N664AW
Service difficulty reports · 234
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 = 'N664AW' 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 = 'N664AW' 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 USAA2010121393025Lens · missingFLT 12 - SMF-PHX - EMERGENCY LIGHTS - RED EMERGENCY FLOOR LIGHTING EXIT LENS MISSING FROM FORWARD BULKHEAD. REPLACED EMERGENCY LIGHT LENS PER AMM 33-51-13. OPERATIONAL CHECK WAS GOOD.SDR USAA2010120992937Epsu · inoperativeFLT 77 - EMERGENCY POWER SUPPLY UNIT (10WL) FAULT. MAINTENANCE REMOVED AND REPLACED THE EPSU IAW AIRBUS MAINTENANCE MANUAL 33-51-38.SDR USAA2010120992936Wire · shortedFLT 77-SEA - EEL - FIRST CLASS DIVIDER EMERGENCY LIGHT WIRES SHORTED. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY IAW ELECTRICAL STANDARD PRACTICES MANUAL 20-48-25.SDR USAA2010112692666Light · missingFLT 77 - SEA - EEL - RED WALL-MOUNTED EMERGENCY LIGHT ASSEMBLY IS MISSING FROM LEFT WINDSCREEN. MAINTENANCE INSTALLED RED WALL-MOUNTED EMERGENCY LIGHT ASSEMBLY IAW AIRBUS MAINTENANCE MANUAL 33-51-18.SDR USAA2010110192461Lens · missingFLT 552 - MCO-PHL - EMERGENCY LIGHTS - ROW 9 EMERGENCY EXIT LIGHT LENS MISSING. REPLACED ROW 9 EMERGENCY LIGHT LENS AS REQUIRED.SDR USAA2010083091860Hinge Fitting · wornMAJOR REPAIR - ELONGATED HOLE & WEAR AT NR 2 HINGE FITTING OF LEFT AFT NOSE LANDING GEAR DOOR ASSEMBLY BETWEEN FR18 TO FR20 & BETWEEN S39R TO S40R, Y440. REPLACED NR 2 HINGE FITTING OF LEFT AFT NOSE LANDING GEAR DOOR ASSEMBLY BETWEEN FR18 TO FR20 & BETWEEN S3SDR USAA2010083091859Hinge Fitting · wornSAL - C6 - MAJOR REPAIR - ELONGATED HOLE & WEAR AT NR 2 HINGE FITTING OF RIGHT AFT NOSE LANDING GEAR DOOR ASSEMBLY BETWEEN FR18 TO FR20 & BETWEEN S39R TO S40R, -Y440. REPLACED NR 2 HINGE FITTING OF RIGHT AFT NOSE LANDING GEAR DOOR ASSEMBLY BETWEEN FR18 TO FR2SDR USAA2010083091862Hinge Fitting · wornSAL - C6 - MAJOR REPAIR - ELONGATED HOLE & WEAR AT NR 1 HINGE FITTING OF RIGHT AFT NOSE LANDING GEAR DOOR ASSEMBLY BETWEEN FR18 TO FR20 & BETWEEN S39R TO S40R, -Y440. REPLACED NR 1 HINGE FITTING OF RIGHT AFT NOSE LANDING GEAR DOOR ASSEMBLY BETWEEN FR18 TO FR2SDR USAA2010083091861Hinge Fitting · wornMAJOR REPAIR - ELONGATED HOLE & WEAR AT NR 1 HINGE FITTING OF LEFT AFT NOSE LANDING GEAR DOOR ASSEMBLY BETWEEN FR18 TO FR20 & BETWEEN S39R TO S40R, Y440. REPLACED NR 1 HINGE FITTING OF LEFT AFT NOSE LANDING GEAR DOOR ASSEMBLY BETWEEN FR18 TO FR20 & BETWEEN SSDR USAA2010082691815Bellcrank · out of adjustSAL - C6 - MAJOR REPAIR - OUT OF ADJUSTMENT IS DIMENSION "A" BETWEEN STRIKER LEVER & DAMPER MECHANISM AT R-2 DOOR. PERFORMED DIMENSION "A" BETWEEN STRIKER LEVER & DAMPER MECHANISM AT R-2 DOOR IAW A320 AMM 52-13-14-820-002.SDR USAA2010082691814Bellcrank · out of adjustSAL - C6 - MAJOR REPAIR - OUT OF ADJUSTMENT RIGGING POINT TORSION BAR BELLCRANK (COMPENSATION MECHANISM) AT R-2 DOOR. PERFORMED ADJUSTMENT RIGGING POINT TORSION BAR BELLCRANK (COMPENSATION MECHANISM) AT R-2 DOOR IAW A320 AMM 52-13-21.SDR USAA2010082691813Bellcrank · out of adjustSAL - C6 - MAJOR REPAIR - OUT OF ADJUSTMENT RIGGING POINT TORSION BAR BELLCRANK (COMPENSATION MECHANISM) AT R-1 DOOR. PERFORMED ADJUSTMENT RIGGING POINT TORSION BAR BELLCRANK (COMPENSATION MECHANISM) AT R-1 DOOR IAW A320 AMM 52-11-21.SDR USAA2010083091863Hinge Fitting · excess playSAL - C6 - MAJOR REPAIR - EXCESSIVE PLAY ON NR 1 RUDDER HINGE FITTING. REPLACED NR 1 RUDDER HINGE FITTING ASSEMBLY IAW A320 SRM 51-72-11.SDR USAA2010082691816Fitting · excess playSAL - C6 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 2 RUDDER HINGE FITTING. REPLACED NR 2 RUDDER HINGE FITTING IAW A320 AMM 51-72-11.SDR USAA2010010890050Cylinder · defectiveFLT 493 - DEN - EES - R2 DOOR DAMPER CYLINDER FAILS TO HOLD CHARGE. MAINTENANCE REPLACED R2 DOOR DAMPER CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-13-14.SDR USAA2009091892563Valve · stuckFLT 12 - PHX - RETURN TO FIELD - CREW RECEIVED ENGINE NR 1 BEARING 4 SYSTEM HIGH PRESSURE FAULT. AFTER RECEIVING A SECOND ACARS MESSAGE OF OIL QUANTITY SLOWLY DROPPING, CREW ELECTED TO RETURN TO PHX. MAINTENANCE FOUND THE SCAVENGE VALVE STUCK CLOSED. REMOVESDR USAA2009060891420Indicator · faultyFLT 181 - PHX - EMERGENCY EGRESS SYSTEM - R-2 DOOR SLIDE FAILS STEP 17 PAGE 14 OF 34 CARD R1C25311 "TEST THE DOOR MOUNTED "CABIN PRESSURE" INDICATOR. MAINTENANCE RELAMPED CABIN PRESSURE INDICATOR PER STANDARD PRACTICES. RETESTED SYSTEM - OPERATIONAL CHECK NOSDR USAA920081539Pump · inoperativeFLT 438 TPA-LAS - EMERGENCY LANDING - CREW REPORTED `HYD G RSVR LO LVL` AND `HYD G ENG 1 PUMP LOW PR` INDICATIONS. AN EMERGENCY WAS DECLARED DUE TO POSSIBLE LOSS OF NOSE WHEEL STEERING ON LANDING. THE ACFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. SDR AWXA200700536Sill · corrodedSAL - FOUND CORROSION ON BULK CARGO DOOR LOWER SILL, FR 60 - FR 61, -Y625 TO -Y680. REPAIRED BULK CARGO DOOR LOWER SILL, FR 60 - FR 61, -Y625 TO -Y680 IAW A320 SRM 53-41-49.SDR AWXA200700535Dummy Rail · corrodedSAL - FOUND CORROSION ON MAIN CABIN DUMMY RAIL, FR12 - FR16, +Y503.2. REPLACED MAIN CABIN DUMMY RAIL, FR12 - FR16, +Y503.2 IAW A320 SRM 51-42-11.SDR AWXA200700526Floor Panel · corrodedSAL - CORROSION ON AFT LAV AND GALLEY FLOOR PANEL 261 FF, FR 66 - FR 68. REPLACED AFT LAV AND GALLEY FLOOR PANEL 261 FF, FR 66 - FR 68 IAW A320 SRM 51-72-11.SDR AWXA200700525Floor Panel · corrodedSAL - CORROSION ON AFT LAV AND GALLEY FLOOR PANEL 262 FF, FR 66 - FR 68. REPLACED AFT LAV AND GALLEY FLOOR PANEL 262 FF, FR 66 - FR 68 IAW A320 SRM 51-72-11.SDR AWXA200700522Seat Track · corrodedSAL - FOUND CORROSION ON CABIN RAIL SEAT/FLOORBEAM, FR 64 TO FR 66, -Y1292. REPLACED CABIN RAIL