# N639AW: 1995 Airbus Industrie A320-232, registration cancelled 2006-03-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 24, 2006 - Exported to: India - 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: 471 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 19, 1995 - Certificate issued: December 31, 1998 - Last registry action: July 30, 2003 - Mode S code: A85F40 - Owner when cancelled: [Castle Harbour Leasing Inc](https://openairdocs.org/faa-owner/CASTLE%20HARBOUR%20LEASING%20INC) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N639AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=639AW - Page: https://openairdocs.org/deregistered/N639AW-2006-03-24 From the FAA registry file of November 7, 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 (56, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AWXA200501114](https://openairdocs.org/sdr/AWXA200501114), Sep 23, 2005: BELLOWS. INOPERATIVE. LAS - AIR TURNBACK - FLT 372 - DURING CLIMB CREW REPORTED THAT THE AIRCRAFT WOULD NOT HOLD CABIN CLIMB THRU 23000. CABIN AT 9900 AND CLIMBING, ECAM ACTION FOLLO - [SDR AWXA200500723](https://openairdocs.org/sdr/AWXA200500723), Jun 17, 2005: POWER SUPPLY. MALFUNCTIONED. DURING 4 DAY CHECK, FOUND LT MID CABIN SLIDE ARM LIGHT ALWAYS ON. MX REMOVED AND REPLACED MID CABIN LT EMERGENCY POWER SUPPLY IAW AMERICA WEST AIRLINES TASK CAR - [SDR AWXA200500698](https://openairdocs.org/sdr/AWXA200500698), Jun 13, 2005: POWER SUPPLY. INOPERATIVE. LAS - EEL - FLT 741 - IN LAS PILOT REPORTED LEFT EMERGENCY WING EXIT ON ECAM DOOR PAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT POWER - [SDR AWXA200500671](https://openairdocs.org/sdr/AWXA200500671), Jun 3, 2005: LIGHT. INOPERATIVE. PERFORMING OPERATIONAL TEST OF EMERGENCY LIGHTING, TEST DON'T PASS. - [SDR AWXA200500675](https://openairdocs.org/sdr/AWXA200500675), May 24, 2005: PANEL. CORRODED. DURING C-8 CHECK FOUND CORROSION ON LOWER SURFACE OF SIDEWALL PANEL 151EF IN THE AFT CARGO COMPARTMENT FROM FS 49 TO FS 53. MAINTENANCE FOUND THE CORROSION ON L - [SDR AWXA200600798](https://openairdocs.org/sdr/AWXA200600798), May 21, 2005: SPAR. CRACKED. SAL - DURING C8 CHECK DISCOVERED CRACK IN HOLE NR 84 OF THE LT WING REAR SPAR, LT GEAR SUPPORT RIB 5 POSITION THAT REQUIRED OVERSIZE BEYOND SERVICE BULLETIN LIM - [SDR AWXA200500674](https://openairdocs.org/sdr/AWXA200500674), May 20, 2005: FLOOR PANEL. CORRODED. DURING C-8 CHECK, FOUND CORROSION ON LOWER SURFACE OF SIDE WALL PANEL 152 MF FROM FS 56 TO FS 58. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORRO - [SDR AWXA200600800](https://openairdocs.org/sdr/AWXA200600800), May 19, 2005: SPAR. CRACKED. SAL - DURING C8 CHECK DISCOVERED CRACK IN THE NR 52, 54 AND 55 HOLES OF THE LT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE. REQUIRES OVERSIZING THE HOLES BEYOND - [SDR AWXA200600799](https://openairdocs.org/sdr/AWXA200600799), May 14, 2005: SPAR. CRACKED. SAL - DURING C8 CHECK DISCOVERED CRACK IN HOLE NR 54 OF THE RT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE. REQUIRES OVER SIZING THE HOLE BEYOND SERVICE BULLETI - [SDR AWXA200500629](https://openairdocs.org/sdr/AWXA200500629), May 11, 2005: FLOORBEAM. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1162 AT FS 68 TO FS 69. MAINTENANCE REMOVED FLOORBEAM Y1162 AT FS 68 TO FS 69; FABRICATED A NEW REP - [SDR AWXA200500635](https://openairdocs.org/sdr/AWXA200500635), May 8, 2005: NUT. CORRODED. SAL - LANDING GEAR - DURING C08 CHECK, CORROSION WAS FOUND ON THE RETAINING NUT FOR THE FWD PINTLE BEARING ON THE RT MAIN LANDING GEAR. MAINTENANCE REMOVED AND - [SDR AWXA200500676](https://openairdocs.org/sdr/AWXA200500676), May 6, 2005: FLOOR PANEL. CORRODED. SAL - MAJOR REPAIR - DURING C-8 CHECK FOUND CORROSION ON FLOOR PANEL 222FF LOCATED IN FORWARD GALLEY FROM FR 16 TO FR 20. MAINTENANCE BLENDED OUT DAMAGED AREA O - [SDR AWXA200500642](https://openairdocs.org/sdr/AWXA200500642), May 6, 2005: WEB. CRACKED. SAL - MAJOR REPAIR - DURING C-8 CHECK, A 5/8 INCH CRACK WAS FOUND IN WEB AT FR 11 AND FLOOR STR Y770. MAINTENANCE REMOVED CRACKED WEB FROM FS 8 TO FS 11. FABRIC - [SDR AWXA200500639](https://openairdocs.org/sdr/AWXA200500639), May 6, 2005: SHEAR PLATE. CRACKED. DURING C08 CHECK, A CRACK WAS FOUND AT SHEAR PLATE -Y1300 BETWEEN FS 68 TO FS 69. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE -Y1300 BETWEEN FS 68 TO FS 69 IAW - [SDR AWXA200500638](https://openairdocs.org/sdr/AWXA200500638), May 6, 2005: SHEAR PLATE. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND AT SHEAR PLATE Y1200 BETWEEN FS 69 TO FS 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE Y1200 BETWEEN FS 69 TO - [SDR AWXA200500637](https://openairdocs.org/sdr/AWXA200500637), May 6, 2005: SHEAR PLATE. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND AT SHEAR PLATE -Y1300 BETWEEN FS 69 TO FS 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE -Y1300 BETWEEN FS 69 T - [SDR AWXA200500636](https://openairdocs.org/sdr/AWXA200500636), May 6, 2005: FITTING. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK, GALVANIC CORROSION WAS FOUND AT LOWER SILL R1 DOOR -Y1732 BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED AND REPLACED THE C - [SDR AWXA200500633](https://openairdocs.org/sdr/AWXA200500633), May 6, 2005: FLOOR SUPPORT. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y254 BETWEEN FS 16 AND FS 18. MAINTENANCE REMOVED FLOORBEAM Y254 BETWEEN FS 16 A - [SDR AWXA200500632](https://openairdocs.org/sdr/AWXA200500632), May 6, 2005: FLOOR SUPPORT. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y189 BETWEEN FS 20 TO FS 23. MAINTENANCE REMOVED FLOORBEAM -Y189 AT FS 20 T - [SDR AWXA200500630](https://openairdocs.org/sdr/AWXA200500630), May 6, 2005: FLOOR SUPPORT. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y254 AT FR 12 TO FR 20. MAINTENANCE INSTALLED NEW FLOORBEAM -Y254 AT FR 12 T - [SDR AWXA200500566](https://openairdocs.org/sdr/AWXA200500566), May 6, 2005: DUMMY RAIL. CORRODED. SAL - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM DUMMY RAIL Y503.2 AT FR 16. MAINTENANCE REMOVED DAMAGED DUMMY RAIL Y503.2 AT FR - [SDR AWXA200500565](https://openairdocs.org/sdr/AWXA200500565), May 6, 2005: SILL. CORRODED. SAL - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SILL BEAM -Y1292 AT CUTOUT FOR R-2 DOOR AROUND GIRT BAR FITTING RIVET HEADS & NU - [SDR AWXA200500640](https://openairdocs.org/sdr/AWXA200500640), May 5, 2005: SHEAR PLATE. CRACKED. DURING C08 CHECK, A CRACK WAS FOUND AT SHEAR PLATE Y1300 BETWEEN FS 68 TO FS 69. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE Y1300 BETWEEN FS 68 TO FS 69 IAW A - [SDR AWXA200500634](https://openairdocs.org/sdr/AWXA200500634), May 5, 2005: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON FLOORBEAM DUMMY RAIL Y920 BETWEEN FS 65 AND FS 67. MAINTENANCE REMOVED DAMAGED DUMMY RAIL - [SDR AWXA200500631](https://openairdocs.org/sdr/AWXA200500631), May 5, 2005: SILL. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM SILL Y1732 AT FR 66. MAINTENANCE REPLACED FLOORBEAM SILL Y1732 AT FR 66 IAW A320 - [SDR AWXA200500620](https://openairdocs.org/sdr/AWXA200500620), May 5, 2005: SEAT TRACK. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON SEAT TRACK BEAM Y1292 BETWEEN FS 64 TO FS 67. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y1292 BE - [SDR AWXA200500554](https://openairdocs.org/sdr/AWXA200500554), May 5, 2005: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK BEAM Y765 AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y76 - [SDR AWXA200500643](https://openairdocs.org/sdr/AWXA200500643), May 4, 2005: FLOORBEAM. CRACKED. SAL - MAJOR REPAIR - DURING C-8 CHECK A 3/8 INCH CRACK WAS FOUND IN FLOORBEAM UPPER FLANGE -Y254 AT FR 27 + 19". MAINTENANCE CUTOUT CRACK IN FLOORBEAM -Y254 BET - [SDR AWXA200500628](https://openairdocs.org/sdr/AWXA200500628), May 4, 2005: SEAT TRACK. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK BEAM Y1292 AT FS 41 TO FS 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y - [SDR AWXA200500627](https://openairdocs.org/sdr/AWXA200500627), May 4, 2005: SEAT TRACK. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK BEAM Y1292 AT FS 53. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y1292 AT F - [SDR AWXA200500626](https://openairdocs.org/sdr/AWXA200500626), May 4, 2005: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK BEAM -Y765 AT FR24 TO FR35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK - [SDR AWXA200500625](https://openairdocs.org/sdr/AWXA200500625), May 4, 2005: SEAT TRACK. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON LT INBOARD SEAT TRACK BEAM Y765 AT FS 45. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 AT FS45 - [SDR AWXA200500624](https://openairdocs.org/sdr/AWXA200500624), May 3, 2005: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BEAM -Y765 AT FS 12 TO FS 24. MAINTENANCE REMOVED CORRODED SECTION O - [SDR AWXA200500623](https://openairdocs.org/sdr/AWXA200500623), May 3, 2005: SEAT TRACK. CORRODED. DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BEAM -Y765 AT FS 41 TO FS 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y7 - [SDR AWXA200500622](https://openairdocs.org/sdr/AWXA200500622), May 3, 2005: SEAT TRACK. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BEAM -Y1292 AT FS 41 TO FS 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM - [SDR AWXA200500621](https://openairdocs.org/sdr/AWXA200500621), May 3, 2005: SEAT TRACK. CORRODED. DURING C08 CHECK, EXFOLIATION CORROSION WAS FOUND ON RT SEAT TRACK BEAM -Y1292 AT FS 12 TO FS 24. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y1292 - [SDR AWXA200500619](https://openairdocs.org/sdr/AWXA200500619), May 3, 2005: SEAT TRACK. CORRODED. DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON SEAT TRACK BEAM -Y765 BETWEEN FS 36 TO FS 41. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y765 BE - [SDR AWXA200500013](https://openairdocs.org/sdr/AWXA200500013), Jan 5, 2005: CABLE. PULLED. PHX - EEL - DURING E-08 CHECK FUNCTIONAL TEST OF THE EMERGENCY LIGHT SYSTEM, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 RT WAS FOUND INOPERATIVE. MAINTENANC - [SDR AWXA200400989](https://openairdocs.org/sdr/AWXA200400989), Sep 9, 2004: BATTERY. DISCHARGED. 