AIRBUS A330-200 2009 Airbus A330-200
2009 Airbus A330-200AIRBUS A330-200
AIRCRAFT IDENTIFICATIONAircraft ModelManufacturer Serial NumberManufacture DateAircraft RegistrationEngines ModelSharklets/WingletsNoise Abatement ComplianceApproach CategoryETOPSOver WaterAIRBUS A330-223Q1 – 2009TBAPW4168AYESStage IV iaw. ICAO Annex 16, Volume 1CAT III Capable180 minYESWEIGHTS, OPERATIONALMetricMaximum Taxi Weight (MTW)Maximum Take Off Weight (MTOW)Maximum Landing Weight (MLW)Maximum Zero Fuel Weight (MZFW)Operator s Empty Weight (OEW)Maximum PayloadMaximum Fuel CapacityAuxiliary Fuel Capacity233 900 (kg)233 000 (kg)182 000 (kg)170 000 (kg)121 397 (kg)48 632 (kg)139 090 (Litres)NoneUS Customary515 661 (lbs.)513 677 (lbs.)401 241 (lbs.)374 786 (lbs.)267 635 (lbs.)107 215 (lbs.)36 746 (USG)NoneAIRFRAME STATUSTotal Airframe Hours 32 048Total Cycles 6 525Status Date 23-AUG-2017NOTE: WV 022MAINTENANCE STATUSC - Check interval 24 MO6Y - Check interval 72 MO12Y - Check interval 144 MOLast C - Check 5C on 26 – APR – 2017 at 32 043 FH & 6 524 FCLast 6Y – Check 10 – NOV – 2014 at 26 331 FH & 4 937 FCLast 12Y – Check NONENext C – Check APR – 2019Next 6Y – Check NOV – 2020Next 12Y - Check JAN – 2021A330-200MSN. TBAPage 2 of 10
ENGINE / APU DETAILSManufacturerModelThrust RateENGINE / APU STATUSSerial NumberTotal Time Since NewTotal Cycles Since NewLast Shop VisitHours Since Last Shop VisitCycles Since Last Shop VisitLast OverhaulHours Since Last OverhaulCycles Since Last OverhaulFirst LLP LimiterStatus DateLDG DETAILSManufacturerPart NumberSerial NumberPositionCycles Since NewLast Overhaul DateCycles Since OverhaulRemaining CyclesOverhaul Due DateOverhaul IntervalEngine 1Engine 2Pratt & WhitneyPW4168A68 600 LbfPratt & WhitneyPW4168A68 600 LbfGTCP 331-350CEngine 1Engine 2APUTBA27 3365 424MAR-2015(EPR)4 7451 253NONEN/AN/A7 17623-AUG-2017TBA27 0165 413SEP-2016(EPR)72NONEN/AN/A7 18723-AUG-2017TBA5 7466 739NLGD23581100-16TBANLG6 525NONEN/A10 475JAN-201917 000 CYCor 10 YearsBrakes & Part NumberWheels & Part Number BF Goodrich P/N: 3-159623-AUG-2017Status DateA330-200MSN. TBALH 7RH MLGMessier Dowty10-210101-00310-210201-003TBATBALH MLGRH MLG6 5256 525NONENONEN/AN/A10 47510 475JAN-2019JAN-201917 000 CYC17 000 CYCor 10 Yearsor 10 YearsBF Goodrich P/N: 2-1577-XBF Goodrich P/N: 3-154623-AUG-201723-AUG-2017Page 3 of 10
ENGINE Pos.#1 - LLPSTAGELP COMRESSOR / FAN MODULELPC - DRUM ROTOR (1.3,1.6,2,3,4 STAGES)LPC - FRONT HUBLPC -/LPT TURB SHAFT COUPLINGHP COMRESSOR MODULEHPC - 5TH STAGE DISKHPC - DRIVE SHAFTHPC - DRUM ROTOR (13-15 STAGES)HPC - DRUM ROTOR (6-12 STAGES)HPC - FRONT HUBHPC - INLET/DIFFUSER AIRSEAL (REF 1435)HP TURBINE MODULEHPT - FRONT T1 HUBHPT - REAR INTERMEDIATE T2 HUBHPT - T1 AIRSEAL OUTER ROTATING (REF 1752)HPT - T1 RING AIRSEAL (REF 1756)HPT - T2 AIRSEAL (ROTATING)HPT - T2 BLADE RETAINING PLATELP TURBINE MODULELPT - 3RD STAGE AIRSEAL (REF 1224)LPT - 3RD STAGE DISKLPT - 4TH STAGE AIRSEALLPT - 4TH STAGE DISKLPT - 5TH STAGE AIRSEALLPT - 5TH STAGE REAR HUBLPT - 6TH STAGE DISKLPT - 3RD STAGE AIRSEALLPT - 7TH STAGE DISKLPT - SHAFT - FRONT COMPR DRIVEA330-200PART NO.SERIAL LDLDC152715 00015 00015 0009 5769 5769 G689915 00015 00015 00015 00015 00015 0009 5769 57610 2599 5769 5769 5 00015 00012 60015 00013 90015 0009 5769 5767 1769 5768 4769 DB5387CLDLDF949315 00015 00015 00015 00015 00015 00015 00015 00015 00015 0009 5769 5769 5769 5769 5769 5769 5769 5769 5769 576MSN. TBAREMAINPage 4 of 10
