Ground Clearances charts are reference distances calculated forA/C weight and CG conditions.The conditions used in the calculations are maximum A/C weight (minimum groundclearances) and a typical A/C maintenance weight (typical ground clearances formaintenance).
2-3-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
P N V U T S R O
MRW227 900 kg502 433 lb
Am ftm ftm
EMPTY CG 18%
BC1C2D1
FR 26FR 72
FR 27FR 10FR 13FR 15
PWRR
YVUVUTS
MKJH
E6E5E4E3E2E1D2
1.061.13
7.8017.413.525.552.162.702.472.422.222.393.075.085.048.448.063.114.98
3.483.71
25.5957.1211.5518.21
7.098.868.107.947.287.84
10.0716.6716.5427.6926.4410.2016.34
0.830.90
7.4716.973.165.151.902.382.262.262.062.242.934.894.878.087.882.934.82
2.712.95
24.5155.6810.3716.906.237.817.417.416.767.359.61
16.0415.9826.5125.859.61
15.81
0.880.96
7.3716.683.054.931.912.302.352.422.252.433.135.025.037.928.013.085.00
2.893.15
24.1754.7110.0016.17
6.267.547.717.947.387.97
10.2716.4616.5025.9826.2710.1016.40
ft
OWE (109 000) MAXIMUM RAMPWEIGHT CG 37.6%
MAXIMUM RAMPWEIGHT CG 20.6%
Z E1E2E3
FR 20
FR 20FR 37FR 56FR 45FR 87
N
Z
8.31 27.26 7.87 25.82 7.59 24.89O
RR
MVUJC2
YK
E6HE4GROUNDLINESDOOR SILLHEIGHTS
A D1 B
C1
D2
E5 R
9.23 30.28 8.90 29.20 8.79 28.83P
3.617.92
11.8425.98
3.257.46
10.6624.48
3.137.21
10.2723.65
6.22 20.41 6.08 19.95 6.29 20.63F_AC_020300_1_0060101_01_02
2.742.982.923.02
8.999.799.599.91
2.452.702.642.71
8.038.858.658.90
2.412.672.612.65
7.918.778.558.68
Ground ClearancesGround Clearances MRW 227 900 kg
FIGURE 3
2-3-0Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
P N V U T S R O
MRW233 900 kg515 660 lb
Am ftm ftm
EMPTY CG 18%
BC1C2D1
FR 26FR 72
FR 27FR 10FR 13FR 15
PWRR
YVUVUTS
MKJH
E6E5E4E3E2E1D2
1.061.13
7.8017.413.525.552.162.702.472.422.222.393.075.085.048.448.063.114.98
3.483.71
25.5957.1211.5518.21
7.098.868.107.947.287.84
10.0716.6716.5427.6926.4410.2016.34
0.820.89
7.4616.953.155.131.892.372.262.252.062.242.934.894.878.067.872.934.82
2.692.92
24.4855.6110.3316.836.207.787.417.386.767.359.61
16.0415.9826.4425.829.61
15.81
0.870.95
7.3616.673.044.911.912.292.352.412.242.433.135.025.037.918.013.085.00
2.853.12
24.1554.699.97
16.116.277.517.717.917.357.97
10.2716.4716.5025.9526.2810.1016.40
ft
OWE (109 000) MAXIMUM RAMPWEIGHT CG 37.4%
MAXIMUM RAMPWEIGHT CG 20.6%
Z E1E2E3
FR 20
FR 20FR 37FR 56FR 45FR 87
N
Z
8.31 27.26 7.85 25.75 7.57 24.84O
RR
MVUJC2
YK
E6HE4GROUNDLINESDOOR SILLHEIGHTS
A D1 B
C1
D2
E5 R
9.23 30.28 8.88 29.13 8.78 28.81P
3.617.92
11.8425.98
3.257.46
10.6624.48
3.127.19
10.2423.59
6.22 20.41 6.08 19.95 6.29 20.64
2.742.982.923.02
8.999.799.599.91
2.442.692.632.70
8.008.838.628.86
2.412.672.602.64
7.898.758.538.66
F_AC_020300_1_0070101_01_02
Ground ClearancesGround Clearances MRW 233 900 kg
FIGURE 4
2-3-0Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-4-0 Interior Arrangements
**ON A/C A330-200 A330-300
Interior Arrangements
1. This section gives the standard interior arrangements configuration.
2-4-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-4-1 Typical Configuration
**ON A/C A330-200 A330-300
Typical Configuration
1. This section gives the typical configuration for A330 pax version
2-4-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
FO
RW
AR
D P
AS
SE
NG
ER
/CR
EW
DO
OR
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
FO
RW
AR
D P
AS
SE
NG
ER
/CR
EW
DO
OR
NO
TE
:F
OR
DO
OR
SIZ
ES
SE
E C
HA
PT
ER
2−
7
PA
SS
EN
GE
R S
EA
TS
(29
5 T
OT
AL)
12 F
IRS
T C
LAS
S
241
EC
ON
OM
Y C
LAS
S
CO
AT
ST
OW
AG
E
ST
OW
AG
E
GA
LLE
Y
LAV
AT
OR
Y
AT
TE
ND
AN
TS
SE
AT
42 B
US
INE
SS
CLA
SS
VCC
ITE
MD
ES
IGN
AT
ION
A C G L S
(12)
(4)
(7)
(9)
(1)
A
A AA
A A
A A
A A
AA
GG
GG
GG
G
C C
CC
L LLL
L L L L
L
S
F_AC_020401_1_0010101_01_00
Typical ConfigurationFIGURE 1
2-4-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
FO
RW
AR
D P
AS
SE
NG
ER
/CR
EW
DO
OR
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
FO
RW
AR
D P
AS
SE
NG
ER
/CR
EW
DO
OR
NO
TE
:F
OR
DO
OR
SIZ
ES
SE
E C
HA
PT
ER
2−
7
PA
SS
EN
GE
R S
EA
TS
(25
3 T
OT
AL)
12 F
IRS
T C
LAS
S
205
EC
ON
OM
Y C
LAS
S
TR
OLL
EY
36 B
US
INE
SS
CLA
SS
VC
C
CO
AT
ST
OW
AG
E
ST
OW
AG
E
GA
LLE
Y
LAV
AT
OR
Y
AT
TE
ND
AN
TS
SE
AT
ITE
MD
ES
IGN
AT
ION
A C G L S
(12)
(2)
(6)
(8)
(1)
Tr
(2)
A
A AA
AA
AA
A A
A AC
C
G
GG
G
G G
L L L LLL
L LS
Tr
Tr
F_AC_020401_1_0020101_01_00
Typical ConfigurationFIGURE 2
2-4-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-5-0 Passenger Compartment Cross Section
**ON A/C A330-200 A330-300
Passenger Compartment Cross-section
1. This section gives the typical passenger compartment cross-section configuration of A330 models.
2-5-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
AB
C C D
C D C D
F N M
C C D
H
K K
F G
222 in5.640 m
208 in5.290 m
FIRST CLASS, 6 ABREAST BUSINESS CLASS, 7 ABREAST
TOURIST CLASS, 8 ABREAST CHARTER CLASS, 9 ABREAST
A − 54.0 in (1371.6 mm)B − 21.0 in (533 mm)C − 39.6 in (1006 mm)D − 17.7 in (450 mm)E − 72.0 in (1829 mm)F − 19.0 in (483 mm)
G − 48.0 in (1219 mm)H − 19.8 in (503 mm)K − 41.5 in (1054.1 mm)M − 57.1 in (1450 mm)N − 16.5 in (419 mm)
91.7 in2.330 mA E
H C
M
F_AC_020500_1_0010101_01_00
Passenger Compartment Cross-sectionFIGURE 1
2-5-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-6-0 Cargo Compartments
**ON A/C A330-200 A330-200F A330-300
Cargo Compartment
1. This section gives the cargo compartments location and dimensions.
2-6-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-6-1 Lower Deck Cargo Compartments (Loading combinations)
**ON A/C A330-200 A330-200F A330-300
Lower Deck Cargo Compartments
**ON A/C A330-300
1. This table gives cargo compartments loading combinations.
Cargo Hold Volume
Cargo Compartment Palletized volume Containerized volume
Forward Door size (h × w) 2442 ft3 (69.150 m3) 2844 ft3 (80.533 m3)
66.89 in (1.699 m) x 106.34 in(2.701 m)
66.89 in (1.699 m) x 106.34 in(2.701 m)
based on LD3 (IATA E NAS3610-2K2C) container volume
Aft Door size (h × w) 1628 ft3 (46.100 m3) 2212 ft3 (62.637 m3)
66.3 in (1.684 m) x 107.1 in(2.720 m)
based on 96 in × 125 in palletsloaded to height of 64 in (1.626
m)
based on LD3 (IATA E NAS3610-2K2C) container volume
Bulk Door size (h × w)
37.3 in (0.947 m) x 37.3 in (0.947m)
695 ft3 (19.680 m3)
**ON A/C A330-200 A330-200F
2. This table gives cargo compartments loading combinations.
Cargo Hold Volume
Cargo Compartment Palletized volume Containerized volume
Forward Door size (h × w) 1628 ft3 (46.100 m3) 2212 ft3 (62.637 m3)
66.89 in (1.699 m) x 106.34 in(2.701 m)
based on 96 in × 125 in palletsloaded to height of 64 in (1.626
m)
based on LD3 (IATA E NAS3610-2K2C) container volume
Aft Door size (h × w) 1628 ft3 (46.100 m3) 1896 ft3 (53.689 m3)
66.3 in (1.684 m) x 107.1 in(2.720 m)
based on 96 in × 125 in palletsloaded to height of 64 in (1.626
m)
based on LD3 (IATA E NAS3610-2K2C) container volume
Bulk Door size (h × w)
37.3 in (0.947 m) x 37.3 in (0.947m)
695 ft3 (19.680 m3)
2-6-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
3.18 m
4.15 m
5.640 m
(125.0 in)
(163.4 in)
0.95 m(37.4 in)
(222.0 in)
2.70 m(106.3 in)
(159.1 in)
AFT CARG0COMPARTMENT
BULK CARGOCOMPARTMENT
FWD CARG0COMPARTMENT
TYPICAL SECTIONSFR20 TO FR39.2
AND FR53.2 TO FR65
TOP OF CARGO COMPT
CARGO COMPT FLOOR
(159.1 in)4.04 m
11.82 m 10.19 m(38.8 ft) (33.4 ft)
4.04 m
15.01 m 12.32 m(49.3 ft) (40.5 ft)
FWD : 1.713 m (67.6 in)AFT : 1.67 m (65.7 in)
2.73 m
(107.5 in)
−200:
−300:
F_AC_020601_1_0030101_01_00
Lower Deck Cargo CompartmentsFIGURE 1
2-6-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
−HALF−SIZE CONTAINERS NAS 3610−2K2C AS PER IATA CONTOUR E
−HALF−SIZE CONTAINERS NAS 3610−2K2C AS PER IATA CONTOUR C
−FULL−SIZE CONTAINERS NAS 3610−2L2C AS PER IATA CONTOUR F
CARGO FLEXIBILITY−LOADING COMBINATIONS
AFT FWD AFTFWDTYPICAL LOADING COMBINATIONS−STANDARD AIRCRAFT
FWD CARG0 COMPT
AFT CARG0 COMPT
4 4
LIMITED TO MAX GROSS WEIGHT 3500 lb (1587 kg) EACH OR 60.4 in X 61.5 in PALLETS NAS 3610−2K3P
LIMITED TO MAX GROSS WEIGHT 3500 lb (1587 kg) EACH
OR 60.4 in X 61.5 in PALLETS NAS 3610−2K3P,2L4P
−96 in X 125 in PALLETS NAS 3610−2M1P,2P,3P LIMITED TO MAX GROSS WEIGHT 10200 lb (4626 kg) EACH (WITH POTENTIAL FOR EXTENSION TO 11250 lb (5103 kg)
PLUS−HALF−SIZE CONTAINERS NAS 3610−2K2C AS PER IATA CONTOUR E OR N LIMITED TO MAX GROSS WEIGHT 3500 lb (1587 kg) EACH
−OR 60.4 IN x 61.5 IN PALLETS NAS 3610−2K3P LIMITED TO MAX GROSS WEIGHT 3500 lb (1587 kg) EACH
−OR 60.4 in x 125 in PALLETS NAS 3610−2L3P, 2L4P LIMITED TO MAX GROSS WEIGHT 7000 lb (3174 kg) EACH
−OR FULL−SIZE CONTAINERS NAS 3610−2L2C AS PER IATA CONTOUR P LIMITED TO MAX GROSS WEIGHT 7000 lb (3174 kg) EACH
A330−300 A330−200
18 14 14 12
79 7 6
9 7 7 6
6
2
2
1
1
−
−
−
−
2
2
1
1
4
LIMITED TO MAX GROSS WEIGHT 7000 lb (3174 kg) EACH
F_AC_020601_1_0040101_01_00
Loading CombinationsFIGURE 2
2-6-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-6-2 Main Deck Cargo Compartments (Loading combinations)
**ON A/C A330-200F
Main Deck Cargo Compartments (Loading combinations)
1. This section gives main deck loading combinations.
2-6-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
1R
1L
2R
2L
3R
3L
4R
4L
5R
5L
6R
6L
7R
7L
8R
8L
9R
9L
10R
10L
11R
11L23 24 25 26
22 HCU−6/E (MILITARY) ULDs
4 HCU−6/E (MILITARY) ULDs
ABR
ABL
BCR
BCL
CER
CEL
EFR
EFL
FHR
FHL
HJR
HJL
JKR
JKL
KMR
KML
MPR
MPL
PRR
PRLTS U
ABL
BCR
BCL
CER
CEL
EFR
EFL
FHR
EFL
HJR
HJL
JKR
JKL
KMR
KML
MPR
MPLSSRR TTPP
18 x 96 in x 125 in ULDs
SIDE BY SIDE (SBS)
20 ULDs
88 in x 125 in (SBS)3 ULDs
88 in x 125 in (SR)
4 x 96 in x 125 in ULDs
SINGLE ROW (SR)
ABR
F_AC_020602_1_0010101_01_00
88" x 108"
Main Deck Cargo CompartmentsLoading combinations
FIGURE 1
2-6-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
AA BB CC DD EE FF GG HH JJ KK LL MM PP RR SS TT
16 ULDs
96 in x 125 in
17 ULDs
88 in x 125 in
AA BB CC DD EE FF GG HH JJ KK LL MM PP RR SS TT UU
AB BC CE EF FH HJ JK KM MP PPAMA
RR SS TT
9 AMA ULDs
96 in x 125 in
4 ULDs
96 in x 125 in SR
AB BC CE EF FH HJ JK KM MP
9 AMA ULDs
96 in x 125 in
4 ULDs
96 in x 125 in
R S T U
F_AC_020602_1_0020101_01_00
AMA
Main Deck Cargo CompartmentsLoading combinations
FIGURE 2
2-6-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
42 AYY ULDs
AYY1R1C
1L
2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R
2C 3R 4C 5C 6C 7C 8C 9C 10C 11C 12C 13C 14C
2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L
1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R
1L 2L 3L 4L 5L 6L 7L 8L 9L 10L15R 16R 17R
15L 16L 17L
1L 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L
2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R
15 16 17
15R 16R 17R
15L 16L 17L
1R
88 in x 62 in
6 AYY ULDs
14 AYY ULDs + 10 AMU ULDs
14 AYY ULDs + 14 SAA ULDs
6 AYY ULDs
SAA
88 in x 62 in
88 in x 62 in
3 SAA ULDs
AYY
AYY
AMJ
F_AC_020602_1_0030101_01_00
Main Deck Cargo CompartmentsLoading combinations
FIGURE 3
2-6-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-6-3 Main and Lower Deck Cross-sections
**ON A/C A330-200F
Main and Lower Deck Cross-sections
1. This section gives Main and Lower Deck Cross-sections for cargo version.
2-6-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
LD6 / AAFCONTAINER AKE AKE
LD3 LD3ALF / AAF / AMF
CONTAINER PALLET
62"
96"
96"
AMA
125"
96"
96"
AMF96" x 125"
LD988" x 125"
88"
96"
REFERENCE CARGO CONFIGURATION LAYOUT
OPTIONAL CARGO CONFIGURATIONS
PALLETS88" x 108"/125"SIDE BY SIDE
PALLETS96" x 125"
SIDE BY SIDE
88"/96"
88" x 125"
79"
96"
62"
96" AYYSAA
125"
F_AC_020603_1_0010101_01_00
AMU AYY AYY AYY AYY
Main and Lower Deck Cross-sectionsFIGURE 1
2-6-3Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-0 Door Clearances
**ON A/C A330-200 A330-200F A330-300
Doors Clearances
1. This section gives doors clearances.
2-7-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-1 Forward Passenger / Crew Doors
**ON A/C A330-200 A330-200F A330-300
Forward Passenger / Crew Door
1. This section gives forward passenger / crew doors clearances.
2-7-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
CRITICALCLEARANCELIMIT
CL
CL
CL
2.43 m(7 ft 11 in)
0.64 m(2 ft 1 in)
1.07 m(3 ft 6 in)
0.75 m(2 ft 5 in)
5.85 m(19 ft 2 in) 3.00 m
(9 ft 10 in)
1.93 m(6 ft 3 in)
SEECHAPTER
2−3
(10 ft 9 in)3.3 m
G_AC_020701_0_F00AAM0_05_00
0.045 m
(1.77 in)
F_AC_020701_1_0010101_01_00
Forward Passenger / Crew DoorsFIGURE 1
2-7-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
CRITICALCLEARANCELIMIT
CL
CL
CL
2.43 m(7 ft 11 in)
0.64 m(2 ft 1 in)
1.07 m(3 ft 6 in)
0.75 m(2 ft 5 in)
5.85 m(19 ft 2 in) 3.00 m
(9 ft 10 in)
1.93 m(6 ft 3 in)
SEECHAPTER
2−3
(10 ft 9 in)3.3 m
0.045 m
(1.77 in)
F_AC_020701_1_0020101_01_00
Forward Passenger / Crew DoorsFIGURE 2
2-7-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-2 Mid Passenger / Crew Doors
**ON A/C A330-200 A330-300
Mid Passenger / Crew Door
1. This section gives mid passenger / crew doors clearances.
2-7-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
(TOP OF FLOOR)
CL
CL
CL
(FROM NOSE)
0.75 m(2 ft 5 in)
1.07 m(3 ft 6 in)
2.43 m(7 ft 11 in)
A330−200: 14.561 m (47ft 9 in)
A330−300: 17.741 m (58 ft 2 in)
0.64 m(2 ft 1 in)
3.41 m(11 ft 2 in)
(6 ft 3 in)
SEECHAPTER
2−3
1.93 m
A
A
A AF_AC_020702_1_0010101_01_00
(1.77 in)0.045 m
Mid Passenger / Crew DoorFIGURE 1
2-7-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-3 Emergency Exits
**ON A/C A330-200 A330-300
Emergency Exits
1. This section gives emergency exits doors clearances.
2-7-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
CL
(TOP OF FLOOR)
CL
CL
0.75 m(2 ft 5 in)
1.07 m(3 ft 6 in)
3.2 m(10 ft 5 in)
0.64 m(2 ft 1 in)
(FROM NOSE)A330−200: 32.767 m (107 ft 6 in)
A330−300: 35.961 m (117 ft 11 in)
1.66 m(5 ft 5 in)
2−3
SEECHAPTER
A A
A
A
F_AC_020703_1_0010101_01_00
2.43 m(7 ft 11 in)
0.03 m(1.18 in)
Emergency ExitsFIGURE 1
2-7-3Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-4 Aft Passenger / Crew Doors
**ON A/C A330-200 A330-300
Aft Passenger / Crew Doors
1. This section gives Aft passenger / crew doors clearances.
2-7-4Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
CRITICALCLEARANCE
LIMIT
CL
CL CL
CL
2.43 m(8 ft)
1.07 m(3 ft 6 in)
0.75 m(2 ft 5 in)
3 m(9 ft 10 in)
1.99 m(6 ft 6 in)
0.64 m(2 ft 1 in)
A330−200: 45.628 m (149 ft 8 in)
A330−300: 50.956 m (167 ft 2 in)
(FROMNOSE)
SEECHAPTER
2−3
A A
A
A
F_AC_020704_1_0010101_01_00
0.045 m(1.8 in)
Aft Passenger / Crew DoorsFIGURE 1
2-7-4Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-5 Forward Cargo Compartment Doors
**ON A/C A330-200 A330-300
Forward Cargo Compartment Doors
1. This section gives forward cargo compartment doors clearances for pax version.
2-7-5Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
(FROM NOSE)
CL
CL
CL
SEECHAPTER
2−3
CL
9.53 m(31 ft 3 in)
0.64 m(2 ft 1 in)
6.37 m(20 ft 10 in)
2.7 m(8 ft 10 in)
1.70 m(5 ft 6 in)
2.04 m(6 ft 8 in)
5.27 m(17 ft 3 in)
MID PASSENGER/CREW DOOR CREW DOORFORWARD PASSENGER/
A A
A
A
F_AC_020705_1_0010101_01_00
FORWARD CARGOCOMPARTMENT DOOR
Forward Cargo Compartment DoorsFIGURE 1
2-7-5Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
Forward Cargo Compartment Doors
1. This section gives forward cargo compartment doors clearances for cargo version.
2-7-5Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
CL
CL
SEECHAPTER
2−3
CL
1.70 m(5 ft 6 in)
2.04 m(6 ft 8 in)
5.27 m(17 ft 3 in)
FORWARD CARGOCOMPARTMENT DOOR
9.53 m (31 ft 3 in) (FROM NOSE)
CREW DOORFORWARD
A A
2.7 m(8 ft 10 in)
A
A
FWD
F_AC_020705_1_0020101_01_01
Forward Cargo Compartment DoorsFIGURE 2
2-7-5Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
PW= 8.45 m (27 ft 8 in)RR= 8.13 m (26 ft 8 in)
9.92m(32 ft 6 in)
2.44 m(8 ft 1 in)
2.58 m(8 ft 5.5 in)
3.36 m(11 ft)
4.6 m(15 ft 1 in)
PW= 18.253 m (59 ft 10 in)RR= 18.081 m (59 ft 3 in)
(FROM NOSE)
(FROM NOSE)
CL
SEECHAPTER
2−3
3.69 m(12 ft 1.2 in)
4.07 m(13 ft 1 in)
A
A
A AF_AC_020705_1_0030101_01_01
Forward Cargo Compartment DoorsFIGURE 3
2-7-5Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-6 Aft Cargo Compartment Doors
**ON A/C A330-200 A330-200F A330-300
Aft Cargo Compartment Doors
1. This section gives Aft cargo compartment doors clearances.
2-7-6Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
SEECHAPTER
2−3
1.68 m(5 ft 6 in)
2.03 m(6 ft 7 in)
5.19 m(17 ft)
(FROM NOSE)A330−200: 38.978 m(127 ft 10 in)
AFT CARGO COMPARTMENT DOOR
(9 ft 1in)2.78 m
AFT PASSENGER/CREW DOOR
CL
CL
CL
CL
A A
A
A
BULK CARGOCOMPARTMENT DOOR
F_AC_020706_1_0010101_01_01
Aft Cargo Compartment DoorsFIGURE 1
2-7-6Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
SEECHAPTER
2−3
1.68 m(5 ft 6 in)
2.03 m(6 ft 7 in)
5.19 m(17 ft)
(FROM NOSE)A330−300: 44.36 m(145 ft 6 in)
AFT CARGO COMPARTMENT DOOR
(9 ft 1in)2.78 m
AFT PASSENGER/CREW DOOR
CL
CL
CL
CL
A A
A
A
BULK CARGOCOMPARTMENT DOOR
F_AC_020706_1_0030101_01_00
Aft Cargo Compartment DoorsFIGURE 2
2-7-6Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
SEECHAPTER
2−3
1.68 m(5 ft 6 in)
2.03 m(6 ft 7 in)
5.19 m(17 ft)
(FROM NOSE)
A330−200F: 38.978 m (127 ft 10 in)
AFT CARGO COMPARTMENT DOOR
(9 ft 1in)2.78 m
CL
CL
CL
CL
A A
A
A
BULK CARGOCOMPARTMENT DOOR
F_AC_020706_1_0020101_01_01
Aft Cargo Compartment DoorsFIGURE 3
2-7-6Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-7 Bulk Cargo Compartment Doors
**ON A/C A330-200 A330-300
Bulk Cargo Compartment Doors
1. This section gives the bulk cargo compartment doors clearances for pax version.
2-7-7Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
CL
CL
CL
SEECHAPTER
2−3
CL
1.11 m(3 ft 7 in)
0.95 m(3 ft 1 in)
1.41 m(4 ft 7 in)
1.07 m(3 ft 6 in)
(FROM NOSE)A330−200: 42.014 m (137 ft 10 in)
A330−300: 47.342 m (155 ft 3 in)
AFT PASSENGER/CREW DOOR(REF)
AFT CARGO COMPARTMENT DOOR
A
A
BULK CARGOCOMPARTMENT DOOR
A A
F_AC_020707_1_0010101_01_00
Bulk Cargo Compartment DoorsFIGURE 1
2-7-7Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
Bulk Cargo Compartment Doors
1. This section gives the bulk cargo compartment doors clearances for cargo version.
2-7-7Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
(FROM NOSE)A330−200F: 42.014 m (137 ft 10 in)
CL
SEECHAPTER
2−3
0.95 m(3 ft 1 in)
1.11 m(3 ft 7 in)
FWD
A
A
BULK CARGOCOMPARTMENT DOOR
AFT CARGOCOMPARTMENT DOOR
CL
CL
1.41 m(4 ft 7 in)
1.07 m(3 ft 6 in)
A A
F_AC_020707_1_0020101_01_00
Bulk Cargo Compartment DoorsFIGURE 2
2-7-7Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-8 Main and Center Landing Gear Doors
**ON A/C A330-200 A330-300
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances for pax version.
2-7-8Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
A
A
GROUND LINE
A/C
C L
81°
3.96 m(13 ft)
1.56 m(5 ft 1 in)
Z−2 m (6 ft 6 in)
3.03 m(9 ft 11in)
2.34 m(7 ft 8 in)
1.1 m(3 ft 7 in)
2.7 m(8 ft 10 in)
A330−200: 26.786 m (87 ft 10 in)
A330−300: 29.45 m (96 ft 7 in)
0.23 m(9 in)
F_AC_020708_1_0010101_01_00
Main Landing Gear DoorsFIGURE 1
2-7-8Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances for cargo version.
2-7-8Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
A330−200F: 26.786 m (87 ft10 in) 3.96 m(13 ft)
GROUND LINE
A/C
C L
81°
1.56 m(5 ft 1 in)
Z−2 m (6 ft 6 in)
3.03 m(9 ft 11in)
2.34 m(7 ft 8 in)
1.1 m(3 ft 7 in)
2.7 m(8 ft 10 in)
0.23 m(9 in)
A
A
F_AC_020708_1_0020101_01_00
Main Landing Gear DoorsFIGURE 2
2-7-8Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-9 Radome
**ON A/C A330-200 A330-200F A330-300
Radome
1. This section gives the radome clearances.
2-7-9Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
67°
CL
STA 7662.5FR1
1.32
5 m
(4 ft
4 in
)1.
25 m
(4 ft
1 in
)
1.65 m(5 ft 4 in)
F_AC_020709_1_0010101_01_00
RadomeFIGURE 1
2-7-9Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-10 APU and Nose Landing Gear Doors
**ON A/C A330-200 A330-300
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances for pax version.
2-7-10Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
FUSELAGE DATUM LINE
FR95
FR101
5.83
m(1
9 ft
1 in
)
6.55
m(2
1 ft
5 in
)
1.82
m(5
ft 1
1 in
)
1.49 m(4 ft 10 in)
F_AC_020710_1_0010101_01_00
APU and Nose Landing Gear DoorsFIGURE 1
2-7-10Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances for cargo version.
2-7-10Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
FUSELAGE DATUM LINE
FR95
FR101
5.83
m(1
9 ft
1 in
)
6.55
m(2
1 ft
5 in
)
1.38 m(4 ft 6 in)
2.00
m(6
ft 6
in)
FWD
F_AC_020710_1_0020101_01_00
APU and Nose Landing Gear DoorsFIGURE 2
2-7-10Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
AIRPLANE PERFORMANCE
3-1-0 General Information
**ON A/C A330-200 A330-200F A330-300
General Information
1. This section gives standard day temperatures.
Section 3-2 indicates payload range information at specific altitudes recommended for long rangecruise with a given fuel reserve condition.
Section 3-3 represents FAR/JAR takeoff runway length requirements at ISA and ISA +15˚C(+27˚F) for engine conditions for FAA/EASA certification :
- PRATT & WHITNEY (PW 4000).- ROLLS-ROYCE (RR Trent 700).- GENERAL ELECTRIC (GE CF6-80E1). (A330-200 and A330-300 only)
Section 3-4 represents FAR/JAR landing runway length requirements for FAA/EASA certification.
Section 3-5 indicates final approach speeds.