SEAT/FLOORBEAM, FR 64 TO FR 66, -Y1292 IAW A320 SRM 51-72-11.SDR AWXA200700521Floorbeam · corrodedSAL - FOUND CORROSION ON CABIN FLOORBEAM, FR 66 TO FR 67, - Y1162 TO -Y1292. REPLACED CABIN FLOORBEAM, FR 66 - FR 67, -Y1162 TO -Y1292 IAW A320 SRM 51-72-11.SDR AWXA200700520Floorbeam · corrodedSAL - CORROSION ON CABIN FLOORBEAM, FR 68 - 6" TO FR 69, - Y1162. REPLACED CABIN FLOORBEAM , FR 68 - FR 69, -Y1162 IAW A320 SRM 51-72-11.SDR AWXA200700519Floorbeam · corrodedSAL - CORROSION ON CABIN FLOORBEAM, FR 66 + 6" TO FR 67 + 17", + Y1162 TO +Y1292. REPLACED CABIN FLOORBEAM, FR 66 - FR 68, +Y1162 TO +Y1292 IAW A320 SRM 51-72-11.SDR AWXA200700518Floorbeam · corrodedSAL - FOUND CORROSION ON CABIN FLOORBEAM, FR 68.6" TO FR 69 + 3", + Y1162. REPLACED CABIN FLOORBEAM, FR 68 - FR 69 + 3", +Y1162 IAW A320 SRM 51-72-11.SDR AWXA200700527Floorbeam · corrodedSAL - FOUND CORROSION ON MAIN CABIN FLOORBEAM, FR 66 + 6" TO FR 70, -Y765. REPLACED MAIN CABIN FLOORBEAM, FR 66 + 6" TO FR 70, -Y765 IAW A320 SRM 51-72-11.SDR AWXA200600596Bleed Valve · malfunctionedFLL - FLT 771 - CREW REPORTED THAT AT 5000 FT, NR 1 ENGINE STALLED, EPR ROLLED BACK TO IDLE AND CAPT PULLED THROTTLE BACK THEN WHEN ENG RECOVERED PUT THROTTLE BACK IN CLIMB DETENT. CREW RETURNED TO FLL AND LANDED W/O FURTHER EVENT. MX PERFORMED BOROSCOPE IAWSDR AWXA200600569Bleed Valve · malfunctionedDURING CLIMB-OUT, APPROX 8500' REPORTED NR 1 ENG COMPRESSOR STALL WITH A LOUD BANG, FIREBALL, & EPR DROP TO NEARLY "0" THEN RECOVERY. REPORTED ECAM ANNUNCIATED "COMPRESSOR STALL" THEN CLEARED AS ENG RESUMED NORMAL OPS. RETURNED TO ATL. MX T/S IAW AIRBUS 320SDR AWXA200600153Proximity Sensor · faultyPHX - AIR TURN BACK - FLT 632 - AFTER T/O CREW REPORTED THAT THE GEAR WAS NOT UP AND LOCKED. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE FAULT OCCURRED ON THE LGCIU SYSTEM 2 AND THE ECAM INDICATION FOR THE RT MLG DOORSDR AWXA200500483Actuator · leakingON DESCENT, RECEIVED ECAM MESSAGE FOR NR 1 ENGINE HYDRAULIC PUMP POW PRESSURE/ GREEN SYSTEM LOW PRESSURE, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. UPON ARRIVAL AT GATE MAINTENANCE FOUND HYDRAULIC FLUID DRIPPING FROM THE TAIL SECTION, APPLIED HYDRASDR AWXA200400847Poppet Valve · wornAFTER TAKEOFF FROM PHX EN ROUTE FOR IAH, HEARD A LOUD AIR NOISE IN CABIN AND RATE OF CLIMB INCREASED TO 1000 FT PER MINUTE. HAD NO AIRFLOW IN COCKPIT, TURNED OFF RT PACK PER MX CONTROL, THERE WAS NO INCREASE IN FLOW FROM LT PACK, WHEN HIGH PRESSURE VALVES OPESDR AWXA200300969Seal · tornDURING CLIMB OUT OF LAS EN ROUTE FOR BWI RECEIVED ECAM WARNING FOR GREEN HYD SYS LOW PRESSURE. TURNED OFF GREEN HYDRAULIC PUMP AND TURNED ON POWER TRANSFER UNIT, THEN RECEIVED ECAM MESSAGE FOR LOW GREEN HYDRAULIC QUANTITY WHICH WAS FOLLOWED BY A YELLOW HYDRAUL
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