# N605AW: 1997 Airbus Industrie A320-232, registration cancelled 2009-07-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 2, 2009 - Exported to: Ireland - Status when cancelled: Triennial form not returned - Airframe: [Airbus Industrie A320-232](https://openairdocs.org/model/airbus-industrie-a320-232) (registry code 3930326) - Engine: [IAE V2500SERIES](https://openairdocs.org/engine/iae-v2500series) (registry code 34601) - Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs) - Serial number: 543 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 25, 2000 - Certificate issued: January 25, 2000 - Last registry action: October 21, 2008 - Mode S code: A7D9E7 - Owner when cancelled: [International Lease Finance Corp](https://openairdocs.org/faa-owner/INTERNATIONAL%20LEASE%20FINANCE%20CORP) - Location: [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles) - Owner type: Corporation - Owner's area on the map: 34.0564° N, 118.4137° W: Placed by OpenAirDocs at the center of ZIP code 90067, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N605AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=605AW - Page: https://openairdocs.org/deregistered/N605AW-2009-07-02 From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Airbus Industrie A320-232: https://openairdocs.org/model/airbus-industrie-a320-232.md ## Service difficulty reports (143, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA2009042090933](https://openairdocs.org/sdr/USAA2009042090933), Apr 2, 2009: CYLINDER. LOW PRESSURE. SAL - C1 - EES - LOW PRESSURE IN EMERGENCY CYLINDER ACCUMULATOR IN DOOR 841. CHARGED DAMPER & EMERGENCY CYLINDER ACCUMULATOR IN DOOR 841 IAW A320 AMM 52-10-00-6 - [SDR USAA2009041490884](https://openairdocs.org/sdr/USAA2009041490884), Mar 31, 2009: ANGLE. CRACKED. CRACK SUPPORT ANGLE GUTTER BETWEEN FR15 TO FR21 BETWEEN S6L TO S8L. REPLACED SUPPORT ANGLE GUTTER BETWEEN FR15 TO FR21 BETWEEN S6L TO S8L IAW SRM 51-72-11. - [SDR USAA2009032390649](https://openairdocs.org/sdr/USAA2009032390649), Mar 18, 2009: SLIDE. LOW PRESSURE. FLT 655 - PHX - EMERGENCY EGRESS SYSTEM - L1 DOOR SLIDE NEEDS CHANGED, INDICATION IN RED. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR SLIDE. - [SDR USAA2009013090231](https://openairdocs.org/sdr/USAA2009013090231), Jan 29, 2009: CYLINDER. LOW PRESSURE. FLT 306 CLT-LAS - EMERGENCY EQUIPMENT - R-1 ENTRANCE DOOR ASSIST BOTTLE CHARGE LOW. MAINTENANCE SERVICED R-1 DOOR ASSIST BOTTLE. - [SDR USAA920080448](https://openairdocs.org/sdr/USAA920080448), Feb 18, 2008: SKIN. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON FUSELAGE EXTERNAL SKIN, BS 3310 / FR 69 - BS 3366 / FR 70, S31R - S32R AROUND THE OVERBOARD VENT. REPAIRED FUSELAGE - [SDR USAA920080382](https://openairdocs.org/sdr/USAA920080382), Feb 2, 2008: FLOORBEAM. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3207 / FR 67, +Y1280. REPLACED CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3207 / F - [SDR USAA920080441](https://openairdocs.org/sdr/USAA920080441), Jan 31, 2008: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON SEAT TRACK, BS 1377 / FR 32, -Y765. REPAIRED SEAT TRACK, BS 1377 / FR 32, -Y765 IAW A320 SRM 53-00-15. - [SDR USAA920080440](https://openairdocs.org/sdr/USAA920080440), Jan 31, 2008: SHEAR PLATE. CRACKED. SAL - MAJOR REPAIR - C8 CHECK - CRACKED CABIN TRAY / SHEAR PLATE, BS 3257 / FR 68, -Y1732. REPLACED CABIN TRAY / SHEAR PLATE, BS 3257 / FR 68, -Y1732 IAW A320 S - [SDR USAA920080380](https://openairdocs.org/sdr/USAA920080380), Jan 29, 2008: FITTING. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON THE L2 DOOR CUTOUT LOWER CENTER SHAPE SILL FITTING, BS 3257 /FR 68, S23L. REPLACED THE L2 DOOR CUTOUT LOWER CENTER - [SDR USAA920080379](https://openairdocs.org/sdr/USAA920080379), Jan 29, 2008: FLOORBEAM. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN SEAT RAIL BEAM, BS 3043 / FR 64 - BS 3158 / FR 66, +Y1242. REPLACED CABIN SEAT RAIL BEAM, BS 3043 / FR 64 - B - [SDR USAA920080310](https://openairdocs.org/sdr/USAA920080310), Jan 27, 2008: FLOOR SUPPORT. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - NR 6039301, CORROSION ON FLOOR SUPPORT, BS 709/FR 16 - BS 760/FR 18, +Y254. REPLACED FLOOR SUPPORT BS 709/FR 16 - BS 760/FR 18, - [SDR USAA920080378](https://openairdocs.org/sdr/USAA920080378), Jan 25, 2008: SHEAR PLATE. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1250. REPLACED CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 - [SDR USAA920080377](https://openairdocs.org/sdr/USAA920080377), Jan 24, 2008: FLOORBEAM. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3366 / FR 70, +Y515. REPLACED CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3366 / FR - [SDR USAA920080376](https://openairdocs.org/sdr/USAA920080376), Jan 24, 2008: SHEAR PLATE. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1250. REPLACED CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 - [SDR USAA920080375](https://openairdocs.org/sdr/USAA920080375), Jan 24, 2008: FLOORBEAM. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, -Y765. REPLACED CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR - [SDR USAA920080452](https://openairdocs.org/sdr/USAA920080452), Jan 23, 2008: SKIN. SATURATED. SAL - MAJOR REPAIR - C8 CHECK - RIGHT ELEVATOR UPPER SURFACE HAS 12 AREAS THAT HAVE INDICATION OF WATER ENTRAPMENT. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A3 - [SDR USAA920080383](https://openairdocs.org/sdr/USAA920080383), Jan 23, 2008: FLOOR PANEL. CORRODED. SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN FLOOR PANEL 261 FF, BS 3158 / FR 66 - BS 3257 / FR 68, +Y1160. REPLACED CABIN FLOOR PANEL 261 FF, BS 3158 / F - [SDR AWXA200700206](https://openairdocs.org/sdr/AWXA200700206), Jan 12, 2007: SENSOR. OUT OF ADJUST. FLIGHT 297: MSP - LAS - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CREW LOWERED LDG GEAR HANDLE PER ECAM AND THE "L/G GEAR NOT UPLOCKED" ECAM MSG REMAINED. DEC - [SDR AWXA200601568](https://openairdocs.org/sdr/AWXA200601568), Aug 28, 2006: BATTERY PACK. FAILED. LAS - DURING OVERNIGHT MAINTENANCE, THE EMERGENCY LIGHT BATTERY AT LEFT CABIN FAILED TEST PER T/C I8M05319 (CIDS PANEL CK). MAINTENANCE REPLACED THE BATTERY PAC - [SDR AWXA200601125](https://openairdocs.org/sdr/AWXA200601125), Jul 6, 2006: FITTING. CRACKED. CRACK FOUND ON HOLE NR 17, FORWARD PINTLE FITTING LT WING. CRACK ON HOLE NR 17 OF FWD PINTLE FITTING LEFT WING WAS REPAIRED IAW PART C OF AWA ER NR 26 -5721 - 0 - [SDR AWXA200601124](https://openairdocs.org/sdr/AWXA200601124), Jul 6, 2006: FITTING. CRACKED. CRACK FOUND ON HOLE NR 16 OF FWD PINTLE FITTING LT. CRACK ON HOLE NR 16 OF FWD PINTLE FITTING LEFT WING WAS REPAIRED IAW PART C OF AWA ER NR 26 - 5721 - 06181 - - [SDR AWXA200601116](https://openairdocs.org/sdr/AWXA200601116), Jul 3, 2006: SKIN. DENTED. TRAINING EDGE OF ELEVATOR UPPER SURFACE LEFT THIS TO 24 " OB OF RIB 8 L= 1 BY W = 4 APPROXIMATELY. REPAIRED IAW SRM A 320 - 55 - 21 - 11 FIG 213. PROTECTIVE TRE - [SDR AWXA200601246](https://openairdocs.org/sdr/AWXA200601246), Jul 2, 2006: FITTING. CORRODED. SAL - MAJOR REPAIR - CHECK NR. C7. NR 5910101. CORROSION AROUND THE HOLE NR 71 OF ACTUATING CYLINDER ANCHORAGE LT WING. CORROSION AROUND THE HOLE NR 71 OF ACTUA - [SDR AWXA200601245](https://openairdocs.org/sdr/AWXA200601245), Jul 2, 2006: SPAR. CORRODED. SAL - MAJOR REPAIR - CHECK NR C7. NR 5910106. CORROSION AROUND HOLE NO. 55 OF REAR SPAR LEFT WING. CORROSION AROUND THE HOLE NO. 55 OF REAR SPAR LEFT WING WAS R - [SDR AWXA200601244](https://openairdocs.org/sdr/AWXA200601244), Jul 2, 2006: FITTING. CORRODED. SAL - MAJOR REPAIR - CHECK NO. C7. NR NO. 5909898. CORROSION AROUND THE HOLE NO. 62 