AW119Kx General Presentation Decembre 2014 - Estado Mayor Conjunto.pdf

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AW119Kx

Base erea IV Brigada

Mendoza - 2-3-de Diciembre de 2014

AW119Kx Offers:

More Room Than Any Other Light Single Turbine Helicopter

High Level of Performance

Great Safety, fail safe design and redundancy of main systems

Modern Avionics

High Flexibility

Competive Acquisition & Maintenance Costs

Value Propositions

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2000 2005 2010

Derived from the AW109Power and incorporating features typical of a light twin

helicopter the A119Koala has benefitted from continuous improvement in capabilities,

performance and technologies to meet the evolving Customer requirements

AW119 Koala Development

AW119Koala

AW119Ke

AW119Kx

Product Evolution AW119 AW119Kx

Sales (as of Noviembre 2014)

more than 240 aircraft (order & options) in 33 countries by 104 customers

Fleet leader:

Tri-State Care Flight

SN 14032 5700 FH

Fleet & Sales Data

15%

7%

10%

21%13%

34%

EMS/SAR

Military

Govern. & Law Enf.

Utility

Offshore

Corp/Vip

24%

13%

13%19%

31%

Europe

Asia & Australasia

Africa

C. & S. America

North America

By areas

By applications

Leading Safety Features

Fully Articulated Titanium Rotor &

Composite Main Rotor Blades

High Visibility Reinforced

Windshield

Large Unobstructed Cabin for

Higher Flexibility

Dual Hydraulic System

Redundant Electrical System

Redundant Fuel System

1002 SHP P&W Single Turbine Engine

30 Minute Run-dry Transmission

Main Features

WEIGHT SUMMARY

Maximum Take Off Weight (internal load) 2850 kg Maximum Take Off Weight (external load) 3150 kg Basic Empty Weight 1455 kg

VOLUMES PILOT & PAX CABIN 4.96 m3

BAGGAGE COMPARTMENT 0.95 m3

1 Pilot +7 pax SEATING

MINIMUM CREW: ONE PILOT PASSENGERS: SEVEN

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Safety by design

Cocoon type crash protective airframe High inertia rotor blades for safe autorotation

Transmission

dry run

capability:

30 min

Windshield bird strike protection

Redundancy of

main systems

Redundancy Of All Main Systems:

Hydraulic System

Fuel System

Electrical System

Automatic Stabilization System:

2 Modes Of Operations

SAS

Att Hold

High Level Of Safety In Case Of Failure

HYDRAULIC SYSTEM ELECTRICAL SYSTEM

FUEL SYSTEM AUTOMATIC STABILIZATION

SYSTEM

Safety Redundancy of Main Systems

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Main and Tail Rotor

MAIN ROTOR

Fully articulated titanium rotor hub with composite

blades and elastomeric bearings

For smooth and stable control response in all flight

conditions including autorotation

Reduced maintenance

TAIL ROTOR

Steel rotor hub with composite blades

High lateral lateral controllability

Take Off Power 1002 shp

Max Continuous Power 872 shp

ENGINE with EEC (Electronic Engine Control)

Take Off Power (5min) 917 shp

Max Continuous Power 900 shp

Run Dry Capability 30 min

TRANSMISSION

AGUSTAWESTLAND

PRATT & WHITNEY PT6B-37A

Engine & Transmission Ratings

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Performance

(ISA, SL, MTOW)

VNE 281 km/h 152 kts

Max Cruise Speed 257 km/h 139 kts

HIGE 3352 m 11000 ft

HOGE 2225 m 7300 ft

Service Ceiling 4572 m 15000 ft

Max Range (*) 954 km 515 nm

Max Endurance (*) 5 h 20 min

(*) with 688 kg of usable fuel (no reserve) @ 5000 ft

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Stability and yaw control

Lateral wind up to 40 kts

High controllability assuring safe operational conditions

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Modular Fuel system

3-CELL: 484 kg - 605 l

4-CELL: 568 kg - 711 l

5-CELL: 696 kg - 870 l

No reduction of useful volumes in cabin and in baggage compartment

Modular design

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Configuration:

SAR/Surveillance

1 Litter

2 Litters

Training

Passenger

Transport

Litter

Copilot

Pilot

Hoist

Operator

Seat

Hoist

Instructor

Seat

Fuel

Tanks

Medical

Attendants

Seats

Six Pax

Seats

Operational Flexibility

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0,95

3,45

1,51

0

1

2

3

4

5

6

AW119Ke

m3 Cockpit

Cabin

Baggage compartment

Internal Volume

Baggage compartment

Maximum load: 150 kg

High comfort for passengers in the cabin

Baggage compartment separated from cabin & easily accessible

5,91

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1/2 pilots + 6/7 passengers

1/2 pilots + 1 stretcher + 4/5 passengers

1/2 pilots + 2 stretcher + 2/3 passengers

Convertible Interior

High flexibility

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Space and Comfort

Unique Single Engine with separate cabin

Corporate/VIP interior

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EMS Interior

1 or 2 longitudinal litters with no intrusion into the cockpit

2 attendants + 2 patients as the larger twin engine h/c

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New Glass Cockpit

Ergonomic cockpit with improved situational awareness and reduced pilot workload

MFD PFD

ICS control

panel (pilot)

ICS control

panel (co-pilot)

The AW119Ke is offered with one of the most modern and integrated glass cockpit today available in the market, similar to the ones installed on larger and heavier helicopters. The AW119Ke VFR avionic package consists of the Garmin G1000H integrated flight deck system, civil certified FAA. Engine information are integrated in the G1000H avionic suite. The AW119Ke avionic suite allows also IFR training.

FLIR image displayed on MFD

Electronic

Standby Instrument

System

Garmin G1000H Glass Cockpit

Caution,

Warning

switches

PFD displays:

Airspeed

Attitude

Altitude

Heading

Slip/skid indicators

360 HSI

COM 1/2 Communication

frequencies

VOR/LOC 1/2 NAV frequencies

Clock

XPDR current status

Primary Flight Display

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The system can create and store up to 1,000 user-defined waypoints

Flight planning on the system consists of building a flight plan by entering waypoints one

at a time, adding waypoints along airways, and

inserting departures, airways, arrivals, or

approaches

Up to 99 flight plans with up to 99 waypoints each can be created and stored in memory

Flight plans can be imported from a SD Card or exported to a SD Card from the Stored

Flight Plan Page

Waypoints can be added to the active flight plan or any stored flight plan

FMS - FLIGHT PLANNING

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SVS 3D Synthetic Vision System

Provides realistic, real-time 3D virtual reality

view of the helicopter attitude and flight

trajectory and the outside world

in any weather conditions

CLEAR SKY

CLOUDS / FOG

NIGHT

Synthetic Vision

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TAWS Terrain Awareness Warning System

Provides a map of terrain and sounds an audible

warning if the airplane approaches too close to terrain or

a structure

HTAWS & HITS

HITS Highway In The Sky

Displays the desired navigation route in 3D using a series

of skyway boxes

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Digital moving map

Provides real-time flight information on the map that illustrates the position

and direction of the aircraft

Digital Moving Map

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New Nose Equipment Layout

New

New

New

New

New

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Optional equipment

Electrical rescue hoist

204 kg (450 lbs)

50 m Cable

Cargo hook (1400 kg) Emergency floats

Dual cargo hook (1400 kg/500 kg)

Fire Fighting Equipment

Operational Strengths:

Greatest water volume capacity

High altitude performance

Wide temperature range

Belly tank: 1200 l Bambi Bucket: 910 l

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Rear view mirrors

Electrically adjustable and electrically heated mirror Fixed rear view mirror

The pilot monitors the sling load during flight

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Crew doors windows

High visibility doors Bubble window (on the RH cockpit door)

Better visibility on sling load during operations

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Configuration ADDITIONAL EQUIPMENT

Baggage compartment extensions (1.9 m)

Dual controls

Fuel cap with key-lock

Reinforced windshields (pilot and co-pilot)

Rotor Brake

Sliders on cockpit doors windows

Windshield wipers (pilot/copilot) with wiper switch on cyclic grip

INTERIOR

Bleed air heater

Primer finished cabin walls

UTILITY CONVERTIBLE INTERIOR

Soundproofing

Painted liners

Seats covered with leatherette

3 aft facing seats (central bench) with individually foldable black panels

3 fwd facing seats (aft bench) with individually foldable black panels

Provision for locking system for stretcher on back panel seats, aft and central bench

3-point shoulder harness with inertial reels and black coloured safety belts for all

passenger seats

Reading lights, advisory lights

Cabin loudspeakers

Rubber carpet

PAINTING

AgustaWestland painting scheme, metallic colours from Company selection

AVIONIC EQUIPMENT

Active Noise Reduction (ANR) headset (Qty 3)

ELT C406-N HM Artex

Radio altimeter FreeFlight RA-4500

UTILITY EQUIPMENT

188 USgal fuel system

Bubble Windows

External hoist (450 lb) provision

External hoist (450 lb) removable

Search Light Spectrolab SX-5 Starburst

Wire strike protection system

Estimated Equipped Empty Weight: 1737 kg 2% tolerance

Data contained in this presentation are preliminary and represent AgustaWestland best estimation.