Standard day temperatures for the altitude shown are tabulated below :
Standard day temperatures for the altitude
Altitude Standard Day Temperature
FEET METERS ˚F ˚C0 0 59.0 15.02000 610 51.9 11.14000 1219 44.7 7.16000 1829 37.6 3.18000 2438 30.5 -0.8
3-1-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-2-0 Payload / Range
**ON A/C A330-200 A330-200F A330-300
Payload / Range
1. Payload / Range
3-2-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-2-1 ISA Conditions
**ON A/C A330-200 A330-300
ISA Conditions
1. This section gives the payload / range at ISA conditions for pax version.
3-2-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
170
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0010101_01_01
PAYLOAD / RANGEPW 4000 Series Engine
FIGURE 1
3-2-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
170
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0020101_01_01
PAYLOAD / RANGERR TRENT 700 Series Engine
FIGURE 2
3-2-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
0102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
170
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0030101_01_01
PAYLOAD / RANGEGE CF6-80E1 Series Engine
FIGURE 3
3-2-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
175
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0040101_01_01
PAYLOAD / RANGEPW 4000 Series Engine
FIGURE 4
3-2-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0 lb
)
RA
NG
E(n
m)
RA
NG
E(k
m)
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0050101_01_01
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
175
TM
AX
TA
KE
−O
FF
WE
IGH
T :
233
T
PAYLOAD / RANGERR TRENT 700 Series Engine
FIGURE 5
3-2-1Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
0
102030405060708090
100
110
120
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
9000
8500 16
000
5000
6000
7000
8000
9000
1000
011
000
1200
013
000
1400
015
000
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
175
T
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0
MA
X T
AK
E−
OF
F W
EIG
HT
: 23
3 T
PA
YLO
AD
(kg)
0
1000
095
00
1700
018
000
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
F_AC_030201_1_0060101_01_01
PAYLOAD / RANGEGE CF6-80E1 Series Engine
FIGURE 6
3-2-1Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
ISA Conditions
1. This section gives the payload / range at ISA conditions for cargo version.
3-2-1Page 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
173
TM
AX
TA
KE
−O
FF
WE
IGH
T :
233
T
PA
YLO
AD
(kg)
160
150
140
130
120
110
100 90 80 70 60 50 40 30 20 10 0
70 0
00
65 0
00
60 0
00
55 0
00
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0 0
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
010
0020
0030
0040
0050
0060
0070
0080
00
1600
014
000
1200
010
000
8000
6000
9000
1000
0
1800
040
0020
000
F_AC_030201_1_0070101_01_01
PAYLOAD / RANGERR TRENT 700 Series Engine
FIGURE 7
3-2-1Page 9
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
178
TM
AX
TA
KE
−O
FF
WE
IGH
T :
227
T
PA
YLO
AD
(kg)
160
150
140
130
120
110
100 90 80 70 60 50 40 30 20 10 0
70 0
00
65 0
00
60 0
00
55 0
00
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0 0
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
010
0020
0030
0040
0050
0060
0070
0080
00
1600
014
000
1200
010
000
8000
6000
9000
1000
0
1800
040
0020
000
F_AC_030201_1_0080101_01_01
PAYLOAD / RANGERR TRENT 700 Series Engine
FIGURE 8
3-2-1Page 10
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
173
TM
AX
TA
KE
−O
FF
WE
IGH
T :
233
T
PA
YLO
AD
(kg)
160
150
140
130
120
110
100 90 80 70 60 50 40 30 20 10 0
70 0
00
65 0
00
60 0
00
55 0
00
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0 0
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
010
0020
0030
0040
0050
0060
0070
0080
00
1600
014
000
1200
010
000
8000
6000
9000
1000
0
1800
040
0020
000
F_AC_030201_1_0090101_01_01
PAYLOAD / RANGEPW 4000 Series Engine
FIGURE 9
3-2-1Page 11
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
PA
YLO
AD
(100
0lb)
RA
NG
E(N
M)
RA
NG
E(K
M)
NO
TE
:M
AX
ZE
RO
FU
EL
WE
IGH
T :
178
TM
AX
TA
KE
−O
FF
WE
IGH
T :
227
T
PA
YLO
AD
(kg)
160
150
140
130
120
110
100 90 80 70 60 50 40 30 20 10 0
70 0
00
65 0
00
60 0
00
55 0
00
50 0
00
45 0
00
40 0
00
35 0
00
30 0
00
25 0
00
20 0
00
15 0
00
10 0
00
5 00
0 0
MA
X S
TR
UC
TU
RA
L P
AY
LOA
D
010
0020
0030
0040
0050
0060
0070
0080
00
1600
014
000
1200
010
000
8000
6000
9000
1000
0
1800
040
0020
000
F_AC_030201_1_0100101_01_01
PAYLOAD / RANGEPW 4000 Series Engine
FIGURE 10
3-2-1Page 12
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-3-0 FAR / JAR Takeoff Weight Limitation
**ON A/C A330-200 A330-200F A330-300
FAR / JAR Takeoff Weight Limitation
1. FAR / JAR Takeoff Weight Limitation
3-3-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-3-1 ISA Conditions
**ON A/C A330-200 A330-200F A330-300
FAR / JAR Takeoff Weight Limitation
1. This section gives the takeoff weight limitation at ISA conditions.
3-3-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
02
46
8
0 2 4 6 8
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
V.M
.C
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
F_AC_030301_1_0010101_01_01
Takeoff Weight LimitationISA Conditions - PW 4000 Series Engine
FIGURE 1
3-3-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
02
46
8
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235
20 4 6 8
TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
V.M
.C
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
F_AC_030301_1_0020101_01_01
Takeoff Weight LimitationISA Conditions - RR TRENT 700 Series Engine
FIGURE 2
3-3-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
02
46
8
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235
TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)V
.M.C
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION0 2 4 6 8
F_AC_030301_1_0030101_01_01
Takeoff Weight LimitationISA Conditions - GE CF6-80E1 Series Engine
FIGURE 3
3-3-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-3-2 ISA +15˚C (ISA +27˚F) Conditions
**ON A/C A330-200 A330-200F A330-300
ISA +15 ˚C (ISA +27 ˚F) Conditions
1. This section gives the takeoff weight limitation at ISA +15˚C (ISA +27˚F) conditions.
3-3-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
02
46
8
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235
0 2 4 6 8
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
V.M
.C
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
F_AC_030302_1_0010101_01_01
FAR / JAR Takeoff Weight LimitationISA +15˚C (ISA +27˚F) Conditions - PW 4000 Series Engine
FIGURE 1
3-3-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
0 2 4 6 8
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
V.M
.C
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
02
46
8
F_AC_030302_1_0020101_01_01
FAR / JAR Takeoff Weight LimitationISA +15˚C (ISA +27˚F) Conditions - RR TRENT 700 Series Engine
FIGURE 2
3-3-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
RU
NW
AY
LE
NG
TH
(100
0 F
t)
RU
NW
AY
LE
NG
TH
(100
0 m
)
NO
TE
:
02
46
8
320
340
360
380
400
420
440
460
480
500
520
540
560
300
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
DIN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
OT
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T
46
810
1214
162 0.5
11.
52
2.5
33.
54
4.5
5
255
135
155
175
195
215
235
0 2 4 6 8
TA
KE
−O
FF
WE
IGH
T10
00 L
b10
00 K
g
BR
AK
E E
NE
RG
Y L
IMIT
AT
ION
V.M
.C
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 F
t)
F_AC_030302_1_0030101_01_01
FAR / JAR Takeoff Weight LimitationISA +15˚C (ISA +27˚F) Conditions - GE CF6-80E1 Series Engine
FIGURE 3
3-3-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-4-0 FAR / JAR Landing Field Length
**ON A/C A330-200 A330-200F A330-300
Landing Field Length
1. Landing Field Length
3-4-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-4-1 ISA Conditions All series engines
**ON A/C A330-200 A330-200F A330-300
ISA Conditions All series engine
1. This section gives the landing field length.
3-4-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
.T
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.F
AR
/JA
R L
AN
DIN
GLE
NG
TH
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
(100
0 m
)(1
000
Ft) 15
050
020
025
040
045
030
035
0
230
7010
020
015
0
3456782.
5 1
1.52
24
68
10S
EA
LE
VE
L
(100
0 F
t)A
IRF
IELD
ELE
VA
TIO
N
F_AC_030401_1_0010101_01_01
ISA
CO
ND
ITIO
NS
CO
NF
. FU
LL
FAR / JAR Landing Field LengthISA Conditions - PW 4000 Series Engine
FIGURE 1
3-4-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
.T
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.F
AR
/JA
R L
AN
DIN
GLE
NG
TH
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
(100
0 m
)(1
000
Ft)
46
810
150
500
200
250
400
450
300
350
230
7010
020
015
0
3456782.
5 1
1.52
SE
A L
EV
EL
2
AIR
FIE
LD E
LEV
AT
ION
(100
0 F
t)
F_AC_030401_1_0020101_01_01
ISA
CO
ND
ITIO
NS
CO
NF
. FU
LL
FAR / JAR Landing Field LengthISA Conditions - RR TRENT 700 Series Engine
FIGURE 2
3-4-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
NO
TE
:T
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
.T
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.F
AR
/JA
R L
AN
DIN
GLE
NG
TH
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
(100
0 m
)(1
000
Ft)
46
810
150
500
200
250
400
450
300
350
230
7010
020
015
0
3456782.
5 1
1.52
SE
A L
EV
EL
2
AIR
FIE
LD E
LEV
AT
ION
(100
0 F
t)
F_AC_030401_1_0030101_01_01
ISA
CO
ND
ITIO
NS
CO
NF
. FU
LL
FAR / JAR Landing Field LengthISA Conditions - GE CF6-80E1 Series Engine
FIGURE 3
3-4-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-5-0 Final Approach Speed
**ON A/C A330-200 A330-200F A330-300
Final Approach Speed
1. Final Approach Speed
3-5-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-5-1 Final Approach Speed
**ON A/C A330-200 A330-200F A330-300
Final Approach Speed
1. This section gives the final approach speed.
3-5-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
NO
TE
:
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
GT
HE
AIR
CR
AF
T.
C.A
.S (
Kts
)
90100
110
120
130
140
150 20
024
028
032
036
040
044
048
0
220
100
120
140
160
180
200
80
F_AC_030501_1_0010101_01_01
LAN
DIN
G G
EA
R E
XT
EN
DE
DC
ON
F. F
ULL
V R
EF
Final Approach SpeedPW 4000 Series Engine
FIGURE 1
3-5-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
NO
TE
:
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
GT
HE
AIR
CR
AF
T.
C.A
.S (
Kts
)
90100
110
120
130
140
150
200
240
280
320
360
400
440
480
220
100
120
140
160
180
200
80
F_AC_030501_1_0020101_01_01
LAN
DIN
G G
EA
R E
XT
EN
DE
DC
ON
F. F
ULL
V R
EF
Final Approach SpeedRR TRENT 700 Series Engine
FIGURE 2
3-5-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
NO
TE
:
GR
OS
S W
EIG
HT
(100
0 K
g)
GR
OS
S W
EIG
HT
(100
0 Lb
)
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LY.
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
GT
HE
AIR
CR
AF
T.
C.A
.S (
Kts
)
90100
110
120
130
140
150 20
024
028
032
036
040
044
048
0
220
100
120
140
160
180
200
80
F_AC_030501_1_0030101_01_01
LAN
DIN
G G
EA
R E
XT
EN
DE
DC
ON
F. F
ULL
V R
EF
Final Approach SpeedGE CF6-80E1 Series Engine
FIGURE 3
3-5-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A330-200 A330-200F A330-300
General Information
1. This section provides airplane turning capability and maneuvering characteristics.
For ease of presentation, this data has been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,it reflects the turning capability of the aircraft in favorable operating circumstances. This data shouldonly be used as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft type.
In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary in the level of performance, over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea or high risk of jet blast damage. For these reasons, ground maneuvering requirements should becoordinated with the using airlines prior to layout planning.
4-1-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-2-0 Turning Radii
**ON A/C A330-200 A330-200F A330-300
Turning Radii
1. This section gives the turning radii.
4-2-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
NOTE: SEE NEXT PAGES FOR DIMENSIONS
R5
R3
R6
R4
55°
R2
60°
65°
72°
R1
F_AC_040200_1_0040101_01_02
Turning RadiiAll ModelsFIGURE 1
4-2-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
19.4°20°
TYPE OFTURN
2
EFFECTIVESTEERING ANGLE
STEERINGANGLE
68.3224
A330−300 TURNING RADII
mft
80.8265
79.6261
R4
105.1345
R5
81.5267
R6
89.7294
WING NOSE TAIL
NOTE: ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNSDEPENDING ON THE SITUATIONTYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLE TURN; ANDDIFFERENTIAL BRAKING TO INITIATE THE TURN ONLYTYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE TURN; ANDNO DIFFERENTIAL BRAKING AT ALL
R1 R2 R3RMLG LMLG NLG
24.2°25°252.1171
64.7212
64.6212
88.9292
67.0220
74.7245
29.0°30°241.0135
53.6176
54.7179
78.0256
57.6189
64.8213
33.8°35°232.9108
45.5149
47.7156
70.0230
51.0167
58.0190
38.6°40°226.788
39.3129
42.7140
63.8209
46.6153
52.7173
43.2°45°221.771
34.3113
39.1128
58.8193
43.3142
48.5159
47.8°50°217.658
30.299
36.2119
54.7179
40.8134
45.5149
52.2°55°214.247
26.888
34.1112
51.4169
38.9128
42.9141
56.3°60°211.337
23.978
32.4106
48.5159
37.5123
40.9134
60.1°65°28.929
21.571
31.2102
46.2152
36.5120
39.3129
63.8°72° (MAX)26.722
19.363
30.098
44.1145
35.5116
38.1125
48.2°50°117.357
29.998
36.1118
54.5179
40.7134
45.1148
52.9°55°113.645
26.286
33.7111
50.8167
38.6127
42.6140
57.6°60°110.434
23.075
31.8104
47.7156
36.9121
40.5133
62.1°65°17.625
20.166
30.5100
44.9147
35.9118
38.5126
67.8°72° (MAX)14.515
17.156
29.095
41.9137
34.7114
36.9121
TURNING RADII TABLE
mftmftmftmftmftmftmftmftmftmft
mftmftmftmftmft
IT IS POSSIBLE TO GET LOWER VALUES THAN THOSEFROM TYPE 1 BY APPLYING DIFFERENTIAL BRAKINGDURING THE WHOLE TURN. F_AC_040200_1_0020101_01_02
Turning RadiiSteady State Turning Radii
FIGURE 2
4-2-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
19.2°20°
TYPE OFTURN
2
EFFECTIVESTEERING ANGLE
STEERINGANGLE
60.5198
mft
72.7239
70.8232
R4
98.2322
R5
72.7239
R6
81.3267
WING NOSE TAIL
NOTE: ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNSDEPENDING ON THE SITUATIONTYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLE TURN; ANDDIFFERENTIAL BRAKING TO INITIATE THE TURN ONLYTYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE TURN; ANDNO DIFFERENTIAL BRAKING AT ALL
R1 R2 R3RMLG LMLG NLG
23.9°25°246.0151
58.3191
57.5189
84.1276
59.9197
68.1223
28.6°30°236.2119
48.5159
48.7160
74.6245
51.6169
59.3195
33.3°35°229.195
41.4136
42.6140
67.6222
46.0151
53.2175
38.0°40°223.677
35.9118
38.4126
62.2204
42.3139
48.3158
42.5°45°219.163
31.5103
34.7114
58.2191
38.9128
45.2148
46.9°50°215.651
27.992
32.2106
54.7179
36.7120
42.2138
51.2°55°212.641
24.982
30.399
51.9170
35.1115
40.2132
5.1°60°210.133
22.574
28.995
49.6163
33.9111
38.5126
59.6°65°28.227
20.567
27.891
47.7156
33.0108
37.2122
62.0°72° (MAX)26.421
18.761
27.189
46.0151
32.5107
35.9118
48.4°50°114.648
26.988
31.9105
53.6176
36.5120
41.3135
52.2°55°111.839
24.179
30.199
51.0167
35.0115
39.4129
57.7°60°18.829
21.169
28.694
47.9157
33.7111
37.0121
62.2°65°16.521
18.661
27.791
45.5149
33.2109
35.2115
68.1°72° (MAX)13.612
15.752
26.085
43.3142
32.0105
34.2112
mftmftmftmftmftmftmftmftmftmft
mftmftmftmftmft
IT IS POSSIBLE TO GET LOWER VALUES THAN THOSEFROM TYPE 1 BY APPLYING DIFFERENTIAL BRAKINGDURING THE WHOLE TURN.
A330−200/200F TURNING RADII
TURNING RADII TABLE
F_AC_040200_1_0030101_01_02
Turning RadiiSteady State Turning Radii
FIGURE 3
4-2-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-3-0 Minimum Turning Radii
**ON A/C A330-200 A330-200F A330-300
Minimum Turning Radii
1. This section gives the minimum turning radii.
4-3-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
NOTE: TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLETURN; AND DIFFERENTIAL BRAKING TOINITIATE THE TURN ONLYTYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE
67.8°72° (MAX)
TYPE OFTURN
1
EFFECTIVESTEERING ANGLE
STEERINGANGLE
X
26.4
87
A330−300 MINIMUM TURNING RADII
m
ft
Y
10.7
35
A
46.2
152
R3
29.0
95
R4
41.9
137
R5
34.7
114
R6
36.9
121
NLG WING NOSE TAIL
63.8°72° (MAX)226.5
87
m
ft
13.3
44
49.4
162
30.0
98
44.1
145
35.5
116
38.1
125
R5
R3
X
Y
A
MINIMUM TURNINGWIDTH
TURN; AND NO DIFFERENTIAL BRAKING AT ALL
NOTE: IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
R4
R6
F_AC_040300_1_0010101_01_03
Minimum Turning RadiiFIGURE 1
4-3-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
NOTE: TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLETURN; AND DIFFERENTIAL BRAKING TOINITIATE THE TURN ONLYTYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE
68.1°72° (MAX)
TYPE OFTURN
1
EFFECTIVESTEERING ANGLE
STEERINGANGLE
X
24.2
79
A330−200/200F MINIMUM TURNING RADII
m
ft
Y
9.3
31
A
41.5
136
R3
26.0
85
R4
41.0
135
R5
32.0
105
R6
34.2
112
NLG WING NOSE TAIL
62.0°72° (MAX)223.4
77
m
ft
12.3
40
45.6
150
27.1
89
45.1
148
32.5
107
35.9
118
R5
R3
X
Y
A
MINIMUM TURNINGWIDTH
TURN; AND NO DIFFERENTIAL BRAKING AT ALL
NOTE: IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
F_AC_040300_1_0070101_01_00
R4
R6
Minimum Turning RadiiFIGURE 2
4-3-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A330-200 A330-200F A330-300
Visibility from Cockpit in Static Position.
1. This section gives the visibility from cockpit in static position.
4-4-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
135
62
NOTEPILOT’S EYEPOSITION
7 ft 10.7 in2.40 m
45 ft 1.3 in13.75 m
21 ft 10.6 in6.67 m
°
°
°
19 20’
PILOT’S EYE POSITION
0.53 m1 ft 9 in
25°
111°
36°30°
42°
30°36°
62°
42°
115°
135°
F_AC_040400_1_0010101_01_00
Visibility from Cockpit in Static PositionFIGURE 1
4-4-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
135
NOTEPILOT’S EYEPOSITION
7 ft 10.7 in2.40 m
51 ft 8 in15.75 m
21 ft 10.6 in6.67 m
°
°
19 20’
0.53 m1 ft 9 in
25°
111°
115°
135°
F_AC_040400_1_0030101_01_00
PILOT’S EYE POSITION
62°
36°
62°
36°30°
42°
30°
42°
Visibility from Cockpit in Static PositionFIGURE 2
4-4-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A330-200 A330-200F A330-300
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths.
4-5-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A330-200 A330-200F A330-300
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn - runway to taxiway.
4-5-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
APPROX 10.6 m(35 ft)
(15 ft)APPROX 4.7 m
45 m(150 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m(75 ft)
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
NLG PATH
MLG PATH
F_AC_040501_1_0010101_01_01
135˚ Turn - Runway to TaxiwayJudgemental Oversteer Method
FIGURE 1
4-5-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
TURN R = 45 m(150 ft)
FILLET R = 25.5 m(85 ft)
APPROX 1.3 m
ADDITIONAL FILLET TO MEET4.5 m (15 ft) EDGE CLEARANCE
(4 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
45 m(150 ft)
RUNWAY
23 m(75 ft)
NLG PATH
MLG PATH
CENTERLINE
TAXIWAYCENTERLINE
F_AC_040501_1_0060101_01_00
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE 2
4-5-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
FAA LEAD−IN FILLET
L = 75 m (250 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
(19 ft)APPROX R = 5.9 m
APPROX 11.3 m(37 ft)
45 m(150 ft)
23 m(75 ft)
NLG PATH
MLG PATH
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
F_AC_040501_1_0020101_01_01
135˚ Turn - Runway to TaxiwayJudgemental Oversteer Method
FIGURE 3
4-5-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
FAA LEAD−IN FILLET
L = 75 m (250 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
(15 ft)APPROX 4.5 m
45 m(150 ft)
23 m(75 ft)
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
NLG PATH
MLG PATH
F_AC_040501_1_0070101_01_00
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE 4
4-5-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A330-200 A330-200F A330-300
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn - runway to taxiway.
4-5-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
45 m(150 ft)
23 m(75 ft)
(45 ft)APPROX 13.8 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
(37 ft)APPROX 11.2 m
NLG PATH
MLG PATH
F_AC_040502_1_0010101_01_01
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
90˚ Turn - Runway to TaxiwayJudgemental Oversteer Method
FIGURE 1
4-5-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m(75 ft)
TURN R = 45 m(150 ft)
(17 ft)APPROX 5.1 m
FILLET R = 25.5 m(85 ft)
45 m(150 ft) NLG PATH
MLG PATH
F_AC_040502_1_0080101_01_00
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE 2
4-5-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
(45 ft)APPROX 13.6 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m
45 m(150 ft)
23 m(75 ft)
(47 ft)APPROX 14.3 m
FAA LEAD−IN FILLETL = 75 m (250 ft)
NLG PATH
MLG PATH
(150 ft)
F_AC_040502_1_0020101_01_01
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
90˚ Turn - Runway to TaxiwayJudgemental Oversteer Method
FIGURE 3
4-5-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
(24 ft)APPROX 7.3 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
(150 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m(75 ft)
NLG PATH
MLG PATH
45 m
F_AC_040502_1_0090101_01_00
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE 4
4-5-2Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-3 180˚ Turn on a Runway
**ON A/C A330-200 A330-200F A330-300
180˚ Turn on a Runway
1. This section gives the 180˚ turn on a runway.
4-5-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
NOTE: TYPE 1 VALUES.IT IS POSSIBLE TO GET LOWER VALUES THANTHOSE FROM TYPE 1 BY APPLYING DIFFERENTIALBRAKING DURING THE WHOLE TURN.
4.5 m(15 ft)
R6 = 36.9 m(121 ft)
R4 = 41.9 m(137 ft)
APPROX 55.2 m(181 ft)
R3 = 29 m(95 ft)
R5 = 34.7 m(114 ft)
4.5 m(15 ft)
NLG PATH
MLG PATH
RUNWAY CENTERLINE
F_AC_040503_1_0130101_01_00
180˚ Turn on a Runway180˚ Turn on a Runway
FIGURE 1
4-5-3Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
4.5 m(15 ft)
R6 = 34.2 m(112 ft)
R4 = 43.3 m(142 ft)
APPROX 50.5 m(166 ft)
R3 = 26 m(85 ft)
R5 = 32 m(105 ft)
4.5 m(15 ft)
NOTE: TYPE 1 VALUES.IT IS POSSIBLE TO GET LOWER VALUES THANTHOSE FROM TYPE 1 BY APPLYING DIFFERENTIALBRAKING DURING THE WHOLE TURN.
RUNWAY CENTERLINE
NLG PATH
MLG PATH
F_AC_040503_1_0140101_01_00
180˚ Turn on a Runway180˚ Turn on a Runway
FIGURE 2
4-5-3Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-4 135˚ Turn - Taxiway to Taxiway
**ON A/C A330-200 A330-200F A330-300
135˚ Turn - Taxiway to Taxiway
1. This section gives the 135˚ turn - taxiway to taxiway.
4-5-4Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
FILLET R = 25.5 m(85 ft)
APPROX 13.6 m(45 ft)
TAXIWAY CENTERLINE
TURN R = 45 m(150 ft)
APPROX 5.3 m(17 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m(75 ft)
TAXIWAY CENTERLINE
(75 ft)23 m
NLG PATH
MLG PATH
F_AC_040504_1_0030101_01_01
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteer Method
FIGURE 1
4-5-4Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
(75 ft)23 m
FILLET R = 25.5 m(85 ft)
APPROX 2.5 m(8 ft)
TAXIWAY CENTERLINE
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
ADDITIONAL FILLET TO MEET4.5 m (15 ft) EDGE CLEARANCE
TAXIWAY CENTERLINE
23 m(75 ft)
NLG PATH
MLG PATH
F_AC_040504_1_0070101_01_00
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE 2
4-5-4Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
(75 ft)23 m
FILLET R = 25.5 m(85 ft)
APPROX 13 m(43 ft)
TAXIWAY CENTERLINE
TURN R = 45 m(150 ft)
APPROX 6.3 m(21 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m(75 ft)
TAXIWAY CENTERLINE
NLG PATH
MLG PATH
F_AC_040504_1_0040101_01_01
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteer Method
FIGURE 3
4-5-4Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
FILLET R = 25.5 m(85 ft)
APPROX 5.5 m(18 ft)
TAXIWAY CENTERLINE
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
TAXIWAY CENTERLINE 23 m(75 ft)
(75 ft)23 m
NLG PATH
MLG PATH
F_AC_040504_1_0080101_01_00
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE 4
4-5-4Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-5 90˚ Turn - Taxiway to Taxiway
**ON A/C A330-200 A330-200F A330-300
90˚ Turn - Taxiway to Taxiway
1. This section gives the 90˚ turn - taxiway to taxiway.
4-5-5Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
TAXIWAY CENTERLINE
(75 ft)
TAXIWAY CENTERLINEAPPROX 12.2 m
(40 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
APPROX 10.4 m(34 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m
23 m(75 ft)
NLG PATH
MLG PATH
F_AC_040505_1_0030101_01_01
90˚ Turn - Taxiway to TaxiwayJudgemental Oversteer Method
FIGURE 1
4-5-5Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
APPROX 3.8 m(12 ft)
4.5 m (15 ft) EDGE CLEARANCEADDITIONAL FILLET TO MEET
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
TAXIWAY CENTERLINE
(75 ft)23 m NLG PATH
MLG PATH
TAXIWAY CENTERLINE
23 m(75 ft)
F_AC_040505_1_0100101_01_00
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE 2
4-5-5Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
TAXIWAY CENTERLINE
TAXIWAY CENTERLINE
APPROX 13 m(43 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
APPROX 14.4 m(47 ft)
(75 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m
23 m(75 ft)
NLG PATH
MLG PATH
F_AC_040505_1_0040101_01_01
90˚ Turn - Taxiway to TaxiwayJudgemental Oversteer Method
FIGURE 3
4-5-5Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
23 m(75 ft)
TAXIWAY CENTERLINE(20 ft)APPROX 6.2 m
FILLET R = 25.5 m(85 ft)
TAXIWAY CENTERLINE
FAA LEAD−IN FILLETL = 75 m (250 ft)
23 m(75 ft)
TURN R = 45 m(150 ft)
NLG PATH
MLG PATH
F_AC_040505_1_0110101_01_00
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE 4
4-5-5Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-6-0 Runway Holding Bay (Apron)
**ON A/C A330-200 A330-200F A330-300
Runway Holding Bay (Apron)
1. This section gives the runway holding bay (Apron).
4-6-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
6.1 m(20 ft)
6.1 m(20 ft)
COORDINATE WITH USING AIRPLANE FOR SPECIFICPLANNED OPERATING PROCEDURES.
