N652AW
Service difficulty reports · 289
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 = 'N652AW' 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 = 'N652AW' 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 USAA920081220Seat Track · corrodedSAL - C7 - MAJOR REPAIR - NR 61075158 - CORROSION ON SEAT RAIL ASSEMBLY BEAM AT FR 64 TO FR 66, BL Y1292. REPAIRED CORROSION ON SEAT RAIL ASSY BEAM AT FR 64 TO FR 66, BL Y1292 IAW SRM 51-72-11. (K)SDR AWXA200700242Fitting · corrodedSAL-MAJOR REPAIR- BC-6 CHECK- FOUND CORROSION ON CENTRAL FITTING AROUND R1 DOOR CUT OUT FLOOR LEVEL, FR 16 - FR 20, S23R. REPLACED CENTRAL FITTING ON R1 DOOR CUT OUT FLOOR LEVEL, FR16 - FR20, S23R IAW A320 SRM 51-72-11.SDR AWXA200700244Frame · corrodedSAL - FOUND CORROSION ON SUPPORT FRAME, FR 69 - FR 70, S-23R. REPLACED SUPPORT FRAME LOCATED ON , FR 69 - FR 70, S-23R, IAW A320 SRM 51-72-11, PAGE 1, 2 AND 51-42-11.SDR AWXA200700241Shear Plate · corrodedSAL- MAJOR REPAIR- BC-6 CHECK- FOUND CORROSION ON RIGHT CABIN FLOOR SHEAR PLATE, FR 69 - FR 70, S-23R. REPLACED RIGHT CABIN FLOOR SHEAR PLATE, FR 69 - FR 70, S-23R IAW A320 SRM 51-71-11, PAGE 1-2 AND 51-42-11 PAGE 23, FIG 8.SDR AWXA200700239Fitting · corrodedSAL- MAJOR REPAIR - BC-6 CHECK - FOUND CORROSION ON L1 DOOR CUT OUT FLOOR LEVEL CENTRAL FITTING, FR 16 - FR 20, S-23L. REPLACED L1 DOOR CUT OUT FLOOR LEVEL CENTRAL FITTING, FR 16- FR 20, S-23L, IAW A320 SDR 51-42-11 AND 51-72-11.SDR AWXA200700238Beam · corrodedSAL- MAJOR REPAIR - FOUND CORROSION ON MAIN CABIN LONGITUDINAL BEAM, +Y1292, FR 66 +5" - FR 67 + 15". REPLACED MAIN CABIN LONGITUDINAL BEAM, +Y1292, FR 66 +5" - FR 67 + 15" IAW A320 SRM 51-72-11 PAGE 1 AND 2.SDR AWXA200700216Sill · corrodedSAL - FOUND CORROSION ON MAIN CABIN SILL BEAM, +Y1732, FR 67+16". REPAIRED MAIN CABIN SILL BEAM, +Y1732, FR 67+16" IAW A320 SRM 53-41-14.SDR AWXA200700243Floorboard · corrodedSAL- MAJOR REPAIR - FOUND CORROSION ON MAIN CABIN FLOORBOARD 221FF, FR 16 - FR 20, +Y1292 TO +Y1732. REPLACED MAIN CABIN FLOORBOARD 221FF, FR 16 - FR 20, +Y1292 TO +Y1732, IAW A320 ARM 51-72-11 AND AWA TASK CARD CIC53302.SDR AWXA200700237Beam · corrodedSAL- MAJOR REPAIR - FOUND CORROSION ON MAIN CABIN LONGITUDINAL BEAM AT -Y1292, FR 68 - FR 69. REPLACED MAIN CABIN LONGITUDINAL BEAM AT -Y1292, FR 68 - FR 69, IAW A320 SRM 51-72-11.SDR AWXA200700217Floor Support · corrodedSAL - FOUND CORROSION ON MAIN CABIN LONGITUDINAL BEAM, -Y1292, FR 66 + 4" TO FR 68 - 4". REPLACED MAIN CABIN LONGITUDINAL BEAM, -Y1292, FR 66 + 4" TO FR 68 - 4" IAW A320 SRM 51-72-11.SDR AWXA200700228Floorboard · corrodedSAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732. REPLACED MAIN CABIN FLOORBOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53303.SDR AWXA200700218Floor Panel · corrodedSAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD 262 FF, FS 66 - FS 68, -Y1292 TO -Y1732. REPLACED MAIN CABIN FLOORBOARD 262 FF, FS 66 - FS 68, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53303.SDR AWXA200600239Pin · corrodedPHX - DURING ENGINEERING MODIFICATION, M4L32101, MAINTENANCE DISCOVERED CORROSION LOCATED ON THE RT MLG ACTUATOR OUTBOARD ATTACH PIN. PIN WAS REMOVED AND REPLACED IAW M4L32101.SDR AWXA200600238Pin · corrodedPHX - DURING ENGINEERING MODIFICATION, M4L32101, MAINTENANCE DISCOVERED CORROSION LOCATED ON THE LT MLG ACTUATOR OUTBOARD ATTACH PIN. PIN WAS