ENGINE Pos.#2 - LLPSTAGELP COMRESSOR / FAN MODULELPC - DRUM ROTOR (1.3,1.6,2,3,4 STAGES)LPC - FRONT HUBLPC -/LPT TURB SHAFT COUPLINGHP COMRESSOR MODULEHPC - 5TH STAGE DISKHPC - DRIVE SHAFTHPC - DRUM ROTOR (13-15 STAGES)HPC - DRUM ROTOR (6-12 STAGES)HPC - FRONT HUBHPC - INLET/DIFFUSER AIRSEAL (REF 1435)HP TURBINE MODULEHPT - FRONT T1 HUBHPT - REAR INTERMEDIATE T2 HUBHPT - T1 AIRSEAL OUTER ROTATING (REF 1752)HPT - T1 RING AIRSEAL (REF 1756)HPT - T2 AIRSEAL (ROTATING)HPT - T2 BLADE RETAINING PLATELP TURBINE MODULELPT - 3RD STAGE AIRSEAL (REF 1224)LPT - 3RD STAGE DISKLPT - 4TH STAGE AIRSEALLPT - 4TH STAGE DISKLPT - 5TH STAGE AIRSEALLPT - 5TH STAGE REAR HUBLPT - 6TH STAGE DISKLPT - 7TH STAGE DISKLPT - SHAFT - FRONT COMPR DRIVELPT - THRUST BALANCE AIRSEALA330-200PART NO.SERIAL LDLDC153715 00015 00015 0009 5879 5879 G690115 00015 00015 00015 00015 00015 0009 5879 5879 5879 5879 5879 5 00015 00012 60015 00013 90015 0009 5879 5877 1879 5878 4879 DF9499CLDLDE602915 00015 00015 00015 00015 00015 00015 00015 00015 00015 0009 5879 5879 5879 5879 5879 5879 5879 5879 5879 587MSN. TBAREMAINPage 5 of 10
MAJOR AVIONICS EQUIPMENTDESCRIPTIONATA 22 – Automatic Flight ControlsFlight Management Guidance ComputerMCDU (Multifunction Control Display Unit)MANUFACTURERPART NUMBERQTYThales AvionicsThales AvionicsC13039CA01C19266BA013Thales AvionicsRockwell CollinsRockwell 100-1020-023321Thales AvionicsS1821502-021AIRBUS SASL3-COMM.LA2E20202T400002100-4043-0221Litton Aero ProductsL3-COMM.Thales AvionicsACSSRockwell CollinsThales OptroniqueRockwell CollinsRockwell 7-020822-0329-020066-50014-02023211222212ATA 23 – CommunicationsRADIO Management PanelVHF COMM. Transceivers (Incl. 8.33 & FM imm.)HF COMM. TransceiversSSCVR (Cockpit Voice Recorder) (120 min)ATA 25 – FurnishingsELT – Emergency Locator Transmitter Fixed(121.5 / 243 / 406 MHz)ATA 31 - Indication and Recording SystemFWC (Flight Warning Computer)SSFDR (Solid State Flight Data Recorder) (25 Hr&256 Words/sec)ATA 34 – NavigationADIRU (Air Data Inertial Reference Unit)ATC Transponder (Mode S – ELS & EHS Compliant)ATC / TCAS Control UnitT2CAS Computer (TAWS)WR (Weather Radar) TransceiverRA (Radio Altimeter) TransceiverVOR (VHF Omnidirectional Range) (Incl. FM imm.)DME (Distance Measurement Equipment) InterrogatorADF ReceiverCAA REQUIREMENTSEASA TCDSEGPWSArea NavigationElementary Surveillance (ELS)Enhanced Surveillance (EHS)Predictive WindshearGPS InstalledSATCOM InstalledELT 121.5 / 406 MHzRVSM / FM Immunity & 8.33 KHz Chanel spacingTCASCockpit Door Surveillance esYesYesYesYesYesMSN. TBANOTEsBRNAV & PRNAVChange 7.1Page 6 of 10
INTERIOR CONFIGURATIONGalleys 5 (G1; G2; G5; G6; G7)7 (1 4 2)Lavatories11Attendant SeatsIn Flight Entertainment Yes (Panasonic eX2 ISV)SeatsBusiness ClassEconomy ClassA330-200Catering StandardCargo ConfigurationCockpit ConfigurationCREW RestATLASSemi-Auto CLS BulkStandard (2 2)2 Bunks (FWD)QuantityManufacturerPart Number24259SICMAWEBER AIRCRAFT14052XX-XXX862082-XXXMSN. TBAPage 7 of 10
CARGO CONFIGURATIONCargo ConfigurationCargo VolumeLoad LimitationA330-200CLS Bulk132.4 3Metres37 578 KgDesignee (Fire Detection/Protection) classULDsMain Cargo Door(s)MSN. TBAC26 x LD-3106” x 66”Page 8 of 10