NOTES:
12.2 m(40 ft)
45 m(150 ft)
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
23 m(75 ft)
190 m(625 ft)
90 m(300 ft)
HOLDINGPOINT
F_AC_040600_1_0010101_01_01
97.3 m(319 ft)
Runway Holding Bay (Apron)FIGURE 1
4-6-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-7-0 Airplane Parking
**ON A/C A330-200 A330-200F A330-300
Airplane Parking
1. The following figures and charts show the rectangular space required for parking against the terminalbuilding.
The rectangle includes allowance for swinging the airplane on arrival and departure.- Steering Geometry- Minimum Parking Space Requirements
4-7-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
73.85
PARKING45° ENTRY PUSH OUT
PARKINGSTRAIGHT ENTRY PUSH BACK
PARKING90° ENTRY PUSH OUT
67.2356
.53 68
.26
82.5
7
96.76
F_AC_040700_1_0010101_01_00
Airplane ParkingSteering Geometry
FIGURE 1
4-7-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
100.7773
.85
PARKINGPARALLEL IN POWER OUT
PARKING45° ENTRY POWER OUT
95.89
72.0
2
F_AC_040700_1_0020101_01_00
Airplane ParkingSteering Geometry
FIGURE 2
4-7-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
0
20
40
60
80
100
120
140
160
180
200
220
240
260
280
300
10
20
30
40
50
60
70
80
90
100
0 10 20 30 40 50 60 70 80 90 100 110
0 20 40 60 80 100 120 140 160 180 200 220 240 260 280 300 320 340
DISTANCE ALONG TERMINAL (m)
DISTANCE ALONG TERMINAL (ft)
(m)
DISTANCE OUTFROM TERMINAL
45° ENTRY PUSH OUT
STRAIGHT ENTRY PUSH BACK
PARALLEL IN POWER OUT
45° ENTRY POWER OUT
90° ENTRY PUSH OUT
F_AC_040700_1_0040101_01_00
Airplane ParkingMinimum Parking Space Requirements
FIGURE 3
4-7-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
PARKINGSTRAIGHT ENTRY PUSH BACK
93.68
82.1
6
PARKING90° ENTRY PUSH OUT
63.89 75.3053
.39 66
.14
PARKING45° ENTRY PUSH OUT
F_AC_040700_1_0030101_01_00
Airplane ParkingSteering Geometry
FIGURE 4
4-7-0Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
73.8
5PARKING
PARALLEL IN POWER OUT
PARKING45° ENTRY POWER OUT
99.42
95.89
71.3
6
F_AC_040700_1_0050101_01_00
Airplane ParkingSteering Geometry
FIGURE 5
4-7-0Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F
0
20
40
60
80
100
120
140
160
180
200
220
240
260
280
300
10
20
30
40
50
60
70
80
90
100
0 10 20 30 40 50 60 70 80 90 100 110
0 20 40 60 80 100 120 140 160 180 200 220 240 260 280 300 320 340
DISTANCE ALONG TERMINAL (m)
DISTANCE ALONG TERMINAL (ft)
(m)
DISTANCE OUTFROM TERMINAL
PARALLEL IN POWER OUT45° ENTRY POWER OUT
90° ENTRY PUSH OUT
STRAIGHT ENTRY PUSH BACK
45° ENTRY PUSH OUT
F_AC_040700_1_0060101_01_00
Airplane ParkingMinimum Parking Space Requirements
FIGURE 6
4-7-0Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
**ON A/C A330-200 A330-200F A330-300
TERMINAL SERVICING
1. Terminal servicing
This chapter provides typical ramp layouts, corresponding minimum turnaround time estimations,locations of ground service points and service requirements.The information given in this chapter reflects ideal conditions. Actual ramp layouts and servicerequirements may vary according to local regulations, airline procedures and the airplane condition.
Section 5.1 shows typical ramp layouts for passenger aircraft at the gate or on an Open Apron andfreighter aircraft on an Open Apron.
Section 5.2 shows the minimum turnaround schedules for full servicing arrangements (turnroundstations).
Section 5.3 shows the minimum turnaround schedule for reduced servicing arrangements (en routestations).
Section 5.4 gives the locations of ground service connections, the standard of connections used andtypical capacities and requirements.
Section 5.5 provides the engine starting pneumatic requirements for different engine types anddifferent ambient temperatures.
Section 5.6 provides the air conditioning requirements for heating and cooling (pull-down and pull-up)using ground conditioned air for different ambient temperatures.
Section 5.7 provides the air conditioning requirements for heating and cooling to maintain a constantcabin air temperature using low pressure conditioned air.
Section 5.8 shows the ground towing requirements taking into account different ground surface andaircraft conditions.
5-0-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-1-0 Airplane Servicing Arrangements
**ON A/C A330-200 A330-300
Airplane Servicing Arrangements
1. This section provides typical ramp layouts, showing the various GSE items in position during typicalturnaround scenarios for the passenger aircraft.
These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for the positioning and operation on the ramp.
The associated turnaround station is given in the section 5-2-1 for Full Servicing Turn Round Charts.
The associated minimum turnaround time for Transit Turn Round Charts is given in a section 5-3-1.
5-1-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
Airplane Servicing Arrangements
1. Airplane Servicing Arrangements
This section provides typical ramp layouts, showing the various GSE items in position during typicalturnaround scenarios for the passenger aircraft.
These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for the positioning and operation on the ramp.
The associated turnaround station is given in the section 5-2-1 for Full Servicing Turn Round Charts.
5-1-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-1-1 Symbols Used on Servicing Diagrams
**ON A/C A330-200 A330-200F A330-300
Symbols Used on Servicing Diagrams
1. This table gives the symbols used on servicing diagrams.
Ground Support Equipment
AC AIR CONDITIONING UNITAS AIR START UNIT
CAT CATERING TRUCKCB CONVEYOR BELT
CLEAN CLEANING TRUCKFUEL FUEL HYDRANT DISPENSER or TANKERGPU GROUND POWER UNIT
LD CL LOWER DECK CARGO LOADERLV LAVATORY VEHICLE
MD CL MAIN DECK CARGO LOADERPBB PASSENGER BOARDING BRIDGE
PS PASSENGER STAIRSTOW TOW TRACTORULD ULD TRAINWV POTABLE WATER VEHICLE
5-1-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-1-2 Loading (Open Apron)
**ON A/C A330-200 A330-300
Loading (Open Apron)
1. This section gives the typical ramp layout for the passenger aircraft on an Open Apron.
5-1-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
GPU
TOW
PS CAT
PS CAT
AS
CATPS
AC LD CL
LD CL
LV
WVULD BULK
FUEL
ULD
FUEL
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
CB
F_AC_050102_1_0010101_01_01
Airplane Servicing ArrangementsTypical Ramp Layout (Open Apron)
FIGURE 1
5-1-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
GPU
TOW
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
F_AC_050102_1_0070101_01_00
CATPS
PS CAT
CATPS
AS
ULD
ULD
CB BULK
LV
FUELFUEL
ACLD CL
LD CL
WV
Airplane Servicing ArrangementsTypical Ramp Layout (Open Apron)
FIGURE 2
5-1-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
Loading (Open Apron)
1. This section gives the typical ramp layout for cargo version on an Open Apron.
5-1-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
WV
PS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
F_AC_050102_1_0020101_01_02
GPU
AS
LV
ULDLD CL
LD CL
AC
ULD
BULKULDCB
FUELFUEL
MD CL
TOW
Airplane Servicing ArrangementsTypical Ramp Layout (Open Apron)
FIGURE 3
5-1-2Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-1-3 Loading (Passenger Bridge)
**ON A/C A330-200 A330-300
Loading (Passenger Bridge)
1. This section gives the typical ramp layout for the passenger aircraft at a gate with 2 passengerboarding bridges.
5-1-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
CAT
CAT
CLEAN CAT
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
GP
U
AS
AC
ULDLD CL
LD CL
ULD
LV
F_AC_050103_1_0010101_01_01
BULKCB
FUELFUEL
PBB
PBB
TOW
WV
Airplane Servicing ArrangementsTypical Ramp Layout (gate area)
FIGURE 1
5-1-3Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
F_AC_050103_1_0060101_01_00
AS
GP
U
AC LD CL
CAT
CAT
CAT
LD CL
LV
CLEAN
WV
BULK
ULD
CB
FUEL FUEL
PBB
PBB
TOW
ULD
Airplane Servicing ArrangementsTypical Ramp Layout (gate area)
FIGURE 2
5-1-3Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-2-0 Terminal Operations - Full Servicing Turn Round Charts
**ON A/C A330-200 A330-200F A330-300
Terminal Operations - Full Servicing Turn Round Charts
1. This section provides a series of charts showing typical activities during turnaround at destinationairports.
This data is provided to show the general scope and type of activities involved in ramp operationsduring the turnaround of an aircraft.
Varying Airline practices and operating circumstances may result in different sequences and differenttime intervals to do the activities shown.
5-2-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-2-1 Full Servicing Turn Round Charts
**ON A/C A330-200 A330-300
Full Servicing Turn Round Charts
**ON A/C A330-200
1. Assumptions for full servicing turn round chart.
A. PASSENGER BOARDING/DEBOARDING (PB/D)
Deboarding : 293 passengers (30 business + 263 tourists)- For full servicing, all passengers deboard and board- Doors used: L1 + L2- Deboarding:
- 160 pax at L1 (30 business and 130 tourists) and 133 pax at L2- Deboarding rate = 25 pax/min- Priority deboarding for premium passengers
- Boarding:- 30 pax at L1 and 263 pax at L2- Boarding rate = 15 pax/min
- Last Pax Seating Allowance (LPS) + headcounting = + 4 min
B. CARGO- 6 LD3 + 2 pallets for AFT CC- 8 LD3 + 2 pallets for FWD CC- 1 000 kg (2 205 lb) in Bulk CC- LD-3 off-loading/loading times:
- off-loading = 1.2 min/LD-3- loading = 1.4 min/LD-3
- Pallet loading times:- off-loading = 2.4 min/pallet- loading = 2.8 min/pallet
- Bulk off-loading/loading times:- off-loading = 9.2 min/t- loading = 10.5 min/t
C. REFUELLING- Block fuel for Nominal Range through 4 nozzles- 115 000 liters (30 380 US gal) at 50 psi- Dispenser positioning or removal = 3 min (fuel truck change) / if any = 5 min
D. CLEANING- Cleaning is performed in available time
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
E. CATERING- 3 catering vehicles- 36 Full size trolley: 10 FST at R1, 9 FST at R2 and 17 FST at R4- FST exchange time = 1.5 min/FST
F. GROUND HANDLING/SERVICING- Start of operations :
(1) Bridges = t0 = 0(2) Others = t0 + 1 min
- Vehicle positioning/removal = 2 min (fuel truck excluded)- Ground Power Unit (GPU) = up to 2 × 90 kVA- Air conditioning = two carts- Potable water servicing: replenish 700 l (185 US gal); flow rate: 60 l/min (15.85 US
gal/min)- Waste water servicing (draining + rinsing): discharge 700 l (185 US gal)- Dollies per tractor = 4
**ON A/C A330-300
2. Assumptions for full servicing turn round chart.
A. PASSENGER BOARDING/DEBOARDING (PB/D)
Deboarding : 332 passengers (30 business + 302 tourists)- For full servicing, all passengers deboard and board- Doors used: L1 + L2- Deboarding:
- 180 pax at L1 (30 business and 150 tourists) and 152 pax at L2- Deboarding rate = 25 pax/min- Priority deboarding for premium passengers
- Boarding:- 30 pax at L1 and 302 pax at L2- Boarding rate = 15 pax/min
- Last Pax Seating Allowance (LPS) + headcounting = + 4 min
B. CARGO- 8 LD3 + 2 pallets for AFT CC- 12 LD3 + 2 pallets for FWD CC- 1 000 kg (2 205 lb) in Bulk CC- LD-3 off-loading/loading times:
- off-loading = 1.2 min/LD-3- loading = 1.4 min/LD-3
- Pallet loading times:- off-loading = 2.4 min/pallet- loading = 2.8 min/pallet
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
- Bulk off-loading/loading times:- off-loading = 9.2 min/t- loading = 10.5 min/t
C. REFUELLING- Block fuel for Nominal Range through 4 nozzles- 89 100 l (23 538 US gal) at 50 psi- Dispenser positioning or removal = 3 min (fuel truck change) / if any = 5 min
D. CLEANING- Cleaning is performed in available time
E. CATERING- 3 catering vehicles- 39 Full size trolley: 8 FSTE at R1, 13 FSTE at R2 and 18 FSTE at R4- FST exchange time = 1.5 min/FST
F. GROUND HANDLING/SERVICING- Start of operations :
(1) Bridges = t0 = 0(2) Others = t0 + 1 min
- Vehicle positioning/removal = 2 min (fuel truck excluded)- Ground Power Unit (GPU) = up to 2 × 90 kVA- Air conditioning = two carts- Potable water servicing: replenish 700 l (185 US gal); flow rate: 60 l/min (15.85 US
gal/min)- Waste water servicing (draining + rinsing): discharge 700 l (185 US gal)- Dollies per tractor = 4
5-2-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
F_AC_050201_1_0010101_01_01
0 10 20 30 40 50 60 70
DEBOARDING/BOARDING AT L1
HEADCOUNTING
CATERING AT R1
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
DEBOARDING/BOARDING AT L2
CATERING AT R2
CATERING AT R4
CARGO AFT CC
TRT : 60 min
POSITIONING/REMOVAL
ACTIVITY
AVAILABLE TIME
Full Servicing Turn Round ChartsTurn Round Time 60 min.
FIGURE 1
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Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
0 10 20 30 40 50 60 70
DEBOARDING/BOARDING AT L1
HEADCOUNTING
CATERING AT R1
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
DEBOARDING/BOARDING AT L2
CATERING AT R2
CATERING AT R4
CARGO AFT CC
TRT : 64 min
POSITIONING/REMOVAL
ACTIVITY
F_AC_050201_1_0020101_01_01
AVAILABLE TIME
Full Servicing Turn Round ChartsTurn Round Time 64 min.
FIGURE 2
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
Full Servicing Turn Round Charts
1. Assumptions for full servicing turn round chart.
A. PASSENGER BOARDING/DEBOARDING (PB/D)
4 Couriers- Door used: L1- Deboarding:
- 4 couriers at L1- Deboarding rate = 25 pax/min
- Boarding:- 4 couriers at L1- Boarding rate = 15 pax/min
B. CARGO100% cargo exchange- 22 pallets on MD CC- 4 pallets for AFT CC- 2 LD3 + 4 pallets for FWD CC- 1 000 kg (2 205 lb) in Bulk CC- LD-3 off-loading/loading times:
- off-loading = 1.2 min/LD-3- loading = 1.4 min/LD-3
- Lower Deck pallet loading times:- off-loading = 2.4 min/pallet- loading = 2.8 min/pallet
- Bulk off-loading/loading times:- off-loading = 9.2 min/t- loading = 10.5 min/t
C. REFUELLING- Block fuel for Nominal Range through 4 nozzles- 115 000 l (30 380 US gal) at 50 psi- Dispenser positioning or removal = 3 min (fuel truck change) / if any = 5 min
D. CLEANING- Courier area cleaning is performed in available time
E. CATERING- Catering of galley (if installed) is performed through door L1 (standard units only) and in
available time.
F. GROUND HANDLING/SERVICING- Start of operations :
5-2-1Page 6
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
(1) Stair = t0 = 0(2) Others = t0 + 1 min
- Vehicle positioning/removal = 2 min (fuel truck excluded)- Ground Power Unit (GPU) = up to 2 × 90 kVA- Air conditioning = two carts- Potable water servicing: replenish 700 l (185 US gal); flow rate: 60 l/min (15.85 US
gal/min)- Waste water servicing (draining + rinsing): discharge 700 l (185 US gal)- Dollies per tractor = 4
5-2-1Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
0 10 20 30 40 50 60 70
DEBOARDING/BOARDING AT L1
CATERING AT L1
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CARGO AFT CC
TRT : 62 min
POSITIONING/REMOVAL
ACTIVITY
F_AC_050201_1_0050101_01_01
CARGO MD
AVAILABLE TIME
AVAILABLE TIME
Full Servicing Turn Round ChartsTurn Round Time 62 min.
FIGURE 3
5-2-1Page 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-3-0 Terminal Operations - Transit Turn Round Charts
**ON A/C A330-200 A330-300
Terminal Operations - Transit Turn Round Charts
1. This section provides a series of charts showing typical activities during turnaround at transit airports.
This data is provided to show the general scope and type of activities involved in ramp operationsduring the turnaround of an aircraft.
Varying Airline practices and operating circumstances may result in different sequences and differenttime intervals to do the activities shown.
5-3-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-3-1 Transit Turn Round Charts
**ON A/C A330-200 A330-300
Transit Turn Round Charts
**ON A/C A330-200
1. Assumptions for transit turn round chart.
A. PASSENGER BOARDING/DEBOARDING (PB/D)
Deboarding : 293 passengers (30 business + 263 tourists)- 50% pax in transit, all passengers deboard and board- Doors used: L1 + L2- Deboarding:
- 160 pax at L1 (30 business and 130 tourists) and 133 pax at L2- Deboarding rate = 25 pax/min- Priority deboarding for premium passengers
- Boarding:- 30 pax at L1 and 263 pax at L2- Boarding rate = 15 pax/min
- Last Pax Seating Allowance (LPS) + headcounting = + 4 min
B. CARGO
For transit, 50% of luggages are exchanged in one cargo compartment only- 1 container loader for AFT CC- 5 LD3 for AFT CC- LD-3 off-loading/loading times:
- off-loading = 1.2 min/LD-3- loading = 1.4 min/LD-3
C. REFUELLING- Refueling through 2 nozzles- For transit, fuel uplift is 30% of maximum fuel uplift. (Max = 139 090 l (36 744 US gal))
Note: local rules and regulations to be respected- Passengers boarding can start before refuel is finished- Dispenser positioning or removal = 3 min (fuel truck change) / if any = 5 min
D. CLEANING- Cleaning is performed in available time
E. CATERING- Time needed just for additional meals- Assumptions: 10 min
5-3-1Page 1
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
F. GROUND HANDLING/SERVICING- Start of operations :
(1) Bridges = t0 = 0(2) Others = t0 + 1 min
- Vehicle positioning/removal = 2 min (fuel truck excluded)- Ground Power Unit (GPU) = up to 2 × 90 kVA- Air conditioning = two carts- No potable water servicing- No waste water servicing- Dollies per tractor = 4
**ON A/C A330-300
2. Assumptions for transit turn round chart.
A. PASSENGER BOARDING/DEBOARDING (PB/D)
Deboarding : 332 passengers (30 business + 302 tourists)- 50% pax in transit, all passengers deboard and board- Doors used: L1 + L2- Deboarding:
- 165 pax at L1 (30 business and 135 tourists) and 167 pax at L2- Deboarding rate = 25 pax/min- Priority deboarding for premium passengers
- Boarding:- 30 pax at L1 and 302 pax at L2- Boarding rate = 15 pax/min
- Last Pax Seating Allowance (LPS) + headcounting = + 4 min
B. CARGO
For transit, 50% of luggages are exchanged in one cargo compartment only- 1 container loader for AFT CC- 5 LD3 for AFT CC- LD-3 off-loading/loading times:
- off-loading = 1.2 min/LD-3- loading = 1.4 min/LD-3
C. REFUELLING- Refueling through 2 nozzles- For transit, fuel uplift is 30% of maximum fuel uplift. (Max = 97 530 l (25 765 US gal))
Note: local rules and regulations to be respected- Passengers boarding can start before refuel is finished- Dispenser positioning or removal = 3 min (fuel truck change) / if any = 5 min
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
D. CLEANING- Cleaning is performed in available time
E. CATERING- Time needed just for additional meals- Assumptions: 10 min
F. GROUND HANDLING/SERVICING- Start of operations :
(1) Bridges = t0 = 0(2) Others = t0 + 1 min
- Vehicle positioning/removal = 2 min (fuel truck excluded)- Ground Power Unit (GPU) = up to 2 × 90 kVA- Air conditioning = two carts- No potable water servicing- No waste water servicing- Dollies per tractor = 4
5-3-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
0 5 15 20 25 30 35 40
DEBOARDING/BOARDING AT L1
HEADCOUNTING
CATERING AT R1
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
DEBOARDING/BOARDING AT L2
CATERING AT R2
CATERING AT R4
CARGO AFT CC
TRT : 44 min
POSITIONING/REMOVAL
ACTIVITY
F_AC_050301_1_0010101_01_01
10 45 50
AVAILABLE TIME
Transit Turn Round ChartsTurn Round Time 44 min.
FIGURE 1
5-3-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
0 10 20 30 40 50 60 70
DEBOARDING/BOARDING AT L1
HEADCOUNTING
CATERING AT R1
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
DEBOARDING/BOARDING AT L2
CATERING AT R2
CATERING AT R4
CARGO AFT CC
TRT : 48 min
POSITIONING/REMOVAL
ACTIVITY
F_AC_050301_1_0020101_01_01
AVAILABLE TIME
Transit Turn Round ChartsTurn Round Time 48 min.
FIGURE 2
5-3-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-0 Ground Service Connections
**ON A/C A330-200 A330-200F A330-300
Ground Service Connections
1. Ground Service Connections.
5-4-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-1 Ground Service Connections Layout
**ON A/C A330-200 A330-300
Ground Service Connections Layout
1. This section gives the ground service connections layout.
Ground Service Connections Layout
1 -- OXYGEN SYSTEM2 -- EXTERNAL POWER (ELECTRICAL)
3 -- POTABLE WATER DRAIN4 -- LOW PRESSURE PRE-CONDITIONING5 -- HIGH PRESSURE AIR PRE-CONDITIONING AND ENGINE STARTING6 -- IDG OIL FILLING7 -- ENGINE OIL FILLING8 -- PRESSURE REFUEL9 -- OVERWING REFUEL10 -- HYDRAULIC GROUND POWER SUPPLY (YELLOW)
11 -- HYD RESERVOIR FILLING AND GROUND POWER SUPPLY (GREEN)
12 -- HYD RESERVOIR AIR PRESSURIZATION & GROUND POWER SUPPLY (BLUE)
13 -- NITROGEN CHARGING FOR HYDRAULIC ACCUMULATORS14 -- REFUEL/DEFUEL PANEL
15 -- POTABLE WATER FILLING16 -- TOILET SERVICING17 -- APU OIL FILLING18 -- GROUNDING POINTS
5-4-1Page 1
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
2
8
17
17
9
8
9
9
8
1 2 3 4
513
6
7
7
6
14 3 15
1611
12
18
18
18
18
18
181 3 4 5 6 7 1012
1311 3 15 16
10
F_AC_050401_1_0010101_01_00
Ground Service ConnectionsFIGURE 1
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Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
Ground Service Connections Layout
1. Ground Service Connections Layout
Ground Service Connections Layout
1 -- POTABLE WATER SERVICE PANEL2 -- REMOTE WATER DRAIN3 -- HYDRAULIC GROUND POWER SUPPLY (YELLOW)
4 -- IDG OIL FILLING4.1 -- ENGINE OIL FILLING5 -- WASTE WATER PANEL6 -- ELECTRICAL GROUND POWER RECEPTACLES7 -- LOW PRESSURE AIR8 -- FUEL GRAVITY FILLING9 -- AIR CHARGING FOR HYDRAULIC ACCUMULATORS10 -- HYD RESERVOIR FILLING AND GROUND POWER (GREEN)
11 -- HYD RESERVOIR AIR CHARGING & GROUND POWER (BLUE)
12 -- REFUEL/DEFUEL COUPLING
13 -- HIGH PRESSURE AIR14 -- APU OIL FILLING15 -- REFUEL/DEFUEL PANEL
5-4-1Page 3
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
F_AC_050401_1_0020101_01_01
1424.146 25
14
8
12
4.1
4
135
8
12
7
2 16 2
11
9153
10
Ground Service ConnectionsFIGURE 2
5-4-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-2 Grounding Points
**ON A/C A330-200 A330-200F A330-300
Grounding Points
**ON A/C A330-200 A330-200F
1. Grounding Points.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
On Nose Landing Gear leg :6.67 m(21.88 ft) on centerline
1.40 m(4.59 ft)
On left Main Landing Gearleg :
28.37 m(93.08 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
On right Main LandingGear leg :
28.37 m(93.08 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
A. The grounding stud on each landing gear leg is designed for use with a clip-on connector (suchas Appleton TGR).
B. The grounding studs are used to connect the aircraft to an approved ground connection on theramp or in the hangar for :- refuel/defuel operations.- maintenance operations.- bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tyre is sufficient.
**ON A/C A330-300
2. Grounding Points.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DISTANCE : Meters (ft)
On Nose Landing Gear leg :6.67 m(21.88 ft) on centerline
1.40 m(4.59 ft)
On left Main Landing Gearleg :
31.53 m(103.44 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
On right Main LandingGear leg :
31.53 m(103.44 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
A. The grounding stud on each landing gear leg is designed for use with a clip-on connector (suchas Appleton TGR).
B. The grounding studs are used to connect the aircraft to an approved ground connection on theramp or in the hangar for :- refuel/defuel operations.- maintenance operations.- bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tyre is sufficient.
5-4-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
(1)(2)
LANDINGGEAR
GROUND CABLE(OPTIONAL)
GROUNDINGPOINT
GROUNDINGPOINT
NOSE GEAR MAIN GEAR
AA
A
F_AC_050402_1_0010101_01_00
Ground Service ConnectionsGrounding Points
FIGURE 1
5-4-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
NOTE:
RIB22
RIB23
A
A
R SIDE SYMETRICAL
B
A
B
F_AC_050402_1_0020101_01_00
Ground Service ConnectionsGrounding Points
FIGURE 2
5-4-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-3 Hydraulic System
**ON A/C A330-200 A330-200F A330-300
Hydraulic System
1. Ground service panels.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
Green System :41.3 m(135.50 ft)
1.34 m(4.40 ft)
2.23 m(7.32 ft)
Yellow System :35.4 m(116.14 ft)
1.30 m(4.27 ft)
1.95 m(6.40 ft)
Blue System :34.41 m(112.89 ft)
1.28 m(4.20 ft)
1.94 m(6.36 ft)
2. Reservoir Pressurization.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
One 1/4 in. self sealingconnection common to the3 reservoirs.(Blue System GroundService Panel) :
34.47 m(113.09 ft)
1.41 m(4.63 ft)
1.89 m(6.20 ft)
**ON A/C A330-200 A330-200F
3. Accumulator Charging, 5 connections.
(one for each accumulator) for :
5-4-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
Yellow Systemaccumulator:
35.55 m(116.63 ft)
1.43 m(4.69 ft)
1.91 m(6.27 ft)
Green Systemaccumulator:
41.52 m(136.22 ft)
1.33 m(4.36 ft)
2.19 m(7.19 ft)
Blue System accumulator:34.54 m
(113.32 ft)1.38 m(4.53 ft)
1.9 m(6.23 ft)
Blue system brakeaccumulator:
34.54 m(113.32 ft)
1.24 m(4.07 ft)
1.9 m(6.23 ft)
**ON A/C A330-300
4. Accumulator Charging, 5 connections.
(one for each accumulator) for :
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
Yellow Systemaccumulator:
35.55 m(116.63 ft)
1.43 m(4.69 ft)
1.91 m(6.27 ft)
Green Systemaccumulator:
41.52 m(136.22 ft)
1.33 m(4.36 ft)
2.19 m(7.19 ft)
Blue System accumulator:34.54 m
(113.32 ft)1.38 m(4.53 ft)
1.9 m(6.23 ft)
Blue system brakeaccumulator:
34.54 m(113.32 ft)
1.18 m(3.87 ft)
1.9 m(6.23 ft)
**ON A/C A330-200 A330-200F A330-300
5. Reservoir Filling, 2 connections.
One self-sealing connection for pressurized supply on the Green system ground service panel.
5-4-3Page 2
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@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
One handpump fillingconnection.
41.31 m(135.53 ft)
1.3 m(4.27 ft)
2.11 m(6.92 ft)
6. Reservoir Drain.
One 3/8 in. self-sealing connection on reservoir for :
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
Green System :29.03 m(95.24 ft)
2.12 m(6.96 ft)
2.40 m(7.87 ft)
Yellow System :33.17 m
(108.83 ft)0.70 m(2.30 ft)
3.80 m(12.47 ft)
Blue System :29.03 m(95.24 ft)
2.12 m(6.96 ft)
2.40 m(7.87 ft)
7. Ground Test.
Three 1 in. self-sealing connections and three 1-1/2 in. self-sealing connections (one pair per system)
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUNDGreen System groundservice panel:
34.92 m(114.57 ft)
1.35 m(4.43 ft)
2.2 m(7.22 ft)
Yellow System groundservice panel:
29.03 m(95.24 ft)
1.30 m(4.27 ft)
2.0 m(6.56 ft)
Blue System groundservice panel:
28.03 m(91.96 ft)
1.28 m(4.20 ft)
2.0 m(6.56 ft)
5-4-3Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-4 Electrical System
**ON A/C A330-200 A330-200F A330-300
Electrical System
**ON A/C A330-200 A330-300
1. Electrical System.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDEL SIDE
MEAN HEIGHTFROM
GROUNDTwo standard 6 pinconnectors ISO R 461specification.
7.2 m(23.62 ft) on centerline
1.98 m(6.50 ft)
A. Supply :115/200 Volt, 3-Phase, 400 Hz.
B. Electrical connectors for servicing :- AC outlets : Hubbel 5258.- DC outlets : Hubbel 7472.- Vacuum cleaner outlets : Hubbel 5258.
**ON A/C A330-200F
2. Electrical System.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDEL SIDE
MEAN HEIGHTFROM
GROUNDTwo standard 6 pinconnectors ISO R 461specification.
7.2 m(23.62 ft) on centerline
2.29 m(7.51 ft)
A. Supply :115/200 Volt, 3-Phase, 400 Hz.
B. Electrical connectors for servicing :- AC outlets : Hubbel 5258.- DC outlets : Hubbel 7472.- Vacuum cleaner outlets : Hubbel 5258.
