N269AU, cancelled Jun 18, 2004

Service difficulty reports · 60

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 = 'N269AU' AND deregistration_id = 'N269AU-2004-06-18'
  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.

SDR USAA010865Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED, AFT END OF AIRSTAIR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-03. (M)Jul 7, 2001 · N269AU · Boeing 7372B7 · Fuselage Structure (General)SDR USAASB01160Flap · jammedEWR - FLT 2671 - DURING DESCENT, AIRCRAFT ENCOUNTERED TRAILING EDGE FLAP ASYMMETRY. CAPTAIN REQUESTED TO LAND AT EWR INSTEAD OF LGA DUE TO THE HIGHER LANDING SPEEDS FOR THIS TYPE OF FAILURE. AFTER LANDING AT EWR, WITHOUT INCIDENT, CAPTAIN REPORTED THAT THE LJun 4, 2001 · N269AU · Boeing 7372B7 · Trailing Edge Flap Control SystemSDR USAA010296Skin · crackedTPA - FOUND SKIN CRACKED .75 INCH, LOWER HINGE BETWEEN STRINGER 9 AND 10 RT AFT STATION 947. INSTALLED DOUBLER PER SRM 53-30-3 FIG 33. (M)Mar 20, 2001 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA010187Skin · crackedTPA - FOUND SKIN CRACKED .75 INCH, LOWER HINGE CUTOUT BETWEEN STRINGER 9 AND 10R AFT STATION 947. INSTALLED DOUBLER PER SRM 53-30-3 FIG 33N AND TR 53-30-11. (M)Feb 28, 2001 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB01048Engine · failedMCO - FLT 2727 - ON CLIMB-OUT FROM FLL, EN ROUTE TO LGA, CAPTAIN REPORTED THAT THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND METAL IN THE TAILPIPE OF Feb 15, 2001 · N269AU · Boeing 7372B7 · Engine (Turbine/Turboprop)SDR USAASB00338Indicator · faultyCLT - FLT 2700 - EN ROUTE FROM BWI-MSY, THE CREW OBSERVED HYDRAULIC QTY DECREASING BELOW 1.8 GALLON VALUE IN FLIGHT. DURING INITIAL CONFIGURATION, QUANTITY WAS OBSERVED BELOW 1.4 GALLON VALUE. INITIAL QUANTITY LEAVING BWI WAS AT 3.2 GALLONS ON INDICATOR. FLNov 30, 2000 · N269AU · Boeing 7372B7 · Hydraulic Quantity IndicatorSDR USAASB00229Power Supply · failedIAD - MAINTENANCE FOUND THE OUTBOARD EXTERIOR EMERGENCY LIGHT FOR THE RIGHT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY. OPERATIONAL CHECK NORMAL. (M)Aug 17, 2000 · N269AU · Boeing 7372B7 · Emergency LightingSDR USAA000452Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 1.125 INCH, AFT END OF E/E COOLING DUCT OUTLET. INSTALLED DOUBLER PER TR 53-30-04 AND DWG 65C33930. (M)Mar 23, 2000 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA000385Skin · crackedTPA - FOUND FUSELAGE SKIN 2.24 INCH CRACKED, STATION 767, STRINGER 19R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Mar 20, 2000 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99260Acm · weakBWI - FLT 2741 - FLT ON MX DELAY IN BDL, WHEREAS MX PLACED THE RT PACK ON MEL. FLT DEPARTED BDL AND WHILE FLYING OVER PHL, THE LT PACK WOULD ONLY HOLD CABIN PRESSURE TO 9,500 FT. CAPT ELECTED TO DIVERT TO BWI WHERE THE FLT LANDED W/O FURTHER INCIDENT. NO EMOct 27, 1999 · N269AU · Boeing 7372B7 · Cabin Cooling SystemSDR USAASB99159Fire Loop · failedMCO-BWI - FLT 2662, AT APPROX FL330, CREW RECEIVED AND APU FIRE DETECTION LIGHT. CREW SHUTDOWN THE APU. WITH A/C BEING DOWN TO ONE SOURCE OF ELECT POWER, CREW DIVERTED FLIGHT TO THE NEAREST SUITABLE AIRPORT AT RDU. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NJun 30, 1999 · N269AU · Boeing 7372B7 · Fire DetectionSDR USAASB99075Battery Pack · dischargedCLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M572, RIGHT SIDE, AND THE POWER SUPPMar 18, 1999 · N269AU · Boeing 7372B7 · Emergency LightingSDR 99ZZZM244Power Supply · failedCLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M572, RIGHT SIDE, AND THE POWER SUPPMar 18, 1999 · N269AU · Boeing 7372B7 · Emergency LightingSDR USAASB99074Battery Pack · dischargedALB - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT, LEFT SIDE. OPERATIONAL CHECK GOOD. (M)Mar 14, 1999 · N269AU · Boeing 7372B7 · Emergency LightingSDR USAASB99046Battery Pack · dischargedBWI - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Feb 20, 1999 · N269AU · Boeing 7372B7 · Emergency LightingSDR USAASB99018Fire Light · illuminatedILM - FLT 439 - ON DESCENT INTO ILM, THE CREW REPORTED THAT THE APU FIRE WARNIG LIGHT ILLUMINATD WITH THE APU ON MEL AND SHUTDOWN. THE APU IS SCHEDULED FOR REPLACEMENT DUE TO PERFORMANCE. CAPTAIN STATED THAT THE FLIGHT WAS AT 12,000 FEET WHEN THE FIRE WARNINJan 23, 1999 · N269AU · Boeing 7372B7 · Fire DetectionSDR USAASB98340Wire · brokenPIT - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT FAULT TO THE M192 BATTERY PACK CANNON PLUG D1494, PIN 5. REPAIRED GROUND WIRE FROM PIN NR 5 ON CANNON PLUG D1494. OPERATIONAL CHECK GOOD. (M)Dec 29, 1998 · N269AU · Boeing 7372B7 · Light System WiringSDR USAASB98258Supply Duct · failedLGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LGOct 1, 1998 · N269AU · Boeing 7372B7 · Air Distribution SystemSDR 98ZZZM890Pack Control Vlv · failedLGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LGOct 1, 1998 · N269AU · Boeing 7372B7 · Air Distribution SystemSDR 98ZZZM889Press Regulator · failedLGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LGOct 1, 1998 · N269AU · Boeing 7372B7 · Air Distribution SystemSDR 98ZZZM888Mix Chamber Duct · failedLGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LGOct 1, 1998 · N269AU · Boeing 7372B7 · Air Distribution SystemSDR USAA980468Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT LWR THRESHOLD SUPPORT ZEE AREA FWD SERVICE DOOR STATION 300 TO 340 ZEE ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-1. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980467Frame · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A CRACK OUTBOARD FRAME CHORD BS 727 STRINGER 15L. INSTALLED DOUBLERS, FILLERS AND STRAPS PER EA 62502. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA980466Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 6 INCH AREA OF CORROSION LBL 54 STATION 887 TO STATION 1016. CORROSION TASK NR C53-107-02. REPLACED WITH IDENTICAL PART PER SRM 53-10-01. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980464Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 24 INCH AREA OF CORROSION CLIP NUT HOLES BS 1016 BETWEEN LBL 12 AND LBL 36 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-9. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA980463Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980462Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727A STRINGER 6R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980461Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 747 STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980460Floorbeam · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK BS 663 BBL .07 UPPER CHORD LONGITUDINAL FLOORBEAM. INSTALLED SPLICE ANGLES, STRAPS AND REINFORCED ANGLES PER EA 62511 AND BOEING S/B737-57-1210. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA980459Web · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK BS 230.5 WL 187 BL 0 RETRACT ACT FITTING SUPPORT WEB NLG. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1, BOEING 737-200. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980458Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SEVERAL SCREW HOLES ON FLOORBEAM STATION 947.5. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP TO FLOORBEAM PER SRM 53-10-9. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA980457Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 4L STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980456Floorbeam · crackedCLT - DURING Q-4 CHECK HFEC INSPECTION, FOUND A 1.5 INCH CRACK BS 520 WL 208 LBL 24 FLOORBEAM. INSTALLED REPAIR ANGLE PER EA 62449 SB 737-53-1120 REV 1 PART VI. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980455Floorbeam · crackedCLT - DURING Q-4 CHECK HFEC INSPECTION, FOUND A 1.5 INCH CRACK BS 520 WL 208 RBL 24 FLOORBEAM. INSTALLED REPAIR ANGLES PER EA 62449 SB 737-53-1120 REV 1. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA980454Floorbeam · crackedCLT - DURING Q-1 CHECK HFEC INSPECTION, FOUND .25 INCH CRACK BS 520 RBL 45 FLOORBEAM 'T' CAP RADIUS. INSTALLED REPAIR ANGLES PER EA 62449 BOEING SB 737-53-1120 REV 1. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA980453Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND CLIP NUT HOLES STATION 344 FLOORBEAM BL 0 TO LBBL 42. REPAIRED 'T' CAP SPLICED DOUBLER PER SRM 53-10-13. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA980452Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 10R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980451Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 8R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980450Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980449Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 2R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980448Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 2R, STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980447Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 747 STRINGER 7L STRINGER TIE CLIP. REPAIRED PER EO 5939G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980446Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 706 STRINGER 9L. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980445Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK STATION 500B STRINGER 10L STRINGER TIE CLIP. REPAIRED PER SRM 51-10-1 AND EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980444Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER TIE CLIP STATION 616 S 1. REPAIRED PER EO 5393G227 REV 'A'. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980439Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN RADIUS SUPPORT BRACKET FOR NLG AT BEAM VERT FLANGE STATION 259 WL 192 ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-1. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980438Skin · crackedCLT - DURING Q-1 CHECK EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK LOWER FORWARD CORNER LEFT AFT ENTRY DOOR CUTOUT STATION 962 WL 208 SKIN. INSTALLED TRIPLER PER SRM 53-30-03 FIG 24. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980437Skin · dentedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH LONG .875 INCH WIDE AND .09375 INCH DEEP DENT BETWEEN STATION 987.5 AND STATION 1006 STRINGER 17L SKIN. FABRICATED DOUBLER PER SRM 53-30-3 FIG 61. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USA980469Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT CLIP NUTS STATION 344 FLOORBEAM BL 0 LBL 42. CORROSION TASK NR C53-107-01. FABRICATED REPAIR PER TR 53-10-13 'T' CAP. (M)Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAASB98158Duct · crackedTPA - FLT 940 - DURING CLIMB-OUT FROM TPA AT FL200, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPTAIN RETARDED THROTTLE ON THE NR 1 ENGINE TO IDLE AND THE LIGHT EXTINGUISHED. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD AT TPA. FLT LANDED WITHOUT INJun 26, 1998 · N269AU · Boeing 7372B7 · Air Intake Anti/De-Ice System
Back to N269AU, cancelled Jun 18, 2004