PERFORMANCEA330-200MSN. TBAPage 9 of 10
DELIVERY CONDITIONSThe Aircraft will be delivered at an EASA or FAA approved maintenance facility in a location to be advised.Airframe:In January 2017, the Aircraft shall be fresh out of a C-Check. At delivery, there shallbe no scheduled tasks accomplishment required before January 2019, 6,000 flighthours and 1,500 cycles, whichever is the most limiting factor.Engines:Each Engine shall have no more than 5,000 flight hours and 1,500 cycles since lastperformance restoration shop visit and sufficient EGT margin, with no defectpresent, to allow at least 6,000 flight hours and 1,500 cycles until next expectedremoval.Each engine LLP shall have no less than 1,500 cycles life remaining until removal.APU:The APU shall have no more than 2,000 APU hours since last APU performancerestoration.Landing Gear:Landing gear shall not be due restoration before January 2019, or within 4,000cycles, according to the manufacturer MPD.Components:Each component installed on the Aircraft shall be serviceable and be supported byan EASA Form 1 or FAA Form 8130.Each component installed on the Aircraft that has a flight hour, cycle or calendarlimit, shall not be due removal before April 2018, 6,000 flight hours, 1,500 cycles,whichever is the most limiting factor.Paint:Aircraft shall be painted white.Interior Configuration:Aircraft shall be in 24 B/C 259 Y/C configuration.Airworthiness Directives:All airworthiness directives issued by EASA and / or the FAA which requirecompliance before January 2018, 1,450 flight hours or 275 cycles, whichever ismost limiting, from delivery of the Aircraft shall have been complied with.Aircraft Documents:Aircraft shall have complete, up to date technical records, documentation andmanuals and shall include full back to birth traceability for life limited parts.Certification:Aircraft shall meet all the requirements for, and be eligible for an immediatecertificate of airworthiness issued by, and registration with, an EASA member stateand immediate operation in an EASA member state in full compliance with EASAOPS regulation.Aircraft shall have either a certificate of airworthiness or an export certificate ofairworthiness.Inspection:A330-200At Buyer’s cost, the Seller will perform a maximum power assurance run on eachEngine and at Bayer’s cost the Seller will perform an acceptance flight, of aduration not more than 2 hours as necessary to demonstrate the satisfactoryoperation of the Aircraft, with the Buyer or Buyer’s representative as observer.Following such acceptance flight, a representative of the Buyer, at Buyer’s cost, willperform a complete hot and cold section video borescope on each Engine. Buyershall not be obliged to accept delivery of the Aircraft unless any defects ordeficiencies found during such inspections have been rectified at Seller’s cost.MSN. TBAPage 10 of 10
A330-200 MSN. TBA Page 3 of 10 . ENGINE / APU DETAILS . Engine 1 Engine 2 APU Manufacturer Pratt & Whitney. Pratt & Whitney. Honeywell Model . PW4168A GTCP 31-350C. Thrust Rate 68 600 Lbf68. ENGINE / APU STATUS . Engine 1 Engine 2 APU Serial Number TBA. TBA. Total Time Since New . 27 33 601 5 746. Total Cycles Since New . 5 424 413 6 739 .
