N656AW
Service difficulty reports · 242
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 = 'N656AW' 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 = 'N656AW' 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 USAA2011052600003Seat Track · corrodedCORROSION ON RAIL SEAT BETWEEN FR54 TO FR56, -Y765. PERFORMED PERMANENT REPAIR ON SEAT TRACK FR54 TO FR56 -Y765 IAW A320 SRM 53-41-15.SDR USAA2011052600002Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL 131JF BETWEEN FR31 TO FR34 & BETWEEN Y765 TO Y970.8. REPLACED FLOOR PANEL 131JF IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.SDR USAA2011052600001Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL 151HF BETWEEN FR53 TO FR56 & BETWEEN Y765 TO Y970.8. REPLACED FLOOR PANEL 151HF IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.SDR USAA2011052300004Web · crackedCRACK ON WEB OF COCKPIT FLOOR BETWEEN FR8 TO FR11, -Y165. REPLACED WEB OF COCKPIT FLOOR BETWEEN FR8 TO FR11, -Y165 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53113219.SDR USAA2011051991910Web · crackedSAL - S5 - CRACK ON WEB BETWEEN FR8 TO FR11, Y765. REPLACED WEB BETWEEN FR8 TO FR11, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53113219.SDR USAA2011052600007Support Bracket · corrodedLEVEL 2 GALVANIC CORROSION ON SUPPORT BRACKET AT FR19 + INCHES, S23R. REPLACED SUPPORT BRACKET AT FR19 + INCHES, S23R IAW A320 SRM A320 51-72-11 & AIRBUS DRAWING D53110339.SDR USAA2011052600012Skin · saturatedTRAPPED WATER INDICATION WAS FOUND IN THE LT ELEVATOR UPPER SKIN BETWEEN THS STA 181 TO STA 227 & BETWEEN RIB 5 TO RIB 6. REPAIRED LT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PAR 5E.SDR USAA2011052600011Elevator · saturatedTRAPPED WATER INDICATION WAS FOUND IN THE LT ELEVATOR UPPER SKIN BETWEEN THS STA 181 TO STA 227 & BETWEEN RIB 5 TO RIB 6. REPAIRED LT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PARA 5E.SDR USAA2011052600010Skin · saturatedTRAPPED WATER INDICATION WAS FOUND IN THE RT ELEVATOR UPPER SKIN BETWEEN THS STA 227 TO STA 271 & BETWEEN RIB 6 TO RIB 7. REPAIRED WITNESS HOLE INSPECTION ON RT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11.SDR USAA2011052500008Skin · saturatedTRAPPED WATER INDICATION FOUND ON RIGHT ELEVATOR UPPER SKIN BETWEEN THS STA 404 STA 466 & BETWEEN RIB 10 TO RIB 11. REPAIRED WITNESS HOLE PERFORATION RIGHT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11.SDR USAA2011052500007Skin · saturatedTRAPPED WATER INDICATION FOUND ON LEFT ELEVATOR UPPER SKIN BETWEEN THS STA 560 TO STA 601 & BETWEEN RIB 13 TO RIB 14. REPAIRED WITNESS HOLE PERFORATION LEFT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11.SDR USAA2011052500005Skin · saturatedTRAPPED WATER INDICATION FOUND ON RIGHT ELEVATOR UPPER SKIN BETWEEN THS STA 181 TO STA 227 & BETWEEN RIB 5 TO RIB 6. REPAIRED WITNESS HOLE PERFORATION RIGHT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11.SDR USAA2011052500004Skin · saturatedTRAPPED WATER INDICATION FOUND ON RIGHT ELEVATOR UPPER SKIN BETWEEN THS STA 181 TO STA 227 & BETWEEN RIB 5 TO RIB 6. REPAIRED WITNESS HOLE PERFORATION RIGHT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11.SDR USAA2011052500003Skin · saturatedTRAPPED WATER INDICATION FOUND ON RIGHT ELEVATOR UPPER SKIN BETWEEN THS STA 342-STA 404 & BETWEEN RIB 9 TO RIB 10. REPAIRED WITNESS HOLE PERFORATION RIGHT HAND ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11.SDR USAA2011052500002Skin · saturatedTRAPPED WATER INDICATION FOUND ON RIGHT ELEVATOR UPPER SKIN BETWEEN THS STA 342 TO STA 404 & BETWEEN RIB 9 TO RIB 10. REPAIRED WITNESS HOLE PERFORATION RIGHT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11.SDR USAA2011051891902Fitting · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT L1 DOOR BETWEEN FR17 TO FR19, S23L. REPLACED CENTER FITTING AT L1 DOOR BETWEEN FR17 TO