N822AW
Service difficulty reports · 195
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 = 'N822AW' AND registry_match = 'registration' 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 = 'N822AW' AND registry_match = 'registration' 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 USAA2012090500064Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON RUDDER NR 4 HINGE FITTING AT STA 206. REPLACED RUDDER HINGE NR 4 IAW A319 SRM 51-42-11 AND A319 AMM 55-36-41-400-001.SDR USAA2012071700014Actuator · faultyON TAKEOFF ROLL AT APPROXIMATELY 70-80 KTS, ENGINE NR 1 COMPRESSOR VANE FAULT. REJECTED TAKEOFF AND SHUT DOWN ENGINE PER ECAM. REMOVED AND REPLACED NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW AIRBUS MAINTENANCE MANUAL 75-00-00-710-031C.SDR USAA2012061900009Bleed Valve · malfunctionedAIRCRAFT REJECTED TAKEOFF WITH ENGINE 1 EPR LOW WITH INDUCED YAW DURING TAKEOFF ROLL AT 30 KNOTS. CHECKED VSV AND LUBED IAW AMM 73-32-42-2 AND CHECKED STAGES 7 AND 10 BLEED VALVES. REPLACED 7A VALVE. COMPLIED WITH HIGH POWER ASSURANCE TEST IAW JOBCARD 26L00SDR USAA2011080400005Slide · low pressureR2 DOOR SLIDE PRESSURE AT 'RED' BAND. REMOVED AND REPLACED R2 DOOR SLIDE AS PER JOBCARD 26L00025010.SDR USAA2010031990611Lens · brokenFLT 34 - LAX - EEL - 8R SEAT EMERGENCY LIGHT LENS BROKEN. MAINTENANCE REPLACED LENS.SDR USAA2009122893431Power Supply · dischargedFLT 574 - PHX-TPA - EMERGENCY LIGHTS - FORWARD EMERGENCY LIGHT POWER SUPPLY UNIT FAULT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD.SDR USAA2009120193272Slide · defectiveNON-ROUTINE: 26C83152002 / 002 / 5001959 - BC6 / BRIDGE CHECK - PIT - EMERGENCY EQUIPMENT - L1 DOOR SLIDE RELEASE CABLE DISCONNECT TO PAWL SAFETY WIRE FOUND TO BE BROKEN AT RELEASE ASSEMBLY UPON RE-INSTALLATION. REMOVED AND REPLACED SLIDE PACK ASSEMBLY.SDR USAA2009081492122Slide · failedFLT 415 - TPA-PHX - R1 SLIDE FAIL EMERGENCY LIGHT CHECK. REMOVED AND REPLACED R1 SLIDE ASSEMBLY PER JOB CARD R1C25305.SDR USAA2009072491906Reservoir · low pressureFLT 312 - BOS - LAS - EMERGENCY EQUIPMENT - CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) FAULT LIGHT IN CRUISE. CIDS TEST MESSAGE SLIDE LOW PRESSURE. REMOVED AND REPLACED LEFT OFF WING ESCAPE SLIDE INFLATION RESERVOIR PER MAINTENANCE MANUAL 25-62-46-401. NO SDR USAA2009071691840Battery · dischargedFLT 204 - OAK - PHX - EMERGENCY LIGHTS - AFT LEFT JUMPSEAT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT LEFT JUMPSEAT EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.SDR USAA2009060191358Battery Pack · dischargedLOGPAGE:4453280 - FLT 496 - PHX-DEN - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHTS "EPSU INTERNAL LOAD EMERGENCY LIGHT, AFT LEFT, ESPU INTERNAL LOAD FORWARD LEFT" MESSAGES WERE PRESENT. REMOVED AND REPLACED BATTERY PACKS FOR EMERGENCY POWER SUPPLY UNITS 11WL ANDSDR USAA920081944Flashlight · inoperativeLOG PAGE 8357407 FLT NR 511 PHX-OMA EMERGENCY LIGHT FLIGHT ATTENDANT FORWARD FLASHLIGHT INOPERATIVE. R&R FLASHLIGHT. OPS CHECK WAS GOOD.SDR AWXA200601918Epsu · dischargedPHX - EEL - EMERGENCY LIGHT SYSTEM TEST FAILS FAULTS 10WL EPSU. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL PER MM 33-51-38-4, OPS CHECK WAS GOOD.SDR AWXA200601497Support · crackedSAL - FOUND CRACK ON OUTBOARD EXTENSION ANGLE SUPPORT ON ENGINE NR 1 PYLON. ANGLE SUPPORT ON ENGINE NR 1 PYLON WAS REPLACED IAW A319 SRM 51-72-11, PAGE 1-2.SDR AWXA200601484Seat Track · wornSAL - WEAR LOCATED ON SEAT TRACK, FR 21 + 15", +Y765 IN MAIN CABIN. REPAIRED SEAT TRACK, FS 21 + 15", +Y765 IN MAIN CABIN IAW A319 SRM 53-00-15 PAGE 211, FIG 202.SDR AWXA200601493Web · corrodedSAL - FOUND CORROSION ON WEB AT FLOOR STRUCTURE IN PASSENGER CABIN, -Y1265 BETWEEN FR 69 TO FS 70. WEB REPLACED IN PASSENGER CABIN FROM FS 69 TO FS 70, -Y1265 IAW SRM 51-72-11, PAGE 1, AND 2.SDR AWXA200601471Floorbeam · corrodedSAL - CORROSION ON FLOORBEAM AT FLOOR STRUCTURE IN PASSENGER CABIN -Y 1165 FS 67 + 14" AND - Y 1265 FS 67 + 3". FLOORBEAM LOC PAX CABIN - Y 1165 FS 66 + 4" TO FS 67 + 15" WAS REPLACED IAW SRM 51-72-11 PAGE 1, 2 DWG D53472040.SDR AWXA200601469Floorbeam · corrodedSAL - FOUND CORROSION ON FLOORBEAM AT FLOOR STRUCTURE IN PAX CABIN - Y 1292 AND FS 66. FLOORBEAM LOCATED ON - Y 1292 FROM FS 64 TO FS 66 + 4" REPLACED IAW SRM 51-72-11.SDR AWXA200601468Floorbeam · corrodedSAL - FOUND CORROSION ON FLOORBEAM OF FLOOR STRUCTURE IN PAX CABIN Y 1292 AND FS 66. FLOOR BEAM LOC PAX CABIN Y 1292 FS 64 TO FS 66 + 4" WAS REPLACED IAW SRM A319 51-72-11 PAGE 1-2.SDR AWXA200601467Shear Plate · corrodedSAL - FOUND CORROSION ON WEB AT FLOOR STRUCTURE IN PAX CABIN Y 1265 AND BETWEEN FS 69 TO FS 70. REPLACED WEB AT FLOOR STRUCTURE IN PAX CABIN Y 1265 AND FS 69 TO FS 70 IAW 51-72-11 PAGE 1 AND 2 SRM.SDR AWXA200601466Floor Support · corrodedSAL - FOUND CORROSION LOCATED ON FLOOR STRUCTURE BEAM FS 16 Y 254 PAX CABIN. PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE BEAM FS 16 Y 254 PAX CABIN IAW SRM A319 53-00-14 PAGE 219 TO 224 FIG 204 SHEET 1.SDR AWXA200601465Seat Track · wornSAL - WEAR ON SEAT TRACK FLOOR STRUCTURE PAX CABIN Y 1292 FR 68 + 5 PERFORMED REPAIR PERMANENT IAW SRM 53-00-15 PAGE 201 TO 206 FIG NR 201 ON SEAT TRACK PAX CABIN Y 1292 FR 63 + 5.SDR AWXA200601464Floor Support · corrodedSAL - FOUND CORROSION ON FLOOR SUPPORT AT FLOOR STRUCTURE IN PAX CABIN, Y 1165 FS 67 + 18" AND -Y 1195, FR 68, FLOOR SUPPORT LOC PAX CABIN - Y 1165 FS 67 + 16" TO FS 69 + 3" WAS REPLACED IAW SRM 51-72-11 PAGE 1 + 2 DWG D53472040.SDR AWXA200601488Floorbeam · corrodedSAL - CORROSION ON FLOORBEAM AT FLOOR SUPPORT STRUCTURE IN PASSENGER CABIN +Y1165 AND FR 67 + 11". FLOORBEAM WAS REPLACED IN PASSENGER CABIN +Y1165 BETWEEN FS 66+5 TO FS 67+15" IAW SRM 51-72-11 PAGE 1 AND 2.SDR AWXA200601478Floor Panel · corrodedCHECK NR BC-4. NR 5953533. CORROSION