5-4-4Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-5 Oxygen System
**ON A/C A330-200 A330-200F A330-300
Oxygen System
1. Oxygen System.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDEL SIDE
MEAN HEIGHTFROM
GROUND
OPTION 1 :2.50 m(8.20 ft)
0.53 m(1.74 ft)
3.20 m(10.50 ft)
OPTION 2 :2.50 m(8.20 ft)
0.68 m(2.23 ft)
3.20 m(10.50 ft)
- 0 -- Basic : external charging in the avionic compartment.- 1 -- Option.- 2 -- Option.Zero, one or two service connections (external charging in the avionics compartment) MS22066 Std.
NOTE : Internal Charging Connection Provided.
5-4-5Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-6 Fuel System
**ON A/C A330-200 A330-200F A330-300
Fuel System
**ON A/C A330-200
1. Refuel/defuel access
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUND
Refuel/defuel coupling26.80 m(87.92 ft)
12.60 m(41.33 ft)
12.60 m(41.33 ft)
5.00 m(16.40 ft)
Overwing gravity refuelcap
31.30 m(102.69 ft)
17.20 m(56.43 ft)
17.20 m(56.43 ft)
5.80 m(19.03 ft)
A. Four Standard 2.5 in. connections -- ISO R45 SPEC.
B. Two service connections (gravity refuel).
2. Refuel/defuel control panel.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUND
Refuel/defuel controlpanel
31.10 m(102.03 ft)
0.8 m(2.62 ft)
1.90 m(6.23 ft)
A. Flow Rate : 1580 l/min (417 U.S. gal/min) per connection.
B. Maximum Pressure : 50.00 psi (3.45 bar).
**ON A/C A330-200F
3. Refuel/defuel access
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUND
5-4-6Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DISTANCE : Meters (ft)
refuel/defuel coupling26.80 m(87.92 ft)
12.60 m(41.33 ft)
12.60 m(41.33 ft)
5.10 m(16.73 ft)
Overwing gravity refuelcap
31.30 m(102.69 ft)
17.20 m(56.43 ft)
17.20 m(56.43 ft)
6.10 m(20.01 ft)
A. Four Standard 2.5 in. connections -- ISO R45 SPEC.
B. Two service connections (gravity refuel).
4. Refuel/defuel control panel.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUND
Refuel/defuel controlpanel :
31.10 m(102.03 ft)
0.8 m(2.62 ft)
1.90 m(6.23 ft
A. Flow Rate : 1580 l/min (417 U.S. gal/min) per connection.
B. Maximum Pressure : 50.00 psi (3.45 bar).
**ON A/C A330-300
5. Refuel/defuel access
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUND
Refuel/defuel coupling30.00 m(98.45 ft)
12.60 m(41.33 ft)
12.60 m(41.33 ft)
5.00 m(16.40 ft)
Overwing gravity refuelcap
34.50 m(113.19 ft)
17.20 m(56.43 ft)
17.20 m(56.43 ft)
5.80 m(19.02 ft)
A. Four Standard 2.5 in. connections -- ISO R45 SPEC.
B. Left side option.
C. Two service connections (gravity refuel).
6. Refuel/defuel control panel.
5-4-6Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUND
Refuel/defuel controlpanel :
34.30 m(112.53 ft)
0.8 m(2.62 ft)
1.90 m(6.23 ft)
A. Flow Rate : 1580 l/min (417 U.S. gal/min) per connection.
B. Maximum Pressure : 50.00 psi (3.45 bar).
5-4-6Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-7 Pneumatic System
**ON A/C A330-200 A330-200F A330-300
Pneumatic System
**ON A/C A330-200 A330-200F
1. High Pressure Connectors.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND20.72 m(67.98 ft)
0.84 m(2.76 ft)
1.96 m(6.43 ft)Connections for engine
starting and cabin airconditioning :
21.08 m(69.16 ft)
0.84 m(2.76 ft)
1.94 m(6.36 ft)
A. Two standard 3 in. TC20 connections for engine starting and cabin air conditioning.
2. Low Pressure Connectors.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND19.29 m(63.29 ft)
0.31 m(1.02 ft)
2.08 m(6.82 ft)Connections for
preconditioned air 19.29 m(63.29 ft)
0.76 m(2.49 ft
2.11 m(6.92 ft)
A. Two standard 8 in. connections (SAE - AS4262 TYPE B) for preconditioned air.
**ON A/C A330-300
3. High Pressure Connectors.
5-4-7Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND23.9 m
(78.41 ft)0.84 m(2.76 ft)
1.79 m(5.87 ft)Connections for engine
starting and cabin airconditioning :
24.25 m(79.56 ft)
0.84 m(2.76 ft)
1.79 m(5.87 ft)
A. Two standard 8 in. connections (SAE - AS4262 TYPE B) for preconditioned air.
4. Low Pressure Connectors.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND22.48 m(73.75 ft)
0.31 m(1.02 ft)
1.86 m(6.10 ft)Connections for
preconditioned air 22.48 m(73.75 ft)
0.76 m(2.49 ft)
0.76 m(2.49 ft)
A. Two standard 8 in. connections (SAE - AS4262 TYPE B) for preconditioned air.
5-4-7Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-8 Potable Water System
**ON A/C A330-200 A330-200F A330-300
Potable Water System
**ON A/C A330-200 A330-300
1. Service panel.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
Service panel, located betweenframe 69--70 :
48.15 m(157.97 ft)
0.51 m(1.67 ft)
3.15 m(10.33 ft)
- one heated 3/4 in. quick release filling connection.- one heated 3/4 in. overflow and discharge connection.- one ground pressurization connection.
**ON A/C A330-200F
2. Service panel.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
Service panel, located betweenframe 33-34 :
14.03 m(46.03 ft)
0.76 m(2.49 ft)
2.64 m(8.66 ft)
- one heated 3/4 in. quick release filling connection.- one heated 3/4 in. overflow and discharge connection.- one ground pressurization connection.
**ON A/C A330-200 A330-300
3. Fwd drainage panel.
5-4-8Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUNDFwd drainage panel, locatedbetween frame 28--29comprising :
14.70 m(48.23 ft)
0.60 m(1.97 ft)
1.90 m(6.23 ft)
- one standard 3/4 in. drain connection with back-up mechanical control.
**ON A/C A330-200F
4. Fwd drainage panel.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUNDFwd drainage panel, locatedbetween frame 15A-16comprising :
6.1 m(20.01 ft)
1.7 m(5.58 ft)
3.07 m(10.07 ft)
- one standard 3/4 in. drain connection with back-up mechanical control.- Usable capacity : 100 l (26.42 US gal).
**ON A/C A330-200
5. Aft drainage panel.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUNDAft drainage panel,located between frame55--56 :
40.18 m(131.82 ft)
0.72 m(2.36 ft)
2.46 m(8.07 ft)
- one standard 3/4 in. drain connection with back-up mechanical control.- one standard 3/4 in. overflow and discharge connection with back-up mechanical control.
5-4-8Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
A. Usable capacity :- 700 l (184.92 US gal) standard.- 1050 l (277.38 US gal) standard option.
**ON A/C A330-300
6. Aft drainage panel.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROMGROUND
Aft drainage panel,located between frame51.1--57.2 :
40.18 m(131.82 ft)
0.72 m(2.36 ft)
2.46 m(8.07 ft)
- one standard 3/4 in. drain connection with back-up mechanical control.- one standard 3/4 in. overflow and discharge connection with back-up mechanical control.
A. Usable capacity :- 700 l (184.92 US gal) standard.- 1050 l (277.38 US gal) standard option.
**ON A/C A330-200 A330-200F A330-300
7. Fill rate :
Potable water storage tank installed in ... or ...
Fwd-tank (and opt-tank) [sect.15/16] aft-tank [sect.18]
Pressure :50 psi(3.45 bar)
125 psi(8.62 bar)
50 psi(3.45 bar)
125 psi(8.62 bar)
Flow :45 l/min(11.89 US gal/min)
73 l/min(19.28 US gal/min)
56 l/min(14.79 US gal/min)
85 l/min(22.45 US gal/min)
5-4-8Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-9 Oil System
**ON A/C A330-200 A330-200F A330-300
Oil System
1. Engine Oil Tank and IDG for PW 4000 series engine.
A. Engine Oil Replenishment :
One gravity filling cap and one pressure filling connection per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
Engine Oil Filling:25.7 m
(84.32 ft)10.6 m
(34.78 ft)8.07 m
(26.48 ft)2.23 m(7.32 ft)
(1) Tank capacity :- Full level : 8.00 US gal (30.28 l).- Usable : 5.75 US gal (21.77 l).
B. IDG Oil Replenishment :
One pressure filling connection per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
IDG Oil Pressure FillingConnection:
26.16 m(85.83 ft)
10.07 m(33.04 ft)
8.66 m(28.41 ft)
1.50 m(4.92 ft)
- Max delivery pressure required : 40 psi (2.76 bar).- Max OIL capacity of the IDG : 1.1 US gal (4.16 l).
2. Engine Oil Tank and IDG for RR Trent 700 series engine
A. Engine Oil Replenishment :
One gravity filling cap.
One ozone self sealing pressure fill and overfill connector per engine.
5-4-9Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
Engine Oil Filling:23.9 m
(78.41 ft)7.92 m
(25.98 ft)10.82 m(35.50 ft)
2.05 m(6.73 ft)
(1) Tank capacity :- Full level : 7.18 US gal (27.18 l.- Usable : 6.00 US gal (22.71 l).
B. IDG Oil Replenishment :
One ozone self sealing pressure fill and overfill connector per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
IDG Oil Pressure FillingConnection:
24.38 m(79.99 ft)
9.65 m(31.66 ft)
9.09 m(29.82 ft)
0.8 m(2.62 ft)
- Max delivery pressure required : 40 psi (2.76 bar).- Max OIL capacity of the IDG : 1.12 US gal (4.24 l).
**ON A/C A330-200 A330-300
3. Engine Oil Tank and IDG for GE CF6-80E1 series engine
A. Engine Oil Replenishment :
One gravity filling cap and one pressure filling connection per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
Engine Oil Filling:24.93 m(81.79 ft)
10.00 m(32.81 ft)
8.73 m(28.64 ft)
1.71 m(5.61 ft)
5-4-9Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
(1) Tank capacity :- Full level : 6.49 US gal (24.57 l).- Usable : 6.09 US gal (23.05 l).
B. IDG Oil Replenishment :
One pressure filling connection per engine.
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
ENGINE 1 (Left) ENGINE 2 (Right)
MEANHEIGHT FROM
GROUND
IDG Oil Pressure FillingConnection:
23.03 m(75.56 ft)
7.96 m(26.12 ft
10.77 m(35.33 ft)
2.35 m(7.71 ft)
- Max delivery pressure required : 40 psi (2.76 bar).- Max OIL capacity of the IDG : 1.1 US gal (4.16 l).
5-4-9Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
YELLOW
GREEN
OIL LEVELSIGHTGLASS
OIL TANKCAP
DUSTCOVER
OVERFLOWCONNECTOR
PRESSUREFILL
VALVE
PRESSUREFILL
CONNECTOR
OIL TANK
FULL
1 QT
2 QT
3 QT
FULL
−1 QT
−2 QT
−3 QT
AB
B
FULL
−1 QT
−2 QT
−3 QTCLOSE
OPEN
A
F_AC_050409_1_0010101_01_00
Ground Service ConnectionsEngine Oil Tank - PW 4000 series engine
FIGURE 1
5-4-9Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
1 OIL FILLER CAP
2 OVERFLOW COUPLING
3 PRESSURE FILLCOUPLING
D5324
A
B
B
FULL FULL
LIT
RE
S R
EQ
UIR
ED
US
QU
AR
TZ
RE
QU
IRE
D
5
4
3
2
1
5
4
3
2
1
A
F_AC_050409_1_0020101_01_00
Ground Service ConnectionsEngine Oil Tank - RR Trent 700 series engine
FIGURE 2
5-4-9Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
SIGHT GLASS
TANK FULL
TANK NOT FULLSCUPPER
DRAIN
RELIEFVALVE
OVERFILLPORT
ENGINEOIL TANKFILLER CAP
PRESSUREFILL PORT
5000EN
ENGINE OILTANK
A
B
B
A
F_AC_050409_1_0030101_01_00
Ground Service ConnectionsEngine Oil Tank - GE CF6-80E1 series engine
FIGURE 3
5-4-9Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
RED
YELLOW
GREEN
RED
2
1
PRESSUREFILL VALVE
CONNECTOR
OVERFLOWDRAIN VALVECONNECTOR
OIL LEVELSIGHTGLASS
OIL DIFFERENTIALPRESSUREINDICATOR
A
B
A
B
OVER FULL
ADDOIL
F_AC_050409_1_0040101_01_00
Ground Service ConnectionsIDG Oil Tank - PW 4000 series engine
FIGURE 4
5-4-9Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
OVER FULL
ADDOIL
RED
YELLOW
GREEN
RED
1 SIGHT GLASS
2 DRAIN PLUG
3 OVERFILL DRAIN CONNECTOR
4 PRESSURE FILL CONNECTOR
A
A
F_AC_050409_1_0050101_01_00
Ground Service ConnectionsIDG Oil Tank - RR Trent 700 series engine
FIGURE 5
5-4-9Page 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
1
A
A
B
PRESSUREFILL VALVE
CONNECTOR
OVERFLOWDRAIN VALVECONNECTOR
5
3
B
A
F_AC_050409_1_0060101_01_00
Ground Service ConnectionsIDG Oil Tank - GE CF6-80E1 series engine
FIGURE 6
5-4-9Page 9
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
APU Oil System
**ON A/C A330-200 A330-200F
1. APU Oil System.
APU oil gravity filling cap.
DISTANCE : Meters (ft)
AFT OF NOSE
FROM AIRPLANECENTERLINE(LEFT HAND)
MEAN HEIGHT FROMGROUND
APU Oil Replenishment :55.00 m(180.45 ft)
0.4 m(1.31 ft)
8.00 m(26.25 ft)
A. Tank capacity (usable) :- APU Type : 331-350 : 7.3 l (1.93 US gal).
**ON A/C A330-300
2. APU Oil System.
APU oil gravity filling cap.
DISTANCE : Meters (ft)
AFT OF NOSE
FROM AIRPLANECENTERLINE(LEFT HAND)
MEAN HEIGHT FROMGROUND
APU Oil Replenishment :60.3 m(197.83 ft)
0.4 m(1.31 ft)
8.00 m(26.25 ft)
A. Tank capacity (usable) :- APU Type : 331-350 : 7.3 l (1.93 US gal).
5-4-9Page 10
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
F_AC_050409_1_0070101_01_01
FR95
316AR
315AL
FR101
A
PRESSURE FILLOVERFLOW PORT
OIL SCUPPER
GRAVITY FILLPORT
LUBRIFICATION OIL FILTER
GENERATOR SCAVENGE OIL FILTER
OIL PUMPMODULE5100KT9
A
B
OIL FILLERCAP
OVERFLOW PORT
PRESSUREFILL PORT
OIL SIGHTGLASS
OIL SCUPPER
GRAVITY FILL PORT
B
DO NOT REMOVE OILFILLER CAP WHEN OILLEVEL IS ABOVE FULLMARK ON SIGHT GLASS
FWD
Ground Service ConnectionsAPU Oil Tank
FIGURE 7
5-4-9Page 11
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-10 Vacuum Toilet System
**ON A/C A330-200 A330-200F A330-300
Vacuum Toilet System
**ON A/C A330-200 A330-300
1. Vacuum Toilet System
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDEL SIDE
MEAN HEIGHTFROM
GROUND
Waste Service panel:50.65 m
(166.17 ft)0.09 m(0.30 ft)
3.6 m(11.81 ft)
A. Waste Service panel comprising :- Standard : One standard 4 in. drain connection and two 1 in. flushing connections.- Standard option : One standard 4 in. drain connection and three 1 in. flushing connections.
B. Capacity waste tanks :- Standard : 700 l (184.92 US gal).- Standard option : 1050 l (277.38 US gal).
C. Chemical fluid :- Standard : 36 l (9.51 US gal).- Standard option : 54 l (14.27 US gal).
**ON A/C A330-200F
2. Vacuum Toilet System
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDEL SIDE
MEAN HEIGHTFROM
GROUND
Waste Service panel 1:5.61 m
(18.41 ft)1.43 m(4.69 ft)
2.95 m(9.68 ft)
Waste Service panel 2:6.1 m
(20.01 ft)1.69 m(5.54 ft)
3.15 m10.33 ft)
A. A330-200F has two waste service panels :- First panel : One standard connection Roylyn 1 in for Flushing and filling.
5-4-10Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
- Second panel : One standard Taco type valve 4 in for draining.
NOTE : Handle used for drainage is located on the first panel.
B. Capacity waste tanks :- Standard : 35 l (9.25 US gal).
C. Chemical fluid :- Standard : 9.5 l (2.51 US gal).
5-4-10Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-5-0 Engine Starting Pneumatic Requirements
**ON A/C A330-200 A330-200F A330-300
Engine Starting Pneumatic Requirements
1. Engine Starting Pneumatic Requirements.
5-5-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-5-1 Low Temperatures
**ON A/C A330-200 A330-200F A330-300
Ambient Temperature - 40˚C (- 40˚F) and - 55˚C (- 67˚F)
1. This section provides the engine starting pneumatic requirements for an ambient temperatures of-40˚C (-40˚F) and -55˚C (-67˚F).
5-5-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
40
70
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
3
4
5
60
50
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
3.5
4.5
30
10
1
1.5
2
2.5
0.20 0.40 0.60 0.80 1.00 2.001.801.601.401.20 kg/s
12 24 36 48 60 8472 kg/mn12010896
20
0.5
135°C
185°C
220°C
70s
85s
100s
0°C
35°C
85°C
AIR FLOW REQUIRED AT GROUND CONNECTION
F_AC_050501_1_0010101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature - 40˚C (- 40˚F) -- PW 4000 series engine
FIGURE 1
5-5-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS
kg/mn
100°C
150°C
220°C
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
0°C
40 50 60 70 80 90 1001
2
1.5
3
2.5
3.5
4
5
4.5
30 110 120
30
40
70
60
50
20
180°C
85°C
50s
90s
60s
70s
F_AC_050501_1_0020101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature - 55˚C (- 67˚F) -- RR Trent 700 series engine
FIGURE 2
5-5-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
40
70
80
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
3
4
5
6
60
50
kg/mn
90
100 7
100°C
150°C200°C
220°C
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
50°C
0°C3.5
4.5
5.5
6.5
0 1201009080706040302010 50 110
30
20
1
1.5
2
2.5
MAXIMUM DUCT PRESSURE:60 PSIG
SEA LEVEL
AIR FLOW REQUIRED AT GROUND CONNECTION
Z = 8000 Ft
70s
60s
50s
35s
40s
45s
F_AC_050501_1_0030101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature - 40˚C (- 40˚F) -- GE CF6-80E1 series engine
FIGURE 3
5-5-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-5-2 Ambient Temperatures
**ON A/C A330-200 A330-200F A330-300
Ambient Temperature +0˚C (+32˚F) and +15˚C (+59˚F)
1. This section provides the engine starting pneumatic requirements for an ambient temperatures of0˚C (+32˚F) and +15˚C (+59˚F)
5-5-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
40
70
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
3
4
5
60
50
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
3.5
4.5
30
20
1
1.5
2
2.5
0.20 0.40 0.60 0.80 1.00 2.001.801.601.401.20 kg/s
12 24 36 48 60 8472 kg/mn12010896
20
0.5
85°C
135°C
185°C220°C
35°C
AIR FLOW REQUIRED AT GROUND CONNECTION
95s
80s
65s
50s
F_AC_050502_1_0010101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature +15˚C (+59˚F) -- PW 4000 series engine
FIGURE 1
5-5-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS
kg/mn
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
40 50 60 70 80 90 1001
2
1.5
3
2.5
3.5
4
5
4.5
30 110 120
30
40
70
60
50
20
100°C
150°C180°C
220°C
85°C
0°C
50s
90s
60s70s
F_AC_050502_1_0020101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature 0˚C (+32˚F) -- RR Trent 700 series engine
FIGURE 2
5-5-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
40
70
80
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
3
4
5
6
60
50
kg/mn
90
100 7
100°C
150°C200°C
220°C
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
50°C
0°C3.5
4.5
5.5
6.5
0 1201009080706040302010 50 110
30
20
1
1.5
2
2.5
AIR FLOW REQUIRED AT GROUND CONNECTION
70s
60s
50s
40s
35s
45s
SEA LEVEL
MAXIMUM DUCT PRESSURE:60 PSIG
Z = 8000 Ft
F_AC_050502_1_0030101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature +15˚C (+59˚F) -- GE CF6-80E1 series engine
FIGURE 3
5-5-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-5-3 High Temperatures
**ON A/C A330-200 A330-200F A330-300
Ambient Temperature Upper +38˚C (+100˚F)
1. This section provides the engine starting pneumatic requirements for an ambient temperature upper+38˚C (+100˚F)
5-5-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
40
70
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
3
4
5
60
50
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
3.5
4.5
30
10
1
1.5
2
2.5
0.20 0.40 0.60 0.80 1.00 2.001.801.601.401.20 kg/s
24 36 48 60 8472 kg/mn12010896
20
0.5
55°C85°C
135°C
185°C220°C
50s
60s
80s
AIR FLOW REQUIRED AT GROUND CONNECTION
12
F_AC_050503_1_0010101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature +55˚C (+131˚F) -- PW 4000 series engine
FIGURE 1
5-5-3Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS
kg/mn
100°C
150°C
220°C
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
0°C
40 50 60 70 80 90 10030 110 1200
1
0.5
2
1.5
2.5
3
4
3.5
5
4.5
180°C
85°C
40
70
60
50
30
20
10
90s70s
55s
60s
F_AC_050503_1_0020101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature +40˚C (+104˚F) -- RR Trent 700 series engine
FIGURE 2
5-5-3Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
40
70
80
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
3
4
5
6
60
50
kg/mn
90
100 7
100°C
150°C200°C
220°C
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
50°C
0°C3.5
4.5
5.5
6.5
0 1201009080706040302010 50 110
30
20
1
1.5
2
2.5
70s
60s
50s
40s
35s
45s
AIR FLOW REQUIRED AT GROUND CONNECTION
SEA LEVEL
MAXIMUM DUCT PRESSURE:60 PSIG
Z = 8000 Ft
F_AC_050503_1_0030101_01_00
Engine Starting Pneumatic RequirementsAmbient Temperature +50˚C (122˚F) -- GE CF6-80E1 series engine
FIGURE 3
5-5-3Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-6-0 Ground Pneumatic Power Requirements
**ON A/C A330-200 A330-200F A330-300
Ground Pneumatic Power Requirements
1. Ground Pneumatic Power Requirements.
5-6-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-6-1 Heating
**ON A/C A330-200 A330-200F A330-300
Heating
1. This section provides the ground pneumatic power requirements heating.
5-6-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
3.4
3.2 3
2.8
2.6
2.4
2.2
1.8
1.6
TOTAL AIRFLOW
2.96
3
2.76
9
2.57
5
2.38
1
2.18
7
1.99
3
1.79
9
1.60
5
1.41
1CABIN AIRFLOW
(kg/
s)
CABIN AIRFLOW
TOTAL AIRFLOW
(lb/s
)
2
6.5
5.51
0
4.53
9
7.0
6.0
5.0
RE
CIR
CU
LAT
ION
: O
N
INIT
IAL
CA
BIN
TE
MP
ER
AT
UR
E A
T −
23°
C (
−9.
4°F
)T
EM
PE
RA
TU
RE
AT
GR
OU
ND
CO
NN
EC
TIO
N :
70°
C (
158°
F)
EM
PT
Y C
AB
INE
LEC
TR
ICA
L LO
AD
: 67
50 W
EX
TE
RN
AL
HE
AT
LO
AD
: −
1768
8 W
TIM
E (
min
)
3.55
4.0
3040
5060
7035
4555
6575
80
MA
X. A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
TIM
E T
O H
EA
T C
AB
IN T
O 2
1°C
(69
.8°
F)
ON
GR
OU
ND
(m
in)
AT
CO
NN
EC
TIO
N A
ND
70
deg
C IN
LET
TE
MP
ER
AT
UR
E)
MA
X O
PE
RA
TIN
G C
ON
DIT
ION
S: (
70 m
bar
PR
ES
SU
RE
NO
TE
:H
EA
TIN
GM
AX
. PR
ES
SU
RE
AT
GR
OU
ND
CO
NN
EC
TIO
N M
US
T N
OT
EX
CE
ED
70
mba
r
F_AC_050601_1_0010101_01_01
Ground Pneumatic Power RequirementsHeating
FIGURE 1
5-6-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-6-2 Cooling
**ON A/C A330-200 A330-200F A330-300
Cooling
1. This section provides the ground pneumatic power requirements cooling.
5-6-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
CABIN AIRFLOW
TOTAL AIRFLOW
6.5
5.51
0
7.0
5.0
6.0
35
3.3
3.2
3.1 3
2.9
2.8
2.7
2.5
TOTAL AIRFLOW
2.96
3
2.76
9
2.57
5
2.38
1
CABIN AIRFLOW
(kg/
s)
2.6
(lb/s
)IN
ITIA
L C
AB
IN T
EM
PE
RA
TU
RE
AT
38°
C (
100.
4°F
)
EM
PT
Y C
AB
INE
LEC
TR
ICA
L LO
AD
: 14
000
WS
UN
: 72
19 W
PA
X H
EA
T L
OA
D :
0 W
EX
TE
RN
AL
HE
AT
LO
AD
: 80
40 W
RE
CIR
CU
LAT
ION
: O
N
TE
MP
ER
AT
UR
E A
T G
RO
UN
D C
ON
NE
CT
ION
: 1.
5°C
(34
.7°
F)
F_AC_050602_1_0010101_01_01
2.4
2.18
740
4550
5560
30
4.53
9
MA
X. A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
65
TIM
E T
O C
OO
L C
AB
IN T
O 2
7°C
(80
.6°
F)
ON
GR
OU
ND
(m
in)
NO
TE
:M
AX
. PR
ES
SU
RE
AT
GR
OU
ND
CO
NN
EC
TIO
N M
US
T N
OT
EX
CE
ED
70
mba
rC
OO
LIN
G
Ground Pneumatic Power RequirementsCooling
FIGURE 1
5-6-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-7-0 Preconditioned Airflow Requirements
**ON A/C A330-200 A330-200F A330-300
Preconditioned Airflow Requirements
1. This section gives the preconditioned airflow requirements for cabin air conditioning.
The total airflow must be not more than 3.232 kg/s. If the total airflow is more than this value, itwill be more than the capacity of the outflow valve in the fully open position and a cabin overpressureof more than 2 mbar will occur.
Other Filling capacities and characteristics (hydraulic, electrical, oxygen, fuel, oil, water, toilet) areshown in chapter 5-4.
5-7-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
3.2 3
2.8
2.6
2.4
2.2 2
1.6
TOTAL AIRFLOW
2.96
3
2.76
9
2.57
5
2.38
1
2.18
7
1.99
3
1.79
9
1.60
5
1.41
1
1.21
6
CABIN AIRFLOW(kg/
s)
CABIN AIRFLOW
TOTAL AIRFLOW
(lb/s
)
1.8
6.5
5.51
0
4.53
9
3.55
2.64
7.0
6.0
5.0
3.0
4.0
(°C
)
(°F
)
INLE
T T
EM
PE
RA
TU
RE
−30
−40
CU
RV
E 1
:P
AS
SE
NG
ER
S :
341,
AT
TE
ND
AN
TS
: 10
AN
D C
RE
W M
EM
BE
RS
: 3
RE
CIR
CU
LAT
ION
: O
NE
LEC
TR
ICA
L LO
AD
: 14
000
WS
OLA
R R
AD
IAT
ION
: 72
19 W
CA
BIN
TE
MP
ER
AT
UR
E :
27°
C (
80.6
°F
)
F_AC_050700_1_0010101_01_01
1.4 1
1.2
3.4
−40
−20
−10
010
2030
4050
60
−20
020
4060
8010
012
014
0
O.A
.T =
OU
TS
IDE
AM
BIE
NT
TE
MP
.
O.A
.T =
−23
°C
(−
9.4°
F)
O.A
.T =
−30
°C
(−
22°
F)
O.A
.T =
−40
°C
(−
40°
F)
CU
RV
E 2
,3,4
:
RE
CIR
CU
LAT
ION
: O
NE
LEC
TR
ICA
L LO
AD
: 67
50 W
O.A
.T =
−23
°C
(−
9.4°
F)
O.A
.T =
−30
°C
(−
22°
F)
O.A
.T =
−40
°C
(−
40°
F)
CA
BIN
TE
MP
ER
AT
UR
E :
21°
C (
69.8
°F
)
O.A
.T =
38°
C (
100.