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND HOLE NO. 62 OF A - [SDR AWXA200601243](https://openairdocs.org/sdr/AWXA200601243), Jul 2, 2006: CYLINDER. CORRODED. SAL - MAJOR REPAIR - CHECK NO. C7. NR NO. 5909891. CORROSION AROUND THE HOLE NR 53 OF ACTUATING CYLINDER ANCHORAGE LT WING. CORROSION AROUND THE HOLE NR 53 OF A - [SDR AWXA200601242](https://openairdocs.org/sdr/AWXA200601242), Jul 2, 2006: ATTACH FITTING. CORRODED. SAL - MAJOR REPAIR - CHECK NR C7. NR 5909892. CORROSION AROUND THE HOLE NR 54 OF ACTUATING CYLINER ANCHORAGE LT WING. CORROSION AROUND THE HOLE NR 54 OF ACTUATI - [SDR AWXA200601241](https://openairdocs.org/sdr/AWXA200601241), Jul 2, 2006: SPAR. CORRODED. SAL - MAJOR REPAIR - CHECK NO. C7. NR 5910124. CORROSION AROUND HOLE NR 54 OF REAR SPAR RIGHT WING. CORROSION AROUND HOLE NR 54 OF REAR SPAR RIGHT WING WAS REMO - [SDR AWXA200601162](https://openairdocs.org/sdr/AWXA200601162), Jul 2, 2006: SUPPORT. CORRODED. FOUND CORROSION AROUND HOLE NR 56 OF THE ACTUATING CYLINDER ANCHORAGE RIGHT WING. CORROSION AROUND HOLE NR 56 OF THE ACTUATING CYLINDER ANCHORAGE RIGHT WING WAS - [SDR AWXA200601161](https://openairdocs.org/sdr/AWXA200601161), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND HOLE 56 OF REAR SPAR RIGHT WING. CORROSION AROUND HOLE 56 OF REAR SPAR RIGHT WING WAS REMOVED IAW PART A OF AWA, ER NR 26 - 5721 - 06181 - [SDR AWXA200601160](https://openairdocs.org/sdr/AWXA200601160), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND HOLD NR 79 OF REAR SPAR RIGHT WING. CORROSION AROUND HOLD NR 79 OF REAR SPAR RIGHT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5721 - 0 - [SDR AWXA200601159](https://openairdocs.org/sdr/AWXA200601159), Jul 2, 2006: ATTACH FITTING. CORRODED. FOUND CORROSION AROUND HOLE NR 58 OF ACTUATING CYLINDER ANCHORAGE RIGHT WING. CORROSION AROUND HOLE NR 58 OF ACTUATING CYLINDER ANCHORAGE RIGHT WING WAS REMOVED - [SDR AWXA200601158](https://openairdocs.org/sdr/AWXA200601158), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND HOLE NR 58 OF REAR SPAR RIGHT WING. CORROSION AROUND HOLE NR 58 OF REAR SPAR RIGHT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5721 - 0 - [SDR AWXA200601157](https://openairdocs.org/sdr/AWXA200601157), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND HOLE NR 54 OF REAR SPAR RIGHT WING. CORROSION AROUND HOLE NR 54 OF REAR SPAR RIGHT WING WAS REMOVED IAW PAR A OF ER NR 26 - 5723 - 06181 - [SDR AWXA200601156](https://openairdocs.org/sdr/AWXA200601156), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND HOLE NR 77 OF REAR SPAR RIGHT WING. CORROSION AROUND HOLE NR 77 OF REAR SPAR RIGHT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5721 - 0 - [SDR AWXA200601155](https://openairdocs.org/sdr/AWXA200601155), Jul 2, 2006: SPAR. SCRATCHED. SCATCH WAS FOUND HOLE NR 53 REAR SPAR RIGHT WING. SCATCH FOUND HOLE NR 53 REAR SPAR RIGHT WING WAS REPAIRED IAW ER 26-5721-06181 - ES2. - [SDR AWXA200601154](https://openairdocs.org/sdr/AWXA200601154), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND HOLE NR 75 OF REAR SPAR RIGHT WING. CORROSION AROUND HOLE NR 75 OF REAR SPAR RIGHT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5721 - 0 - [SDR AWXA200601153](https://openairdocs.org/sdr/AWXA200601153), Jul 2, 2006: ATTACH FITTING. CORRODED. FOUND CORROSION AROUND HOLE NR 60 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND HOLE NR 60 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS REMOVED I - [SDR AWXA200601152](https://openairdocs.org/sdr/AWXA200601152), Jul 2, 2006: ATTACH FITTING. CORRODED. FOUND CORROSION AROUND THE HOLE NR 53 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND THE HOLE NR 53 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS R - [SDR AWXA200601151](https://openairdocs.org/sdr/AWXA200601151), Jul 2, 2006: ATTACH FITTING. CORRODED. FOUND