AIRBUS A318 A319 A320 A321. TCDS A.064 issue 02,22 June 2006 and FAA TYPE-CERTIFICATE DATA SHEET. AIRBUS A318 A319 A320 A321 A28NM Revision 4
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1 A Aircraft Specification Summary A YOM: Nov-02 A Airbus S.A.S. Model: Manufacturer: Total Flight Hours 25,210 Total Flight Cycles 9,063 As per:31-dec-09 SPECIFIC DATA EASA TYPE-CERTIFICATE DATA SHEET AIRBUS A318 A319 A320 A321 TCDS A.064 issue 02,22 June 2006 and FAA TYPE-CERTIFICATE DATA SHEET AIRBUS A318 A319 A320 A321 A28NM Revision 4 - Certification base (FAA/EASA) - Entry into Service date: Standard Specification D Issue 5 - Detailed Spec / Build Standard reference EASA TYPE-CERTIFICATE DATA SHEET AIRBUS A318 A319 A320 A321 TCDS A.064 issue 02,22 June 2006 and FAA TYPE-CERTIFICATE DATA SHEET AIRBUS A318 A319 A320 A321 A28NM Revision 4
2 - Type Certificate Data Sheet - Provisions for ELT ELTA AFIRS 220 installation ELT ELTA, ATC Mode S transponder, ADF - Aircraft Major Upgrades- Highlights Aircraft is currently equipped with 150 economy class seats without Live TV screens in the seat back - Configuration - Possible cost issues next Lessee Compliant with ICAO Annex 16, Volume I, Chapter 3 requirements - Noise Compliant - Approach Category CAT III A - Extended Overwater Capability No - Cockpit indications (Metric/English), for FMS, English Units Cockpit Temp, Airco.Temp and Fuel amount: - High Altitude Certification RVSM - Has the aircraft been modified for Weight No increase since manufacturer delivery? - MTW - Maximum Taxi Weight kg lbs - MTOW - Maximum Take Off Weight kg lbs - MLW - Maximum Landing Weight kg lbs - MZFW - Maximum Zero Fuel Weight kg lbs - OEW - Operating Empty Weight LBS Standard Blue Wings colour scheme - Fuselage - Paint scheme - Display Type ECAM - Satcom No Print date: 01-Feb-10 This document has been prepared on the basis of information as made available. It provides basic information and is neither Page 6 of 10 its technical condition or aircraft Any liability is excluded, under contract or HF installed - EASA approval EASA A.C Avionics/Communications - Highlights Live TV system installed, external antenna, IFI and MRM are removed.system is not used to receive stream TV channels. - IFE - Highlights
3 - ETOPS capabilities No - Language on placards English/Spanish Aircraft is currently equipped with 150 economy class seats without Live TV screens in the seat back - Cabin Class Configuration 32", 2x58", 3x29", 40", 38",31",14x32" - Seat Pitch - Approval basis current LOPA and approved AMES EO#A by: EASA approved, AMES EO M MHU when reconfigured for redelivery - Stowage units Overhead bins - Doghouses No Seiling and walls are in white colors, Seats are light grey when new, with usage colour changes to dark grey/greenish - Interior Color Scheme Yes, manufactured and certified by AMES - Class dividers / Partition walls Yes, located one by the #1 door area and second by the class divider - Curtain location - color/spec dark grey fabric, average condition - Carpet color and condition - Standard or Oversized OHSC Doors? Oversized as per Raisback STC Partisions in the front have three screen each partishion with the screen size smaller than 6.8", and each seat, except last row has 6,8" VDU - Other customise equipment - Cockpit seat Manufacturer - Locations PART# TAAI3-03PE Cockpit Observer Seats 2 ea - Flight attendant seat Manufacturer - Sicma 2 forward 4 aft Locations - Number of Flight Attendant Seats 6 each Weber 5150 P/N BB - Cabin seat Manufacturers - Models (P/N) Good condition. No O/H performed - Seat overhaul status and date of last overhaul