4°F
)
60 m
bar
PR
ES
SU
RE
50 m
bar
PR
ES
SU
RE
C1
40 m
bar
PR
ES
SU
RE
30 m
bar
PR
ES
SU
RE
70 m
bar
MA
X P
RE
SS
UR
E A
T C
ON
NE
CT
ION
NO
TE
:M
AX
. PR
ES
SU
RE
AT
GR
OU
ND
CO
NN
EC
TIO
N M
US
T N
OT
EX
CE
ED
70
mba
r
MA
X. A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
NO
PA
SS
EN
GE
R A
ND
AT
TE
ND
AN
T.
Preconditioned Airflow RequirementsFIGURE 1
5-7-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
TOTAL CABIN
(kg/s) (lb/s) (kg/s) (lb/s)
FRESH AIRFLOW
T FL
(°C) (°F)
CURVE 1 CURVE 2
T FL
CURVE 3
T FL
CURVE 4
T FL
(°C) (°F) (°C) (°F) (°C) (°F)
1.40 3.086 1.216 2.681 −31.90 −25.42 49 120.20 54.8 130.64 63.3 145.94
1.60 3.527 1.411 3.110 −24.50 −12.10 45.2 113.36 50.3 122.54 57.5 135.50
1.80 3.968 1.605 3.538 −17.10 1.22 41.7 107.06 46 114.80 52.3 126.14
2.00 4.409 1.799 3.966 −12.00 10.40 39.2 102.56 43 109.40 48.4 119.12
2.20 4.850 1.993 4.394 −8.10 17.42 37.2 98.96 40.7 105.26 45.6 114.08
2.40 5.291 2.187 4.821 −5.00 23.00 35.5 95.90 38.6 101.48 43 109.40
2.60 5.732 2.381 5.249 −2.10 28.22 34.3 93.74 37.1 98.78 41.1 105.98
2.80 6.173 2.575 5.677 0.00 32.00 33.2 91.76 35.7 96.26 39.4 102.92
3.00 6.614 2.769 6.104 2.30 36.14 32.1 89.78 34.5 94.10 37.9 100.22
3.20 7.055 2.963 6.532 4.00 39.20 31.3 88.34 33.5 92.30 36.6 97.88
INLET
TEMP.
[°C]
P = 20
mbar
P = 30
mbar
P = 40
mbar
P = 50
mbar
P = 60
mbar
P = 70
mbar
P = 80
mbar
P = 90
mbar
P = 100
mbar
AIRFLOW [kg/s]
−40 1.60167 1.84954 2.06795 2.26544 2.44707 2.61616 2.77499 2.92524 3.06817
−30 1.56839 1.81111 2.02498 2.21836 2.39622 2.5618 2.71733 2.86446 3.00442
−20 1.5371 1.77497 1.98458 2.1741 2.34842 2.51069 2.66312 2.80731 2.94448
−10 1.50761 1.74092 1.94651 2.13239 2.30336 2.46252 2.61203 2.75345 2.88799
0 1.47975 1.70876 1.91054 2.093 2.26081 2.41702 2.56377 2.70258 2.83463
10 1.45339 1.67831 1.8765 2.05571 2.22053 2.37396 2.51809 2.65443 2.78413
20 1.42838 1.64944 1.84422 2.02034 2.18232 2.33312 2.47477 2.60876 2.73623
30 1.40463 1.622 1.81355 1.98674 2.14603 2.29431 2.43361 2.56537 2.69072
40 1.38202 1.5959 1.78435 1.95476 2.11148 2.25738 2.39443 2.52408 2.64741
50 1.36047 1.57101 1.75653 1.92428 2.07856 2.22218 2.3571 2.48472 2.60612
60 1.33989 1.54725 1.72997 1.89518 2.04712 2.18858 2.32145 2.44714 2.56671
70 1.32023 1.52454 1.70457 1.86736 2.01708 2.15645 2.28737 2.41122 2.52904
TABLE 3.16. AIRFLOW REQUIREMENTS.
TABLE 3.17. AIRFLOW VS INLET TEMPERATURE AND DIFFERENTIAL PRESSURE.
F_AC_050700_1_0020101_01_00
Preconditioned Airflow RequirementsFIGURE 2
5-7-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-8-0 Ground Towing Requirements
**ON A/C A330-200 A330-200F A330-300
Ground Towing Requirements
1. This section provides information on aircraft towing.
The A330 is designed with means for conventional or towbarless towing.Information/procedures can be found for both in chapter 9 of the Aircraft Maintenance Manual.Status on towbarless towing equipment qualification can be found in SIL 09-002.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a tow bar attached to the nose gear leg (refer to AMM chapter 9 for conditions andlimitations). One tow bar fitting is installed at the front of the leg (optional towing fitting for towingfrom the rear of the NLG available).The Main Landing Gears have attachment points for towing or debogging (for details refer to chapter7 of the Aircraft Recovery Manual).
- The first part of this section shows the chart to determine the draw bar pull and tow tractormass requirements as function of the following physical characteristics:- aircraft weight- slope- number of engines at idle
The chart is based on the A330 engine type with the biggest idle thrust.The chart is therefore valid for all A330 models
- The second part of this section supplies guidelines for the tow bar.
Note: information on aircraft towing procedures and corresponding aircraft limitations are given inchapter 9 of the Aircraft Maintenance Manual.
2. Tow bar design guidelines
The aircraft tow bar shall respect the following norms:- SAE AS 1614, ”Main Line Aircraft Tow Bar Attach Fitting Interface”- SAE ARP1915 Revision C, ”Aircraft Tow Bar”- ISO 8267-1, ”Aircraft - Tow bar attachment fitting - Interface requirements - Part 1: Main line
aircraft”- ISO 9667, ”Aircraft ground support equipment - Tow bars”- IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Tow bar”
A conventional type tow bar is required which should be equipped with a damping system to protectthe nose gear against jerks and with towing shear pins :- A traction shear pin calibrated at 28 620 daN (64 340 lbf)
5-8-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
- A torsion pin calibrated at 3 130 m.daN (27 7028 lbf.in)The towing head is designed according to SAE/AS 1614 (issue C) cat. III.
There is a variety of shear pin arrangements and the values of the shear pins depend on them. Wehereafter show two arrangements classically used on tow bars.
5-8-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
50
45
40
35
30
25
20
15
10
5
00 10 20 30 40 50 60 70 80 0 1 2 0 0.5 1.0 1.5 2.0
TOTAL TRACTION WHEEL LOAD [ t ] NO OF ENGINES SLOPE [ % ]
DRAWBAR PULL [ t ]
WET C
ONCRETE =
0.57
HARD SNOW = 0.2
ICE = 0.05
DRY CO
NCRETE
=
0.8
A/C WEIGHT [ t ]
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A330 AT 230 t, AT 1.5% SLOPE,1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (230 t),− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%),− FROM THIS POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL NO OF ENGINES AT IDLE = 2,− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED NUMBER OF ENGINES (1),− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS,− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (18.8 t),− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (32.9 t).
AT IDLE
F_AC_050800_1_0020101_01_01
230210190170150130110
18.8
32.9
1 ENGINE ON
230 tons1.5% SLOPE
BREAKWAY RESISTANCE 6%# OF ENGINES ON FOR PB: 1ENGINE THRUST 1 500 daN
Ground Towing RequirementsFIGURE 1
5-8-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
F_AC_050800_1_0030101_01_00
D1
MF
M
LONGHOLE BLOCKINGLATERAL MOVEMENTS
HOLES FOR SPARE SHEAR PINS
MF
LOCKING/UNLOCKING HANDLE
SHEAR PIND1
L
F F
Fshear
F
Mshear
Fshear
Lshear
M = Fshear
x L
Mshear
= Fshear
x Lshear
Mshear
= F x D1 (Mshear
< M)
D1 = (M/L) x Lshear
/ F
Fshear
= M / L
Mshear
= (M/L) x Lshear
D1 = (M x Lshear
/ (F x L)
A
A
Ground Towing RequirementsTypical tow bar configuration 1
FIGURE 2
5-8-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
F_AC_050800_1_0040101_01_00
MF
D2
OVERSIZED HOLEWRT RETENTION BOLT
M
L
F
F/2
F/2
D2
D2 = (2 x Mshear
) / F D2 = (2 x M x Lshear
) / (F x L)
F M D1 D2
28620 3130 98.4 210.0
[daN] [m.daN] [mm] [mm]
RESULTS FOR A TOWBAR LENGTH OF Lshear
/L = 0.90
Fshear
Fshear
Lshear
Mshear
M = Fshear
x L
Mshear
= Fshear
x Lshear
Mshear
= F/2 x D2 (Mshear
< M)
Fshear
= M / L
Mshear
= (M / L) x Lshear
A
A
Ground Towing RequirementsTypical tow bar configuration 2
FIGURE 3
5-8-0Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
H
MAKE SURE THAT THE DIMENSION "H" OF THE NLG IS NEVER GREATER THAN 310 mm (12.2047 in.) WHEN YOU TOW THE AIRCRAFT.
F_AC_050800_1_0050101_01_00
Ground Towing RequirementsMaximum Extension of the NLG Shock Absorber
FIGURE 4
5-8-0Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Velocities and Temperatures
1. GeneralThis section shows the estimated engine exhaust efflux velocities and temperatures contours forGround Idle, Breakaway, Maximum Takeoff conditions.
6-1-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Velocities Contours - Ground Idle Power
1. This section gives engine exhaust velocities contours at ground idle power
6-1-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
0 60 (18) 40 (12) 20 (6) 0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
PLA
NA
IRP
LAN
EC L
CO
NV
ER
SIO
N F
AC
TO
R1
MP
H =
1.6
km
/h
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
60 (18)
40 (12) 20 (6)
G−
0022
6 (0
000)
102
MP
H68
MP
H51
MP
H34
MP
H13
6 M
PH
34 M
PH
51 M
PH
68 M
PH
102
MP
H13
6 M
PH
ALL
VE
LOC
ITY
VA
LUE
S A
RE
IN S
TA
TU
TE
MIL
ES
PE
R H
OU
R.
GR
OU
ND
IDLE
PO
WE
R, S
EA
LE
VE
L S
TA
TIC
, ZE
RO
WIN
DS
TA
ND
AR
D D
AY
, ZE
RO
RA
MP
GR
AD
IEN
T E
NG
INE
TY
PE
.
F_AC_060101_1_0010101_01_00
Engine Exhaust VelocitiesGround Idle Power - PW 4000 series engine
FIGURE 1
6-1-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
ft
ft
m
m
00
00
0
0
FEET
METERS
50
ELEVATION
100 150
15 30 45
205
5 20
PLAN
200 fps 100 fps 50 fps
200 fps 100 fps 50 fps
10
15
20
40
60
10
15
20
25
60
40
80
(100 fps = 68 MPH = 109 kmph)
(100 fps = 68 MPH = 109 mph)
F_AC_060101_1_0020101_01_00
Engine Exhaust VelocitiesGround Idle Power - RR Trent 700 series engine
FIGURE 2
6-1-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
0
0
ft
0
ft
25
25
50
50
ELEVATION
PLAN
m
15
0
10
5
m
15
0
10
5
0 50 100 150 200FEET
METERS15 30 45 60
V=51.3V=95.3
(100 fps = 68 MPH = 109 kmph)
(100 fps = 68 MPH= 109 kmph)
ft/s6535 MPH
10556 km/h
F_AC_060101_1_0030101_01_01
Engine Exhaust VelocitiesGround Idle Power - GE CF6-80E1 series engine
FIGURE 3
6-1-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Temperatures Contours - Ground Idle Power
1. This section gives engine exhaust temperatures contours at ground idle power.
6-1-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
AIR
PLA
NE
C L
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
125°
F(5
2°C
)
0 60 (18) 40 (12) 20 (6)
060 (18) 40 (12) 20 (6)
150°
F(6
6°C
)
150°
F(6
6°C
)12
5°F
(52°
C)
100°
F(3
8°C
)
100°
F(3
8°C
)
G−
0022
9 (1
294)
TE
MP
ER
AT
UR
ES
AR
E IN
DE
GR
EE
S F
AH
RE
NH
EIT
(D
EG
RE
ES
C)
GR
OU
ND
IDLE
PO
WE
R −
SE
A L
EV
EL
ST
AT
IC, Z
ER
O W
IND
,S
TA
ND
AR
D D
AY
, ZE
RO
RA
MP
GR
AD
IEN
T E
NG
INE
TY
PE
.
PLA
N
F_AC_060102_1_0010101_01_00
Engine Exhaust TemperaturesGround Idle Power - PW 4000 series engine
FIGURE 1
6-1-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
FEET
METERS
50 100 150
15 30 45
ELEVATION
PLAN
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
0
0
113°F(45°C)
95°F(35°C)
77°F(25°C)
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
113°F(45°C)
95°F(35°C)
77°F(25°C)
F_AC_060102_1_0020101_01_00
Engine Exhaust TemperaturesGround Idle Power - RR Trent 700 series engine
FIGURE 2
6-1-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
ELEVATION
PLAN
50 100 150FEET
METERS 15 30 45
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
141°F(60°C)
91°F(31°C)
116°F(47°C)
141°F(60°C)
116°F(47°C)
91°F(31°C)
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
0
0
F_AC_060102_1_0030101_01_01
Engine Exhaust TemperaturesGround Idle Power - GE CF6-80E1 series engine
FIGURE 3
6-1-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Velocities Contours - Breakaway Power
1. This section gives engine exhaust velocities contours at breakaway power
6-1-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
60 (18) 40 (12) 20 (6) 0 60 (1
8) 40 (12) 20 (6) 0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
PLA
NA
IRP
LAN
EC L
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
CO
NV
ER
SIO
N F
AC
TO
R
136
MP
H10
2 M
PH
68 M
PH
51 M
PH
34 M
PH
G−
0324
7 (0
000)
ALL
VE
LOC
ITY
VA
LUE
S A
RE
IN S
TA
TU
TE
MIL
ES
PE
R H
OU
R.
GR
OU
ND
IDLE
PO
WE
R −
SE
A L
EV
EL
ST
AT
IC, Z
ER
O W
IND
ST
AN
DA
RD
DA
Y, Z
ER
O R
AM
P G
RA
DIE
NT
EN
GIN
E T
YP
E.
136
MP
H10
2 M
PH
68 M
PH
51 M
PH
34 M
PH
1 M
PH
= 1
.6 k
m/h
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
F_AC_060103_1_0010101_01_00
Engine Exhaust VelocitiesBreakaway Power - PW 4000 series engine
FIGURE 1
6-1-3Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
ELEVATION
200 fps 100 fps 50 fps
(100 fps = 68 MPH = 109 kmph)
200 fps 100 fps 50 fps
(100 fps = 68 MPH = 109 kmph)ft
ft
m
m
00
00
0
0
FEET
METERS
50 100
15 30
205
5 20
PLAN
10
15
20
40
60
10
15
20
25
60
40
80
150 200 250 300
6045 75 90
F_AC_060103_1_0020101_01_00
Engine Exhaust VelocitiesBreakaway Power - RR Trent 700 series engine
FIGURE 2
6-1-3Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
0
0
ft
2550
ELE
VA
TIO
N
PLA
N
m15 010 5
010
0F
EE
T
ME
TE
RS
30
02550m
15 010 5
200
60
300
400
500
600
9012
015
018
0
105
MP
H65
MP
H35
MP
H
210
MP
H14
5 M
PH
105
MP
H65
MP
H35
MP
H
210
MP
H14
5 M
PH
51.3
V=
V=
154
V=
213
V=
308
(100
fps
= 6
8 M
PH
= 1
09 m
ph)
(100
fps
= 6
8 M
PH
= 1
09 m
ph)
ft
ft/s
65 105
145
210
3510
516
923
333
8
56V
=95
.3M
PH
km/h
F_AC_060103_1_0030101_01_01
Engine Exhaust VelocitiesBreakaway Power - GE CF6-80E1 series engine
FIGURE 3
6-1-3Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Temperatures Contours - Breakaway Power
1. This section gives engine exhaust temperatures contours at breakaway power.
6-1-4Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
60 (18) 40 (12) 20 (6) 0 60 (1
8) 40 (12) 20 (6)
0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
GR
OU
ND
PLA
NE
PLA
NA
IRP
LAN
EC L
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
100°
F(3
8°C
)12
5°F
(52°
C)
(66°
C)
125°
F(5
2°C
)15
0°F
(66°
C)
NO
TE
:T
EM
PE
RA
TU
RE
S A
RE
IN D
EG
RE
ES
FA
HR
EN
HE
IT (
DE
GR
EE
S C
)G
RO
UN
D ID
LE P
OW
ER
− S
EA
LE
VE
L S
TA
TIC
, ZE
RO
WIN
D,
ST
AN
DA
RD
DA
Y, Z
ER
O R
AM
P G
RA
DIE
NT
EN
GIN
E T
YP
E.
G−
0324
6 (0
000)
100°
F(3
8°C
)
150°
F
ELE
VA
TIO
N
F_AC_060104_1_0010101_01_00
Engine Exhaust TemperaturesBreakaway Power - PW 4000 series engine
FIGURE 1
6-1-4Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
ELEVATION
0
FEET
METERS
50 100 150
15 30 45
PLAN
113°F(45°C)
95°F(35°C)
77°F(25°C)
113°F(45°C)
77°F(25°C)
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
0
60(18)
80(24)
40(12)
20(6)
FEET(METERS)
0
95°F(35°C)
F_AC_060104_1_0020101_01_00
Engine Exhaust TemperaturesBreakaway Power - RR Trent 700 series engine
FIGURE 2
6-1-4Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
0
0
ft
0
ft
25
25
50
50
ELEVATION
PLAN
m
15
0
10
5
m
15
0
10
5
0 50 100 150 200FEET
METERS 15 30 45 60
341°F(172°C)
141°F(60°C)
241°F(116°C)
116°F(47°C)
91°F(31°C)
341°F(172°C)
141°F(60°C)
241°F(116°C)
116°F(47°C)
91°F(31°C)
F_AC_060104_1_0030101_01_01
Engine Exhaust TemperaturesBreakaway Power - GE CF6-80E1 series engine
FIGURE 3
6-1-4Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Velocities Contours - Takeoff Power
1. This section gives engine exhaust velocities contours at takeoff power
6-1-5Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
0 60 (18) 40 (12) 20 (6) 0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
PLA
NA
IRP
LAN
EC L
CO
NV
ER
SIO
N F
AC
TO
R1
MP
H =
1.6
km
/h
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
ALL
VE
LOC
ITY
VA
LUE
S A
RE
IN S
TA
TU
TE
MIL
ES
PE
R H
OU
R.
TA
KE
OF
F P
OW
ER
− S
EA
LE
VE
L S
TA
TIC
, ZE
RO
WIN
DS
TA
ND
AR
D D
AY
, ZE
RO
RA
MP
GR
AD
IEN
T E
NG
INE
TY
PE
.
60 (18) 40 (12) 20 (6)
682
MP
H47
7 M
PH
341
MP
H20
4 M
PH
102
MP
H
477
MP
H34
1 M
PH
204
MP
H10
2 M
PH
34 M
PH
TO
740
ft22
5 m
682
MP
H34
MP
HT
O 7
40 ft
225
m
G−
0022
8 (1
294)
68 M
PH
460
ft14
0 m
68 M
PH
460
ft14
0 m
F_AC_060105_1_0010101_01_00
Engine Exhaust VelocitiesTakeoff Power - PW 4000 series engine
FIGURE 1
6-1-5Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
50 fp
s
0
FE
ET
ME
TE
RS
ELE
VA
TIO
N
PLA
N
60
5
101520
250
200
150
100
0
7560
4530
150
m
40 20Ft
50 fp
s
(100
fps
= 6
8 M
PH
= 1
09 k
mph
)
TO
1175
ft35
8 m
TO
1175
ft35
8 m
05
1015
m
40 20Ft
2060
30 25
100
80
50
(100
fps
= 6
8 M
PH
= 1
09 k
mph
)
200
fps
100
fps
200
fps
100
fps
D29
81A
300
90
350
105
TO
470
ft14
3 m
TO
470
ft14
3 m
F_AC_060105_1_0020101_01_00
Engine Exhaust VelocitiesTakeoff Power - RR Trent 700 series engine
FIGURE 2
6-1-5Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
0
0
ft
2550
ELE
VA
TIO
N
PLA
N
m15 010 5
010
0F
EE
T
ME
TE
RS
30
0
ft
2550m
15 010 5
200
60
300
400
500
600
9012
015
018
0
105
MP
H65
MP
H35
MP
H
105
MP
H65
MP
H35
MP
H
V=
V=
V=
154
V=
213
V=
308
(100
fps
= 6
8 M
PH
= 1
09 k
m/h
)
(100
fps
= 6
8 M
PH
= 1
09 k
m/h
)
65 105
145
210
105
169
233
338
35 M
PH
56 k
m/h
51.3
ft/s
95.3
F_AC_060105_1_0030101_01_00
Engine Exhaust VelocitiesTakeoff Power - GE CF6-80E1 series engine
FIGURE 3
6-1-5Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A330-200 A330-200F A330-300
Engine Exhaust Temperatures Contours - Takeoff Power
1. This section gives engine exhaust temperatures contours at takeoff power
6-1-6Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
0
60 (18) 40 (12) 20 (6) 0
FE
ET
ME
TE
RS
050
100
1530
0
150
200
250
300
4661
7691
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
PLA
NA
IRP
LAN
EC L
NO
TE
:
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
60(1
8) 40(1
2) 20 (6)
G−
0023
1 (0
000)
TE
MP
ER
AT
UR
ES
AR
E IN
DE
GR
EE
S F
AH
RE
NH
EIT
(D
EG
RE
ES
C).
TA
KE
OF
F P
OW
ER
− S
EA
LE
VE
L S
TA
TIC
, ZE
RO
WIN
D,
ST
AN
DA
RD
DA
Y, Z
ER
O R
AM
P G
RA
DIE
NT
EN
GIN
E T
YP
E.
250°
F(1
21°
C)
150°
F(6
6°C
)12
5°F
(52°
C)
200°
F(9
3°C
)30
0°F
(149
°C
)10
0°F
(38°
C)
250°
F(1
21°
C)
150°
F(6
6°C
)12
5°F
(52°
C)
200°
F(9
3°C
)30
0°F
(149
°C
)10
0°F
(38°
C)
F_AC_060106_1_0010101_01_00
Engine Exhaust TemperaturesTakeoff Power - PW 4000 series engine
FIGURE 1
6-1-6Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
ftft
mm
00
00
FE
ET
ME
TE
RS
50ELE
VA
TIO
N
100
150
200
250
300
350
1530
4560
7590
105
205
101520 25 20 15 105
80 60 40 20
TO
430
ft(1
31 m
)
TO
430
ft(1
31 m
)
PLA
N
4060
113°
F(4
5°C
)77
°F
(25°
C)
95°
F(3
5°C
)
0 0
113°
F(4
5°C
)77
°F
(25°
C)
95°
F(3
5°C
)
F_AC_060106_1_0020101_01_00
Engine Exhaust TemperaturesTakeoff Power - RR Trent 700 series engine
FIGURE 2
6-1-6Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
0
ft
0
ft
252550 50
ELE
VA
TIO
N
PLA
N
m
15 0
10
5
m
15 0
10
5
5010
015
020
0F
EE
T
ME
TE
RS
1530
4560
250
300
7590
341°
F(1
72°
C)
241°
F(1
16°
C)
141°
F(6
0°C
)11
6°F
(47°
C)
91°
F(3
1°C
)
341°
F(1
72°
C)
241°
F(1
16°
C)
141°
F(6
0°C
)11
6°F
(47°
C)
91°
F(3
1°C
)
00
F_AC_060106_1_0030101_01_00
Engine Exhaust TemperaturesTakeoff Power - GE CF6-80E1 series engine
FIGURE 3
6-1-6Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-2-0 Airport and Community Noise
**ON A/C A330-200 A330-200F A330-300
Airport and Community Noise Data
1. Airport and Community Noise Data
This section gives data concerning engine maintenance run-up noise to permit evaluation of possibleattenuation requirements.
6-2-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-2-1 Noise Data
**ON A/C A330-200 A330-200F A330-300
Noise Data
1. Noise Data for PW 4000 series engine
A. Description of test conditions :
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U. : off ; E.C.S. : Packs off.
B. Engine parameters : 2 engines running
C. Meteorological data
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows :- Temperature : 24.8 ˚C (76.64 ˚F)- Relative humidity : 46%- Atmospheric pressure : 1000 hPa- Wind speed : Negligible- No rain
2. Noise Data for RR Trent 700 series engine
A. Description of test conditions :
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U. : off ; E.C.S. : Packs off.
B. Engine parameters : 2 engines running
C. Meteorological data
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows :- Temperature : 16.8 ˚C (62.24 ˚F)- Relative humidity : 70%- Atmospheric pressure : 1009 hPa- Wind speed : Negligible- No rain
6-2-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
3. Noise Data for GE CF6-80E1 series engine
A. Description of test conditions :
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U. : off ; E.C.S. : Packs off.
B. Engine parameters : 2 engines running
C. Meteorological data
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows :- Temperature : 24.5 ˚C (76.10 ˚F)- Relative humidity : 47%- Atmospheric pressure : 1003.1 hPa- Wind speed : Negligible- No rain
6-2-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
7880
8284
8688
9092
9496
0°10°20°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
98100
102104
106108
110112
350°340°
330°
270°
240°
230°
220°
210°
NOISE REFERENCEPOINT
GROUND IDLE
E.P.R.
N1
CURVE
25% 82.4%
MAX THRUST POSSIBLEON BRAKES
1.016 1.337
30°
40°
50°
320°
310°
300°
290°
280°
250°
260°
F_AC_060201_1_0010101_01_00
Airport and Community NoisePW 4000 series engine
FIGURE 1
6-2-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
7880
8284
8688
9092
9496
0°10°20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
98100
102104
106108
110112
350°340°
330°
320°
310°
300°
290°
280°
270°
260°
250°
240°
230°
220°NOISE REFERENCE
POINT
GROUND IDLE
E.P.R.
N1
CURVE
23% 79.5%
MAX THRUST POSSIBLEON BRAKES
1.017 1.43
210°
F_AC_060201_1_0020101_01_00
Airport and Community NoiseRR Trent 700 series engine
FIGURE 2
6-2-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
7880
8284
8688
9092
9496
0°10°20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
98100
102104
106108
110112
350°340°
330°
320°
310°
300°
290°
280°
270°
260°
250°
240°
230°
220°
210°
NOISE REFERENCEPOINT
GROUND IDLE
N1
CURVE
26% 99.5%
MAX THRUST POSSIBLEON BRAKES
F_AC_060201_1_0030101_01_00
Airport and Community NoiseGE CF6-80E1 series engine
FIGURE 3
6-2-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-3-0 Danger Areas of Engines
**ON A/C A330-200 A330-200F A330-300
Danger Areas of Engines
1. Danger Areas of the Engines.
6-3-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-3-1 Ground Idle Power
**ON A/C A330-200 A330-200F A330-300
Ground Idle Power
1. This section gives danger areas of the engines at ground idle power conditions
6-3-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
INTAKE SUCTIONDANGER AREA
30°
EXHAUST DANGERAREA
SAFE ENTRYAREA
G−00224(0992)
TO 175 ft AT 34 MPHTO 53.35 m AT 54.4 kph
8.2 m(27 ft)
1.7 m(5.5 ft)
F_AC_060301_1_0010101_01_00
Danger Areas of EnginesPW 4000 series engine
FIGURE 1
6-3-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
TO 256 ft (78 m) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA MINIMUM POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
30°
3.75 ft10 ft
D4816
(3 m)(1 m)
F_AC_060301_1_0020101_01_00
Danger Areas of EnginesRR Trent 700 series engine
FIGURE 2
6-3-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
INLET SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST WAKE DANGER. WIND 105 km/h/57 kts OR GREATER
TO
54.90 m/180 ft A
FT
FA
N N
OZ
ZLE
7.62 m(25 ft)
1.25
m(4
.1 ft
)
45°
30°
RAD
IUS
F_AC_060301_1_0030101_01_00
Danger Areas of EnginesGE CF6-80E1 series engine
FIGURE 3
6-3-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-3-2 Breakaway Power
**ON A/C A330-200 A330-200F A330-300
Breakaway Power
1. This section gives danger areas of the engines at breakaway conditions.
6-3-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
INTAKE SUCTIONDANGER AREA
EXHAUST DANGERAREA
TO 290 ft AT 34 MPHTO 88.4 m m AT 54.4 kph
(37 ft)11.3 m
G−03248 (0000)
F_AC_060302_1_0010101_01_00
Danger Areas of EnginesPW 4000 series engine
FIGURE 1
6-3-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
(8 ft)2.4 m
(25 ft)7.6 m
30°TO 150 m (490 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA BREAKAWAY POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
F_AC_060302_1_0020101_01_00
Danger Areas of EnginesRR Trent 700 series engine
FIGURE 2
6-3-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
INLET SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST WAKE DANGER. WIND 105 km/h/57 kts OR GREATER
TO
48.8 m/160 ft A
FT
FA
N N
OZ
ZLE
(50 ft)15.2 m
45°
(5 ft
)1.