CORROSION AROUND THE HOLE NR 73 ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND THE HOLE NR 73 ACTUATING CYLINDER ANCHORAGE LEFT WING WAS REMOVED - [SDR AWXA200601150](https://openairdocs.org/sdr/AWXA200601150), Jul 2, 2006: ATTACH FITTING. CORRODED. FOUND CORROSION AROUND THE HOLE NR 62 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND THE HOLE NR 62 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS R - [SDR AWXA200601149](https://openairdocs.org/sdr/AWXA200601149), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND THE HOLE NR 57 OF REAR SPAR LEFT WING. CORROSION AROUND THE HOLE NR 57 OF REAR SPAR LEFT WING WAS REMOVED IAW ER NR 26 - 5721 - 06181 - E - [SDR AWXA200601148](https://openairdocs.org/sdr/AWXA200601148), Jul 2, 2006: ATTACH FITTING. CORRODED. FOUND CORROSION AROUND HOLE NR 61 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND HOLE NR 61 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS REMOVED I - [SDR AWXA200601147](https://openairdocs.org/sdr/AWXA200601147), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND THE HOLE NR 60 OF REAR SPAR LEFT WING. CORROSION AROUND HOLE NR 60 OF REAR SPAR LEFT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5721 - - [SDR AWXA200601145](https://openairdocs.org/sdr/AWXA200601145), Jul 2, 2006: ATTACH FITTING. CORRODED. FOUND CORROSION AROUND HOLE NR 55 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND HOLE NR 55 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS REMOVED I - [SDR AWXA200601144](https://openairdocs.org/sdr/AWXA200601144), Jul 2, 2006: SPAR. CORRODED. FOUND CORROSION AROUND THE HOLE NR 53 OF REAR SPAR LEFT WING. CORROSION AROUND THE HOLE NR 53 OF REAR SPAR LEFT WING WAS REMOVED IAW 26 - 5727 - 06181 - ES2 ITE - [SDR AWXA200601142](https://openairdocs.org/sdr/AWXA200601142), Jul 2, 2006: ATTACH BRACKET. CORRODED. FOUND CORROSION AROUND THE NR 54 HOLE OF CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND THE HOLE NR 54 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS REMOVED IAW - [SDR AWXA200601140](https://openairdocs.org/sdr/AWXA200601140), Jul 2, 2006: ATTACH BRACKET. CORRODED. CORROSION AROUND THE HOLE NR 52 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND HOLE NR 52 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS REMOVED IAW - [SDR AWXA200601139](https://openairdocs.org/sdr/AWXA200601139), Jul 2, 2006: ATTACH BRACKET. CORRODED. FOUND CORROSION AROUND HOLE NR 56 OF ACTUATING CYLINDER ANCHORAGE LEFT WING. CORROSION AROUND HOLE NR 56 OF ACTUATING CYLINDER ANCHORAGE LEFT WING WAS REMOVED I - [SDR AWXA200601137](https://openairdocs.org/sdr/AWXA200601137), Jul 2, 2006: SPAR. CRACKED. CRACK FOUND ON HOLE NR 17 FWD REAR SPAR OF PINTLE FITTING LEFT WING. CRACK ON HOLE NR 17 REAR SPAR PINTLE FITTING LEFT WING WAS REPAIRED IAW PART C OF AWA ER NR All 143: https://openairdocs.org/deregistered/N605AW-2009-07-02/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB MIA01LA224](https://openairdocs.org/ntsb/MIA01LA224), Aug 20, 2001: Airbus Industrie A320-232 (N605AW), Needles, CA, no damage. Probable cause: an inadvertent in-flight encounter with turbulence. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20010820038359A](https://openairdocs.org/incident/20010820038359A), Aug 20, 2001: Airbus A320232 (N605AW), Tampa, FL, No damage. (.19) On August 20, 2001, about 0404 eastern daylight time, an Airbus A320-232, N605AW, operated by america west as flight 579, as a title 14 CFR part 121… ## Other aircraft with N605AW - [Registered now](https://openairdocs.org/aircraft/N605AW): Saurenman Edward E SAW-REVO, S/N SAW-1001 - [Cancelled 1990-08-17](https://openairdocs.org/deregistered/N605AW-1990-08-17): British Aerospace BAE 146 SERIES 200A, S/N E2016. N-number assigned, not yet registered --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.