AIRBUS A320-200 · A320-200 CEO Page 4 of 9 MAJOR AVIONICS EQUIPMENT Descripton Manufacturer Part Number QTY ATA 22 - Automati FFlght ControFs OPS Honeywell PS4087600-905 2 Flight

SPECIFICATION SUMMARY

AIRBUS A320-200

Rev.: No. 1 Date: 19-JAN-2018

Confidentiality and Disclaimer:

All rights reserved. This document is the sole property of t h e S e l l e r . This document has been drafted and distributed for information purposes only. This document may not be reproduced or (re) distributed or otherwise utilized in part or whole without the express prior written permission of t h e S e l l e r . While the information presented in this document is given in good faith based upon the most current information available to t h e S e l l e r , changes or modifications with respect to the subject aircraft and the associated records and documentation may be made at any time. No express or implied warranty or representation is made and this document may not be regarded as establishing any obligation on the part of t h e S e l l e r or any of its affiliates. It is expected that interested parties will conduct an independent physical inspection of the aircraft and associated records and documentation.

A320-200 CEO Page 2 of 9

WEIGHTS, OPERATIONAL European US

Maximum Taxi Weight (MTW) 73`900 (kg) 162`922 (Lbs)

Maximum Take Of Weight (MTOW) 73`500 (kg) 162`040 (Lbs)

Maximum Landing Weight (MLW) 64`500 (kg) 142`198 (Lbs)

Maximum Zero Fuel Weight (MZFW) 60`500 (kg) 133`380 (Lbs)

Operatonal Weight Empty (OWE) 42`246 (kg)* 93`137 (Lbs) *

Fuel Capacity (FC) 23`859 (Ltr) 6`303 (USG) * ESTIMATED

AIRFRAME STATUS Total Airframe Hours 0:00 *

Total Cycles 0 *

Status Date 19-JAN-2018 * ASSUME UP TO 10 FH & 05 FC FROM FACTORY

MAINTENANCE STATUS C - Check interval 7`500 FH & 5`000 FC & 24 MO

6Y - Check interval 72 MO

12Y - Check interval 144 MO

Last C – Check N/A

Last 6Y – Check N/A

Last 12Y – Check N/A

Next C – Check in 7`500 FH & 5`000 FC & 24 MO

Next 6Y – Check in 72 MO

Next 12Y – Check in 144 MO NOTE: The Operator`s approved Maintenance Programme is conforming to the Manufacturer`s MPD.