REMOVED AND REPLACED IAW M4L32101.SDR AWXA200501498Power Supply · inoperativeLAS - EEL - DURING INSPECTION DISCOVERED, THE AFT EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY IAW AMERICA WEST AIRLINES TASK CARD R1C33303. OPERATIONAL CHECKS WERE GOOD. VENDOR DID NOT CONFSDR AWXA200501481Warning System · malfunctionedDURING TAKEOFF, CREW REPORTED ECAM MESSAGE (ENG 1 COMPRESSOR VANE). CREW ABORTED TAKEOFF AT ESTIMATED 60 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING IAW SRM 75-30-00-810-843 AND TASKCARD FSM 71312, NO FAULTSSDR AWXA200501088Power Supply · inoperativeATL - EEL - DURING 8 DAY CHECK DISCOVERED THE AFT GALLEY EMERGENCY POWER SUPPLY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY POWER SUPPLY IAW AIRBUS 320 AMM 33-51-38-000-001. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200501087Power Supply · inoperativeATL - EEL - DURING 8 DAY CHECK DISCOVERED THE FORWARD GALLEY EMERGENCY POWER SUPPLY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY POWER SUPPLY IAW AIRBUS 320 AMM 33-51-38-000-001. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200500484Servo · faultyNOSE WHEEL STEERING FAILURE - ON SHORT AND FINAL APPROACH INTO CUN EN ROUTE FROM PHX WITH LANDING GEAR DOWN ECAM INDICATED NOSE WHEEL STEERING FAULT (2), GREEN HYDRAULIC PRESSURE WAS NORMAL AND LANDING WAS NORMAL. AFTER CLEARING RUNWAY RECYCLED ANTI-SKID SWITSDR AWXA200401129Computer · inoperativeAFTER TAKEOFF EN ROUTE LOST ALL FUEL QUANTITY INDICATIONS, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE R/R FUEL QTY INDICATION COMPUTER (FQIC) IAW AMM 28-42-34, OS CHK GOOD. FUNCTIONAL TESTING OF FQIC S/N 1772 PRODUCED NO FAILURES OR FAULTS. UNISDR AWXA200401110Idg · malfunctionedON TAKEOFF AT LAS, RECEIVED ECAM WARNING NR 2 ENG IDG LOW OIL PRESSURE, REJECTED TAKEOFF AT 80 KTS. MX ISSUED MEL 24-20-01, COND. 2 "NR 2 IDG INOP". PERFORMED FAULT ISOLATION PER TSM, ITEM 4 - 4A2, NO WIRING FAULTS NOTED. REMOVED AND REPLACED NR 2 ENG IDG IAW SDR AWXA200401063Battery · dischargedDURING 4-DAY CHECK, FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM THE FORWARD LT EMERGENCY LIGHT BATTERY FAILED TEST AT EMERGENCY POWER SUPPLY UNIT (10WL). MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATSDR AWXA200400363Seal · tornAFTER TAKEOFF FROM MSP EN ROUTE FOR LAS RECEIVED ECAM MESSAGE NOSE LANDING GEAR (NLG) SHOCK ABSORBER FAULT, TURNED BACK TO MSP AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE MET AIRCRAFT BACK AT GATE AND FOUND THE NLG SHOCK ABSORBER FLAT. SERVICE NLG SHOCK STSDR AWXA200400213Wire Harness · brokenPHX - EEL - DURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1 LT AND 11 RT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WIRE HARNESSES AT SEAT ROWS 1 LT AND 11 RT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400196Floorbeam · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM AT FR 70, Y765 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 68 AND FR 70, Y765 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472209; INSTALLED REPAIR PART IASDR AWXA200400195Floorbeam · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 66, Y512 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 64 AND FR 67, Y512 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIGSDR AWXA200400194Floorbeam · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 66, Y765 