4 - Seat electronic box Manufacturer - P/N Live TV Driessen G1 P/N and G5 P/N Galley Manufacturer - Galley Locations G1 and G5 - Galley Standard Atlas standard 11 ea Trolleys, 3 ea waste Boxes, 7 ea Ovens - Galley Inserts - Galley Power Galley area on the doors AC - Lavatory Locations Forward and aft A, D and E - Emergency Floor Lighting Seat mounted - Evacuation slides or slide rafts Yes - Life vests / cushions; due dates Yes, under the seat - Forward Yes - Aft Yes - Bulk Yes - Cargo Loading System No - Cargo Compartment Ventilation System Yes - Cargo Compartment Heating System No - Category / Class Yes Print date: 01-Feb-10 This document has been prepared on the basis of information as made available. It provides basic information and is neither Page 7 of 10 its technical condition or aircraft Any liability is excluded, under contract or - Smoke detection installed? Yes - Fire protection installed? Yes liters kg 6304 Gallons lbs - Usable Fuel capacity:standard- Wing and Center Taks - Fuel tank locations - Additional refuel/defuel coupling and No - Brakes Manufacturer & Part Number Messier Buggati - Brake material (Steel/Carbon) Carbon - Brake Cooling Fans Yes - MLG Wheel Manufacturer & Part Number Messier Dowty D NLG Wheel Manufacturer & Part Number Messier Dowty Aft Tow Fitting Yes - Tyre Pressure Indicating System Installed? No - In-situ replenishment facility for cockpit No oxygen cylinder - Cockpit oxygen cylinder capacity & material - Passenger oxygen system extended supply No
5 duration - Number of oxygen mask per box 3 - Gasper Air Installation no - APU Model Honeywell GTCP131-9A - Airstairs No - Door Configuration; Entrance-, Exit-, Standard A320 Emergency and Service Doors. - Engine Model V2527-A5 - General information (operational, AFM, etc) lbs - Systems; Vibration, Chip detection, etc. Yes - Type Certificates - EGPWS Yes - Enhanced Surveillance No - ELT / 406 mhz Portable - Reinforced cockpit door Yes - Cockpit entrance surveillance YES, Part of Live TV system Capable of 8.33 Yes before Delivery - RVSM, FM Immunity and 8.33 khz channel spacing - RNP/NAV; FMC, GPS, AMMR Yes - FAR associated with EIS2 EIS 1 AOC D till with additional FAX from LBA - AOC - last issue date (list capability such as CAT, RVSM, etc) RVSM-YES-till CAT IIIA - JAR OPS - last issue date (list capability such as CAT, RVSM, etc) - Certificate of Registration C of R: Last issue Issued on date: - Noise Certificate: Last issue date: Issued on #19814 Issued on till Radio License: Last issue date: till date of issue Certificate of Insurance: Last issued - Expires date: - Are the last seat burn certificates available: Yes Issued by previous Owner/Operator on , -- Are all engine shop reports available? No shop visits at this date - Are all logbooks available? Yes - Is a file available per Engine for applicable Yes and non-applicable engine AD's? - Major irregularities like incidents: None
6 Print date: 01-Feb-10 This document has been prepared on the basis of information as made available. It provides basic information and is neither Page 8 of 10 its technical condition or aircraft Any liability is excluded, under contract or SN: Model: TSN: CSN: as per: Location: SV date: TSSV: CSSV: ENGINES /APU * Lowest Limiter: * in the curent operated thrust: V11844 V2527-A5 15,843 5, Dec-09 D-ANNJ #1 14,261 V11845 V2527-A5 15,843 5, Dec-09 D-ANNJ #2 14,261 P2758 GTCP131-9A 5,965 7, Dec-09 D-ANNJ 08-Nov-06 2,668 3, May-05 4,422 6,164 Days : FH: FC: Date / Days: FH: FC: AIRFRAME 4C/6Y 27-Jun ,898 2,256 2,190 24,000 18,000 1,272 18,102 15,744 Last performed 19,312 6,807 Since Check: Remaining: Projected (calc. first due) 25-Jun-13 29,392 10,987 8C/12Y 26-Nov-02 2,592 25,210 9,063 4,380 48,000 36,000 1,788 22,790 26,937 Last performed 0 0 Since Check: Remaining: Projected (calc. first due) 23-Nov-14 31,089 11,767 Part Name: Serial No. Location Yrs Days FH FC LANDING GEARS MLG - LH Leg and MDG LH Since New: 7.2 2,612 25,210 9,063 Dressings 1,058 10,937 Program: Overhaul 3,650 20,000 Remaining: Last event: 26-Nov MLG - RH Leg and MDG RH Since New: 7.2 2,612 25,210 9,063 Dressings 1,058 10,937 Program: Overhaul 3,650 20,000
