N639AW, cancelled Mar 24, 2006

Service difficulty reports · 56

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N639AW' AND deregistration_id = 'N639AW-2006-03-24'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AWXA200501114Bellows · inoperativeLAS - 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 FOLLOWED. AIRCRAFT RETURNED TO LAS, DECLARED EMERGENCY, AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE Sep 23, 2005 · N639AW · Airbus A320232 · Cabin Cooling SystemSDR AWXA200500723Power Supply · malfunctionedDURING 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 CARD R1C33303. OPS CHECKS GOOD.Jun 17, 2005 · N639AW · Airbus A320232 · Emergency LightingSDR AWXA200500698Power Supply · inoperativeLAS - 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 SUPPLY UNIT 11WL, S/N 0485. OPERATIONAL CHECKS GOOD.Jun 13, 2005 · N639AW · Airbus A320232 · Emergency LightingSDR AWXA200500671Light · inoperativePERFORMING OPERATIONAL TEST OF EMERGENCY LIGHTING, TEST DON'T PASS.Jun 3, 2005 · N639AW · Airbus A320232 · Emergency LightingSDR AWXA200500675Panel · corrodedDURING 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 LOWER SURFACE OF SIDEWALL PANEL 151EF IN THE AFT CARGO COMPARTMENT TO BE OUT OF LIMITS. FABRICATED May 24, 2005 · N639AW · Airbus A320232 · Cargo CompartmentsSDR AWXA200600798Spar · crackedSAL - 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 LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 84 HOLE OF THE LT WING REARMay 21, 2005 · N639AW · Airbus A320232 · Wing SparSDR AWXA200500674Floor Panel · corrodedDURING 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 CORRODED PANEL AND FABRICATED REPLACEMENT FLOOR PANEL. INSTALLED FABRICATED REPAIR PARTS WITH ORIGINALMay 20, 2005 · N639AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200600800Spar · crackedSAL - 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 SERVICE BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 52, 5May 19, 2005 · N639AW · Airbus A320232 · Wing SparSDR AWXA200600799Spar · crackedSAL - 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 BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 54 HOLE OF THE RT WINMay 14, 2005 · N639AW · Airbus A320232 · Wing SparSDR AWXA200500629Floorbeam · corrodedDURING 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 REPLACEMENT FLOORBEAM PER DWG D53472088; INSTALLED REPAIR PART IAW A320 SRM 51-42-11.May 11, 2005 · N639AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500635Nut · corrodedSAL - 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 REPLACED RETAINING NUT IAW A320 SRM 57-26-13.May 8, 2005 · N639AW · Airbus A320232 · Wing, Landing Gear Attach FittingsSDR AWXA200500676Floor Panel · corrodedSAL - 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 ON FLOOR PANEL 222FF LOCATED IN FORWARD GALLEY FROM FR 16 TO FR 20 AND FABRICATED REPAIR DOUBLER IAWMay 6, 2005 · N639AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200500642Web · crackedSAL - 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. FABRICATED A NEW REPLACEMENT WEB PER DRAWING D53113322, INSTALLED REPAIR PART IAW A320 SRM 51-42-11.May 6, 2005 · N639AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500639Shear Plate · crackedDURING 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 A320 SRM 51-42-11, PAGE 7.May 6, 2005 · N639AW · Airbus A320232 · Fuselage Main, StructureSDR AWXA200500638Shear Plate · corrodedDURING 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 FS 70 IAW A320 SRM 51-72-11.May 6, 2005 · N639AW · Airbus A320232 · Fuselage Main, StructureSDR AWXA200500637Shear Plate · corrodedDURING 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 TO FS 70 IAW A320 SRM 51-72-11.May 6, 2005 · N639AW · Airbus A320232 · Fuselage Main, StructureSDR AWXA200500636Fitting · corrodedSAL - 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 CORRODED FITTING AT LOWER SILL R1 DOOR -Y1732 BETWEEN FS 16 AND FS 20 IAW A320 SRM 51-72-11AND DRAWIMay 6, 2005 · N639AW · Airbus A320232 · Fuselage Main, Attach FittingsSDR AWXA200500633Floor Support · corrodedSAL - 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 AND FS 18; FABRICATED A NEW REPLACEMENT FLOORBEAM PER A320 SRM 53-11-14, PAGE 213 AND 214, FIGURE 20May 6, 2005 · N639AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500632Floor Support · corrodedSAL - 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 TO FS 23; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53111473; INSTALLED REPAIR PART IAW A320 SMay 6, 2005 · N639AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500630Floor Support · corrodedSAL - 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 TO FR 20 IAW A320 SRM 51-42-11.May 6, 2005 · N639AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500566Dummy Rail · corrodedSAL - 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 16; FABRICATED A NEW REPLACEMENT DUMMY RAIL PER DWG D53112826; INSTALLED REPAIR PART IAW A320 SRM May 6, 2005 · N639AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500565Sill · corrodedSAL - 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 & NUT PLATES BETWEEN FR 67 AND FR 68. MAINTENANCE CUT OUT DAMAGE ON LOWER SILL BEAM -Y1292; FABRICATED May 6, 2005 · N639AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500640Shear Plate · crackedDURING 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 A320 SRM 51-42-11, PAGE 7 AND A320 SRM 51-72-11.May 5, 2005 · N639AW · Airbus A320232 · Fuselage Main, StructureSDR AWXA200500634Seat Track · corrodedSAL - 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 Y920 BETWEEN FS 65 AND FS 67; FABRICATED A NEW REPLACEMENT DUMMY RAIL PER DWG D53472040; INSTALLEDMay 5, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500631Sill · corrodedSAL - 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 SRM 51-72-11.May 5, 2005 · N639AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500620Seat Track · corrodedDURING 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 BETWEEN FS 64 TO FS 67; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PARMay 5, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500554Seat Track · corrodedSAL - 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 Y765 AT FR 66; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320May 5, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500643Floorbeam · crackedSAL - 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 BETWEEN FS 27 AND FS 28. FABRICATED A FILLER AND REPAIR ANGLE AND INSTALLED REPAIR PART IAW 53-21-11 May 4, 2005 · N639AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500628Seat Track · corrodedDURING 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 Y1292 AT FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PMay 4, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500627Seat Track · corrodedDURING 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 FS 53; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 5May 4, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500626Seat Track · corrodedSAL - 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 BEAM -Y765 AT FR24 TO FR35; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIMay 4, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500625Seat Track · corrodedDURING 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; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42May 4, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500624Seat Track · corrodedSAL - 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 OF SEAT TRACK BEAM -Y765 AT FS 12 TO FS 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM;May 3, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500623Seat Track · corrodedDURING 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 -Y765 AT FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PARMay 3, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500622Seat Track · corrodedDURING 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 -Y1292 AT FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIRMay 3, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500621Seat Track · corrodedDURING 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 AT FS 12 TO FS 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART May 3, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500619Seat Track · corrodedDURING 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 BETWEEN FS 36 TO FS 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PARMay 3, 2005 · N639AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500013Cable · pulledPHX - 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. MAINTENANCE FOUND BOTH WIRES PULLED OUT OF THE TERMINALS AT EMERGENCY ESCAPE PATH LIGHT FIXTURE SEAT ROW 12 RJan 5, 2005 · N639AW · Airbus A320232 · Light System WiringSDR AWXA200400989Battery · discharged8-DAY CHECK - DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM THE RT OVER WING EMERGENCY LIGHT BATTERY PACK FAULTED. MAINTENANCE REMOVED AND REPLACED THE RT EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.Sep 9, 2004 · N639AW · Airbus A320232 · Emergency LightingSDR AWXA200400916Module · inoperativeDURING F-05 CHECK MAINTENANCE FOUND THE FORWARD LT PARTITION EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD LT PARTITION EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.Aug 20, 2004 · N639AW · Airbus A320232 · Emergency LightingSDR AWXA200300008Uplock Sensor · out of adjustAIR TURN BACK AFTER TAKEOFF EN ROUTE RETRACTED LANDING GEAR, NLG REMAINED DOWN. PERFORMED ECAM PROCEDURES, CYCLED LANDING GEAR; NO CHANGE, NLG REMAINED DOWN AND LOCKED, MAIN GEAR INDICATED UNSAFE. RECYCLED GEAR, ALL GEAR ASSY RETRACTED, BUT LT, RT MAIN GEAR DJan 3, 2003 · N639AW · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR AWXA200201152Pressure Switch · failedON 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. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE (GREEN HYD SYS) ENGINE DRIVEN PUMP IAW AMM 29-11-51-000-010Nov 23, 2002 · N639AW · Airbus A320232 · Hydraulic Pressure SensorSDR AWXA200200126Doubler · gougedLAS - 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 POSION CAUSING 4 EA. GOUGES BETWEEN FRAMES 60 - 61 AND STR 40 - 44 L/H. MAINTENANCE ACCOMPLISHED INTERIFeb 12, 2002 · N639AW · Airbus A320232 · Fuselage Main, Plate/SkinSDR AWXA0002216Fitting · corrodedDiscrepancy/Corrective Action: RH MLG Door Actuator Fitting PN# D533-72613-60400, Fastener Hole Has Corrosion.Corrective Action: Repaired As Per AWA ER 26-5315-01250-JS2Sep 11, 2001 · N639AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA0000324Floorbeam · corrodedC-CHECK, CORROSION LEVEL 2. CABIN FLOOR SUPPORT AT FR66, Y512 LT WL 2 CORRODED BEYOND LIMITS. FABRICATED FLOOR SUPPORT IAW DRAWING D53472094002, FPI COMPLIED IAW AIRBUS NTM 51-80--00, INSTALLED REPAIR IAW A320 SRM 51-72-11, TREATED AND PRIMED IAW A320 SRMMay 23, 2000 · N639AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA0000044Computer · unserviceableAT 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 OPERATED NORMAL. DE-MODED ACFT AFTER FMGC -108 UPGRAGE PER E.O. 22-10-28. REPLACED FLIGHT MANAGEMENT ANJan 31, 2000 · N639AW · Airbus A320232 · Auto Throttle SystemSDR AWXA9900296Radio Panel · unservicableNR 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 23-13-13-401 AND MEL'D (C/N 1109370) NR 3 RMP. THEN REMOVED AND REPLACED NR 3 RMP.Sep 5, 1999 · N639AW · Airbus A320232 · Audio Integrating SystemSDR AWXA9800216Elac · malfunctionedDURING 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 27-93-00, OK FOR SERVICE.Nov 1, 1998 · N639AW · Airbus A320232 · Flight Control SystemSDR AWXA9700584Inlet · dirtyCABIN CREW REPORTS STRONG ODOR IN CABIN DURING FLIGHT. HIGH FLOW PACK OPERATION INCREASED ODOR. WASHED APU INLET, DOOR INLET AND COMPARTMENT. NO EXTERNAL OIL LEAKS NOTED, SMELL CHECK OK.Sep 25, 1997 · N639AW · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR AWXA9700476Prox Sensor · failedLANDING 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 NLG DOOR PROX SENSOR 37GA, BITE CHECK NORMAL.Aug 27, 1997 · N639AW · Airbus A320232 · Landing Gear Position and Warning
Back to N639AW, cancelled Mar 24, 2006