5 m
30°
RAD
IUS
F_AC_060302_1_0030101_01_00
Danger Areas of EnginesGE CF6-80E1 series engine
FIGURE 3
6-3-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-3-3 Takeoff Power
**ON A/C A330-200 A330-200F A330-300
Takeoff Power
1. This section gives danger areas of the engines at max takeoff conditions
6-3-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
30°
INTAKE SUCTIONDANGER AREA
EXHAUST DANGERAREA
PW 4164 / PW 4168 −TAKEOFFG − 00225 (0493)
TO 740 ft AT 34 MPHTO 225.5 m AT 54.4 kph
2 m6.5 ft
54 ft16.5 m
F_AC_060303_1_0010101_01_00
Danger Areas of EnginesPW 4000 series engine
FIGURE 1
6-3-3Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
30°
TO 2100 ft (640 m) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA TAKE−OFF POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
2.4 m(8 ft)
7.6 m(25 ft)
F_AC_060303_1_0020101_01_00
Danger Areas of EnginesRR Trent 700 series engine
FIGURE 2
6-3-3Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-300
INLET SUCTION DANGER AREA
ENTRY CORRIDOR
TO 274.30 m
/900 ft AFT FA
N N
OZZLE
EXHAUST WAKE DANGER. WIND 105 km/h / 57Kts OR GREATER
G_AC_060303_0_F00CAM0_00_00
(6 ft)1.80 m
15.25 m(50 ft)
45°
40°
RADIUS
F_AC_060303_1_0030101_01_00
Danger Areas of EnginesGE CF6-80E1 series engine
FIGURE 3
6-3-3Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A330-200 A330-200F A330-300
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures.
6-4-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-4-1 APU
**ON A/C A330-200 A330-200F A330-300
APU - GARRETT
1. This section gives APU exhaust velocities and temperatures
6-4-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
20
METERS
0
5 10 15
FEET
0
10 20 30 40 50
0
60
0
10
5
10
20
30
40
METERS FEET
20
METERS
0
5 10 15
FEET
0
10 20 30 40 50
0
60
0
10
5
10
20
30
40
METERS FEET
121°C
93°C
149°C177°C
15 m/s
FD
315.5°C
204°C260°C
427°C
18 m/s24 m/s
30.5 m/s46 m/s
61 m/s
FD
F_AC_060401_1_0010101_01_00
Exhaust Velocities and TemperaturesAPU -- GARRETT GTCP 331-350
FIGURE 1
6-4-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
PAVEMENT DATA
7-1-0 General Information
**ON A/C A330-200 A330-200F A330-300
General Information
1. General Information
A brief description of the pavement charts that follow will help in airport planning.
To aid in the interpolation between the discrete values shown, each airplane configuration is shownwith a minimum range of five loads on the main landing gear.
All curves on the charts represent data at a constant specified tire pressure with :- the airplane loaded to the maximum ramp weight- the CG at its maximum permissible aft position.
Pavement requirements for commercial airplanes are derived from the static analysis of loads imposedon the main landing gear struts.
Section 7-2-0 presents basic data on the landing gear footprint configuration, maximum ramp weightsand tire sizes and pressures.
Section 7-3-0 shows the maximum vertical and horizontal pavement loads for certain criticalconditions at the tire-ground interfaces.
Section 7-4-1 contains charts to find these loads throughout the stability limits of the airplane at reston the pavement.
These main landing gear loads are used as the point of entry to the pavement design charts, whichfollow, interpolating load values where necessary.
All Load Classification Number (LCN) curves shown in Section 7-6-1 and Section 7-8-2 have beendeveloped from a computer program based on data provided in International Civil AviationOrganisation (ICAO) document 7920-AN/865/2, Aerodrome Manual, Part 2, ”Aerodrome PhysicalCharacteristics”, Second Edition, 1965.
The flexible pavement charts in Section 7-6-1 show LCN against equivalent single wheel load, andequivalent single wheel load against pavement thickness.
The rigid pavement charts in Section 7-8-2 shown LCN against equivalent single wheel load, andequivalent single wheel load against radius of relative stiffness.
7-1-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Section 7-9-0 provides ACN data prepared according to the ACN/PCN system as referenced in ICAOAnnex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations.” Fourth Edition July 2004,incorporating Amendments 1 to 6.
The ACN/PCN system provides a standardized international airplane/pavement rating systemreplacing the various S, T, TT, LCN, AUW, ISWL, etc... rating systems used throughout the world.
ACN is the Aircraft Classification Number and PCN is the corresponding Pavement ClassificationNumber.
An aircraft having an ACN equal to or less than the PCN can operate without restriction on thepavement.
Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.
The derived single wheel load is defined as the load on a single tire inflated to 1.25 Mpa (181 psi)that would have the same pavement requirements as the aircraft.
Computationally the ACN/PCN the system uses PCA program PDILB for rigid pavements and S-77-1for flexible pavements to calculate ACN values. The Airport Authority must decide on the method ofpavement analysis and the results of their evaluation shown as follows :
PCNPAVEMENT
TYPESUBGRADECATEGORY
TIRE PRESSURE CATEGORY EVALUATION METHOD
R -- Rigid A -- High W -- No Limit T -- Technical
F -- Flexible B -- Medium X -- To 1.5 Mpa (217 psi) U -- Using Aircraft
C -- Low Y -- To 1.0 Mpa (145 psi)
D -- Ultra Low Z -- To 0.5 Mpa (73 psi)
Section 7-9-1 shows the aircraft ACN values for flexible pavements.
The four subgrade categories are :- A. High Strength CBR 15- B. Medium Strength CBR 10- C. Low Strength CBR 6- D. Ultra Low Strength CBR 3
Section 7-9-2 shows the aircraft ACN for rigid pavements.
7-1-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
The four subgrade categories are :- A. High Strength Subgrade k = 150 MN/m3 (550 pci)- B. Medium Strength Subgrade k = 80 MN/m3 (300 pci)- C. Low Strength Subgrade k = 40 MN/m3 (150 pci)- D. Ultra Low Strength Subgrade k = 20 MN/m3 (75 pci)
A. Flexible Pavement
Section 7-5-1 uses procedures in Instruction Report No S-77-1 ”Procedures for Development ofCBR Design Curves”, dated June 1977 and as modified according to the methods described inICAO Aerodrome Design Manual, Part 3.
Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCN Method), and utilizing the alphafactors approved by ICAO in October 2007.
The report was prepared by the U.S. Army Corps Engineers Waterways Experiment Station,Soils and Pavement Laboratory, Vicksburg, Mississippi.
The line showing 10 000 coverages is used to calculate Aircraft Classification Number (ACN).
The procedure that follows is used to develop flexible pavement design curves such as thoseshown in Section 7-5-1.- With the scale for pavement thickness at the bottom and the scale for CBR at the top, an
arbitrary line is drawn representing 10 000 coverages.- Incremental values of the weight on the main landing gear are then plotted.- Annual departure lines are drawn based on the load lines of the weight on the main landing
gear that is shown on the graph.
B. Rigid pavement
Section 7-7-1 gives the rigid pavement design curves that have been prepared with the use ofthe Westergaard Equation. This is in general accordance with the procedures outlined in thePortland Cement Association publications, ”Design of Concrete Airport Pavement”, 1973 and”Computer Program for Airport Pavement Design”, (Program PDILB), 1967 both by Robert G.Packard.
The procedure that follows is used to develop rigid pavement design curves such as those shownin Section 7-7-1.- With the scale for pavement thickness on the left and the scale for allowable working stress
on the right, an arbitrary line load line is drawn. This represents the main landing gearmaximum weight to be shown.
7-1-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
- All values of the subgrade modulus (k values) are then plotted.- Additional load lines for the incremental values of weight on the main landing gear are
drawn on the basis of the curve for k = 80 MN/m3 already shown on the graph.
7-1-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-2-0 Landing Gear Footprint
**ON A/C A330-200 A330-200F A330-300
Landing Gear Footprint
1. This section gives the Landing Gear Footprint.
7-2-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
22 180 mm (72 ft 9.2 in)
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
WING GEAR TIRE SIZE 1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE 14.2 bar (206 psi)
NOSE GEAR TIRE SIZE 1 050 x 395R16
NOSE GEAR TIRE PRESSURE 12.7 bar (184 psi)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
1 981 mm(78 in)
710 mm(27.95 in)
192 900 kg(425 275 lb)
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 192 000 kg − A330−200
and MTOW 233 000 kg − A330−200
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0030101_01_02
Landing Gear FootprintMTOW 192 000 kg
FIGURE 1
7-2-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
22 180 mm (72 ft 9.2 in)
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
710 mm(27.95 in)
WING GEAR TIRE SIZE 1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE 14.2 bar (206 psi)
NOSE GEAR TIRE SIZE 1 050 x 395R16
NOSE GEAR TIRE PRESSURE 12.7 bar (184 psi)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT202 900 kg(447 325 lb)
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 233 000 kg − A330−200
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0130101_01_01
Landing Gear FootprintMTOW 202 000 kg
FIGURE 2
7-2-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
22 180 mm (72 ft 9.2 in)
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
WING GEAR TIRE SIZE 1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE 14.2 bar (206 psi)
NOSE GEAR TIRE SIZE 1 050 x 395R16
NOSE GEAR TIRE PRESSURE 12.7 bar (184 psi)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT210 900 kg(464 950 lb)
1 981 mm(78 in)
710 mm(27.95 in)
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 210 000 kg − A330−200
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0140101_01_01
Landing Gear FootprintMTOW 210 000 kg
FIGURE 3
7-2-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
22 180 mm (72 ft 9.2 in)
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE 14.2 bar (206 psi)
NOSE GEAR TIRE SIZE 1 050 x 395R16
NOSE GEAR TIRE PRESSURE 12.7 bar (184 psi)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
1 981 mm(78 in)
220 900 kg(487 000 lb)
1 400 x 530R23 or 54 x 21−23 (bias)
710 mm(27.95 in)
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 233 000 kg − A330−200
and MTOW 233 000 kg − A330−200
F_AC_070200_1_0050101_01_02
10 684 mm(35 ft 0.6 in)
Landing Gear FootprintMTOW 220 000 kg
FIGURE 4
7-2-0Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
22 180 mm (72 ft 9.2 in)
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE 14.2 bar (206 psi)
NOSE GEAR TIRE SIZE 1 050 x 395R16
NOSE GEAR TIRE PRESSURE 12.7 bar (184 psi)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
1 981 mm(78 in)
230 900 kg(509 050 lb)
1 400 x 530R23 or 54 x 21−23 (bias)
710 mm(27.95 in)
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 233 000 kg − A330−200
and MTOW 233 000 kg − A330−200
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0150101_01_01
Landing Gear FootprintMTOW 230 000 kg
FIGURE 5
7-2-0Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
22 180 mm (72 ft 9.2 in)
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE 14.2 bar (206 psi)
NOSE GEAR TIRE SIZE 1 050 x 395R16
NOSE GEAR TIRE PRESSURE 12.7 bar (184 psi)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
1 981 mm(78 in)
233 900 kg(515 650 lb)
1 400 x 530R23 or 54 x 21−23 (bias)
710 mm(27.95 in)
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 233 000 kg − A330−200
and MTOW 233 000 kg − A330−200
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0160101_01_01
Landing Gear FootprintMTOW 233 000 kg
FIGURE 6
7-2-0Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
22 180 mm (72 ft 9.2 in)
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
WING GEAR TIRE SIZE 1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE 14.2 bar (206 psi)
NOSE GEAR TIRE SIZE 1 050 x 395R16
NOSE GEAR TIRE PRESSURE 12.7 bar (184 psi)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
1 981 mm(78 in)
710 mm(27.95 in)
227 900 kg(502 425 lb)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MTOW 227 000 kg − A330−200F
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0170101_01_01
Landing Gear FootprintMTOW 227 000 kg
FIGURE 7
7-2-0Page 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
22 180 mm (72 ft 9.2 in)
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
WING GEAR TIRE SIZE 1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE 14.2 bar (206 psi)
NOSE GEAR TIRE SIZE 1 050 x 395R16
NOSE GEAR TIRE PRESSURE 12.7 bar (184 psi)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
1 981 mm(78 in)
710 mm(27.95 in)
233 900 kg(515 650 lb)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MTOW 233 000 kg − A330−200F
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0180101_01_01
Landing Gear FootprintMTOW 233 000 kg
FIGURE 8
7-2-0Page 9
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
See Section 7−4−1− Figure: Landing Gear Loadingon Pavement − MTOW 184 000 kg − A330−300
13.1 bar (190 psi)
MAXIMUM RAMP WEIGHT184 900 kg(407 625 lb)
WING GEAR TIRE SIZE
10.7 bar (155 psi)
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0060101_01_02
Landing Gear FootprintMTOW 184 000 kg
FIGURE 9
7-2-0Page 10
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
See Section 7−4−1− Figure: Landing Gear Loadingon Pavement − MTOW 218 000 kg − A330−300
13.3 bar (193 psi)
MAXIMUM RAMP WEIGHT205 900 kg
(453 925 lb)
WING GEAR TIRE SIZE
10.9 bar (158 psi)
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0190101_01_01
Landing Gear FootprintMTOW 205 000 kg
FIGURE 10
7-2-0Page 11
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
See Section 7−4−1− Figure: Landing Gear Loadingon Pavement − MTOW 230 000 kg − A330−300
14.2 bar (206 psi)
MAXIMUM RAMP WEIGHT205 900 kg
(453 925 lb)
WING GEAR TIRE SIZE
11.4 bar (165 psi)
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0200101_01_01
Landing Gear FootprintMTOW 205 000 kg
FIGURE 11
7-2-0Page 12
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
See Section 7−4−1− Figure: Landing Gear Loadingon Pavement − MTOW 230 000 kg − A330−300
14.5 bar (210 psi)
MAXIMUM RAMP WEIGHT205 900 kg
(453 925 lb)
WING GEAR TIRE SIZE
11.6 bar (168 psi)
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0210101_01_01
Landing Gear FootprintMTOW 205 000 kg
FIGURE 12
7-2-0Page 13
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
13.1 bar (190 psi)
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
10.7 bar (155 psi)
(469 375 lb)212 900 kg
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 212 000 kg − A330−300
and MTOW 215 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0070101_01_02
Landing Gear FootprintMTOW 212 000 kg
FIGURE 13
7-2-0Page 14
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
13.3 bar (193 psi)
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
10.9 bar (158 psi)
(469 375 lb)212 900 kg
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 215 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0220101_01_01
Landing Gear FootprintMTOW 212 000 kg
FIGURE 14
7-2-0Page 15
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
14.5 bar (210 psi)
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
11.6 bar (168 psi)
(469 375 lb)212 900 kg
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 215 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0230101_01_01
Landing Gear FootprintMTOW 212 000 kg
FIGURE 15
7-2-0Page 16
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
13.3 bar (193 psi)
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
10.9 bar (158 psi)
(475 975 lb)215 900 kg
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 215 000 kg − A330−300
and MTOW 215 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0240101_01_01
Landing Gear FootprintMTOW 215 000 kg
FIGURE 16
7-2-0Page 17
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm
(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
13.3 bar (193 psi)
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
10.9 bar (158 psi)
(480 375 lb)217 900 kg
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 217 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0080101_01_02
Landing Gear FootprintMTOW 217 000 kg
FIGURE 17
7-2-0Page 18
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm
(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
14.2 bar (206 psi)
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
11.4 bar (165 psi)
(480 375 lb)217 900 kg
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 217 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0250101_01_01
Landing Gear FootprintMTOW 217 000 kg
FIGURE 18
7-2-0Page 19
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm
(78 in)
25 375 mm (83 ft 3 in)
710 mm(27.95 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
13.3 bar (193 psi)
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
10.9 bar (158 psi)
(486 600 lb)218 900 kg
See Section 7−4−1 Figure: Landing Gear Loading onPavement − MTOW 218 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0260101_01_01
Landing Gear FootprintMTOW 218 000 kg
FIGURE 19
7-2-0Page 20
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
25 375 mm (83 ft 3 in)
14.2 bar (206 psi)
11.4 bar (165 psi)
230 900 kg(509 050 lb)
710 mm(27.95 in)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MTOW 230 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0090101_01_02
Landing Gear FootprintMTOW 230 000 kg
FIGURE 20
7-2-0Page 21
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
25 375 mm (83 ft 3 in)
14.5 bar (210 psi)
11.6 bar (168 psi)
230 900 kg(509 050 lb)
710 mm(27.95 in)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MTOW 230 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0270101_01_01
Landing Gear FootprintMTOW 230 000 kg
FIGURE 21
7-2-0Page 22
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1 397 mm(55 in)
NOTE: DIMENSIONS IN MILLIMETERS(FEET AND INCHES IN BRACKETS).
1 981 mm(78 in)
1 050 x 395R16
1 400 x 530R23 or 54 x 21−23 (bias)
WING GEAR TIRE PRESSURE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
25 375 mm (83 ft 3 in)
14.5 bar (210 psi)
11.6 bar (168 psi)
233 900 kg(515 650 lb)
710 mm(27.95 in)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MTOW 233 000 kg − A330−300
10 684 mm(35 ft 0.6 in)
F_AC_070200_1_0280101_01_01
Landing Gear FootprintMTOW 233 000 kg
FIGURE 22
7-2-0Page 23
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-3-0 Maximum Pavement Loads
**ON A/C A330-200 A330-200F A330-300
Maximum Pavement Loads
1. This section gives Maximum Pavement Loads
7-3-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
1
lbkg
lbkg
lbkg
lbK
glb
kglb
kg
V(N
G) MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
H
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
(1)
FW
D C
G =
18
% M
AC
(2)
MR
W =
210
900
kg
AF
T C
G =
38.
1 %
MA
CM
RW
= 2
02 9
00 k
g A
FT
CG
= 3
8.4
% M
AC
MR
W =
192
900
kg
AF
T C
G =
38.
8 %
MA
C
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
38
740
220
050
ST
AT
IC B
RA
KIN
G
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
T M
AX
(2) 9
9 82
0
ST
AT
IC L
OA
D A
T
(1)
56
250
25
510
85
400
MO
DE
L
MA
XIM
UM
RA
MP
WE
IGH
T
−20
0 4
64 9
50 2
10 9
00
2V
NG
VM
G (
PE
R S
TR
UT
)3
45
72
250
32
770
176
050
79
850
H (
PE
R S
TR
UT
)6 A
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
ST
EA
DY
BR
AK
ING
DE
CE
LER
AT
ION
−20
0 4
47 3
25 2
02 9
00 5
4 15
0 2
4 56
0 8
2 27
5 3
7 32
0 2
11 9
00 9
6 12
0 6
9 52
5 3
1 53
0 1
69 5
25 7
6 90
0
−20
0 4
25 2
75 1
92 9
00 5
1 55
0 2
3 38
0 7
8 37
5 3
5 55
0 2
01 7
00 9
1 49
0 6
6 10
0 2
9 98
0 1
61 3
75 7
3 20
0
V(N
G)
V(M
G)
H
@ 1
0 ft/
s@
10
ft/s
AF
T C
.GM
OS
T F
WD
C.G
F_AC_070300_1_0010101_01_00
Maximum Pavement LoadsFIGURE 1
7-3-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
1
lbkg
lbkg
lbkg
lbK
glb
kglb
kg
V(N
G)
V(M
G)
ST
AT
IC B
RA
KIN
G
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
T M
AX
(2)
ST
AT
IC L
OA
D A
T
(1)
MO
DE
L
MA
XIM
UM
RA
MP
WE
IGH
T
−20
0
2V
NG
VM
G (
PE
R S
TR
UT
)3
45
H (
PE
R S
TR
UT
)6 A
T IN
ST
AN
TA
NE
OU
S
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
ST
EA
DY
BR
AK
ING
DE
CE
LER
AT
ION
−20
0
−20
0
(1)
MR
W =
233
900
kg
FW
D C
G =
21.
4 %
MA
C
MR
W =
230
900
kg
FW
D C
G =
21
% M
AC
M
RW
= 2
20 9
00 k
g F
WD
CG
= 1
9.57
% M
AC
(2)
MR
W =
233
900
kg
AF
T C
G =
37.
4 %
MA
C
MR
W =
230
900
kg
AF
T C
G =
37.
5 %
MA
C
MR
W =
220
900
kg
AF
T C
G =
37.
79 %
MA
C
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
75
675
34
330
184
225
83
560
87
270
487
000
220
900
56
300
25
540
86
750
39
350
230
275
104
450
109
080
79
100
35
880
192
400
25
570
88
100
39
960
240
475
509
050
230
900
56
375
80
125
36
350
194
825
88
370
515
650
233
900
40
150
243
525
110
470
56
400
25
580
88
525
@ 1
0 ft/
s@
10
ft/s
MO
ST
FW
D C
.G.
AF
T C
.G.
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
GH
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
H
F_AC_070300_1_0020101_01_00
Maximum Pavement LoadsFIGURE 2
7-3-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
1
lbkg
lbkg
lbkg
lbK
glb
kglb
kg
V(N
G)
V(M
G)
H
ST
AT
IC B
RA
KIN
G
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
T M
AX
(2)
ST
AT
IC L
OA
D A
T
(1)
MO
DE
L
MA
XIM
UM
RA
MP
WE
IGH
T
2V
NG
VM
G (
PE
R S
TR
UT
)3
45
H (
PE
R S
TR
UT
)6 A
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
G C
OE
FF
ICIE
NT
= 0
.8
ST
EA
DY
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
s@
10
ft/s
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
GH
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
(1)
(2)
MR
W =
233
900
kg
AF
T C
G =
37.
4 %
MA
CM
RW
= 2
27 9
00 k
g A
FT
CG
= 3
7.57
% M
AC
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
86 1
5010
7 69
078
075
35 4
2018
9 92
525
570
87 7
0039
790
237
400
−20
0F50
2 42
522
7 90
056
350
80 1
2536
350
194
825
88 3
70−
200F
515
650
233
900
40 1
5024
3 52
511
0 47
0
MO
ST
FW
D C
.G.
56 4
0025
580
88 5
25
AF
T C
.G.
MR
W =
233
900
kg
FW
D C
G =
21.
4 %
MA
CM
RW
= 2
27 9
00 k
g F
WD
CG
= 2
0.58
% M
AC
F_AC_070300_1_0060101_01_00
Maximum Pavement LoadsFIGURE 3
7-3-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1
lbkg
lbkg
lbkg
lbK
glb
kglb
kg
V(N
G)
V(M
G)
H
ST
AT
IC B
RA
KIN
G
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
T M
AX
(2)
ST
AT
IC L
OA
D A
T
(1)
MO
DE
L
MA
XIM
UM
RA
MP
WE
IGH
T
2V
NG
VM
G (
PE
R S
TR
UT
)3
45
H (
PE
R S
TR
UT
)6 A
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
G C
OE
FF
ICIE
NT
= 0
.8
ST
EA
DY
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
s@
10
ft/s
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
GH
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
(1)
FW
D C
G =
15
% M
AC
(2)
MR
W =
205
900
kg
AF
T C
G =
39.
6 %
MA
CM
RW
= 1
84 9
00 k
g A
FT
CG
= 4
0.1
% M
AC
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
70
960
88
700
63
350
28
730
156
450
21
050
68
825
31
210
195
550
−30
0 4
07 6
25 1
84 9
00 4
6 40
0
70
550
32
000
174
000
78
930
−30
0 4
53 9
25 2
05 9
00 3
4 62
0 2
17 5
00 9
8 66
0
MO
ST
FW
D C
.G.
51
575
23
390
76
325
AF
T C
.G.
F_AC_070300_1_0030101_01_00
Maximum Pavement LoadsFIGURE 4
7-3-0Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
104
270
103
340
101
060
1
lbkg
lbkg
lbkg
lbK
glb
kglb
kg
V(N
G)
V(M
G)
H
ST
AT
IC B
RA
KIN
G
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
T M
AX
(2)
ST
AT
IC L
OA
D A
T
(1)
MO
DE
L
MA
XIM
UM
RA
MP
WE
IGH
T
2V
NG
VM
G (
PE
R S
TR
UT
)3
45
H (
PE
R S
TR
UT
)6 A
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
ST
EA
DY
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
s@
10
ft/s
MO
ST
FW
D C
.G.
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
217
900
kg
FW
D C
G =
16.
11 %
MA
C
MR
W =
215
900
kg/
212
900
kg
FW
D C
G =
15
% M
AC
(2)
MR
W =
217
900
kg
AF
T C
G =
39.
12 %
MA
CM
RW
= 2
15 9
00 k
g A
FT
CG
= 3
9.2
% M
AC
MR
W =
212
900
kg
AF
T C
G =
36.
5 %
MA
C
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
35
860
229
875
52
950
24
020
79
075
−30
0 4
80 3
75 2
17 9
00 7
4 65
0 3
3 86
0 1
83 9
00 8
3 42
0
−30
0 4
75 9
75 2
15 9
00 5
4 02
5 2
4 50
0 7
9 90
0 3
6 24
0 2
27 8
25 7
3 97
5 3
3 55
0 1
82 2
50 8
2 67
0
−30
0 4
69 3
75 2
12 9
00 5
3 27
5 2
4 17
0 7
8 82
5 3
5 76
0 2
22 8
00 7
2 95
0 3
3 09
0 1
78 2
50 8
0 85
0
AF
T C
.G.
F_AC_070300_1_0040101_01_00
Maximum Pavement LoadsFIGURE 5
7-3-0Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
1
lbkg
lbkg
lbkg
lbK
glb
kglb
kg
V(N
G)
V(M
G)
H
ST
AT
IC B
RA
KIN
G
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
T M
AX
(2)
ST
AT
IC L
OA
D A
T
(1)
MO
DE
L
MA
XIM
UM
RA
MP
WE
IGH
T
2V
NG
VM
G (
PE
R S
TR
UT
)3
45
H (
PE
R S
TR
UT
)6 A
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
ST
EA
DY
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
s@
10
ft/s
MO
ST
FW
D C
.G.
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
GH
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
(1)
MR
W =
233
900
kg
FW
D C
G =
18.
4 %
MA
C
MR
W =
230
900
kg
FW
D C
G =
18
% M
AC
M
RW
= 2
18 9
00 k
g F
WD
CG
= 1
5 %
MA
C
(2)
MR
W =
233
900
kg
AF
T C
G =
38.
6 %
MA
C
MR
W =
230
900
kg
AF
T C
G =
38.
7 %
MA
C
MR
W =
218
900
kg
AF
T C
G =
39.
1 %
MA
C
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
75
000
34
020
184
750
83
800
88
260
−30
0 4
82 6
00 2
18 9
00 5
4 75
0 2
4 84
0 8
0 97
5 3
6 73
0 2
30 9
25 1
04 7
50
110
330
79
100
35
880
194
575
24
240
81
200
36
830
243
225
−30
0 5
09 0
50 2
30 9
00 5
3 42
5
80
125
36
350
197
050
89
380
−30
0 5
15 6
50 2
33 9
00 3
7 02
0 2
46 3
25 1
11 7
30 5
3 52
5 2
4 27
0 8
1 62
5
AF
T C
.G.
F_AC_070300_1_0050101_01_00
Maximum Pavement LoadsFIGURE 6
7-3-0Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-4-0 Landing Gear Loading on Pavement
**ON A/C A330-200 A330-200F A330-300
Landing Gear Loading on Pavement
**ON A/C A330-200
1. General
In the example shown in Section 7-4-1, Figure: Landing Gear Loading on Pavement - MTOW 192000 kg - A330-200The Gross Aircraft Weight is 145 000 kg (319 670 lb) and the percentage of weight on the MainLanding Gear is 94.9 %.For these conditions the total weight on the Main Landing Gear Group is 137 600 kg (303 245 lb).
**ON A/C A330-200F
2. General
In the example shown in Section 7-4-1, Figure: Landing Gear Loading on Pavement - MTOW 227000 kg - A330-200FThe Gross Aircraft Weight is 190 000 kg (418 880 lb) and the percentage of weight on the MainLanding Gear is 94.5 %.For these conditions the total weight on the Main Landing Gear Group is 179 560 kg (395 860 lb).
**ON A/C A330-300
3. General
In the example shown in Section 7-4-1, Figure: Landing Gear Loading on Pavement - MTOW 184000 kg - A330-300The Gross Aircraft Weight is 145 000 kg (319 670 lb) and the percentage of weight on the MainLanding Gear is 95.95 %.For these conditions the total weight on the Main Landing Gear Group is 139 120 kg (306 705 lb).