7 Remaining: Last event: 26-Nov NLG - Nose Landing Gear B NLG Since New: 7.2 2,612 25,210 9,063 1,058 10,937 Program: Overhaul 3,650 20,000 Remaining: Last event: 26-Nov AVIONICS / COMMUNICATIONS 01N65900 ELT FIX 1 VHF Comm Transceiver Data Radio (VDR) VHF Comm Transceiver Data Radio (VDR) VHF Comm Transceiver Data Radio (VDR) ATC Transponder ATC Transponder TCAS II Computer Radio Altimeter Transceiver Radio Altimeter Transceiver Weather RadarTransceiver VOR Receiver VOR Receiver DME Interrogator DME Interrogator M563 Portable ELT 1 FCDC - FLIGHT CONTROL DATA CON FCDC - FLIGHT CONTROL DATA CON RACK, LTV PHASE MRM MRM MRM IF INTERFACE - IFI RF DISTRIBUTION AMPLIFIER-RDA SEB-Seat Electronic box ANTENNA - EXTERNAL LIVE TV CONTROLLER - ANTENNA CONTROLLER - ANTENNA ANTENNA, GPS LIVE TV 0 - Are all shop reports available? Yes for this Type APU there are no Ads, only Optional SBs - Is a file available per APU for applicable and non-applicable APU AD's? See Q-Item List/file, at BWG see Dent and backle Chart - Summary of Damages and Repairs - Listing of Damages and Repairs Yes Print date: 01-Feb-10 This document has been prepared on the basis of information as made available. It provides basic information and is neither Page 9 of 10 its technical condition or aircraft Any liability is excluded, under contract or
8 Flight 350E Warning Computer 1 350E Flight Warning Computer 1 SDAC - System Data Acquisition Concentrator 350E SDAC - System Data Acquisition Concentrator 350E Display Unit-DU Display Unit-DU Display Unit-DU Display Unit-DU Display Unit-DU Display Unit-DU ELAC ELAC Multipurpose Control Display Unit Multipurpose Control Display Unit VDU- in seat display unit 6.8" V3 RADOME Multi Purpose Printer Multi Mode Receiver (MMR) Multi Mode Receiver (MMR) VIDEO SERVER UNIT- VSU 1 93N6035 Remote control panel DMC - Display Management Computer DMC - Display Management Computer DMC - Display Management Computer HF Comm Transceiver (Voice Only) 1 Ground Proximity Warning Computer, Enhanced Flight Data Recorder (SSFDR) Cockpit Voice Recorder(SSCVR) 1 AC68A200 MDDU 1 B372BAM0509 SEC - Spoiler and Elevator Computer 1 B372BAM0509 SEC - Spoiler and Elevator Computer 1 B372BAM0509 SEC - Spoiler and Elevator Computer 1 B397BAM0513 Flight Augmentation Computer 1 B397BAM0513 Flight Augmentation Computer 1 CFDIU-Centralized Fault Display Interface Unit B401ACM507 1 BC2065C SELCAL Decoder (AMU) 1 C12850AC02 FLIGHT CONTROL UNIT 1 Flight Management Guidance Computer C13042BA01 1 Flight Management Guidance Computer C13042BA01 1 Flight Data Interface & Management Unit ED48A100 1 HG2030AD11 Air Data Inertial Reference Unit 1 HG2030AD11 Air Data Inertial Reference Unit 1 HG2030AD11 Air Data Inertial Reference Unit 1 Z010H000521A CIDS Director 1 Z010H000521A CIDS Director 1 Print date: 01-Feb-10 This document has been prepared on the basis of information as made available. It provides basic information and is neither Page 10 of 10
9 its technical condition or aircraft Any liability is excluded, under contract or
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