ON FLOOR PANEL AT RT DOOR IN PASSENGER CABIN BETWEEN FR66 TO FR68. FLOOR PANEL NR 262 FF BETWEEN FR 66 TO FR 68, WAS REPLACED.SDR AWXA200601477Floor Panel · corrodedCHECK NR BC-4. NR 5953532. CORROSION ON FLOOR PANEL AT LT DOOR IN PASSENGER CABIN BETWEEN FR 66 TO FR 68. FLOOR PANEL NO. 261 FF BETWEEN FR 66 TO FR 68, WAS REPLACED.SDR AWXA200601480Seat Track · corrodedSAL - FOUND CORROSION ON SEAT TRACK ON FLOOR STRUCTURE IN PASSENGER CABIN +Y1292, AND FS 42+17", FS 43+919", FS 44+7", FS 45+19", FS 41+10". SEAT TRACK LOCATED BETWEEN FR 41 TO 47/51 WAS REPLACED IAW SRM A319 51-72-11 PAGE 1 TO 2.SDR AWXA200601476Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM AT FLOOR STRUCTURE IN PASSENGER CABIN, +Y1215, FS 68. FLOORBEAM AT FLOOR STRUCTURE IN PASSENGER CABIN +Y1215, BETWEEN FS 68-4" TO FS 69+3". MAINTENANCE REPLACED IAW A319 SRM 51-72-11, PAGE 1 TO 2.SDR AWXA200601475Seat Track · corrodedSAL - CORROSION FOUND ON SEAT TRACK ON FLOOR STRUCTURE IN PASSENGER CABIN -Y765, AND FS 41+11", FS 45+18". SEAT TRACK LOCATED BETWEEN FS 41 TO FS 46+16" -Y765. PASSENGER CABIN WAS REPLACED IAW SRM A319 51-72-11.SDR AWXA200601474Seat Track · corrodedSAL - CORROSION ON SEAT TRACK ON FLOOR STRUCTURE IN PASSENGER CABIN, +Y1292, FS 37, FS 38+5", FS 40. MAINTENANCE REPLACED SEAT TRACK FROM FRAME 36 TO FS 41 IN PASSENGER CABIN, +Y1292 IAW A319 SRM 51-72-11, AND INSTALLED FASTENER IAW A319 SRM 51-42-11.SDR AWXA200601499Floor Panel · debondedSAL - THE FLOOR PANEL NR 151 PE IN THE AFT CARGO COMPARTMENT WAS FOUND WITH THE DOUBLER DISBONDED. THE FLOOR PANEL NR 151 PE, AND THE DOUBLER WAS FABRICATED AS PER IRM 9701 REV F, PAR 8. THE DOUBLER WAS FABRICATED IAW AWA CARD M2M53301, SRM 53-02-00 PARA 8GHSDR AWXA200601498Floor Panel · debondedSAL - THE FLOOR PANEL NR 131AF IN THE FWD CARGO COMPARTMENT WAS FOUND WITH THE DOUBLER DISBONDED. THE FLOOR PANEL NR 131 AF, AND THE DOUBLER WAS FABRICATED AS PER IRM 9701, REF F, PAR 8. THE DOUBLER WAS FABRICATED IAW AWA CARD M2M53301, SRM 53-02-00, PARA 8GSDR AWXA200601473Sill · corrodedSAL - FOUND CORROSION ON LOWER SILL AT PASSENGER CABIN -Y1442, AND FS 66. PERFORMED PERMANENT REPAIR ON LOWER SILL FS 66, - Y1442, PASSENGER CABIN IAW A319 SRM 53-41-14, FIG 201 SHEET 4.SDR AWXA200600846Solenoid Valve · malfunctionedLAS - DURING CLIMB THRU FL210, ENG 2 STALL IND RECEIVED ON ECAM WITH ASSOCIATED YAW. NR 2 ENG EPR FLUX FROM 1.37 TO 1.1 SEVERAL TIMES RAPIDLY. 1 MIN LATER RECEIVED ACARS FAULT MSG, "VSV/BLD VLVE/LPC2". MX PERFORMED BORESCOPE OF A5 ENG HPC IAW AWA TASK CARD SDR AWXA200501181Valve · malfunctionedPDURING TAXI OUT, PARKING BRAKE WOULD NOT RELEASE BRAKE PRESSURE. CREW CYCLED CIRCUIT BREAKERS PER MOC WITH NO HELP. MAINTENANCE WENT OUT TO THE AIRCRAFT AND MANUALLY BLED OFF BRAKE PRESSURE. AIRCRAFT TOWED TO GATE WITHOUT FURTHER EVENT. MAINTENANCE PREFORSDR AWXA200501131Flashlight · dischargedPHX - EEL - DURING 4 DAY CHECK, DISCOVERED THE AFT FLIGHT ATTENDANT INBOARD FLASHLIGHT DIM. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT INBOARD EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200500722Engine · malfunctionedDURING TAKEOFF AT T/O POWER SETTING, APPROX 1.04 EPR, ACFT VEERED LEFT. REJECTED TAKEOFF BEFORE FURTHER POWER. NO ABNORMAL INDICATIONS NOTED BUT SUSPECTED NR 1 ENG LAGGED NR 2 ENG IN SPOOLING UP. RAN ENGINES UP TO 70 PERCENT N1 PER MAINTENANCE CONTROL. ALLSDR AWXA200500445Outflow Valve · malfunctionedON CLIMB OUT OF PHX EN ROUTE TO ABQ WHILE PASSING THROUGH 800 FT RECEIVED ECAM WARNING FOR AVIONICS VENT SYSTEM FAULT, TURNED BACK TO PHX FOR REPAIR. ISSUED MEL 21-26-04, COND. 1 "SKIN AIR OUTLET VALVE". MAINTENANCE REMOVED AND REPLACED SKIN AIR OUTLET VALVE 2SDR AWXA200401077Computer · malfunctionedDURING CLIMB-OUT OF LAS EN ROUTE FOR PHL AT 7000 FT, RECEIVED ECAM WARNING AVIONICS VENT SKIN AIR VALVE FAULT, FOLLOWED ECAM INSTRUCTIONS THAT RESULTED WITH AN ECAM VENT BLOWER FAULT AND VENT EXTRACT FAULT, AS A RESULT LOST WEATHER RADAR, TURNED BACK TO LAS ANSDR AWXA200400159Warning Light · illuminatedLAS - ABORTED TAKEOFF - FLT 0108 - DURING TAKEOFF AT LAS EN ROUTE FOR LAX RECEIVED ECAM MESSAGES FOR VENT SKIN VALVE FAULT AND VENT AVIONICS SYSTEM FAULT, REJECTED TAKEOFF AT 70 KTS. MAINTENANCE RESET THE AEVC SYSTEM, OPERATIONAL CHECK WAS GOOD IAW AMM TASK 2SDR AWXA200301446Light · inoperativeLAX - EEL - DURING 8-DAY CHECK AT LAX EMERGENCY LIGHT ON LT FORWARD PARTITION FLOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED & REPLACED EMERGENCY LIGHT AT LT FORWARD PARTITION FLOOR, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200774Bearing · failedSTL - DIVERSION - FLT 0695 - EN ROUTE FROM CMH TO LAX THE NR 2 ENGINE COMPRESSOR STALLED TWO TIMES AT FL 370, EGT RED LINED AND OIL PRESSURE PEAKED AT 330 PSI THEN SLOWLY DROPPED TO -0- PSI, SHUTDOWN ENGINE PER ECAM INSTRUCTIONS AND DIVERTED TO STL. ENGINE ISSDR AWXA200200090Outflow Valve · malfunctionedWHILE ENROUTE FROM PHX TO RNO AIRCRAFT EXPERIENCED A CABIN PRESSURE CONTROLLER (CPC) SYSTEM NR 1 FAULT AND A FLUCTUATION OF PLUS OR MINUS 2000 FEET PER MINUTE OPERATION IN MANUAL MODE. ON THE PREVIOUS FLIGHT CPC SYSTEM NR 2 WAS PLACED ON MEL 21-31-01 CONDITIONSDR AWXA0002205Relief Valve · rupturedMCI- UNSCHEDULED LANDING - FLT 77 - ON CLIMBOUT FROM BOS EN ROUTE TO PHX ECAM MESSAGE FOR FUEL AUTO FEED FAULT APPEARED, CREW DESELECTED AUTO AND MONITORED THE FUEL PAGE. ALL FUEL WAS BEING USED FROM LT MAIN TANK WITH X-FEED CLOSED. WITH LEFT PUMPS OFF FUEL SDR AWXA0001256Outflow Valve · malfunctionedCMH-DIVERTED FLIGHT- ON CLIMBOUT THE CABIN PRESSURE RATE FLUCTUATED FROM -600 FPM TO +1400 FPM. PRESSURIZATION SYSTEM 1 FAILED. AUTO SWITCH TO SYSTEM 2 AND CABIN PRESSURE FLUCTUATIONS CONTINUED. THE OUTFLOW VALVE CYCLED CONTINOUSLY, EVEN IN LEVEL FLIGHT AT
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