7-4-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-4-1 Landing Gear Loading on Pavement
**ON A/C A330-200 A330-200F A330-300
Landing Gear Loading on Pavement
1. This section gives Landing Gear Loading on Pavement
7-4-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
5045403530252015
110
115
120
125
130
135
140
145
150
155
160
165
170
175
180
185
190
195
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
100
0 kg
110
115
120
125
130
135
140
145
150
155
160
165
170
175
180
185
190
195
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
LANDING
CG FOR ACNCALCULATION
MLW = 180 000 kg
MTOW = 192 000 kg
TAKE OFF
TAKE OFF & LANDING
MZFW = 168 000 kg
F_AC_070401_1_0010101_01_02
Landing Gear Loading on PavementMTOW 192 000 kg
FIGURE 1
7-4-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
5045403530252015
110
120
130
140
150
160
170
180
190
200
210
220
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
100
0 kg
110
120
130
140
150
160
170
180
190
200
210
220
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
MTOW = 210 000 kg
LANDINGTAKE OFF & LANDING
TAKE OFF
CG FOR ACNCALCULATION
MLW = 180 000 kg
MZFW = 168 000 kg
F_AC_070401_1_0020101_01_02
Landing Gear Loading on PavementMTOW 210 000 kg
FIGURE 2
7-4-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
5045403530252015
110
120
130
140
150
160
170
180
190
200
210
220
230
240
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
100
0 kg
110
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
MTOW = 202 000 kg
MTOW = 230 000 kg
MTOW = 220 000 kg
CG FOR ACNCALCULATIONS
LANDINGTAKE OFF &LANDING
TAKE OFF
MZFW = 168 000 kg
MTOW = 233 000 kg
F_AC_070401_1_0030101_01_02
MLW = 180 000 kg
Landing Gear Loading on PavementMTOW 233 000 kg
FIGURE 3
7-4-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
50454030 35252015
110
120
130
140
150
160
170
180
190
200
210
220
230
240
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
110
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
TAKE OFF & LANDING
LANDING
MZFW = 170 000 kg
MTOW = 220 000 kg
MTOW = 192 000 kg
TAKE OFF
MTOW = 230 000 kg
MTOW = 233 000 kg
CG FOR ACNCALCULATION
MLW = 182 000 kg
F_AC_070401_1_0040101_01_03
Landing Gear Loading on PavementMTOW 233 000 kg
FIGURE 4
7-4-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
110
120
130
140
150
160
170
180
190
200
210
220
230
240
110
120
130
140
150
160
170
180
190
200
210
220
230
240
86 88 90 92 94 96 98 100
5045403530252015
LANDING
CG FOR ACNCALCULATION
TAKE OFF & LANDING
TAKE OFF
MZFW = 178 000 kg
MLW = 187 000 kg
MTOW = 227 000 kg
F_AC_070401_1_0140101_01_02
Landing Gear Loading on PavementMTOW 227 000 kg
FIGURE 5
7-4-1Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
110
120
130
140
150
160
170
180
190
200
210
220
230
240
110
120
130
140
150
160
170
180
190
200
210
220
230
240
86 88 90 92 94 96 98 100
5045403530252015
LANDING
TAKE OFF & LANDING
TAKE OFF
CG FOR ACNCALCULATION
MLW = 182 000 kg
MTOW = 233 000 kg
MZFW = 173 000 kg
F_AC_070401_1_0150101_01_02
Landing Gear Loading on PavementMTOW 233 000 kg
FIGURE 6
7-4-1Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
504540353025201510
110
115
120
125
130
135
140
145
150
155
160
165
170
175
180
185
190
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
100
0 kg
110
115
120
125
130
135
140
145
155
160
165
170
175
180
185
190
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
MLW = 174 000 kg
TAKE OFF & LANDING
TAKE OFF
LANDING
MTOW = 184 000 kg
MZFW = 164 000 kg
150
F_AC_070401_1_0050101_01_01
CG FOR ACNCALCULATIONS
Landing Gear Loading on PavementMTOW 184 000 kg
FIGURE 7
7-4-1Page 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
504540353025201510
110
120
130
140
150
160
170
180
190
200
210
220
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
100
0 kg
110
120
130
140
150
160
170
180
190
200
210
220
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
MTOW = 212 000 kg
MLW = 174 000 kg
MZFW = 164 000 kg
TAKE OFF
LANDING
CG FOR ACNCALCULATION
F_AC_070401_1_0060101_01_01
TAKE OFF & LANDING
Landing Gear Loading on PavementMTOW 212 000 kg
FIGURE 8
7-4-1Page 9
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
504540353025201510
110
120
130
140
150
160
170
180
190
200
210
220
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
110
120
130
140
150
160
170
180
190
200
210
220
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
CG FOR ACNCALCULATION
MTOW = 215 000 kg
MLW = 177 000 kg
MZFW = 167 000 kg
TAKE OFF
LANDING
F_AC_070401_1_0070101_01_01
MTOW = 212 000 kg
TAKE OFF & LANDING
Landing Gear Loading on PavementMTOW 215 000 kg
FIGURE 9
7-4-1Page 10
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
504540353025201510
110
120
130
140
150
160
170
180
190
200
210
220
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
110
120
130
140
150
170
190
210
220
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
CG FOR ACNCALCULATION
TAKE OFF & LANDING
TAKE OFF
LANDING
MTOW = 215 000 kg
MTOW = 212 000 kg
MLW = 177 000 kg
MZFW = 167 000 kg
200
180
160
F_AC_070401_1_0080101_01_02
Landing Gear Loading on PavementMTOW 215 000 kg
FIGURE 10
7-4-1Page 11
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
504540353025201510
110
120
130
140
150
160
170
180
190
200
210
220
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
110
120
130
140
150
160
170
180
190
200
210
220
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
CG FOR ACNCALCULATION
TAKE OFF
TAKE OFF & LANDING
LANDING
MTOW = 217 000 kg
MLW = 179 000 kg
MZFW = 169 000 kg
F_AC_070401_1_0090101_01_01
Landing Gear Loading on PavementMTOW 217 000 kg
FIGURE 11
7-4-1Page 12
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
504540353025201510
110
120
130
140
150
160
170
180
190
200
210
220
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
110
120
130
140
150
160
170
180
190
200
210
220
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
TAKE OFF
LANDINGTAKE OFF & LANDING
CG FOR ACNCALCULATION
MTOW = 217 000 kg
MLW = 179 000 kg
MZFW = 169 000 kg
F_AC_070401_1_0100101_01_01
Landing Gear Loading on PavementMTOW 217 000 kg
FIGURE 12
7-4-1Page 13
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
504540353025201510
110
120
130
140
150
160
170
180
190
200
210
220
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
110
120
130
140
150
160
170
180
190
200
210
220
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
LANDINGTAKE OFF & LANDING
TAKE OFF
MTOW = 218 000 kg
MLW = 182 000 kg
MZFW = 172 000 kg
CG FOR ACNCALCULATION
MTOW = 205 000 kg
F_AC_070401_1_0110101_01_01
Landing Gear Loading on PavementMTOW 218 000 kg
FIGURE 13
7-4-1Page 14
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
10 5045403530252015
110
120
130
140
150
160
170
180
190
200
210
220
230
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
110
120
130
140
150
160
170
180
190
200
210
220
230
240
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
240
MLW = 185 000 kg
CG FOR ACNCALCULATIONS
LANDINGTAKE OFF
TAKE OFF & LANDING
MTOW = 205 000 kg
MZFW = 173 000 kg
MTOW = 230 000 kg
F_AC_070401_1_0120101_01_01
Landing Gear Loading on PavementMTOW 230 000 kg
FIGURE 14
7-4-1Page 15
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
10 5045403530252015
110
120
130
140
150
160
170
180
190
200
210
220
230
240
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− x
1 0
00 k
g
110
120
130
140
150
160
170
180
190
210
220
230
240
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
x 1
000
kg
LANDINGTAKE OFF
TAKE OFF & LANDING
CG FOR ACNMTOW = 212 000 kg
MTOW = 233 000 kg
200
CALCULATIONS
MLW = 187 000 kg
MZFW = 175 000 kg
F_AC_070401_1_0130101_01_01
Landing Gear Loading on PavementMTOW 233 000 kg
FIGURE 15
7-4-1Page 16
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A330-200 A330-200F A330-300
Flexible Pavement Requirements - US Army Corps of Engineers Design Method
**ON A/C A330-200
1. General
To find a Flexible Pavement Thickness, the Subgrade Strength (CBR), the Annual Departure Leveland the weight on one Main Landing must be known.
In the example shown in Section 7-5-1 Figure : Flexible Pavement Requirements - MTOW 233 000kg - A330-200- A ”CBR” value of 10- An Annual Departure level of 3 000- And the load on one Main Landing Gear of 80 000 kg (176 370 lb)- The required Flexible Pavement Thickness is 49 cm (19.25 inches).
The line showing 10 000 Coverages is used to calculate Aircraft Classification Number (ACN).
**ON A/C A330-200F
2. General
To find a Flexible Pavement Thickness, the Subgrade Strength (CBR), the Annual Departure Leveland the weight on one Main Landing must be known.
In the example shown in Section 7-5-1 Figure : Flexible Pavement Requirements - MTOW 233 000kg - A330-200F- A ”CBR” value of 10- An Annual Departure level of 3 000- And the load on one Main Landing Gear of 80 000 kg (176 370 lb)- The required Flexible Pavement Thickness is 49 cm (19.25 inches).
The line showing 10 000 Coverages is used to calculate Aircraft Classification Number (ACN).
**ON A/C A330-300
3. General
To find a Flexible Pavement Thickness, the Subgrade Strength (CBR), the Annual Departure Leveland the weight on one Main Landing must be known.
7-5-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
In the example shown in Section 7-5-1 Figure : Flexible Pavement Requirements - MTOW 212 000kg - A330-300- A ”CBR” value of 10- An Annual Departure level of 3 000- And the load on one Main Landing Gear of 80 000 kg (176 370 lb)- The required Flexible Pavement Thickness is 49 cm (19.25 inches).
The line showing 10 000 Coverages is used to calculate Aircraft Classification Number (ACN).
7-5-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method S-77-1
**ON A/C A330-200 A330-200F A330-300
Flexible Pavement Requirements - US Army Corps of Engineers Design Method
1. This section gives Flexible Pavement Requirements.
7-5-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
3 6 10 15 20 604030
60403020156 103
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 TIRESTIRE PRESSURE CONSTANT AT 14.2 BAR (206 PSI)
10 000 COVERAGES USED FOR ACN CALCULATIONS
110 470 kg (243 525 lb)100 000 kg (220 460 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
80
8050
50
WEIGHT ON ONE MAIN LANDING GEAR
90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
*1 2003 0006 00015 00025 000
20 YEAR PAVEMENT LIFE
ANNUAL DEPARTURES
*
F_AC_070501_1_0010101_01_01
ALPHA FACTOR = 0.8
Flexible Pavement RequirementsMTOW 233 000 kg
FIGURE 1
7-5-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
3 6 10 15 20 604030
60403020156 103
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 TIRESTIRE PRESSURE CONSTANT AT 14.2 BAR (206 PSI)
80
8050
50
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
10 000 COVERAGES USED FOR ACN CALCULATIONS
*1 2003 0006 00015 00025 000
20 YEAR PAVEMENT LIFE
ANNUAL DEPARTURES
*
110 470 kg (243 525 lb)100 000 kg (220 460 lb)
WEIGHT ON ONE MAIN LANDING GEAR
90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
ALPHA FACTOR = 0.8
F_AC_070501_1_0060101_01_00
Flexible Pavement RequirementsMTOW 233 000 kg
FIGURE 2
7-5-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
3 6 10 15 20 30
3020156 103
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 TIRESTIRE PRESSURE CONSTANT AT 13.1 BAR (189 PSI)
10 000 COVERAGES USED FOR ACN CALCULATIONS
101 060 kg (222 800 lb) 90 000 kg (198 420 lb) 80 000 kg (176 370 lb) 70 000 kg (154 325 lb) 60 000 kg (132 280 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
60 80
60 80
40
40 50
50
WEIGHT ON ONE MAIN LANDING GEAR
*1 2003 0006 00015 00025 000
20 YEAR PAVEMENT LIFE
ANNUAL DEPARTURES
*
F_AC_070501_1_0020101_01_01
ALPHA FACTOR = 0.8
Flexible Pavement RequirementsMTOW 212 000 kg
FIGURE 3
7-5-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
3 6 10 15 20 30
3020156 103
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 TIRESTIRE PRESSURE CONSTANT AT 13.3 BAR (194 PSI)
10 000 COVERAGES USED FOR ACN CALCULATIONS
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
60 80
60 80
40
40 50
50
WEIGHT ON ONE MAIN LANDING GEAR 104 750 kg (230 925 lb) 90 000 kg (198 420 lb) 80 000 kg (176 370 lb) 70 000 kg (154 325 lb) 60 000 kg (132 280 lb)
*1 2003 0006 00015 00025 000
20 YEAR PAVEMENT LIFE
ANNUAL DEPARTURES
*
F_AC_070501_1_0030101_01_01
ALPHA FACTOR = 0.8
Flexible Pavement RequirementsMTOW 218 000 kg
FIGURE 4
7-5-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
103 6 15 20 30
30156 103
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 TIRESTIRE PRESSURE CONSTANT AT 14.2 BAR (206 PSI)
60 80
60 80
40
40 50
50
10 000 COVERAGES USED FOR ACN CALCULATIONS
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR 110 330 kg (243 225 lb) 100 000 kg (220 460 lb) 90 000 kg (198 420 lb) 80 000 kg (176 370 lb) 70 000 kg (154 325 lb)
*1 2003 0006 00015 00025 000
20 YEAR PAVEMENT LIFE
ANNUAL DEPARTURES
*
ALPHA FACTOR = 0.8
F_AC_070501_1_0040101_01_01
Flexible Pavement RequirementsMTOW 230 000 kg
FIGURE 5
7-5-1Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
3 6 10 15 20 30
3020156 103
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400x530R23 TIRESTIRE PRESSURE CONSTANT AT 14.5 BAR (210 PSI)
80 000 kg (176 370 lb) 70 000 kg (154 325 lb)
60 80
60 80
40
40 50
50
10 000 COVERAGES USED FOR ACN CALCULATIONS
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR 111 730 kg (246 325 lb) 100 000 kg (220 460 lb) 90 000 kg (198 420 lb)
*1 2003 0006 00015 00025 000
20 YEAR PAVEMENT LIFE
ANNUAL DEPARTURES
*ALPHA FACTOR = 0.8
F_AC_070501_1_0050101_01_01
Flexible Pavement RequirementsMTOW 233 000 kg
FIGURE 6
7-5-1Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A330-200 A330-200F A330-300
Flexible Pavement Requirements - LCN Conversion
**ON A/C A330-200
1. General
To find the airplane weight that a Flexible Pavement can support, the LCN of the pavement and thethickness (h) must be known.
In the example shown in Section 7-6-1, Figure: Flexible Pavement Requirements LCN - MTOW 233000 kg - A330-200
The thickness ”h” is shown at 762 mm (30 in.) with an LCN of 108.
For these conditions the weight on one Main Landing Gear is 100 000 kg (220 460 lb).
**ON A/C A330-200F
2. General
To find the airplane weight that a Flexible Pavement can support, the LCN of the pavement and thethickness (h) must be known.
In the example shown in Section 7-6-1, Figure: Flexible Pavement Requirements LCN - MTOW 233000 kg - A330-200F
The thickness ”h” is shown at 762 mm (30 in.) with an LCN of 108.
For these conditions the weight on one Main Landing Gear is 100 000 kg (220 460 lb).
**ON A/C A330-300
3. General
To find the airplane weight that a Flexible Pavement can support, the LCN of the pavement and thethickness (h) must be known.
In the example shown in Section 7-6-1, Figure: Flexible Pavement Requirements LCN - MTOW 212000 kg - A330-300
7-6-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
The thickness ”h” is shown at 762 mm (30 in.) with an LCN of 94.
For these conditions the weight on one Main Landing Gear is 90 000 kg (198 416 lb).
7-6-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-6-1 Flexible Pavement Requirements - LCN Conversion
**ON A/C A330-200 A330-200F A330-300
Flexible Pavement Requirements - LCN Conversion
1. This section gives Flexible Pavement Requirements - LCN Conversion.
7-6-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
100
9080
7060
150
120
180
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
BA
R (
206
PS
I)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUVALENT SINGLE WHEEL LOAD [1000 lb]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R11
0 47
0 kg
(
243
525
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
NO
TE
:
F_AC_070601_1_0010101_01_01
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [m
m]
254
508
762
1016
1524
2032
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
Flexible Pavement RequirementsMTOW 233 000 kg
FIGURE 1
7-6-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
100
9080
7060
150
120
180
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
BA
R (
206
PS
I)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUVALENT SINGLE WHEEL LOAD [1000 lb]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R11
0 47
0 kg
(
243
525
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
NO
TE
:
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [m
m]
254
508
762
1016
1524
2032
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
F_AC_070601_1_0060101_01_00
Flexible Pavement RequirementsMTOW 233 000 kg
FIGURE 2
7-6-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
100
9080
7060
150
120
180
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [m
m]
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(189
psi
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R10
1 06
0 kg
(
222
800
lb)
90 0
00 k
g
(198
420
lb)
80 0
00 k
g
(176
370
lb)
70 0
00 k
g
(154
325
lb)
60 0
00 k
g
(132
280
lb)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
NO
TE
:
254
508
762
1016
1 52
42
032
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
F_AC_070601_1_0020101_01_02
Flexible Pavement RequirementsMTOW 212 000 kg
FIGURE 3
7-6-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
100
9080
7060
150
120
180
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.3
BA
R (
194
PS
I)
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R10
4 75
0 kg
(
230
925
lb)
100
000
kg
(22
0 46
0 lb
) 9
0 00
0 kg
(
198
420
lb)
80
000
kg
(17
6 37
0 lb
) 7
0 00
0 kg
(
154
325
lb)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
:
F_AC_070601_1_0030101_01_01
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [m
m]
254
508
762
1016
1524
2032
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
Flexible Pavement RequirementsMTOW 218 000 kg
FIGURE 4
7-6-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
100
9080
7060
150
120
180
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
BA
R (
206
PS
I)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R11
0 33
0 kg
(
243
225
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
NO
TE
:
F_AC_070601_1_0040101_01_01
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [m
m]
254
508
762
1016
1524
2032
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
Flexible Pavement RequirementsMTOW 230 000 kg
FIGURE 5
7-6-1Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
100
9080
7060
150
120
180
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
51015202530354045
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.5
BA
R (
210
PS
I)
WE
IGH
T O
N O
NE
MA
IN
LAN
DIN
G G
EA
R11
1 73
0 kg
(
246
325
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
50
NO
TE
:
F_AC_070601_1_0050101_01_01
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [m
m]
254
508
762
1016
1524
2032
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
Flexible Pavement RequirementsMTOW 233 000 kg
FIGURE 6
7-6-1Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A330-200 A330-200F A330-300
Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A330-200
1. General
To determine a Rigid Pavement Thickness, the Subgrade Modulus (k), the allowable working stressand the weight on one Main Landing Gear must be known.
In the example shown in Section 7-7-1 Figure: Rigid Pavement Requirements - MTOW 233 000 kg -A330-200- a ”k” value of 150 MN/m3 (550 lb/in3)- an allowable working stress of 39 kg/cm2 (550 lb/in2)- the load on one Main Landing Gear of 80 000 kg (176 370 lb) the required Rigid Pavement
Thickness is 22 cm (8.6 inches).
**ON A/C A330-200F
2. General
To determine a Rigid Pavement Thickness, the Subgrade Modulus (k), the allowable working stressand the weight on one Main Landing Gear must be known.
In the example shown in Section 7-7-1 Figure: Rigid Pavement Requirements - MTOW 233 000 kg -A330-200F- a ”k” value of 150 MN/m3 (550 lb/in3)- an allowable working stress of 39 kg/cm2 (550 lb/in2)- the load on one Main Landing Gear of 80 000 kg (176 370 lb) the required Rigid Pavement
Thickness is 22 cm (8.6 inches).
**ON A/C A330-300
3. General
To determine a Rigid Pavement Thickness, the Subgrade Modulus (k), the allowable working stressand the weight on one Main Landing Gear must be known.
In the example shown in Section 7-7-1 Figure: Rigid Pavement Requirements - MTOW 212 000 kg -A330-300- a ”k” value of 150 MN/m3 (550 lb/in3)
7-7-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
- an allowable working stress of 39 kg/cm2 (550 lb/in2)- the load on one Main Landing Gear of 80 000 kg (176 370 lb) the required Rigid Pavement
Thickness is 22 cm (8.6 inches).
7-7-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A330-200 A330-200F A330-300
Rigid Pavement Requirements - Portland Cement Association Design Method
1. This section gives Rigid Pavement Requirements.
7-7-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
7
8
9
10
11
12
13
14
15
(IN
CH
ES
)
200
300
400
500
600
700
800
900
1000
36
34
32
30
28
26
24
22
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
15
20
25
30
35
40
45
50
55
60
65
70
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 TIRESTIRE PRESSURE CONSTANT = 14.2 BAR (206 PSI)
110 470 kg (243 525 lb)100 000 kg (220 460 lb)90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR
[lb/in
²]
[kg/
cm²]
THE VALUES OBTAINED BY USINGTHE MAXIMUM LOAD REFERENCELINE AND ANY VALUES FOR K AREEXACT. FOR LOADS LESS THAN MAXIMUM,THE CURVES ARE EXACT FORK=80 MN/m BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K
REFERENCE:"DESIGN OF CONCRETEAIRPORT PAVEMENTS" AND"COMPUTER PROGRAM FORAIRPORT PAVEMENT DESIGN−PROGRAM PDILB" PORTLANDCEMENT ASSOCIATION
K = 20 MN/mK = 40 MN/mK = 80 MN/mK = 150 MN/m
NOTES:
F_AC_070701_1_0010101_01_00
Rigid Pavement RequirementsMTOW 233 000 kg
FIGURE 1
7-7-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
7
8
9
10
11
12
13
14
15
(IN
CH
ES
)
200
300
400
500
600
700
800
900
1000
36
34
32
30
28
26
24
22
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
15
20
25
30
35
40
45
50
55
60
65
70
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 TIRESTIRE PRESSURE CONSTANT = 14.2 BAR (206 PSI)
110 470 kg (243 525 lb)100 000 kg (220 460 lb)90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR
[lb/in
²]
[kg/
cm²]
THE VALUES OBTAINED BY USINGTHE MAXIMUM LOAD REFERENCELINE AND ANY VALUES FOR K AREEXACT. FOR LOADS LESS THAN MAXIMUM,THE CURVES ARE EXACT FORK=80 MN/m BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K
REFERENCE:"DESIGN OF CONCRETEAIRPORT PAVEMENTS" AND"COMPUTER PROGRAM FORAIRPORT PAVEMENT DESIGN−PROGRAM PDILB" PORTLANDCEMENT ASSOCIATION
K = 20 MN/mK = 40 MN/mK = 80 MN/mK = 150 MN/m
NOTES:
F_AC_070701_1_0060101_01_00
Rigid Pavement RequirementsMTOW 233 000 kg
FIGURE 2
7-7-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
7
8
9
10
11
12
13
14
15
[INC
HE
S]
200
300
400
500
600
700
800
900
1000
36
34
32
30
28
26
24
22
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
15
20
25
30
35
40
45
50
55
60
65
70
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 TIRESTIRE PRESSURE CONSTANT = 13.1 BAR (190 PSI)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
NOTES:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT.
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
FOR LOADS LESS THAN MAXIMUM,
FOR ANY OTHER VALUES OF K
K = 20 MN/mK = 40 MN/mK = 80 MN/mK = 150 MN/m
[lb/in
²]
[kg/
cm²]
K=80 MN/m BUT DEVIATE SLIGHTLYTHE CURVES ARE EXACT FOR
101 060 kg (222 800 lb)90 000 kg (198 420 lb)80 000 kg (176 370 lb)
60 000 kg (132 280 lb)
WEIGHT ON ONE MAIN LANDING GEAR
70 000 kg (154 325 lb)
F_AC_070701_1_0020101_01_00
Rigid Pavement RequirementsMTOW 212 000 kg
FIGURE 3
7-7-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
7
8
9
10
11
12
13
14
15
[INC
HE
S]
200
300
400
500
600
700
800
900
1000
36
34
32
30
28
26
24
22
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
15
20
25
30
35
40
45
50
55
60
65
70
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 TIRESTIRE PRESSURE CONSTANT = 13.3 BAR (194 PSI)
NOTES:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT.
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
FOR LOADS LESS THAN MAXIMUM,
FOR ANY OTHER VALUES OF K
[lb/in
²]
[kg/
cm²]
THE CURVES ARE EXACT FORK=80 MN/m BUT DEVIATE SLIGHTLY
104 750 kg (222 800 lb)100 000 kg (220 460 lb)
90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
WEIGHT ON ONE MAIN LANDING GEAR
K = 20 MN/mK = 40 MN/mK = 80 MN/mK = 150 MN/m
F_AC_070701_1_0030101_01_00
Rigid Pavement RequirementsMTOW 218 000 kg
FIGURE 4
7-7-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
7
8
9
10
11
12
13
14
15[IN
CH
ES
]
200
300
400
500
600
700
800
900
1000
36
34
32
30
28
26
24
22
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
15
20
25
30
35
40
45
50
55
60
65
70
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 TIRESTIRE PRESSURE CONSTANT = 14.2 BAR (206 PSI)
NOTES:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT.
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
FOR LOADS LESS THAN MAXIMUM,
FOR ANY OTHER VALUES OF K
[lb/in
²]
[kg/
cm²]
THE CURVES ARE EXACT FORK=80 MN/m BUT DEVIATE SLIGHTLY
K = 20 MN/mK = 40 MN/mK = 80 MN/mK = 150 MN/m
110 330 kg (243 225 lb)100 000 kg (220 460 lb)90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
WEIGHT ON ONE MAIN LANDING GEAR
F_AC_070701_1_0040101_01_00
Rigid Pavement RequirementsMTOW 230 000 kg
FIGURE 5
7-7-1Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
7
8
9
10
11
12
13
14
15
[INC
HE
S]
200
300
400
500
600
700
800
900
1000
36
34
32
30
28
26
24
22
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
15
20
25
30
35
40
45
50
55
60
65
70
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 TIRESTIRE PRESSURE CONSTANT = 14.5 BAR (210 PSI)
NOTES:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT.
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
FOR LOADS LESS THAN MAXIMUM,
FOR ANY OTHER VALUES OF K
[lb/in
²]
[kg/
cm²]
THE CURVES ARE EXACT FORK=80 MN/m BUT DEVIATE SLIGHTLY
MAXIMUM RAMP WEIGHT AND AFT CGMAXIMUM POSSIBLE MAIN GEAR LOAD AT
GEAR111 730 kg (246 330 lb)100 000 kg (220 460 lb)
90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
WEIGHT ON ONE MAIN LANDING
K = 20 MN/mK = 40 MN/mK = 80 MN/mK = 150 MN/m
F_AC_070701_1_0050101_01_00
Rigid Pavement RequirementsMTOW 233 000 kg
FIGURE 6
7-7-1Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-0 Rigid Pavement Requirements - LCN Conversion
**ON A/C A330-200 A330-200F A330-300
Rigid Pavement Requirements - LCN Conversion
**ON A/C A330-200
1. General
To determine the airplane weight that a Rigid Pavement can support, the LCN of the pavement andthe Radius of Relative Stiffness (L) must be known.
In the example shown in Section 7-8-2, Figure: Rigid Pavement Requirements LCN - MTOW 233 000kg - A330-200
The Radius of Relative Stiffness is shown at 1016 mm (40 in.) with an LCN of 96
For these conditions the weight on one Main Landing Gear is 100 000 kg (220 462 lb)
**ON A/C A330-200F
2. General
To determine the airplane weight that a Rigid Pavement can support, the LCN of the pavement andthe Radius of Relative Stiffness (L) must be known.
In the example shown in Section 7-8-2, Figure: Rigid Pavement Requirements LCN - MTOW 233 000kg - A330-200F
The Radius of Relative Stiffness is shown at 1016 mm (40 in.) with an LCN of 96
For these conditions the weight on one Main Landing Gear is 100 000 kg (220 462 lb)
**ON A/C A330-300
3. General
To determine the airplane weight that a Rigid Pavement can support, the LCN of the pavement andthe Radius of Relative Stiffness (L) must be known.
In the example shown in Section 7-8-2, Figure: Rigid Pavement Requirements LCN - MTOW 212 000kg - A330-300
7-8-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
The Radius of Relative Stiffness is shown at 1016 mm (40 in.) with an LCN of 83
For these conditions the weight on one Main Landing Gear is 90 000 kg (198 420 lb).
