airbus a320-200thales c16221wb01 1 enhanced ground proximity warning computer honeywell 965-1676-002...

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SPECIFICATION SUMMARY Airbus A320-200 Rev.: No. 3 Date: 26-SEP-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.

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Page 1: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

SPECIFICATION SUMMARY

Airbus A320-200

Rev.: No. 3 Date: 26-SEP-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.

Page 2: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 2 of 12

WEIGHTS, OPERATIONAL Metric US Customary

Maximum Taxi Weight (MTW) 77`400 (Kg) 170`637 (Lbs)

Maximum Take Off Weight (MTOW) 77`000 (Kg) 169`756 (Lbs)

Maximum Landing Weight (MLW) 66`000 (Kg) 145`505 (Lbs)

Maximum Zero Fuel Weight (MZFW) 62`500 (Kg) 137`789 (Lbs)

Minimum Weight (MW) 37`230 (kg) 82`079 (Lbs)

Operator`s Empty Weight (OEW) 42`571 (kg) 93`853 (Lbs)

Maximum Structural Payload * 20`200 (kg) 44`533 (Lbs)

Fuel Capacity (FC) 23`860 (Liters) 6`303 (USG) * ESTIMATED

AIRCRAFT IDENTIFICATION

Aircraft Model A320-214

Manufacturer Serial Number TBA

Manufacture Date MAY – 2007

Aircraft Registration TBA

Engines Model CFM56-5B4/P

APU Model GTCP-131-9[A]

DELIVERY SUMMARY

Certification: EASA

Airframe: Fresh from C, 6Y & 12Y-check

Engines: As IS, installed on the aircraft & within the limits of the manufacturer;

MPA Run and BSI to be performed

APU: Serviceable

Landing Gears: As IS, Serviceable & Airworthy

Components: Serviceable & Airworthy

Painting: Painted in White

Interior Conf.: Clean, Normal wear & tear

Airworthiness Directives:

In compliance on the delivery date

Documents & Records:

Up to date, in English

Page 3: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 3 of 12

AIRFRAME STATUS Total Airframe Hours 41`406

Total Cycles 17`822

Status Date 31-AUG-2018 NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS

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 28-OCT-2016 at 34`905 FH & 14`894 FC

Last 6Y – Check 24-JAN-2013 at 21`202FH & 8`713 FC

Last 12Y – Check N/A

Next C – Check 27-OCT-2018

Next 6Y – Check 23-JAN-2019

Next 12Y - Check 02-MAY-2019

ENGINE / APU DETAILS Engine 1 Engine 2 APU

Manufacturer CFMI CFMI Honeywell

Model CFM56-5B4/P CFM56-5B4/P GTCP-131-9[A]

Thrust Rate 27`000 Lbs 27`000 Lbfs

ENGINE / APU STATUS Engine 1 Engine 2 APU

Serial Number TBA TBA TBA

Total Time Since New 28`264 38`058 14`530

Total Cycles Since New 11`769 15`919 23`952

Last Shop Visit 20-APR-2018 26-JAN-2016 14-DEC-2016

Hours Since Last Shop Visit 1`490 7`218 2`131

Cycles Since Last Shop Visit 624 2`894 3`620

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 LLP Limiter 8`231 4`081 21`704

Status Date 23-SEP-2018 23-SEP-2018 23-SEP-2018 NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS

Page 4: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 4 of 12

ENGINE Pos.#1 - LLP

ENGINE TYPE: TSN: 28.264 EFH TSLSV: 0 EFH DATE:

CFM56-5B6/P CSN: 11.769 EFC CSLSV: 0 EFC 23.sept.2018

NO. PART NAME PART NUMBER TOTAL HOURS

TOTAL CYCLES

LIFE LIMIT CYCLES

REMAINING CYCLES

LPC ROTOR ASSY

1 ) SHAFT, FAN 338-010-601-0 28`264 11`769 30`000 18`231

2 ) DISK STG.1, FAN 338-001-504-0 28`264 11`769 30`000 18`231

3 ) SPOOL, BOOSTER 338-001-906-0 28`264 11`769 30`000 18`231

HPC ROTOR ASSY

4 ) FRONT SHAFT, HPC 1386M56P03 28`264 11`769 20`000 8`231

5 ) HPC ROTOR SPOOL STG 1 & 2 1558M31G04 28`264 11`769 20`000 8`231

6 ) HPC ROTOR DISK STG 3 1590M59P01 28`264 11`769 20`000 8`231

7 ) HPCR SPOOL ASSY STG 4-9 1588M89G03 28`264 11`769 20`000 8`231

8 ) CDP ROTATING REAR AIR SEAL 1523M35P01 28`264 11`769 20`000 8`231

HPT ROTOR ASSY

9 ) HPT ROTOR FRONT SHAFT 1873M73P01 28`264 11`769 20`000 8`231

10 ) HPT FRONT ROTATING AIR SEAL 1795M36P02 1`490 `624 20`000 19`376

11 ) DISK - HPT ROTOR 1498M43P06 28`264 11`769 20`000 8`231

12 ) HPT REAR SHAFT 1864M90P05 28`264 11`769 20`000 8`231

LPT ROTOR ASSY

13 ) LPT SHAFT 338-010-005-0 28`264 11`769 25`000 13`231

14 ) LPT ROTOR DISK STG 1 336-001-804-0 28`264 11`769 25`000 13`231

15 ) LPT ROTOR DISK STG 2 336-001-909-0 28`264 11`769 25`000 13`231

16 ) LPT ROTOR DISK STG 3 336-002-006-0 28`264 11`769 25`000 13`231

17 ) LPT ROTOR DISK STG 4 336-002-105-0 28`264 11`769 25`000 13`231

18 ) LPT ROTOR SUPPORT 338-077-502-0 28`264 11`769 25`000 13`231

NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS

Page 5: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 5 of 12

ENGINE Pos.#2 - LLP

ENGINE TYPE: TSN: 38.058 EFH TSLSV: 0 EFH DATE:

CFM56-5B4 CSN: 15.919 EFC CSLSV: 0 EFC 23.sept.2018

NO. PART NAME PART NUMBER TOTAL HOURS

TOTAL CYCLES

LIFE LIMIT CYCLES

REMAINING CYCLES

LPC ROTOR ASSY

1 ) SHAFT, FAN 338-010-601-0 38`058 15`919 30`000 14`081

2 ) DISK STG.1, FAN 338-001-504-0 38`058 15`919 30`000 14`081

3 ) SPOOL, BOOSTER 338-001-906-0 38`058 15`919 30`000 14`081

HPC ROTOR ASSY

4 ) FRONT SHAFT, HPC 1386M56P03 38`058 15`919 20`000 4`081

5 ) HPC ROTOR SPOOL STG 1 & 2 1558M31G04 38`058 15`919 20`000 4`081

6 ) HPC ROTOR DISK STG 3 1590M59P01 38`058 15`919 20`000 4`081

7 ) HPCR SPOOL ASSY STG 4-9 1588M89G03 38`058 15`919 20`000 4`081

8 ) CDP ROTATING REAR AIR SEAL 1523M35P01 38`058 15`919 20`000 4`081

HPT ROTOR ASSY

9 ) HPT ROTOR FRONT SHAFT 1873M73P01 38`058 15`919 20`000 4`081

10 ) HPT FRONT ROTATING AIR SEAL 1795M36P02 38`058 15`919 20`000 4`081

11 ) DISK - HPT ROTOR 1498M43P06 38`058 15`919 20`000 4`081

12 ) HPT REAR SHAFT 1864M90P05 38`058 15`919 20`000 4`081

LPT ROTOR ASSY

13 ) LPT SHAFT 338-010-005-0 38`058 15`919 25`000 9`081

14 ) LPT ROTOR DISK STG 1 336-001-804-0 38`058 15`919 25`000 9`081

15 ) LPT ROTOR DISK STG 2 336-001-909-0 38`058 15`919 25`000 9`081

16 ) LPT ROTOR DISK STG 3 336-002-006-0 38`058 15`919 25`000 9`081

17 ) LPT ROTOR DISK STG 4 336-002-105-0 38`058 15`919 25`000 9`081

18 ) LPT ROTOR SUPPORT 338-077-502-0 33`410 18`325 25`000 6`675

NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS

Page 6: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 6 of 12

LDG DETAILS NLG LH MLG RH MLG Part Number NA28008-10 201581001 201581002

Serial Number TBA TBA TBA

Position NLG LH MLG RH MLG

Hours Since New 43`390 43`390 43`390

Cycles Since New 20`362 20`362 20`362

Last Overhaul Date 08-APR-2017 08-APR-2017 08-APR-2017

Cycles Since Overhaul 2`259 2`259 2`259

Remaining Cycles 17`741 17`741 17`741

Overhaul Due Date 08-APR-2027 08-APR-2027 08-APR-2027

Overhaul Interval 20`000 CYC

or 10 Years

20`000 CYC

or 10 Years

20`000 CYC

or 10 Years

Brakes & Part Number Messier C202255XX

Status Date 12-AUG-2018 12-AUG-2018 12-AUG-2018 NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS

Page 7: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 7 of 12

MAJOR AVIONICS EQUIPMENT DESCRIPTION MANUFACTURER PART NUMBER QTY

ATA 22 - Automatic Flight Controls FMGC Thales Avionics C13043AA06 2 FAC Thales Avionics B397BAM0624 2 FCU Thales Avionics C12850AC03 1 MCDU Thales Avionics C19266DA01 2

ATA 23 – Communication HF Transceiver Honeywell 964-0452-012 1 VHF Transceiver Honeywell 064-50000-0505 3 Cockpit Voice Recorder Honeywell 980-6022-001 1 PRAM / iPRAM (Integrated PRAM) Panasonic RD-AX7675-51 1 Tape Reproducer or CD Player (Audio Entertainment)

Panasonic RD-AX7095-01 1

Tape Reproducer or DVD Player (Video Entertainment)

Panasonic RD-AV1216-01 1

Audio Management Unit TEAM AMU4031SA140204 1 ATA 31 - Indication and Recording System FDR –Flight Data Recorder Honeywell 980-4700-042 1 FDIU – Flight Data Interface Unit Thales Avionics C12860AA02 1 FDIMU – Flight Data Interface and Management Unit

sfim ED48A100 1

Multi-Use Printer Honeywell 8055515-4501 1

ATA 34 – Navigation ADIRU – Air Data Inertial Reference Unit Northrop Grumman 465020-03030316 3 ISIS – Integrated Standby Instrument System

Thales C16221WB01 1

Enhanced Ground Proximity Warning Computer

Honeywell 965-1676-002 1

Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell 940-0351-001 1 ATC Mode S Transponder Honeywell 066-01127-1402 2 DME Interrogator Honeywell 066-50013-0202 2 VOR Receiver Honeywell 066-50012-0212 2 MMR – Multi-Mode Receiver Thales TLS755-01-0101B 2 Radio Altimeter Transceiver Honeywell 066-50007-0232 2 ADF Receiver Rockwell Collins 822-0299-020 1