AIRCRAFT IDENTIFICATION

Aircraf Model Airbus A320-214

Manufacturer Serial Number TBA

Manufacture Date TBA

Aircraf Registraton TBA

Engines Model CFM56-5B

Sharklets Yes

Noise Abatement Compliance Stage IV iaw. ICAO Annex 16, Volume 1

Approach Category CAT IIIB Capable

ETOPS 120 min

Over Water Equipment None

A320-200 CEO Page 3 of 9

ENGINE / APU DETAILS Engine 1 Engine 2 APU

Manufacturer CFMI CFMI Honeywell

Model CFM56-5B4/3 CFM56-5B4/3 GTCP 131-9A

Thrust Rate 27`000 Lbs 27`000 Lbs

ENGINE / APU STATUS Engine 1 Engine 2 APU

Serial Number TBA TBA TBA

Total Time Since New 0:00 * 0:00 * 0:00

Total Cycles Since New 0 * 0 * 0

Last Shop Visit NONE NONE NONE

Hours Since Last Shop Visit N/A N/A N/A

Cycles Since Last Shop Visit N/A N/A N/A

Last Overhaul NONE NONE NONE

Hours Since Last Overhaul N/A N/A N/A

Cycles Since Last Overhaul N/A N/A N/A

First Limiter TBA TBA TBA

Status Date 19-JAN-2018 19-JAN-2018 19-JAN-2018

* ASSUME UP TO 10 FH & 05 FC FROM FACTORY

LDG DETAILS NLG LH MLG RH MLG Manufacturer TBA

Part Number TBA TBA TBA

Serial Number TBA TBA TBA

Positon NLG LH MLG RH MLG

Cycles Since New 0 * 0 * 0 *

Last Overhaul Date NONE NONE NONE

Cycles Since Overhaul N/A N/A N/A

Remaining Cycles 20`000 20`000 20`000

Overhaul Due Date TBA TBA MAY-2026

Overhaul Interval 20`000 CYC

or 10 Years

20`000 CYC

or 10 Years

20`000 CYC

or 10 Years

Brakes & Part Number Messier Messier

Wheels & Part Number Brigestone

30X8.8-R15

Brigestone

46X17-R2

Brigestone

46X17-R20

Status Date 19-JAN-2018 19-JAN-2018 19-JAN-2018

* ASSUME UP TO 05 FC FROM FACTORY

A320-200 CEO Page 4 of 9

MAJOR AVIONICS EQUIPMENT Descripton Manufacturer Part Number QTY

ATA 22 - Automati FFlght ControFs OPS Honeywell PS4087600-905 2 Flight Management Guidance Computer Honeywell 4084076-921 2 MCDU Honeywell D50A000-100 2 ATA 23 – Communliaton Audio Control Panel Team ACP2788AD01 2 Audio Management Unit Team AMU4031SA140204 1 Transceiver VHF/COMM Rockwell Collins 822-1250-020 3 Transceiver HF/COMM Rockwell Collins 822-0990-003 2 Radio Management Panel Thales Avionics C12848CB01 2 ATA 31 - Indliaton and Reiordlng System DMU S/W Teledyne D09SACF05C00000 1 FDIMU Teledyne 2234320-02-02 1 FDIU S/W Teledyne F320-002-0002 1 ATA 34 – Navlgaton MMR - Mult Mode Receiver ILS/GPS Rockwell Collins 822-11821-430 2 Weather Radar (WRX) Honeywell 930-10050002 1 TCAS II Computer Honeywell 940-0351-005 1 Radio Altmeter Transceiver (RA) Rockwell Collins 822-2365-022 2 VOR Receiver Rockwell Collins 822-0297-020 2 DME Interrogator Rockwell Collins 822-2325-020 2 ADF Receiver Rockwell Collins 822-0299-020 1

A320-200 CEO Page 5 of 9

INTERIOR CONFIGURATION Galleys 2 (G1; G5) Catering Standard ATLAS

Lavatories 3 Cargo Confguraton All Bulk + No CLS

Atendant Seats 4 Cockpit Confguraton Standard (2+1)

In Flight Entertainment None

Seats Quantty Manufacturer Model

Economy 180 GEVEN ESSENZA

A320-200 CEO Page 6 of 9

SCN LIST

Desirlpton SCN/Comments

ATA 02 - CERTIFICATION AND EXT LIVERY

CN02.10.120 / 01 15 knots tailwind certfcaton at take-of 02D1012001S1A

CN02.10.120 / 02 15 knots tailwind certfcaton at landing 02D1012002S1A

CN02.12.117 / 05 Compliance status for FAR 121 02D1211705S1A

CN02.12.122 / 03 Compliance status report - EASA regulaton on Air Operatons, PART-CAT.IDE and PART-SPA

02D1212203S1A

CN02.40.101 / B

EXTERNAL LIVERY Medium External livery - 1 or 2 colour(s) for background - 3 / 4 colours for decoraton - Paint system: Primer, top coat - Standard design

02D4020001S2A

Engine Danger Area decals - Feet and Metric distances 11D2010505S1A

Customizaton of exterior markings according to Markings Defniton Document 11D2020001S1A

Alternate paint system (CF primer, Base Coat/Clear Coat) on fuselage & vert. stabilizer - ANAC

51D2270502S1A

Alternate paint system (CF primer, Base Coat/Clear Coat) on nacelles - ANAC 51D2270504S1A

ATA 11 - PLACARDS AND MARKINGS

CN11.00.124 / 01 Installaton of leasing identfcaton plates on engines, LH door frame and Lav A partton 11D0012401S1A

Bilingual passenger placards and lighted signs 11D3011043S1A

CN11.30.131 / 05 Installaton of weight placard on each overwing hatch 11D3013105S1A

ATA 21 - AIR CONDITIONING

CN21.20.108 / 03 Cabin air recirculaton flter cartridge equipment selecton - LE BOZEC, PN 424B200-7 21D2010803S1A

