N660AW
Service difficulty reports · 389
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 = 'N660AW' 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 = 'N660AW' 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 USAA920080433Control Unit · failedPHX - EE - FLT 320 - MX REPORTED SMOKE CARGO LAV FAULT MESSAGE ILLUMINATED. MX REPLACED THE SMOKE DETECTOR CONTROL UNIT (SDCU) 10WQ. OPERATIONAL TEST WAS GOOD.SDR AWXA200700805Bracket · crackedPHX - MAJOR REPAIR - NR 7770898, KEEL BEAM AFT INBOARD CORNER BRACKET (CONNECTION SECTION) CRACKED, FR 40/BS 1753, S42R INSIDE YELLOW HYDRAULIC BAY. REPLACED KEEL BEAM AFT INBOARD CORNER BRACKET (CONNECTION SECTION), FR 40/BS 1753, S42R INSIDE YELLOW HYDRAULSDR AWXA200700130Power Supply · failedPHX - EEL - MID CABIN EMERG LIGHTS INOP. MX REMOVED AND REPLACED EMERG PWR SUPPLY AND BATTERY. OPS CHECK WAS GOOD.SDR AWXA200700095Power Supply · failedPHX - EEL - EMERGENCY LIGHTS ILLUMINATE WHILE EMER LT CB AT HA6 ON PNL 49VU (OVERHEAD) IS PULLED WHILE THE EMERG EXIT LT SWITCH IS OFF. MX REMOVED AND REPLACED ESPU PLUS BATTERY PACK AT RIGHT MID CABIN (12WL). EMERGENCY LIGHTS OPS CK GOOD.SDR AWXA200602064Unknown · smokePHX - SMOKE - AFTER ALL THE PASSENGERS HAD BEEN DEPLANED, SMOKE WAS REPORTED COMING FROM THE APU TAILPIPE. EMERGENCY EQUIPMENT WAS DISPATCHED. MAINTENANCE INSPECTED APU TAILPIPE AND FOUND NO DAMAGE. MAINTENANCE FOUND TANK VENT LINE DRAINS (AFT ONE) NOT ALIGSDR AWXA200601525Slide · unwanted deployBWI - EE - LOG - 7378779 - WHILE ON BOARD THE AIRCRAFT, THE CLEANERS DEPLOYED THE R1 DOOR SLIDE. MAINTENANCE REPLACED THE R1 DOOR SLIDE IAW R1C25305.SDR AWXA200501494Duct · leakingECAM MESSAGE "AIR R WING LEAK". UNABLE TO DEFER DUE TO WEATHER. RETURNED & LANDED W/O INCIDENT. MX PERFORMED LEAK CHK & ENG RUNS. R&R RT CLAMP ON CROSS BLEED VALVE IAW MM. R&R SEAL ON RT WING LE, INBD OF BLEED DUCT. FOUND NR 2 PYLON AIR LEAK AT AFT CLAMPSDR AWXA200501488Floor Panel · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL TWO GALVANIC CORROSION ON 131HF FWD CARGO FLOOR PANEL UPPER SURFACE. CORROSION WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-02-00 TABLE 105. REPLACEMENT PANEL FABRICATED IAW IRM 9701 REV F PAR 8. INSTALLED REPAIR PARSDR AWXA200501487Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON RT INBOARD SEAT TRACK AT FS 38+11". MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 40 IAW AIRBUS 320 SRM 51-42-11.SDR AWXA200501475Pin · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE HINGE PIN FOR THE OUTBOARD SIDE OF THE NR 4 SPOILER. MAINTENANCE REMOVED AND REPLACED THE HINGE PIN, ON THE NR 4 SPOILER IAW AIRBUS 320 AMM 27-64-44-04.SDR AWXA200501476Plate · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON SHEAR PLATE LOCATED BETWEEN FS 69 AND FS 70, Y1162. NO ALLOWABLE DAMAGE LIMITS WERE FOUND. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE BETWEEN FS 69 AN FS 70, Y1162 IAW BOEING 737-300 SRM 51-72-11.SDR AWXA200501459Seat Track · corrodedDURING BC-4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BEAM AT FR66 AND Y1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED AND INSTALLED SEAT RAIL BEAM IAW SRM 51-42-11 FROM FR64 TO FR66 AND Y1292.SDR AWXA200501455Floorbeam · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION SPREAD OUT ON FLOORBEAM BETWEEN FS 16 AND FS 20, Y-1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14. REMOVED AND INSTALLED FLOORBEAM IAW AIRBUS SRM 51-42-11 FROM FS 12 TO FS 24 AND SDR AWXA200501449Dummy Rail · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON DUMMY RAIL LOCATED AT FS 16-2" AND Y503.2. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14. REMOVED AND INSTALLED NEW DUMMY RAIL IAW AIRBUS SRM 51-42-11 FROM FS12 TO FS 16 AND Y503.2.SDR AWXA200501448Floor Support · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON LONGITUDINAL BEAM LOCATED AT FS 68-10" AND Y-1162. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED AND INSTALLED NEW BEAM IAW AIRBUS SRM 51-42-11 FROM FS 66 TO FS 68 AND Y-11SDR AWXA200501445Floor Support · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON LONGITUDINAL BEAM LOCATED AT FS 68 AND Y-1162. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED AND INSTALLED NEW BEAM IAW AIRBUS SRM 51-42-11 AT FS 68 AND Y-1162.SDR AWXA200501477Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FS 58+13" AND Y1292. MAINTENANCE CUT OUT DAMAGED PORTION OF SEAT TRACK FROM FS 58+8" TO FS 59, Y1292 IAW AIRBUS 320 SRM 53-00-15 FIG 201 PAGE 205. FABRICATED L-PROFILE. INSTALLED NEW SECTISDR AWXA200501454Seat Track · corrodedSAL - MAJOR REPAIR - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FR41+3" AND Y1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FR41 TO FR36 AND Y1292.SDR AWXA200501453Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FS 40+14" AND Y765. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FS 36 TO FS 41 AND Y765.SDR AWXA200501452Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FS 38+8 AND Y-1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FS 36 TO FS 41 AND Y-1292.SDR AWXA200501451Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON RT INBOARD SEAT TRACK AT FS 46+14 AND Y-765. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FS 41 TO FS 47 AND Y-765.SDR AWXA200501450Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FS 46+13 AND Y-1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FS 41 TO FS 47 AND Y-1292.SDR AWXA200501447Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE LT OUTBOARD SEAT TRACK AT FS 36 AND Y1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED LT OUTBOARD SEAT TRACK FROM FS 36 TO FS 41 AND Y1292.SDR AWXA200501446Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE LT INBOARD SEAT TRACK AT FS 46+12 AND Y765. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED LT INBOARD SEAT TRACK FROM FS 41 TO FS 47 AND Y765.SDR AWXA200401133Power Supply · faultyLAX - EEL - DURING 4-DAY CHECK, FOUND THE RT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.SDR AWXA200400056Computer · malfunctionedJFK - AIR TURNBACK - FLT 0011 - AFTER TAKEOFF FROM JFK EN ROUTE TO PHX RECEIVED A DUAL FLIGHT MANAGEMENT GUIDANCE COMPUTER FAIL AND IR 3 FAULT, TURNED BACK TO JFK. MAINTENANCE PERFORMED A COMPLETE SYSTEM RESET. PERFORMED AUTO FLIGHT SYSTEM TEST IAW AMM 22-46SDR AWXA200301061Engine · malfunctionedON TAKEOFF AT PHX EN ROUTE FOR BWI NR 2 ENGINE DID NOT PRODUCE FLEX TAKEOFF POWER, EPR ONLY REACHED 1.2, EPR OF 1.4 REQUIRED, REJECTED TAKEOFF AT 78 KTS. MAINTENANCE PERFORMED A HIGH POWER ASSURANCE TEST IAW T/C F5M71312, NO FAULTS WERE NOTED, NR 2 ENGINE EPR SDR AWXA200300789Monitor · malfunctionedON TAKEOFF ROLL AT LAS EN ROUTE FOR LAX THE LT OUTBOARD BRAKE INDICATOR SPIKED TO 610 DEGREES CELSIUS, AND THE LT INBOARD TO 330 DEGREES CELSIUS. REJECTED TAKEOFF UNDER 60 KTS. MAINTENANCE REMOVED AND REPLACED THE LT BRAKE TEMPERATURE MONITOR IAW AMM 32-47-1SDR AWXA200300014Actuator · inoperativeFLT 0660, ON TAKEOFF ROLL EN ROUTE RECEIVED ECAM MESSAGE (ENG 1 COMPRESSOR VANE); REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75306. LUBRICATED VSV, PERFORMED MAINTENANCSDR AWXA200200845Bleed Valve · lack of lubePHX - ABORTED TAKEOFF - FLT 0014 - ON TAKEOFF FROM PHX EN ROUTE FOR JFK THE NR 2 ENGINE EGT EXCEEDED LIMITATIONS, ABORTED TAKEOFF AT APPROXIMATELY 80 KTS. MAINTENANCE DOWNLOADED PREFLIGHT REPORT AND PERFORMED TROUBLESHOOTING TASKS 77-00-00-810-844 INSPECTION SDR AWXA200200746Pump · failedORD - ABORTED TAKEOFF - FLT 0060 - ON TAKEOFF FROM ORD EN ROUTE FOR PHX RECEIVED ECAM INDICATION FOR NR 2 ENGINE COMPRESSOR VANE FAULT. ABORTED TAKEOFF AT 60 KTS.SDR AWXA200200589Filter · contaminatedPHX - AIR TURNBACK - FLT 0256 - WHILE CLIMBING OUT OF PHX EN ROUTE FOR PHL RECEIVED ECAM CAUTION AIR ENGINE NR 1 BLEED FAULT, BLEED TEMPERATURE EXCEEDED 300 DEGREES, TURNED BACK TO PHX DUE TO POSSIBLE ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED THE NR SDR AWXA200200380Power Supply · dischargedATL - EEL - DURING INSPECTION EMERGENCY POWER SUPPLY UNIT 12WL WAS FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD.SDR AWXA0001109Wire · brokenEMERGENCY LIGHT AT SEAT 1B INOP. FOUND AND REPAIRED BROKEN WIRE AT SEAT 1BSDR AWXA0001024Frame · dentedFRAME 23 DENTED AND DEFORMED AT STR 22L. REWORKED FRAME AND NDT IAW SRM 51-73-00SDR AWXA0001023Skin · damagedD: EXT. SKIN AT FRAME 23L AND STR 22L HAS DAMAGED RIVETS. REPLACED FASTENERS WITH DOUBLER IAW SRM 51-42-11SDR AWXA0001022Stringer · dentedSTR 22L AT FRAME 23 DENTED. REWORKED STR IAW SRM 51-73-00 AND NDT IAW SRM 51-10-08SDR AWXA0001021Shear Tie · crackedSKIN SHEAR TIE AT FRAME 23L AND STR 22L CRACKED .200 IN LOWER TWO RADIUS. CLEAT FABED, HEAT TREATED AND INSTALLED IAW SRM 51-26-11SDR AWXA0001020Skin · dentedSKIN DENTED AT STA 8966 FRAME 23 AND STR 20 JUST BEHIND L1 DOOR; DENTED 8X3 .115 AT DEEPEST SPOT. REPAIR CARRIED OUT IAW SRM 53-00-11 FIG 202/203
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