FR19, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2011051891901Fitting · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR17 TO FR19, S23R AT R1 DOOR. REPLACED CENTER FITTING BETWEEN FR17 TO FR19, S23R AT R1 DOOR IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2011051891900Fitting · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON FORWARD CORNER FITTING AT L1 DOOR AT FR16, S23L. REPLACED FORWARD CORNER FITTING AT L1 DOOR AT FR16, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2011051891899Fitting · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON AFT CORNER FITTING AT R1 DOOR AT FR20, S23R. REPLACED AFT CORNER FITTING AT R1 DOOR AT FR20, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2011051891898Fitting · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON AFT CORNER FITTING AT FR20, S23L AT L1 DOOR. REPLACED AFT CORNER FITTING AT FR20, S23L AT L1 DOOR IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.SDR USAA2011051891893Floorbeam · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR67 + 13 INCHES, -Y1292. REPLACED FLOORBEAM AT FR67 + 13 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53472780.SDR USAA2011052600009Seat Track · corrodedCORROSION ON SEAT TRACK AT FR53+1 INCH, Y765. PERFORMED PERMANENT REPAIR ON SEAT TRACK AT FR53+1INCH, Y765 IAW A320 SRM A320 53-00-15.SDR USAA2011060200001Damper · inoperativeSAL - S5 - HARD IMPACT BETWEEN SLIDES & PASSENGER CREW DOOR 831 FOUND DURING OPERATIONAL TEST OF THE DAMPING. REPLACED DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 831. LEAK TEST OK IAW A320 AMM 52-11-14-000-001-0.SDR USAA2011060200002Rod · out of adjustSAL - S5 - DIMENSION "A" IS OUT OF ADJUSTMENT BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 831. PERFORMED ADJUSTMENT OF DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 831 IAW A320 AMM 52-11-14-991-004.SDR USAA2011051891897Dummy Rail · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY AT FR16, Y503.2. REPLACED RAIL DUMMY AT FR16, Y503.2 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112825.SDR USAA2011051891896Seat Track · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR34, -Y1295. REPAIRED SEAT TRACK SECTION AT FR34, -Y1295 IAW A320 SRM 53-21-15.SDR USAA2011051891895Seat Track · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR29 + 11 INCHES TO FR35, Y1292. REPAIRED SEAT TRACK SECTION BETWEEN FR29 + 11 INCHES TO FR35, Y1292 IAW A320 SRM 53-21-15.SDR USAA2011051891894Seat Track · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR29 + 9 INCHES TO FR35, -Y765. REPAIRED SEAT TRACK SECTION BETWEEN FR29 + 9 INCHES TO FR35, -Y765 IAW A320 SRM 53-21-15.SDR USAA2011051991909Damper · damagedSAL - S5 - DURING AN OPERATIONAL TEST OF THE DAMPING WAS FOUND A HARD IMPACT BETWEEN SLIDERS & PASSENGER / CREW DOOR 842. REPLACED THE DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT PASSENGER / CREW DOOR 842 IAW A320 AMM 52-13-14-400-001-0.SDR USAA2010112992675Accumulator · low pressureFLT 307 LAS - EES - R-2 DOOR ASSIST ACCUMULATOR REQUIRES SERVICING. MAINTENANCE SERVICED R-2 DOOR ASSIST ACCUMULATOR IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614.SDR USAA2010090791920Wire · damagedFLT 408 - PHX - EEL - EMERGENCY LIGHT AT ROW 11 LEFT INOPERATIVE. MAINTENANCE REPAIRED WIRING AT ROW 11 LEFT.SDR USAA2010081791686Power Supply · inoperativeSAL - C11 - EEL - ROW 11 ABC RED EMERGENCY EXIT LIGHT INOP. REPLACED EPSU IN ROW 11 ABC IAW A320 AMM 33-51-38-400-001. OPS CHECK GOOD.SDR USAA2010072991533Bottle · low pressureFLT 1539 - SEA - EES - FLIGHT ATTENDANT CIDS PANEL 'CHECK DOOR PSI 1R'. MAINTENANCE SERVICED 1R DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-03-614-001.SDR USAA2010061791152Fastener · missingFLT 307 - LAS - EEL - EMERGENCY POWER SUPPLY FOR EMERGENCY LIGHTS MID RT CABIN, BASE MISSING FASTENER FOR BATTERY. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT MID RT CABIN IAW AIRBUS MAINTENANCE MANUAL 33-51-38-000-001.SDR USAA2010040890732Battery · dischargedFLT 542 - PDX - EEL - AFT LT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE AFT LEFT FLIGHT ATTENDANT FLASHLIGHT. OPERATIONAL CHECK GOOD.SDR USAA2009100192675Fire Warning · false activationFLT 528 - PHX - FALSE FIRE WARNING - IN CRUISE FLIGHT, CREW GOT A LAV SMOKE WARNING MOMENTARILY FOR AFT LEFT LAV. SYSTEM RESET ITSELF AND NO EVIDENCE OF SMOKE WAS FOUND. ALSO NO SUBSEQUENT EVENTS TO DATE.SDR USAA2009082692254Hinge Fitting · excess playSAL - TRIPLE GEAR CHANGE - MAJOR REPAIR - EXCESSIVE PLAY AT AFT HINGE FITTING OF RIGHT AFT NOSE LANDING GEAR DOOR BETWEEN FR19 TO FR20, S41R, -Y510. REPLACED AFT HINGE FITTING OF RIGHT AFT NOSE LANDING GEAR DOOR BETWEEN FR19 TO FR20, S41R, -Y510 IAW A320 CMM SDR USAA2009082492219Wire Harness · faultySAL - TRIPLE GEAR CHANGE - EEL - INOP EMERGENCY LIGHT ON PASSENGER SEAT 19 LEFT. REPLACED HARNESS FOR EMERGENCY LIGHT ON PASSENGER SEAT 19 LEFT IAW B737 AMM 33-51-18.SDR USAA2009082592246Hinge Fitting · excess playSAL - TRIPLE GEAR CHANGE - MAJOR REPAIR - EXCESSIVE PLAY AT FORWARD HINGE FITTING OF RIGHT AFT NOSE LANDING GEAR DOOR BETWEEN FR19 TO FR 20, S41R -Y510. REPLACED FORWARD HINGE FITTING OF RIGHT AFT NOSE LANDING GEAR DOOR BETWEEN FR19 TO FR 20, S41R -Y510 IAW ASDR USAA2009052691281Seal · brokenLOG PAGE 4431308 - FLT 430-LAS - EMERGENCY EQUIPMENT - FORWARD FLIGHT ATTENDANT FLASHLIGHT SEAL BROKEN. MAINTENANCE REPLACED SEAL ON FORWARD FLIGHT ATTENDANT FLASHLIGHT AS REQUIRED.SDR USAA2009041790916Power Supply · dischargedFLT 181 - FLL-PHX - EMERGENCY LIGHTS - SEVERAL EMERGENCY LIGHTS INOPERATIVE THROUGHOUT CABIN. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER MAINTENANCE MANUAL 33-51-38. OPERATIONAL CHECK WAS GOOD.SDR USAA2009010790043Sill · corrodedSAL - C7 - MAJOR REPAIR - NR 6129696 - GALVANIC CORROSION ON LOWER SILL AT R2 DOOR BETWEEN FR68 TO FR68.5, -Y1292. REPAIRED LOWER SILL AT R2 DOOR BETWEEN FR68 TO FR68.5, -Y1292 IAW A320 SRM 53-41-14.SDR USAA2009010590019Floorbeam · corrodedSAL - C7 - MAJOR REPAIR - NR 6129698 - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 +5 INCHES, -Y1292. REPAIRED FLOORBEAM BETWEEN FR64 TO FR66 +5 INCHES, -Y1292 IAW A320 SRM 51-72-11.SDR USAA2009010790045Floor Panel · corrodedSAL - C7 - MAJOR REPAIR - NR 6129498 - CORROSION ON FLOORBOARD PANEL NR 222FF, (R1 DOOR ENTRY). REPLACED FLOORBOARD PANEL NR 222FF, (R1 DOOR ENTRY).SDR USAA2008123192357Floorbeam · corrodedSAL C7 MAJOR REPAIR NR 6129695 GALVANIC CORROSION ON FLOOR BEAM AT -Y765 BTW FR66+5" TO FR70 OF PAX CABIN. REPLACED FLOOR BEAM AT -Y765 BTW FR66+5" TO FR70 OF PAX CABIN IAW A320 SRM 51-72-11.SDR USAA2008123192356Shear Plate · corrodedSAL - C7 - MAJOR REPAIR - NR 6129693 - GALVANIC CORROSION ON SHEAR PLATE BTW FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BTW FR69 TO FR70, -Y1732 IAW A320 SRM 51-72-11 & 51-42-11.SDR USAA2009010690040Dummy Rail · corrodedSAL C7 MAJOR REPAIR NR 6131298 GALVANIC CORROSION ON DUMMY RAIL FLOOR STRUCTURE BETWEEN FR12 TO FR16, Y503. REPLACED DUMMY RAIL FLOOR STRUCTURE BETWEEN FR12 TO FR16, Y503 IAW A320 SRM 51-72-11.SDR USAA2008123192366Web · crackedSAL C7 MAJOR REPAIR NR 6131295 CRACK ON WEB BTW FR68+10" ABOVE STR 23L OF PAX CABIN AT REAR FUSELAGE. REPAIRED WEB BTW FR68+10" ABOVE STR 23L OF PAX CABIN IAW A320 SRM 51-72-11.SDR USAA2009010790044Sill · corrodedSAL - C7 - MAJOR REPAIR - NR 6129688 - GALVANIC CORROSION ON LOWER SILL AT L2 DOOR BETWEEN FR66 TO FR68, Y1732. REPAIRED LOWER SILL AT L2 DOOR BETWEEN FR66 TO FR68, Y1732 IAW A320 SRM 53-41-14.SDR USAA2009010790046Floor Panel · corrodedSAL - C7 - MAJOR REPAIR - NR 6129499 - CORROSION ON FLOORBOARD PANEL NR 261FF, (L2 DOOR ENTRY). REPLACED FLOORBOARD PANEL NR 261FF, (L2 DOOR ENTRY).
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