7-8-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-1 Radius of Relative Stiffness
**ON A/C A330-200 A330-200F A330-300
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
d6.06.57.07.5
K=75 K=100 K=150 K=200 K=250 K=300 K=350 K=400 K=550
8.08.59.09.5
10.010.511.011.512.012.513.013.514.014.515.015.516.016.517.017.518.019.020.021.022.023.024.025.0
31.4833.4335.3437.2239.0640.8842.6744.4346.1847.9049.6051.2852.9454.5956.2257.8359.4361.0262.5964.1565.6967.2368.7570.2671.7674.7377.6680.5583.4186.2489.0491.81
29.3031.1132.8934.6336.3538.0439.7141.3542.9744.5746.1647.7249.2750.8052.3253.8255.3156.7858.2559.7061.1362.5663.9865.3866.7869.5472.2774.9677.6380.2682.8685.44
26.4728.1129.7231.2932.8534.3735.8837.3638.8340.2841.7143.1244.5245.9047.2748.6349.9851.3152.6353.9455.2456.5357.8159.0860.3462.8465.3067.7470.1472.5274.8777.20
24.6326.1627.6529.1230.5731.9933.3934.7736.1437.4838.8140.1341.4342.7243.9945.2646.5147.7548.9850.2051.4152.6153.8054.9856.1558.4860.7763.0465.2867.4969.6871.84
23.3024.7426.1527.5428.9130.2531.5832.8934.1735.4536.7137.9539.1840.4041.6142.8043.9845.1646.3247.4748.6249.7550.8852.0053.1155.3157.4759.6261.7363.8365.9067.95
22.2623.6424.9926.3227.6228.9130.1731.4232.6533.8735.0736.2637.4438.6039.7540.8942.0243.1544.2645.3646.4547.5448.6149.6850.7452.8454.9156.9658.9860.9862.9664.92
21.4222.7424.0425.3226.5827.8129.0330.2331.4232.5933.7534.8936.0237.1438.2539.3540.4441.5142.5843.6444.7045.7446.7747.8048.8250.8452.8454.8156.7558.6860.5862.46
20.7222.0023.2524.4925.7026.9028.0829.2430.3931.5232.6433.7434.8435.9236.9938.0639.1140.1541.1942.2143.2344.2445.2446.2347.2249.1751.1053.0154.8956.7558.5960.41
19.1320.3121.4722.6123.7424.8425.9327.0028.0629.1130.1431.1632.1733.1734.1635.1436.1237.0838.0338.9839.9240.8541.7842.7043.6145.4147.1948.9550.6952.4154.1155.79
RADIUS OF RELATIVE STIFFNESS (L)VALUES IN INCHES
L =
E = Young’s Modulus = 4 x 10 psi
k = Subgrade Modulus, Lbf/in
d = Rigid Pavement Thickness, inches
= Poisson’s Ratio = 0.15
Ed12 (1 − ² ) k = 24.1652
dk
WHERE
3
6
3
4 43
F_AC_070801_1_0010101_01_00
Radius of relative stiffness(Reference : Portland Cement Association)
FIGURE 1
7-8-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-2 Rigid Pavement Requirements - LCN Conversion
**ON A/C A330-200 A330-200F A330-300
Rigid Pavement Requirements - LCN Conversion
1. This section gives Rigid Pavement Requirements - LCN Conversion.
7-8-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
6070
8090
100
5040
3020
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
120
150
6070
8090
100
50LO
AD
CLA
SS
IFIC
AT
ION
NU
MB
ER
(LC
N)
5101520253035404550
NO
TE
: ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R11
0 47
0 kg
(
243
525
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
F_AC_070802_1_0010101_01_01
508
762
1016
1524
2540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [m
m]
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
2032
Rigid Pavement Requirements LCNMTOW 233 000 kg
FIGURE 1
7-8-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
6070
8090
100
5040
3020
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
120
150
6070
8090
100
50LO
AD
CLA
SS
IFIC
AT
ION
NU
MB
ER
(LC
N)
5101520253035404550
NO
TE
: ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R11
0 47
0 kg
(
243
525
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
508
762
1016
1524
2540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [m
m]
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
2032
F_AC_070802_1_0060101_01_00
Rigid Pavement Requirements LCNMTOW 233 000 kg
FIGURE 2
7-8-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
6070
8090
100
5040
3020
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
5010
090
8070
6015
012
0
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
NO
TE
: ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(189
psi
)
WE
IGH
T O
N O
NE
M
AIN
LA
ND
ING
GE
AR
101
060
kg
(22
2 80
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)60
000
kg
(1
32 2
80 lb
)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
F_AC_070802_1_0020101_01_01
508
762
1016
2540
2032
1524
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [m
m]
Rigid Pavement Requirements LCNMTOW 212 000 kg
FIGURE 3
7-8-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
6070
8090
100
5040
3020
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
120
150
6070
8090
100
50LO
AD
CLA
SS
IFIC
AT
ION
NU
MB
ER
(LC
N)
5101520253035404550
NO
TE
: ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.3
bar
(194
psi
)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R10
4 75
0 kg
(
230
925
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
F_AC_070802_1_0030101_01_01
508
762
1016
2540
2032
1524
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [m
m]
Rigid Pavement Requirements LCNMTOW 218 000 kg
FIGURE 4
7-8-2Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
6070
8090
100
5040
3020
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
120
150
6070
8090
100
50LO
AD
CLA
SS
IFIC
AT
ION
NU
MB
ER
(LC
N)
5101520253035404550
NO
TE
: ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R11
0 33
0 kg
(
243
225
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
F_AC_070802_1_0040101_01_01
508
762
1016
2540
2032
1524
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [m
m]
Rigid Pavement Requirements LCNMTOW 230 000 kg
FIGURE 5
7-8-2Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
6070
8090
100
5040
3020
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
6050
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5
NO
TE
: ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x530
R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.5
bar
(210
psi
)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
101520253035404550
120
150
7080
9010
0
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R11
1 73
0 kg
(
243
325
lb)
100
000
kg
(22
0 46
0 lb
)90
000
kg
(1
98 4
20 lb
)80
000
kg
(1
76 3
70 lb
)70
000
kg
(1
54 3
25 lb
)
F_AC_070802_1_0050101_01_01
508
762
1016
2540
2032
1524
MA
XIM
UM
PO
SS
IBLE
MA
ING
EA
R L
OA
D A
T M
AX
IMU
MR
AM
P W
EIG
HT
AN
D A
FT
CG
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [m
m]
Rigid Pavement Requirements LCNMTOW 233 000 kg
FIGURE 6
7-8-2Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-3 Radius of Relative Stiffness (Other values of E and L)
**ON A/C A330-200 A330-200F A330-300
Radius of Relative Stiffness (Other values of ”E” and ”µ”)
1. General
The table of Chapter 7-8-1, Figure: Radius of Relative Stiffness, presents ”L” values based onYoung’s Modulus (E) of 4 000 000 psi and Poisson’s Ratio (µ) of 0.15.
To find ”L” values based on other values of ”E” and ”µ”,See Section 7-8-4, Figure: Radius of Relative Stiffness (Other values of ”E” and ”µ”)
For example, to find an ”L” value based on an ”E” of 3 000 000 psi, the ”E” factor of 0.931 ismultiplied by the ”L” value found in table of Section 7-8-1, Figure: Radius of Relative Stiffness.
The effect of variations of ”µ” on the ”L” value is treated in a similar manner.
7-8-3Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-4 Radius of Relative Stiffness
**ON A/C A330-200 A330-200F A330-300
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-4Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200 A330-200F A330-300
0.80
0.85
0.90
0.95
1.00
1.05
1.10
0 1 2 3 4 5
E F
acto
r
0.995
1.000
1.005
1.010
1.015
0.00 0.05 0.10 0.15 0.20 0.25
NOTE:
EFFECT OF ON VALUES
E, Young’s Modulus (10 , PSI)
EFFECT OF E ON VALUES
, Poisson’s Ratio
Fac
tor
BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE " " VALUES OF TABLE 7−8−1
F_AC_070804_1_0010101_01_00
Radius of Relative Stiffness(Effect E and µ ON ”L” values)
FIGURE 1
7-8-4Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements
**ON A/C A330-200 A330-200F A330-300
ACN/PCN Reporting System - Flexible and Rigid Pavements
**ON A/C A330-200
1. General
To find the ACN of an aircraft on flexible or rigid pavement, the aircraft gross weight and thesubgrade strength must be known.
In the example shown in Section 7-9-1, Figure: Aircraft Classification Number - Flexible Pavement -MTOW 192 000 kg - A330-200- For an Aircraft Gross Weight of 180 000 kg (396 830 lb) and low subgrade strength (code C),
the ACN for the flexible pavement is 51.
In the example shown in Section 7-9-2, Figure: Aircraft Classification Number - Rigid Pavement -MTOW 192 000 kg - A330-200- For an Aircraft Gross Weight of 180 000 kg (396 830 lb) and low subgrade strength (code C),
the ACN for the rigid pavement is 52.
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref : ICAO Aerodrome Design Manual Part 3 Chapter 1 Second Edition 1983).
**ON A/C A330-200F
2. General
To find the ACN of an aircraft on flexible or rigid pavement, the aircraft gross weight and thesubgrade strength must be known.
In the example shown in Section 7-9-1, Figure: Aircraft Classification Number - Flexible Pavement -MTOW 227 000 kg - A330-200F- For an Aircraft Gross Weight of 200 000 kg (440 924 lb) and low subgrade strength (code C),
the ACN for the flexible pavement is 58.
In the example shown in Section 7-9-2, Figure: Aircraft Classification Number - Rigid Pavement -MTOW 227 000 kg - A330-200F- For an Aircraft Gross Weight of 200 000 kg (440 924 lb) and low subgrade strength (code C),
the ACN for the rigid pavement is 59.
7-9-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref : ICAO Aerodrome Design Manual Part 3 Chapter 1 Second Edition 1983).
**ON A/C A330-300
3. General
To find the ACN of an aircraft on flexible or rigid pavement, the aircraft gross weight and thesubgrade strength must be known.
In the example shown in Section 7-9-1, Figure: Aircraft Classification Number - Flexible Pavement -MTOW 184 000 kg - A330-300- For an Aircraft Gross Weight of 170 000 kg (374 786 lb) and low subgrade strength (code C),
the ACN for the flexible pavement is 47.
In the example shown in Section 7-9-2, Figure: Aircraft Classification Number - Rigid Pavement -MTOW 184 000 kg - A330-300- For an Aircraft Gross Weight of 170 000 kg (374 786 lb) and low subgrade strength (code C),
the ACN for the rigid pavement is 47.5.
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref : ICAO Aerodrome Design Manual Part 3 Chapter 1 Second Edition 1983).
7-9-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-9-1 Aircraft Classification Number - Flexible Pavement
**ON A/C A330-200 A330-200F A330-300
Aircraft Classification Number - Flexible Pavement
1. This section gives the Aircraft Classification Number - Flexible Pavement.
7-9-1Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
2030405060708090100 11
012
013
014
015
016
017
018
019
020
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)1
400x
530R
23 T
IRE
S
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.8
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
NP
AV
EM
EN
T −
MT
OW
192
000
kg
− A
330−
200
(x 1
000
kg)
(x 1
000
lb)
250
275
300
325
350
375
400
425
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0010101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 192 000 kg
FIGURE 1
7-9-1Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
2030405060708090100 11
012
013
014
015
016
017
018
019
020
021
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.4
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
ALP
HA
FA
CT
OR
= 0
.8
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0
F_AC_070901_1_0020101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 202 000 kg
FIGURE 2
7-9-1Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
2030405060708090100 11
012
013
014
015
016
017
018
019
020
021
022
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.1
% M
AC
. S
EE
SE
CT
ION
7−
4−1F
IGU
RE
: LA
ND
ING
GE
AR
LO
AD
ING
ON
(x 1
000
kg)
(x 1
000
lb)
250
275
300
325
350
375
400
425
450
475
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
ALP
HA
FA
CT
OR
= 0
.8
PA
VE
ME
NT
− M
TO
W 2
10 0
00 k
g −
A33
0−20
0
F_AC_070901_1_0030101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 210 000 kg
FIGURE 3
7-9-1Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
2030405060708090100
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.79
% M
AC
.
(x 1
000
kg)
(x 1
000
lb)
525
250
275
300
325
350
375
400
425
450
475
SE
E S
EC
TIO
N 7
−4−
1 F
IGU
RE
: LA
ND
IG G
EA
R L
OA
DIN
G O
N1
400x
530R
23 T
IRE
S
110
500
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0040101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 220 000 kg
FIGURE 4
7-9-1Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
2030405060708090100
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.
(x 1
000
kg)
(x 1
000
lb)
525
250
275
300
325
350
375
400
425
450
475
SE
E S
EC
TIO
N 7
−4−
1 F
IGU
RE
: LA
ND
IG G
EA
R L
OA
DIN
G O
N1
400x
530R
23 T
IRE
S
110
500
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0050101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 230 000 kg
FIGURE 5
7-9-1Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.4
% M
AC
.
(x 1
000
kg)
(x 1
000
lb)
525
500
250
275
300
325
350
375
400
425
450
475
SE
E S
EC
TIO
N 7
−4−
1 F
IGU
RE
: LA
ND
ING
GE
AR
LO
AD
ING
ON
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0
2030405060708090100
110 11
012
013
014
015
016
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0060101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 233 000 kg
FIGURE 6
7-9-1Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
2030405060708090100
110 11
012
013
014
015
016
017
018
019
020
021
022
023
024
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.57
% M
AC
.
(x 1
000
kg)
(x 1
000
lb)
525
500
250
275
300
325
350
375
400
425
450
475
SE
E S
EC
TIO
N 7
−4−
1 F
IGU
RE
: LA
ND
ING
GE
AR
LO
AD
ING
ON
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
27 0
00 k
g −
A33
0−20
0F
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0150101_01_02
Aircraft Classification Number -- Flexible PavementMTOW 227 000 kg
FIGURE 7
7-9-1Page 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
2030405060708090100
110 11
012
013
014
015
016
017
018
019
020
021
022
023
024
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.4
% M
AC
.
(x 1
000
kg)
(x 1
000
lb)
525
500
250
275
300
325
350
375
400
425
450
475
SE
E S
EC
TIO
N 7
−4−
1 F
IGU
RE
: LA
ND
ING
GE
AR
LO
AD
ING
ON
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0F
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0160101_01_02
Aircraft Classification Number -- Flexible PavementMTOW 233 000 kg
FIGURE 8
7-9-1Page 9
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090100 11
012
013
014
015
016
017
018
019
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(189
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0.1
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
250
275
300
325
350
375
400
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 1
84 0
00 k
g −
A33
0−30
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0070101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 184 000 kg
FIGURE 9
7-9-1Page 10
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090100 11
012
013
014
015
016
017
018
019
020
021
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.5
bar
(210
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9.6
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
PA
VE
ME
NT
− M
TO
W 2
30 0
00 k
g −
A33
0−30
0
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0080101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 205 000 kg
FIGURE 10
7-9-1Page 11
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090100 11
012
013
014
015
016
017
018
019
020
021
022
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(189
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6.5
% M
AC
.
(x 1
000
kg)
(x 1
000
lb)
475
250
275
300
325
350
375
400
425
450
SE
E S
EC
TIO
N 7
−4−
1 F
IGU
RE
: LA
ND
ING
GE
AR
LO
AD
ING
ON
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
12 0
00 k
g −
A33
0−30
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
− 0
.8
F_AC_070901_1_0090101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 212 000 kg
FIGURE 11
7-9-1Page 12
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090100 11
012
013
014
015
016
017
018
019
020
021
022
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.3
bar
(194
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9.2
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
475
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
15 0
00 k
g −
A33
0−30
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0100101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 215 000 kg
FIGURE 12
7-9-1Page 13
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090100 11
012
013
014
015
016
017
018
019
020
021
022
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9.12
% M
AC
.
(x 1
000
kg)
(x 1
000
lb)
475
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
SE
E S
EC
TIO
N 7
−4−
1 F
IGU
RE
: LA
ND
ING
GE
AR
LO
AD
ING
ON
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
17 0
00 k
g −
A33
0−30
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0110101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 217 000 kg
FIGURE 13
7-9-1Page 14
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090100 11
012
013
014
015
016
017
018
019
020
021
022
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.3
bar
(194
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9.1
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
475
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
18 0
00 k
g −
A33
0−30
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0120101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 218 000 kg
FIGURE 14
7-9-1Page 15
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090100
110 11
012
013
014
015
016
017
018
019
020
021
022
023
024
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
525
500
475
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
PA
VE
ME
NT
− M
TO
W 2
30 0
00 k
g −
A33
0−30
0
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0130101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 230 000 kg
FIGURE 15
7-9-1Page 16
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090100
110 11
012
013
014
015
016
017
018
019
020
021
022
023
024
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.5
bar
(210
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.6
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
525
500
475
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (
ULT
RA
LO
W)
C −
CB
R
6 (
LOW
)B
− C
BR
10
(M
ED
IUM
)A
− C
BR
15
(H
IGH
)
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−30
0
ALP
HA
FA
CT
OR
= 0
.8
F_AC_070901_1_0140101_01_03
Aircraft Classification Number -- Flexible PavementMTOW 233 000 kg
FIGURE 16
7-9-1Page 17
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-9-2 Aircraft Classification Number - Rigid Pavement
**ON A/C A330-200 A330-200F A330-300
Aircraft Classification Number - Rigid Pavement
1. This section gives the Aircraft Classification Number - Rigid Pavement.
7-9-2Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
20304050607080
110
120
130
140
150
160
170
180
190
200
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 40
0x53
0R23
40P
R T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
2 ba
r (2
06 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.8
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E; L
AN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
kg)
(x 1
000
lb)
SU
BG
RA
DE
ST
RE
NG
TH
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
ON
PA
VE
ME
NT
− M
TO
W 1
92 0
00 k
g −
A33
0−20
0
(HIG
H)
250
275
300
325
350
375
400
425
F_AC_070902_1_0010101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 192 000 kg
FIGURE 1
7-9-2Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
20304050607080
110
120
130
140
150
160
170
180
190
200
210
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.4
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
SU
BG
RA
DE
ST
RE
NG
TH
(ULT
RA
LO
W)
(LO
W)
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0
(HIG
H)
(ME
DIU
M)
F_AC_070902_1_0020101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 202 000 kg
FIGURE 2
7-9-2Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
20304050607080
110
120
130
140
150
160
170
180
190
200
210
220
AIR
CR
AF
T G
RO
SS
WE
IGH
T
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.1
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
kg)
(x 1
000
lb)
1 40
0x53
0R23
TIR
ES
SU
BG
RA
DE
ST
RE
NG
TH
(LO
W)
(ME
DIU
M)
C −
K =
40
MN
/mB
− K
=
80 M
N/m
A −
K =
150
MN
/m
D −
K =
20
MN
/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(HIG
H)
ON
PA
VE
ME
NT
− M
TO
W 2
10 0
00 k
g −
A33
0−20
0
475
250
275
300
325
350
375
400
425
450
F_AC_070902_1_0030101_01_02
(ULT
RA
LO
W)
Aircraft Classification Number -- Rigid PavementMTOW 210 000 kg
FIGURE 3
7-9-2Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
2030405060708090
110
120
130
140
150
160
170
180
190
200
210
220
230
240
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.79
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DN
G O
N
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
1 40
0x53
0R23
TIR
ES
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
A −
K =
150
MN
/mB
− K
=
80 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)P
AV
EM
EN
T −
MT
OW
233
000
kg
− A
330−
200
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
525
500
475
250
275
300
325
350
375
400
425
450
F_AC_070902_1_0040101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 220 000 kg
FIGURE 4
7-9-2Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
2030405060708090
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
SU
BG
RA
DE
ST
RE
NG
TH
(ULT
RA
LO
W)
(LO
W)
C −
K =
40
MN
/mB
− K
=
80 M
N/m
A −
K =
150
MN
/m
D −
K =
20
MN
/m
(ME
DIU
M)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0
(HIG
H)
525
500
475
250
275
300
325
350
375
400
425
450
F_AC_070902_1_0050101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 230 000 kg
FIGURE 5
7-9-2Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
2030405060708090
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.4
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
525
500
475
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0060101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 233 000 kg
FIGURE 6
7-9-2Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
2030405060708090
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.57
% M
AC
.S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
525
500
475
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
PA
VE
ME
NT
− M
TO
W 2
27 0
00 k
g −
A33
0−20
0F
SU
BG
RA
DE
ST
RE
NG
TH
(ULT
RA
LO
W)
(LO
W)
C −
K =
40
MN
/mB
− K
=
80 M
N/m
A −
K =
150
MN
/m
D −
K =
20
MN
/m
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0150101_01_01
Aircraft Classification Number -- Rigid PavementMTOW 227 000 kg
FIGURE 7
7-9-2Page 8
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
2030405060708090
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.4
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
525
500
475
250
275
300
325
350
375
400
425
450
1 40
0x53
0R23
TIR
ES
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−20
0F
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0160101_01_01
Aircraft Classification Number -- Rigid PavementMTOW 233 000 kg
FIGURE 8
7-9-2Page 9
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
20304050607080
110
120
130
140
150
160
170
180
190
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(189
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0.1
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
kg)
(x 1
000
lb)
250
275
300
325
350
375
400
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
(ULT
RA
LO
W)
(LO
W)
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
ON
PA
VE
ME
NT
− M
TO
W 1
84 0
00 k
g −
A33
0−30
0
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0070101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 184 000 kg
FIGURE 9
7-9-2Page 10
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
20304050607080
110
120
130
140
150
160
170
180
190
200
210
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.5
bar
(210
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9.6
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
kg)
(x 1
000
lb)
250
275
300
325
350
375
400
425
450
SU
BG
RA
DE
ST
RE
NG
TH
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)
ON
PA
VE
ME
NT
− M
TO
W 2
30 0
00 k
g −
A33
0−30
0
F_AC_070902_1_0080101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 205 000 kg
FIGURE 10
7-9-2Page 11
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
20304050607080
110
120
130
140
150
160
170
180
190
200
210
220
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(189
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6.5
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
kg)
(x 1
000
lb)
475
250
275
300
325
350
375
400
425
450
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)
ON
PA
VE
ME
NT
− M
TO
W 2
12 0
00 k
g −
A33
0−30
0
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0090101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 212 000 kg
FIGURE 11
7-9-2Page 12
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
20304050607080
110
120
130
140
150
160
170
180
190
200
210
220
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.3
bar
(194
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9.2
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
475
250
275
300
325
350
375
400
425
450
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)P
AV
EM
EN
T −
MT
OW
215
000
kg
− A
330−
300
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0100101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 215 000 kg
FIGURE 12
7-9-2Page 13
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
20304050607080
110
120
130
140
150
160
170
180
190
200
210
220
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9.12
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G O
N
(x 1
000
kg)
(x 1
000
lb)
475
250
275
300
325
350
375
400
425
450
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)P
AV
EM
EN
T −
MT
OW
217
000
kg
− A
330−
300
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0110101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 217 000 kg
FIGURE 13
7-9-2Page 14
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
20304050607080
110
120
130
140
150
160
170
180
190
200
210
220
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.3
bar
(194
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9.1
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
kg)
(x 1
000
lb)
450
425
400
375
350
325
300
275
250
475
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)
ON
PA
VE
ME
NT
− M
TO
W 2
18 0
00 k
g −
A33
0−30
0
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0120101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 218 000 kg
FIGURE 14
7-9-2Page 15
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
. S
EE
SE
CT
ION
7−
4−1
FIG
UR
E: L
AN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
kg)
(x 1
000
lb)
525
500
475
250
275
300
325
350
375
400
425
450
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)O
N P
AV
EM
EN
T −
MT
OW
230
000
kg
− A
330−
300
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0130101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 230 000 kg
FIGURE 15
7-9-2Page 16
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
2030405060708090
110
120
130
140
150
160
170
180
190
200
210
220
230
240
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 40
0x53
0R23
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.5
bar
(210
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1.
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.6
% M
AC
.
(x 1
000
kg)
(x 1
000
lb)
525
500
475
250
275
300
325
350
375
400
425
450
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/mC
− K
=
40 M
N/m
B −
K =
80
MN
/mA
− K
= 1
50 M
N/m
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SE
E S
EC
TIO
N 7
−4−
1 F
IGU
RE
: LA
ND
ING
GE
AR
LO
AD
NG
ON
PA
VE
ME
NT
− M
TO
W 2
33 0
00 k
g −
A33
0−30
0
(ULT
RA
LO
W)
(LO
W)
(ME
DIU
M)
(HIG
H)
F_AC_070902_1_0140101_01_02
Aircraft Classification Number -- Rigid PavementMTOW 233 000 kg
FIGURE 16
7-9-2Page 17
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
DERIVATIVE AIRPLANES
8-1-0 Possible Future Derivative Airplane
**ON A/C A330-200 A330-200F A330-300
Possible Future Derivative Airplane
1. General
Other versions of the A330 airplane are being studied to satisfy customer requests.
In the future, this program could have new versions:- Additional passenger capacity,- Additional cargo modularity,- New design version,- Different range or payload.
If these new aircraft definitions are developed, the design and weight will be considered in accordancewith airport facilities.
8-1-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
SCALED DRAWINGS
9-1-0 Scaled Drawing 1 in. = 500 ft.
**ON A/C A330-200 A330-200F A330-300
Scaled Drawing 1 in. = 50 ft.
1. This section provides the Scaled Drawing - 1 in. = 50 ft.
9-1-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
AIR CONDITIONINGA
BULK CARGO COMPT DOORB
CARGO COMPT DOORC
ELECTRICAL
LAVATORY
MAIN LANDING GEARMLG
NOSE GEARNG
PNEUMATICP
PASSENGER/CREW DOORX
E
L
FUEL
POTABLE WATER
F
H²O
LEGEND:
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
MLGMLG
NG XX
E
C
XX
PA
FF
C
XX
BL
H²O
F_AC_090100_1_0010101_01_01
Scaled Drawing1 in. = 50 ft.FIGURE 1
9-1-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
AIR CONDITIONINGA
BULK CARGO COMPT DOORB
CARGO COMPT DOORC
ELECTRICAL
LAVATORY
MAIN LANDING GEARMLG
NOSE GEARNG
PNEUMATICP
PASSENGER/CREW DOORX
E
L
FUEL
POTABLE WATER
F
H²O
LEGEND:
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
XX
E
C
XX
PA
FF
C
XX
BL
H²O
F_AC_090100_1_0050101_01_00
MLGMLG
NG
Scaled Drawing1 in. = 50 ft.FIGURE 2
9-1-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
AIR CONDITIONINGA
BULK CARGO COMPT DOORB
CARGO COMPT DOORC
ELECTRICAL
MAIN LANDING GEARMLG
NOSE GEARNG
PNEUMATICP
PASSENGER/CREW DOORX
E
FUEL
POTABLE WATER
F
H²O
XX
H²OPA
F
CB
C
E
F
LEGEND:
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
F_AC_090100_1_0030101_01_01
MLGMLG
NG
Scaled Drawing1 in. = 50 ft.FIGURE 3
9-1-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
F_AC_090100_1_0020101_01_01
Scaled Drawing1 in. = 50 ft.FIGURE 4
9-1-0Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
F_AC_090100_1_0060101_01_00
Scaled Drawing1 in. = 50 ft.FIGURE 5
9-1-0Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
F_AC_090100_1_0040101_01_01
Scaled Drawing1 in. = 50 ft.FIGURE 6
9-1-0Page 7
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
9-2-0 Scaled Drawing 1 cm. = 500 cm.
**ON A/C A330-200 A330-200F A330-300
Scaled Drawing 1 cm. = 500 cm.
1. This section provides the Scaled Drawing - 1 cm. = 500 cm.
9-2-0Page 1
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
F_AC_090200_1_0010101_01_01
AIR CONDITIONINGA
BULK CARGO COMPT DOORB
CARGO COMPT DOORC
ELECTRICAL
LAVATORY
MAIN LANDING GEARMLG
NOSE GEARNG
PNEUMATICP
PASSENGER/CREW DOORX
E
L
FUEL
POTABLE WATER
F
H²O
LEGEND:
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
XX
E
C
XX
PA
FF
C
XX
BL
H²O
MLGMLG
NG
Scaled Drawing1 cm. = 500 cm.
FIGURE 1
9-2-0Page 2
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
F_AC_090200_1_0050101_01_00
AIR CONDITIONINGA
BULK CARGO COMPT DOORB
CARGO COMPT DOORC
ELECTRICAL
LAVATORY
MAIN LANDING GEARMLG
NOSE GEARNG
PNEUMATICP
PASSENGER/CREW DOORX
E
L
FUEL
POTABLE WATER
F
H²O
LEGEND:
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
XX
E
C
XX
PA
FF
C
XX
BL
H²O
MLGMLG
NG
Scaled Drawing1 cm. = 500 cm.
FIGURE 2
9-2-0Page 3
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
AIR CONDITIONINGA
BULK CARGO COMPT DOORB
CARGO COMPT DOORC
ELECTRICAL
MAIN LANDING GEARMLG
NOSE GEARNG
PNEUMATICP
PASSENGER/CREW DOORX
E
FUEL
POTABLE WATER
F
H²O
XX
H²OPA
F
CB
C
E
F
F_AC_090200_1_0030101_01_01
LEGEND:
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
MLGMLG
NG
Scaled Drawing1 cm. = 500 cm.
FIGURE 3
9-2-0Page 4
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
F_AC_090200_1_0020101_01_01
Scaled Drawing1 cm. = 500 cm.
FIGURE 4
9-2-0Page 5
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-300
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
F_AC_090200_1_0060101_01_00
Scaled Drawing1 cm. = 500 cm.
FIGURE 5
9-2-0Page 6
Jan 01/11
@A330AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A330-200F
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
F_AC_090200_1_0040101_01_01
Scaled Drawing1 cm. = 500 cm.
FIGURE 6
9-2-0Page 7
Jan 01/11
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