Page 8: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 8 of 12

MODIFICATION STATUS COMPLIANCE NOTEs AIRBUS STD. SPEC. D000 02000 / ISSUE Yes

EASA TCDS EASA.A.064

NOISE Abatement Compliance Yes Stage IV iaw. ICAO Annex 16, Volume I, Part II

Approach Category Yes CAT III B

ETOPS Yes 90 min

Over Water capability Yes

Sharklets/Winglets No

Auxiliary Fuel Capacity No

Fuel Tank Inerting System (AIRBUS) No EASA – P by 01-JAN-2012; R – Not required

FAA – P by 28-DEC-2010 / R 100% Fleet by 26-DEC-2017

Nitrogen Gas System (BOEING) N/A

Reinforced Cockpit Door Yes

Cockpit 4th occupant seat Yes

Cargo Fire Suppression Yes

Cargo Loading System No

Cockpit Door Surveillance System Yes

EGPWS Yes

RVSM Yes

TCAS 7.1 Yes EASA – P on 12-MAR-2014 / R on 01-DEC-2015

FAA – Not required

Enhanced Surveillance (EHS) Mode S, ATC Transponder Yes

Elementary Surveillance (ELS) Yes

ATC Mode S Transponder ADS-B Out DO 260B capability No EASA – P on 08-JUN-2016 & R on 07-JUN-2020

FAA – P & R on 01-JAN-2020

Predictive Windshear Yes

Head Up Display (HUD) No EASA / FAA – Not mandatory

CAAC – R - 10% Fleet by 2015 & R - 100% by 2025

Area Navigation (BRNAV & PRNAV) Yes BRNAV = +/- 5 NM RNAV5 & PRNAV = +/- 1 NM RNAV1

Aircraft Performance Based Navigation (PBN) Capability

A/C PBN APPROVAL = RNP APCH (to LNAV/VNAV) Yes

EASA – 3 Phase Approach – Various dates

FAA – Not required

GPS Installed Yes

FM Immunity Yes

VHF 8.33 kHz Chanel spacing Yes EASA – Mandatory above FL195

FAA – Not mandatory

FANS 1/A Installed & Activated No EASA & FAA on NAT between FL350-390

FANS B+ Installed & Activated No

ATN B1 Data Link (CPDLC) Installed Yes EASA – P & R on 05-FEB-2020 for AC > JAN-2003

and R on 01-JAN-2023 for AC < JAN-2003

FAA – Not required

SATCOM Installed No EASA – Not mandatory

FAA – Mandatory, if ETOPS > 180 Mins

CAAC – R - 50% Fleet by 2015 & R - 100% by 2017

CVR with Data Link Recording Yes EASA – P on 08-APR-2014 / R on 01-JAN-2016 CAT.IDE.A195

FAA – P & R on 12-DEC-2010

SSCVR 2Hrs + ULB 90 Days Yes EASA – P & R by 01-JUN-2018

FAA – ULB < 30 Days by 01-DEC-2015 & < 90 Days by 01-

DEC-2015

SSFDR + ULB 90 Days Yes

Low Frequency Underwater Locator Device (ULD) No EASA – P & R by 01-JAN-2019 CAT.IDE.A190

FAA / CAAC – Not required

ELT 121.5 / 406 MHz - Fixed Yes

ELT 121.5 / 243 / 406 MHz - Portable Yes

NOTE: P – PRODUCTION & R - RETROFIT

Page 9: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 9 of 12

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

Lavatories 3 (A; D; E) Ovens/Water Boilers/Coffey Makers 3+5+0

Attendant Seats 6 (2+4) Cargo Configuration Bulk

In Flight Entertainment Yes Cockpit Configuration Standard (2+2)

Seats Quantity Manufacturer Part Number

Economy Class 174 B/E Aerospace 1013165-XXX

Page 10: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 10 of 12

CARGO CONFIGURATION Cargo Configuration Bulk Designee (Fire Detection/Protection) class TBA

Cargo Volume 37.42 3Metres Containers No

Load Limitation 9`435 Kg Main Cargo Door(s) 71” x 48”

Page 11: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 11 of 12

EMERGENCY EQUIPMENT

Page 12: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

A320-200 MSN. TBA Page 12 of 12

PERFORMANCE

Page 13: Airbus A320-200Thales C16221WB01 1 Enhanced Ground Proximity Warning Computer Honeywell 965-1676-002 1 Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell

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