HL7538 Airbus A330-200 1998-07 HL7539 Airbus A330-200 1998-08 HL7552 Airbus A330-200 1999-02 HL8211 Airbus A330-200 2010-06 HL8212 Airbus A330-200 2010-08 HL8227 Airbus A330-200 2011-01 HL8228 Airbus A330-200 2011-01 HL8276 Airbus A330-200 2013-02 HL7550 Airbus A330-300 1997-01 HL7551 Airbus A330-300 1997-04
Cv 1.04 1.67 2.33 3.61 7.12 10.6 4 6.63 11.66 19.69 24 7.00 10.87 17.00 25.00 44 36.32 128 Actuator Model Diagram Num. Maximum Close-Off Pressure (PSI) VSI Electric Acutators 24, 120, or 220 VAC 1005-X 4 200 200 200 200 200 200 200 200 200 200 200 200 200 200 200 200 200 200 1005S-X 4 200 200 200 200 200 200 200 200 200 200 200 200 200 200 200 .
which are 10 Airbus A320-200, 4 Airbus A321-200, 7 Airbus A330-200 and 3 Airbus A330-300. In our package you ll find the modern fleet of an: Airbus A320-200 and Airbus A321-200. To select one of these aircraft go to „Select Aircraft“. From the list „Aircraft manufacturer“ choose the entry „AIRBUS BY AEROSOFT“. TheFile Size: 1MBPage Count: 35
Airbus A330 A330-200 A330-200F A330-300 MTOW (t) 240 233 242 Seats (three-class)/payload (t) 253 70 295 Range (km) 13,900 7,400 11,900 Airbus reached a significant milestone for its widebody twin on 19 July, with the de-livery of the 1,000th A330 to Cathay Pacific, the largest operator of the type. In 2012, the airframer unveiled a pro-gramme .
It was in 1998 at the time of A330-200/300 “high growth weight” 230t certification that the first significant step was performed. A centre wing fuel tank was added to the A330-200 definition, increasing range capability, and both A330-200 and A330-300 were the first Airbus aircraft to be fitted with new navigation technologies as Multi-
such as the Boeing 737-800 or Airbus A380. This is likely to lead to an overestimate in emissions as newer, more efficient planes are not represented. 0 200 400 600 800 1000 1200 0 2000 4000 6000 8000 10000 12000 Distance flown (km) kg CO 2 per seat Airbus A310 Airbus A320 Airbus A330 Airbus A340 Boeing737-400 Boeing 747-200 Boeing 747-400 .
Middle East & Africa airline backlog, A330 Data end August 2009 In-service Backlog Emirates 29 Qatar 29 ETIHAD 16 8 Gulf Air 10 20 Egypt Air 7 5 Air Algerie 5 MEA 4 Afriqiyah 1 2 Air Mauritius 1 1 Yemenia 1 Saudia 8 Oman 5 Libyan 4 Tunis Air 3 Total 103 56 A330-300 range 86% of world population A330-200 for route development
Alfredo López Austin, Universidad Nacional Autónoma de México (UNAM) 4:15 pm – 5:00 pm Questions and Answers from Today’s Panelists . Friday’s symposium presenters (order of appearance): Kevin B. Terraciano Kevin Terraciano is Professor of History, chair of the Latin American Studies Graduate Program, and interim director of the Latin American Institute. He specializes in Colonial .
