N646AW, cancelled May 10, 2006
Service difficulty reports · 61
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 = 'N646AW' AND deregistration_id = 'N646AW-2006-05-10' 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.
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 = 'N646AW' AND deregistration_id = 'N646AW-2006-05-10' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AWXA200600414Battery · inoperativePHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE LEFT FORWARD CABIN EPSU BATTERY PACK HAD -LOW CHARGE-. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD CABIN EPSU BATTERY PACK IAW AMERICA WEST AIRLINES TASK CARD A1C33302. OPERATIONAL CHECKS WERE GOOSDR AWXA200500954Blades · failedDURING CLIMBOUT, 500 AGL, LOUD BANG ACCOMPANIED WITH ACFT YAWING LT 5-10 FT. ENG RECOVERED IMMEDIATELY. ACFT CONTINUED & LANDED WITHOUT FURTHER EVENT. NO EMERGENCY ACTION TAKEN/DECLARED. MX BORESCOPED BOTH ENGINES TO ENSURE INTEGRITY. NO DEFECTS NOTED ON SDR AWXA200500750Battery Pack · dischargedDURING 8-DAY CHECK, FOUND BOTH LT AND RT OVERWING SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT (11WL) AND RT (12WL) BATTERY PACKS IAW AIRBUS MM 33-51-38-04. OPERATIONAL TESTS WERE GOOD.SDR AWXA200500594Epsu · faultyPHX - EEL - DURING 8-DAY CHECK, A LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK. OPERATIONAL CHECK WAS GOOD. BATTERY PACK INFORMATION: MANUFACTURER: DIEHL GMSDR AWXA200500559Flashlight · inoperativeLAS - EMERGENCY EQUIPMENT DURING 8-DAY CHECK, THE AFT FLIGHT ATTENDANT FOLD OUT JUMP SEAT EMERGENCY FLASHLIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401353Slide · delaminatedPHX - EES - DURING 4-DAY CHECK THE LOWER AFT CORNER OF THE RT OVERWING SLIDE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING SLIDE ASSEMBLY IAW T/C R1A25301.SDR AWXA200400561Deu · faultyPHX - EEL DURING 4-DAY CHECK: FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FAILED AT CIDS PANEL. MAINTENANCE REMOVED AND REPLACED DECODER ENCODER UNIT (DEU) B (300RH5) IAW AMM 23-73-47, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400333Flashlight · inoperativePHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT OUTBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400302Bearing · failedPHX - EMERGENCY LANDING - FLT 0272 - ON SHORT AND FINAL INTO PHX EN ROUTE FROM SNA ENCOUNTERED SMOKE AND A STRONG ELECTRICAL BURNING ODOR IN CABIN, DONNED MASKS AND DECLARED EMERGENCY. MAINTENANCE FOUND THE AVIONICS COOLING FAN (EXTRACT FAN) BEARINGS SEIZED CSDR AWXA200301080Diaphragm · leakingDURING INSPECTION FOUND THE L-2 DOOR EMERGENCY OPERATION CYLINDER PRESSURE GAUGE READING ZERO. MAINTENANCE REMOVED AND REPLACED THE DIAPHRAGM IN PERCUSSION MECHANISM OF L-2 DOOR EMERGENCY OPERATION CYLINDER, SERVICED TO PROPER PRESSURE, LEAK AND OPERATIONAL CHSDR AWXA200301008Connector · damagedEN ROUTE, AFTER TAKEOFF BLEEDS OFF RECEIVED ECAM MESSAGE NR 2 ENG BLEED ABNORMAL PRESS. TURNED OFF APU BLEED SWITCH NR 2 ENG BLEED ONLY AT 24 PSI, DIVERTED FOR REPAIR. MAINT REMOVED AND REPLACED BLEED PRESS REG VALVE CTRL SOLENOID (10HA2), DUE TO CLASS 3 FAULTSDR AWXA200300939Lanyard · tornON DECENT, EN ROUTE FROM PHX THE FLIGHT ATTENDANT REPORTED A LOUD SQUEAL COMING FROM THE L-2 DOOR. MAINTENANCE FOUND THE L-2 DOOR SLIDE LOWER LANYARD TORN AND IN THE DOOR SEAL, AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX WHERE THE L-2 DOOR SLIDE WAS REMOVED ASDR AWXA200300598Terminal · brokenDURING C-01 CHECK THE EMERGENCY EXIT LIGHT BETWEEN THE L/H OVER-WING HATCHES WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED A BROKEN EMERGENCY EXIT LIGHT TERMINAL LUG BETWEEN L/H OVER-WING EXITS IAW A320 ESPM 20-48-14, PG. 1-3, OPERATIONAL CHECK WAS GOSDR AWXA200300601Floor Panel · delaminatedDURING C-01 CHECK CENTER WING FLOOR PANEL 241EF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241EF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306.SDR AWXA200300600Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 241FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306.SDR AWXA200300599Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING C-01 CHECK CENTER WING FLOOR PANEL 242FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 242FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70055; INSTALLED REPAIR PART IAW AWA T/C R1C25306.SDR AWXA200300571Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 242GF WAS FOUND DELAMINATED. MAINTENANCE REMOVED CABIN FLOOR PANEL 242GF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D536-70055; INSTALLED NEW PANEL IAW AWA T/C R1C25306, AND A320 SRM 53-02-00, PGSDR AWXA200300597Terminal · brokenDURING C-01 CHECK THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR IAW A320 ESPM 20-48-24, PG. 18, OPERATIONAL CHECK WAS GOOD IAW AMM SUBTASKSDR AWXA200300570Fitting · brokenMCN - EES - DURING C-01 CHECK THE LT OVERWING HATCH SLIDE BOTTLE CABLE FITTING WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING HATCH SLIDE BOTTLE IAW AMM SUBTASK 25-62-46-020-050-A, AND 25-62-46-420-050-A, OPERATIONAL CHECK WAS GOOD IAW AMMSDR AWXA200300096Pipe · leakingLAS - EMERGENCY LANDING - EN ROUTE FROM DFW TO LAS ON DECENT THE GREEN HYDRAULIC SYSTEM FAILED. MAINTENANCE FOUND CHAFED HYDRAULIC RETURN LINE IN LT ENGINE PYLON, REPLACED HYDRAULIC LINE LT PYLON. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP DUE TO POSSIBLE CAVISDR AWXA200200842Cable · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND REPLACED CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200675Scavenge Pump · leakingPHX - FLT 0536 - WHILE AIRCRAFT WAS TAXIING TO GATE, THE AIRCRAFT TAXIING BEHIND REPORTED SEEING A TAILPIPE FIRE AT NR 1 ENGINE TAILPIPE. MAINTENANCE PERFORMED A HOT SECTION BORESCOPE PER T/C 15M72304, NO DEFECTS WERE NOTED. AS A PRECAUTION THE NR 1 ENGINE SDR AWXA200200596Engine · fireFLT 0279 - AFTER LANDING AT IAH INBOUND FROM PHX, AFTER ENGINE SHUTDOWN AT GATE, GROUND CREW OBSERVED FIRE IN THE TAILPIPE OF THE NR 1 ENGINE. FLIGHT CREW MOTORED ENGINE APPROXIMATELY 1 MINUTE BEFORE FLAME EXTINGUISHED, ESTIMATE TAILPIPE FIRE LASTED TOTAL OF 2SDR AWXA200200178Power Supply · dischargedYWG - EEL -C- DURING C-08 CHECK EMERGENCY ESCAPE PATH LIGHTING AT ROWS 13, 17, 19, 24 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-401, OPERATIONAL CHECK PERFORMED IAW T/C F1C33301.SDR AWXA200200129Floor Support · corrodedYWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 66 AND FR 67. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 51-74-00, PG 1. REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRICSDR AWXA200200133Seat Track · corrodedYWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT SEAT TRACK Y254 L/H FR 20. MAINTENANCE REMOVED CORROSION FROM FLOOR SUPPORT SEAT TRACK AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPORTSDR AWXA200200132Seat Track · corrodedYWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SEAT TRACK Y765 R/H FR 16. MAINTENANCE REMOVED FLOOR SEAT TRACK Y765 R/H, FABRICATED NEW FLOOR SEAT TRACK AND INSTALLED REPAIR IAW DWG 53112782.SDR AWXA200200131Floor Support · corrodedYWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 15 AND FR 19. MAINTENANCE REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53112782.SDR AWXA200200130Floor Support · corrodedYWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y254 LT BETWEEN FR 15 AND FR 21. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPORT BEAM Y254 LT, FABRSDR AWXA200200181Frame · damagedYWG - MAJOR REPAIR - C - DURING C-08 CHECK TOOLING HOLES AT FR 38-40 LT TO RT WERE FOUND TO BE OVERSIZED. COLD EXPANDED THE HOLES PER SRM 51-48-00, MAINTENANCE DRILLED HOLES TO APPLICABLE DIAMETER, COUNTERSUNK HOLES TO A MAXIMUM OF 0.4MM, INSTALLED FASTENERS SDR AWXA2002TESTIFrame · crackedTESTSDR AWXA2002TESTJFrame · crackedTESTSDR AWXA2002TESTFFrame · crackedTESTSDR AWXA2002TESTCFrame · crackedTESTSDR AWXA200200145Floor Support · corrodedYWG - MAJOR REPAIR - C - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT Y1292 AT FR 66 RT. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW DWG D53472090, AND SRM 51-42-11.SDR AWXA200200167Floor Support · corrodedYWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND AROUND SCREW HOLES ON FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69; FABRICATED A NEW FLOOR SUPPORT AND INSTALLED REPAIRS ISDR AWXA200200166Floor Support · corrodedYWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND ON FORWARD AND AFT FLOOR SUPPORT IN FORWARD CABIN AT Y254, FR 15-19. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER SRM 53-11-14; REMOVED CORRODED FLOOR SUPPORT; FABRICATSDR AWXA200200007Battery · dischargedPHX - EEL - C - DURING INSPECTION ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. NOTE: AIRCRAFT HAS BEEN PARKED SINCE 30 NOVEMBER, 2001. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS 10WL-13WL, ZONES 221, 241, 242, AND 263 IAW AMM 33-51-38,SDR AWXA0001883Warning System · false activationPHX- AIR TURNBACK - FLT 752- AFTER TAKEOFF, ECAM MESSAGE AFT CARGO DOOR APPEARED AND THE AIRCRAFT WAS RETURNED TO PHX. IN PHX MAINTENANCE INSPECTED THE AFT CARGO DOOR TO ENSURE IT WAS FULLY CLOSED AND LOCKED, WHICH IT WAS. THE AFT CARGO DOOR INDICATION WAS PSDR AWXA0001373Fmc · failedPHX - DIVERTED FLIGHT - 2/14/01 - AFTER TAKEOFF FROM LAS TO BOS THE MCDU FROZE IN THE FLIGHT PLAN MODE; RNAV UNAVAILABLE; THE FLIGHT WAS DIVERTED TO PHX. IN PHX MAINTENANCE REPLACED THE LEFT AND RIGHT FMGC; AFTER REPLACEMENT, CURRENT NAV DATA WAS UPLOADED ANDSDR AWXA0001257Actuator · leakingPHX- EMERGENCY LANDING, FLIGHT CREW HAD ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL. AN UNEVENTFUL LANDING WAS MADE. IN PHX MAINTENANCE FOUND THE RT NR 2 SPOILER SERVO CONTROL LEAKING. THE SERVO CONTROL WAS REPLACED AND THE YELLOW HYDRAULIC SYSTEM SESDR AWXA0001019Servo · malfunctionedPHX - AIR TURNBACK - ON CLIMB OUT AND CRUISE AIRCRAFT HAD LEFT WING DOWN 5 TO 7 DEGREES AND RUDDER TRIM 2.8 DEGREES RT. MOST NOTICABLE AT 250 KTS. AND ABOVE; AT 210 KTS. CONDITION LESS NOTICABLE AND AT 170 KTS. FLAP 2 RUDDER TRIM WAS NORMAL AND AIRCRAFT WAS STSDR AWXA0000091Fire Detector · malfuntionedNR 2 ENGINE FIRE LIGHT AND MASTER FIRE LIGHT INDICATED FIRE, NO ECAM, NO MASTER WARNING. ENGINE 2 SHUTDOWN IN-FLIGHT AND BOTH FIRE BOTTLES FIRED. REMOVED AND REPLACED NR 2 FIRE DETECT UNIT, OPS CK GOOD. TT 0003704 M+E = 26-2612-9-0001. REPLACED NR 1 AND 2SDR AWXA9900353Wire · brokenSEAT 9 RT EMERGENCY EXIT LIGHT INOP. REPAIRED WIRING, OPS CK NML.SDR AWXA9900345Oil Cooler · leakingDURING DESCENT WITH POWER AT IDLE, NOXIOUS ODORS EMANATED FROM THE LT PACK, CAPABLE OF EYE AND THROAT IRRITATION. ISOLATED TO LEAKING OIL COOLER. REMOVED AND REPLACED OIL COOLER AND OZONE FILTERS.SDR AWXA9900343Actuator · failedEMERGENCY DECLARED (NOT BY PILOT) ENG NR 1 COMPRESSOR VANE FAULT ON DESCENT, NO OTHER ABNORMAL ENG INDICATIONS OR FAILURES. FIRST TIME FAULT FADEC CONFIRMS 2.5 BLEED ACTUATOR FAIL CURRENT HISTORY.SDR AWXA9900298B Nut · looseAMBER ECAM MESSAGE, CLASS NR 1. YELLOW HYDRAULIC RESERVOIR LOW QUANTITY. FOUND 'B' NUT LOOSE ON YELLOW HYDRAULIC ACCUMULATOR. TIGHTENED NUT. SERVICED SYSTEM WITH APPROXIMATELY 4 GALLONS.SDR AWXA9900243Pack · malfunctionedNOTICEABLE OFFENSIVE ODOR FROM AIR CONDITIONING SYSTEM DURING CLIMB AND DESCENT. LT PACK PRODUCING SMELL. PLACED ON MEL 21-52-01.SDR AWXA9900227Coalescer · dirtyACRID SMELL AFTER TAKEOFF AND INCREASINGLY WORSE THROUGHOUT THE FLIGHT. SMELL INCREASED FROM SMELL ON GROUND. ACCOMPLISHED TSM 21-00-00-801-810 TO CHECK FOR OIL IN THE APU BLEED AIR SYSTEM, BOTH EXTERNALLY AND INTERNALLY. ALL DUCTING REINSTALLED AND BAY SECSDR AWXA9900225Air Dist · odorSTRONG OILY SMELL AFTER TAKEOFF, BELIEVE TO BE PACK SMELL. STILL COULD SMELL AT CRUISE. INSPECTED APU INLET FOR SIGNS OF OIL, NONE FOUND. RAN ENGINES ALTERNATING BLEEDS, SMELL STRONGEST WITH APU BLEED. INSTALLED MEL 49-10-01, CONTROL NR 106292. *S/D* APU
Back to N646AW, cancelled May 10, 2006