CN21.50.100 / 01 Installaton of an insulaton cover for ozone converters 21D5010001S1A

CN21.70.109 / 07 Installaton of ozone catalytc converters - BASF CORPORATION, PN 20499006 21D7010907S1A

ATA 23 - COMMUNICATIONS

CN23.00.132 / 31 Automatc programmable ELT (406AF) associated with remote control panel in cockpit - ELTA (BFE)

23D0013231S1A

Installaton of CIDS integrated PRAM customized Gold Card (BFE) - KID-SYSTEME GMBH 23D3201301S1A

CN23.32.610 / 01 Entertainment System (Installaton of iPRAM from CIDS - KID-Systeme) 23D3600100G1A

CN23.50.138 / 06 Cockpit hand microphone alternate equipment - HOLMBERG, PN 85-16-12022-05 23D5013806S1A

CN23.51.136 / 27 Boomsets alternate equipment - TELEX COMMUNICATIONS, PN 64300-210 23D5113627S1A

CN23.71.103 / 21 SSCVR alternate equipment - HONEYWELL, PN 980-6032-023 (90 days ULB) 23D7110321S1A

CN23.71.110 / 01 Recorder Independent Power Supply (RIPS) - 28VDC power supply for CVR 23D7111001S1A

CN23.71.120 / 01 System provision for CVR capable of data link recording 23D7112001S1A

CN23.73.021 / 12 Customer provided (picture) screensaver 23D7300100G1A

ATA 25 - EQUIPMENT

CN25.01 / C

CABIN LAYOUT CONFIGURATION as per Drwg ref. 320-25.462 Rev A Issue 1 180 Y/C PAX layout with G1 and G5 galleys (Non-chilled), 3 standard type lavatories, 4 CAS (3 regular and 1 swivel in af cabin), 2 under-bin parttons in FWD cabin (one with window), regular cabin lights (white), No IFE applied.

25D2000200G2A

Compliance with CS25/FAR 25.562 (Head Injury Criteria - HIC) 02D1212303S1A

Installaton of exit-signs and exit-identfers as pictograms - AIRSIGNA (EASA regulaton) 11D3013702S1A

Installaton of passenger seats - GEVEN, model Essenza, E/C (BFE) 25D2167629S1A

Installaton of 16G cabin atendant seat as per customized cabin layout 25D2200211S1A

Headrest for PBE provision for 16G Cabin Atendant Seat as per customized cabin layout 25D2200224S1A

Installaton of new transiton panel at door 1 LH frame lining 25D2321001S1A

Installaton of new transiton panel at door 1 RH frame lining 25D2321002S1A

Interior colour scheme defniton 25D2350001S1A

Installaton of curtains 25D2610001S1A

Installaton of double-sided adhesive tape for carpet 25D2810302S1A

NTF selecton (SFE standard II) - Top layer GERFLOR Batiex AVM282 - OPUS 25D2821007S1A

Galley and galley catering defniton 25D3000100G1A

Installaton of selected literature pocket at lower positon below decor sheet material splitline

25D2710011S1A

CARGO HOLD CONFIGURATION 25D5000100G1A

CN33.50.118 / 01 Installaton of ioor-mounted EEPMS LUFTHANSA T. -1000 / Exit identfer - AIRSIGNA 33D5011801S1A

Installaton of Titanium Grey ioor-mounted EEPMS LUFTHANSA TECHNIK -1000 - whole cabin

33D5012216S1A

Installaton of an improved toilet assembly 38D3111102S1A

Lavatory alternate water faucet - manual type, mat fnish 38D1210901S1A

CN25.02 / A CABIN EMERGENCY EQUIPMENT 25D0000100G1A

A320-200 CEO Page 7 of 9

as per Drwg ref. 320-80.201 and last inputs from dated 18/05/2017

Installaton of demo life vest (BFE) - RFD BEAUFORT LTD, PN 44563001 25D6663014S1A

Installaton of provision for emergency equipment 25D6519672S1A

Cockpit portable halon free fre extnguisher alternate equipment (SFE) - P3, PN P3APP003010A

26D2411501S1A

Installaton of halon free fre extnguisher in cabin (SFE) - P3 Group - PN P3APP003010A 26D2460201S1A