8-DAY CHECK - DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM THE RT OVER WING EMERGENCY LIGHT BATTERY PACK FAULTED. MAINTENANCE REMOVED AND REPLACED THE - [SDR AWXA200400916](https://openairdocs.org/sdr/AWXA200400916), Aug 20, 2004: MODULE. INOPERATIVE. DURING F-05 CHECK MAINTENANCE FOUND THE FORWARD LT PARTITION EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD LT PARTITION EMERGENCY E - [SDR AWXA200300008](https://openairdocs.org/sdr/AWXA200300008), Jan 3, 2003: UPLOCK SENSOR. OUT OF ADJUST. AIR TURN BACK AFTER TAKEOFF EN ROUTE RETRACTED LANDING GEAR, NLG REMAINED DOWN. PERFORMED ECAM PROCEDURES, CYCLED LANDING GEAR; NO CHANGE, NLG REMAINED DOWN AND - [SDR AWXA200201152](https://openairdocs.org/sdr/AWXA200201152), Nov 23, 2002: PRESSURE SWITCH. FAILED. ON CLIMBOUT, RECEIVED ECAM WARNING FOR GREEN HYD SYS NR 1 ENGINE LOW PRESSURE AND FLUID QUANTITY. TURNED BACK TO PHX AND LANDED, TAXIED BACK TO GATE. MAINTENANC - [SDR AWXA200200126](https://openairdocs.org/sdr/AWXA200200126), Feb 12, 2002: DOUBLER. GOUGED. LAS - GROUND DAMAGE / MAJOR REPAIR - FLT 741 - "S" - WHILE POSITIONED AT GATE B23 IN LAS A BAGGAGE CART WAS BLOWN INTO THE LOWER AFT FUSELAGE SKIN 6 O'CLOCK POS - [SDR AWXA0002216](https://openairdocs.org/sdr/AWXA0002216), Sep 11, 2001: FITTING. CORRODED. Discrepancy/Corrective Action: RH MLG Door Actuator Fitting PN# D533-72613-60400, Fastener Hole Has Corrosion.Corrective Action: Repaired As Per AWA ER 26-5315- - [SDR AWXA0000324](https://openairdocs.org/sdr/AWXA0000324), May 23, 2000: FLOORBEAM. CORRODED. C-CHECK, CORROSION LEVEL 2. CABIN FLOOR SUPPORT AT FR66, Y512 LT WL 2 CORRODED BEYOND LIMITS. FABRICATED FLOOR SUPPORT IAW DRAWING D53472094002, FPI COMPLIED IA - [SDR AWXA0000044](https://openairdocs.org/sdr/AWXA0000044), Jan 31, 2000: COMPUTER. UNSERVICEABLE. AT 1000 FT AGL CAPT CALLED FOR CLIMB THRUST, AUTO THROTTLE DROPPED OFF AND ENG NR 1 DROPPED TO IDLE THRUST. RETURNED TO AIRPORT USING MANUAL THRUST WHICH OPERAT - [SDR AWXA9900296](https://openairdocs.org/sdr/AWXA9900296), Sep 5, 1999: RADIO PANEL. UNSERVICABLE. NR 1 RADIO MGT PANEL (RMP) FAILED, FOLLOWED BY SMELL OF SMOKE IN COCKPIT. PULLED VHF-1 AND RMP-1 C/B, SMOKE DISSIPATED. SWAPPED NR 1 AND NR 3 RMP IAW AMM 23-13- - [SDR AWXA9800216](https://openairdocs.org/sdr/AWXA9800216), Nov 1, 1998: ELAC. MALFUNCTIONED. DURING FLAP EXTENSION POS 1 TO POS 2 AND POS 2 TO POS 3 AIRCRAFT ROLLED SHARPLY L/R SHORT DURATION ROLL. REPLACED BOTH ELAC COMPUTERS PER 27-93 AND TESTED PER 2 - [SDR AWXA9700584](https://openairdocs.org/sdr/AWXA9700584), Sep 25, 1997: INLET. DIRTY. CABIN CREW REPORTS STRONG ODOR IN CABIN DURING FLIGHT. HIGH FLOW PACK OPERATION INCREASED ODOR. WASHED APU INLET, DOOR INLET AND COMPARTMENT. NO EXTERNAL OIL LE - [SDR AWXA9700476](https://openairdocs.org/sdr/AWXA9700476), Aug 27, 1997: PROX SENSOR. FAILED. LANDING GEAR FAILED TO COME UP AFTER TAKEOFF, ALL THREE. RECYCLED AND LANDING GEAR RETRACTED OK. FOUND NLG DOOR PROX SENSOR 37GA FAULTING. REMOVED AND REPLACED All 56: https://openairdocs.org/deregistered/N639AW-2006-03-24/reports.md --- 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.