Data is subject to change without notice and is not to be used for operational purposes nor constitute a contractual commitment.

BASIC AIRCRAFT

AVIONIC PACKAGE

Two GDU-1040 10.4 display units providing a Primary Flight Display (PFD) and a Multifunction Display (MFD) and integrating:

Radio tuning controls Flight Management System (FMS) Synthetic Vision System

Two GIA-63H Integrated Avionics Units (IAU) comprising: COM 1&2 NAV 1&2 GPS 1&2

GTX-33H Mode-S Transponder with Extended Squitter (ES) capability Digital Audio Control System (DACS) NAT with two cockpit panels Magnetic Compass indicator L3 Avionics System ESI-2000 Electronic Standby Indicator Engine Hour meter STANDARD EQUIPMENT

28 Ah battery (in lieu of 22 Ah battery)

Active Noise Reduction (ANR) headsets (pilot and co-pilot)

Baggage compartment lights

Crew open door actuators

First aid kit

Fuel drain electrical valves

Portable fire extinguisher

Quick disconnecting chip detectors

Shoulder harness with inertial reels (pilot and co-pilot)

Tail boom strake

ADDITIONAL AVIONIC EQUIPMENT

AC power supply system (2 inverters)

AFCS 3-axis duplex SP-711 Honeywell

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SAR Mission analysis

1 hr:55 min of searching time 100 nm far from base

Data contained in this presentation are preliminary and represent AgustaWestland best estimation.

Data is subject to change without notice and is not to be used for operational purposes nor constitute a contractual commitment.

0

50

100

150

200

250

0 50 100 150 200 250

Sear

ch t

ime

ove

r ar

ea

- m

in

Radius to search area - nm

Mission Weights

Max Gross Weight: 2850 kg

EEW: 1737 kg

Pilot: 85 kg

2 Operators: 85 kg (each)

Rescued person: 85 kg

Fuel Reserve: 40 kg

Flight Assumptions

Temperature: ISA+20C Cruise Altitude: 6000 ft

Loitering: 4000 ft

5 min HOGE for rescuing: 4000 ft

Fuel reserve: 20 min @ 70 kts

Max Range Cruise Speed: 120 kts

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Operational Flexibility

VIP CORPORATE

OFFSHORE

EMS

SAR

AERIAL WORK

LAW ENFORCEMENT

PAX TRANSPORT

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Customer Service and Support

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Regional Offices FSRs

Supply Centers

Service Stations

Headquarter

Back Offices

R&O Centers

24/7 FLEET

OPERATIONS

CENTRE

CUSTOMER SERVICE HEADQUARTER

CUSTOMER SUPPORT &

SERVICES

Innovative Web Services

AW CUSTOMER SUPPORT - LONATE

(ITALY)

AW PHILADELPHIA PHILADELPHIA (USA)

AW DO BRASIL SAO PAOLO (BRAZIL)

AAS LIEGE (BELGIUM)

AW MALAYSIA KUALA LUMPUR (MALAYSIA)

MIDDLE EAST ABU DHABI / DUBAI (UAE)

AW Customer Support & Services

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3 years warranty

2 inspection programs

High overhaul intervals

Customer Service: 24 hr/365 days

Support and Maintenance

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High Operational availability thanks to high limits

TBOs of the main components

Time Between Overhaul

(TBO)

Main transmission assembly 4800 FH

Tail rotor gearbox assembly 4800 FH

Main rotor servo actuator

assembly 1800 FH

Tail rotor servo actuator

assembly 1800 FH

Engine 3000 FH

Main Components TBO

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More Space Than Any Other Light Single Exceptional Flexibility Superior Performance High Productivity Great Reliability

THE A119 KOALA OFFERS:

Conclusion

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