Cockpit PBE alternate equipment (SFE) - AIR LIQUIDE, PN 15-40F-80 35D3110824S1A

ATA 26 - FIRE PROTECTION

CN26.20.103 / 01 APU fre extnguisher alternate equipment - KIDDE AEROSPACE 26D2010301S1A

CN26.21.104 / 01 Engine fre extnguishers alternate equipment - KIDDE AEROSPACE 26D2110401S1A

ATA 31 - INDICATING / RECORDING SYSTEMS

CN31.33.200 / 23 SSFDR alternate equipment (1024 w/s capable) - HONEYWELL (90 days ULB) 31D3320023S1A

ATA 32 - LANDING GEAR

CN32.41.111 / 25 MLG tres selecton - BRIDGESTONE (46X17-R20 radial tres) 32D4111125S1A

CN32.41.120 / 12 NLG tres selecton - BRIDGESTONE (30X8.8-R15 radial tres) 32D4112012S1A

CN32.48.200 / 11 Installaton of universal brake cooling fans on MESSIER wheels and brakes 32D4820011S1A

ATA 34 - NAVIGATION

CN34.41.302 / 10 Alternate full single WXR (ARINC 708A) with weather ahead & hazard functons - HONEYWELL RDR-4000 V2

34D4130210S1A

CN34.42.101 / 14 Digital radio altmeter alternate equipment - ROCKWELL COLLINS - LRA2100 34D4210114S1A

CN34.42.117 / 01 Radio alttude automatc call-outs 34D4211701S1A

CN34.43.204 / 12 TCAS change 7.1 - HONEYWELL TPA-100B (-005) / ATC XPDR - HONEYWELL (-1402) 34D4320412S1A

CN34.52.117 / 02 Compliance with ADS-B OUT regulaton for NRA 34D5211702S1A

ATA 35 - OXYGEN

CN35.11.201 / 04 Cockpit oxygen cylinder alternate equipment 115 cu f (composite) - AVOX SYSTEMS 35D1120104S1A

CN35.20.010 / 01 Installaton of four oxygen masks per box 35D2001001S1A

CN35.20.115 / 01 Alternate lavatory gaseous oxygen supply (15 mim) - FAA AD 2012-11-09

35D2011501S1A

ATA 46 - INFO SYSTEMS - GENERAL

CN46.21.102 / 17 AIRBUS standard AOC sofware from HONEYWELL with units in kgs (by default) 46D2110217S1A

CN46.26.400 / 01 Actvate 4G Cellular Gatelink for Airlines 46D2640001S2A

Install FOMAX 46D2640050S2A

ATA 49 - APU

CN49.001.05 / 02 APU alternate equipment - Honeywell, GTCP 131-9A 49D0010521S1A

ATA 52 - DOOR

CN52.73.100 / 01 Installaton of Inadvertent Slide Deployment Preventon Light (ISDPL) 52D7310001S1A

ATA 53 - FuseFage

CN53.30.050 / 01 Belly fairing panels - extrusion strips 53D3005001S1A

ATA 57 - WINGS

CN57.10.200 / 01 Installaton of Sharklets large wingtp devices 57D1020001S1A

ATA 72 - ENGINE

CN72.00.120 / 01 CFM engines - CFM56-5B4/3 (SAC - Tech Inserton - PIP) at 27 000 lbf nominal thrust (A320-214)

72D0012001S1A

A320-200 CEO Page 8 of 9

MSCN LIST MSCN NUMBER TITLE DESCRIPTION

ATA 21 - AIRCONDITING

21D6100003M1A Introduce improved Air Conditoning System Controller P/N 1803B0000-05

The change consists in the introducton of an improved ACSC (Air Conditoning System Controller) P/N 1803B0000-05.

ATA 22 - AUTO FLIGHT

22D6000016M1A Introduce FAC C sofware standard AA06

This modifcaton installs FAC C sofware standard AA06, replacing standard AA05.

22D8300120M1A Introduce FMGC H2C PC18 (CFM engines)

The change consists in installing FMGC Honeywell standard H2CPC18 on CFM powered a/c.

ATA 24 - ELECTRIC SYSTEM

24D3800102M1A Introduce batery charge limiter P/N 35-0L5-1107-08

In order to prevent obsolescence, the change consists in replacing the current BCL (Batery Charge Limiter) by a new one.