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM AT FR 66, Y765 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472209; INSTALLED REPAIR PART IAW A320 SRM 51-42-11,SDR AWXA200400193Sill · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SILL AT FR 66, Y1732 RT, FORWARD OF R-2 DOOR. MAINTENANCE REMOVED R-2 DOOR LOWER SILL AT FR 66, Y1732 RT; FABRICATED A NEW REPLACEMENT LOWER SILL; INSTALLED REPAIR PART IAW A320 SSDR AWXA200400192Seat Track · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM SEAT RAIL AT FR 66, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM SEAT RAIL AT FR 66, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM SEAT RAIL; INSTALLED REPAIR PART IAW A320SDR AWXA200400191Floorbeam · corrodedDURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM AT FR 68, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG D53472189; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9-14, 16 SDR AWXA200400190Floorbeam · corrodedDURING B-04 CHECK CORROSION WAS FOUND ON FLOORBEAM BETWEEN FR 66 AND FR 68, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 66 AND FR 68, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG D53472172; INSTALLED REPAIR PART IAW A320 SRM 51-4SDR AWXA200400189Seat Track · corrodedDURING B-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR BEAM TEE CAP (SEAT TRACK) AT CLIP NUT LOCATIONS BETWEEN FR 17 AND FR 20, Y1292 RT. MAINTENANCE REMOVED DAMAGED SEAT TRACK BETWEEN BS 7830 AND BS 8000, Y1292 RT; FABRICATED 6 EACH REPASDR AWXA200400197Panel · corrodedMCN - MAJOR REPAIR - DURING B-04 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL PANEL ASSEMBLY BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED AND REPLACED L-2 DOOR SILL PANEL ASSEMBLY IAW T/C O1D25310 & C1D25310.SDR AWXA200200923Cable · brokenPHX - EEL - DURING P-08 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H IAW ESPM 20-25-21; OPS CHECK OF EMERGENCY CABIN LIGHTING WAS GOOD.SDR AWXA200200751Oven · smokePHX - SMOKE - FLT 0504 - BOTH OVENS IN FORWARD GALLEY SMOKE WHEN OVEN IS HEATED. REMOVED AND REPLACED BOTH OVENS IN THE FORWARD GALLEY, OPERATIONALLY CHECKED GOOD.SDR AWXA200200021O-Ring · rupturedLAS - DIVERSION - FLT 522 - C - EN ROUTE FROM PHX TO RNO FLIGHT CREW RECEIVED YELLOW HYDRAULIC SYSTEM FLUID LOSS INDICATION FOLLOWED BY FLIGHT CONTROL DEGRADATION TO ALTERNATE LAW, THIS WAS CAUSED BY LOSS OF NR 2 YELLOW YAW DAMPER, NR 1 YAW DAMPER PREVIOUSLY OSDR AWXA0002214Valve · malfunctionedBOS - USED ALTERNATE GEAR EXTENSION - ON APPROACH THE LANDING GEAR FAILED TO EXTEND WITH THE GEAR SELECTOR IN THE DOWN POSITION, (NO GEAR OR DOOR MOTION SENSED). THE CREW USED ALTERNATE EXTENSION AND GEAR EXTENDED. AN UNEVENTFUL LANDING WAS MADE. IN BOS MX SDR AWXA0002044Packing · damagedBDL- EMERGENCY LANDING - FLT 402 - EN ROUTE FROM PHX RO BDL THE CREW FOUND YELLOW HYDRAULIC QUANTITY DECREASING AND TURNED THE YELLOW SYSTEM HYD PUMP OFF PRIOR TO GETTING A RESERVOIR LOW LEVEL WARNING. ON APPROACH THE YELLOW HYD SYSTEM WAS LOST AND THE CREW CSDR AWXA0001697Control Unit · intermittentLAS - EMERGENCY LANDING, INBOUND TO LAS THE CREW GOT AN ECAM MSG FOR NOSE WHEEL STEERING FAULT. THE AIRCRAFT MADE AN UNEVENTFUL LANDING IN LAS. IN LAS MAINTENANCE TROUBLESHOT IAW TSM 32-51-810-826 AND FOUND WATER IN CONNECTOR 6GC AT THE NOSE WHEEL STEERING S
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