ATA 25 - Equlpment & Furnlshment

25D1011524M1A Remove ashtrays for no smoking cockpit

In order to have a no smoking cockpit, this modifcaton consists in removing the captain and frst ofcer ashtrays from the side-stck consoles.

25D6530202M1A Defne and Install Low Frequency Underwater Locator Beacon (LF-ULB)

This change introduces a Low Frequency Underwater Locator Beacon (LF-ULB).

ATA 27 - FLIGHT CONTROL

27D9310126M1A Introduce ELAC L101 The modifcaton consists in installing ELAC sofware L101.

ATA 32 -LANDING GEAR

32D1100112M1A LANDING GEAR - MAIN GEAR - INCREASE CLEARANCE FOR EV MLG TORQUE LINK DAMPER

The change consists in replacing a washer and a bolt to increase the clearance between the lower torque link and the EV torque link damper retaining bolt.

32D1100113M1A Introduce Stainless Steel connectors on MLG harness

In order to improve corrosion resistance, the change consists in replacing the aluminum alloy connectors by stainless steel connectors at several locatons on the main landing gear.

32D2110011M1A Introduce Stainless Steel connectors on NLG harness

In order to improve corrosion resistance, the change consists in replacing the aluminum alloy connectors by stainless steel connectors at several locatons on the nose landing gear. The Rotary Variable Diferental Transducer (RVDT) sensor is also modifed, with a receptacle made of stainless steel instead of aluminum.

ATA 36 - PNEUMATIC

36D1100014M1A Introduce BMC P/N 733901-1-3 The change consists in a BMC (Bleed Monitoring Computer) sofware update.

ATA 49 - APU

49D0000102M1A Introduce improved ECB P/N 3888579-201 for HWL APU GTCP131-9A

In order to prevent component obsolescence, and to improve robustness, the change consists in an ECB redesign.

A320-200 CEO Page 9 of 9

BFE LIST NO NAME QTY VENDOR P/N

1 FAK 2 Leki S6-01-0005-306

2 EMK 1 Innovint 6240-28

3 UPK 1 Innovint 6240-10E

4 Wheelchair(+Cover) 1 Innovint 2218-N-41(Cover 7260-98)

5 ELT, Potable 1 Leki 01N65920

6 ELT bracket 1 Leki 04N64250 + 04N64265(Cover)

7 ELT, Fixed 1 Leki 01N65900

8 Remote control panel 1 Leki 93N6035

9 Back up antenna 1 Leki 02N64070

10 Life Vest, Passenger 180 RFD BEAUFORT 00002291

11 Life Vest, Cockpit 3 RFD BEAUFORT 00002292

12 Life Vest, Cabin Crew 4 RFD BEAUFORT 00002292

13 Life Vest, Infant 5 RFD BEAUFORT 00002293

14 Life Vest, Spare 5 RFD BEAUFORT 00002291

15 Life Vest, Demo 3 RFD BEAUFORT 44563001

16 Extension Seat Belt 3 AMSAFE 1055-1-011-8029

17 Infant Seat Belt 3 AMSAFE 1055-2-011-8029

18 AED 1 Heartshine Heartsine 360P

19 ATLAS TR-FS 7 Zodiac TK721029

20 ATLAS TR-HS 8 Zodiac TK721034

21 TR-Waste FS 1 Zodiac TG720021

22 Bin-Waste FS 1 Zodiac WA500001

23 TR-Waste HS 1 Zodiac TH720021

24 ATLAS CONT 19 Zodiac DLH294

25 Con/Oven 2 Zodiac 8202-11-0000-01

26 Meal Carrier 2 Zodiac 8202-01-7000

27 Meal Tray 16 Zodiac 8202-01-8000

28 B/Maker 2 Zodiac 64753-001-003

29 W/Heater 2 Zodiac 62197-001-001

30 Rail/w.h & bm 2 Zodiac 64759-151

31 Jug 2 Zodiac 64753-049

32 Carpet 125 Botany 2BWW2696

33 Curtain(FOC) 1 Botany 195BWJ2940

34 Seat Assy 1 Geven D3-01-xxx-xx

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