N268AU, cancelled Dec 9, 2003

Service difficulty reports · 56

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 = 'N268AU' AND deregistration_id = 'N268AU-2003-12-09'
  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 USAASB01321Wire · brokenPVD - THE EMERGENCY LIGHT AT SEAT 12 WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. (M)Nov 20, 2001 · N268AU · Boeing 7372B7 · Light System WiringSDR USAA010622Skin · crackedCLT - FOUND FUSELAGE SKIN HAS APPROXIMATELY .5 INCH CRACK, BS 380, FUSELAGE BELLY S-28L, COOLING DUCT CUTOUT. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-04. (M)Jun 8, 2001 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB0279Fuel Control · failedBWI - FLT 2797 - ON CLIMB-OUT FROM BWI, AT FL080, THE NR 2 ENGINE FLAMED OUT. N1, N2 AND OIL PRESSURE WAS PRESENT. CREW TRIED TO RESTART/RELIGHT NR 2 ENGINE, BUT COULD NOT. AN EMERGENCY WAS DECLARED AND THE PASSENGERS WRE BRIEFED ON EMERGENCY PROCEDURES. FSep 30, 2000 · N268AU · Boeing 7372B7 · Fuel Control/Turbine EnginesSDR USAA001138Frame · corrodedTPA - FOUND FRAME WEB CORRODED 4 INCHES BY 3 INCHES, FRAME STATION 277, LT LOWER LOBE. REPLACED SECTION PER SRM 51-40-2 FIG 1, SRM 53-10-4 FIG 9A EA 66638. (M)Aug 1, 2000 · N268AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAASB00190Structure · vibrationPVD - FLT 2851 - ON CLIMB-OUT FROM BOS, AIRCRAFT EXPERIENCED A CONTINUOUS AIRFRAME VIBRATION OF UNKNOWN SOURCE. ATTEMPTS TO ISOLATE THE NATURE OF THE SOURCE WERE NO HELP. THE ONLY IMPROVEMENT WAS WHEN THE AIRCRAFT SLOWED TO 250 KNOTS. CAPTAIN THOUGHT OF DIVJul 16, 2000 · N268AU · Boeing 7372B7 · Fuselage Main, StructureSDR USAASB00153Flap · jammedTPA - FLT 2797 - AS AIRCRAFT WAS BEING CONFIGURED FOR FINAL APPROACH TO TPA, THE RIGHT INBOARD TRAILING EDGE FLAP BECAME JAMMED WHEN THEY WERE MOVED FROM 10-15 DEGREES. CREW ACCOMPLISHED PROCEDURES AND A GO-AROUND AND DECLARED AN EMERGENCY. FLIGHT LANDED WITJun 1, 2000 · N268AU · Boeing 7372B7 · Trailing Edge Flap Control SystemSDR USAASB00134Hose · failedIAD - FLT 2755 - DURING CLIMB-OUT FROM IAD, THE NOSE LANDING GEAR WOULD NOT RETRACT. CREW NOTICED A DROP IN HYDRAULIC PRESSURE. THE NOSE LANDING GEAR NEVER UNLOCKED AS A STEADY NOSE GEAR GREEN LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO FIELD AT IAD AND May 6, 2000 · N268AU · Boeing 7372B7 · Hydraulic System, MainSDR USAASB00131Start Valve · failedTPA - FLT 2999 - CLIMBING THROUGH 7,000 FEET OUT OF TPA, THE NR 1 ENGINE START VALVE LIGHT ILLUMINATED. CAPTAIN WENT THROUGH PROCEDURES, DECLARED AN EMEREGNCY AND SHUT DOWN THE NR 1 ENGINE PER PROCEDURES. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FUMay 3, 2000 · N268AU · Boeing 7372B7 · Engine Start Valves/ControlsSDR USAASB00121Actuator · failedATL - FLT 2967 - ON DESCENT INTO ATL, WHILE EXTENDING FLAPS, CAPTAIN VISUALLY CONFIRMED THE NR 1 SLAT WAS NOT FULLY EXTENDED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND DECLARED AND EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT AT ATL. MAINTENANCE REApr 23, 2000 · N268AU · Boeing 7372B7 · Leading Edge Slat ActuatorSDR USAASB99199Compressor · stalledBOS - FLT 2851 - AT ROTATION, CREW HEARD AND FELT A LOUD BANG. ALL ENGINE INDICATIONS WERE NORMAL. FLAMES OR A FLASH WERE LATER REPORTED BY A PASSENGER OFF THE RIGHT SIDE OF THE AIRCRAFT. AT APPROXIMATELY 5,000 FT. CAPTAIN DECLARED AN EMERGENCY AND PREPPEDAug 11, 1999 · N268AU · Boeing 7372B7 · Turbine Engine Compressor SectionSDR USAASB99150Wire Harness · failedRDU - FLT 2826 - EN ROUTE FROM MCO TO BOS, DURING CRUISE, CAPT REPORTED PROBLEMS WITH THE NR 2 FUEL GAUGE. GAUGE WAS UNRELIABLE WITH ITS READINGS AND THE NR 1 FUEL GAUGE WAS ALREADY ON MEL. CREW TRIED RESETTING CIRCUIT BREAKER WITH NO HELP. THE NR 2 FUEL GAJun 20, 1999 · N268AU · Boeing 7372B7 · Fuel System WiringSDR USAASB98304Battery Pack · dischargedPHL - MAINTENANCE FOUND THE AFT CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Nov 13, 1998 · N268AU · Boeing 7372B7 · Emergency LightingSDR USAA980554Skin · creasedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CREASE APU DOOR AFT LATCH CUTOUT AT STATION 1146 ON SKIN. INSTALLED DOUBLER PER EA 62761. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980553Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT ENTRY DOORWAY AT LOWER HINGE CUTOUT ON FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 34 AND TR 53-30-11. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980552Stringer · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 6 INCH CORRODED AREA STATION 907, STRINGER 26L. CORROSION TASK NR C53-208-01. INSTALLED NEW STRINGER AND STRINGER SPLICES PER SRM 53-10-3. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA980551Angle · crackedDURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH STATION 727 WL 200 LBL 45 CHORD ANGLE. INSTALLED REPAIR ANGLE PER TR 53-10-03A. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980550Sill · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 6 INCH AREA OF CORROSION BS 300-306 WL 208.10, RBBL 54 FORWARD SERVICE DOOR INNER CHORD. CORROSION TASK NR C53-107-01. INSTALLED NEW 'Z' ANGLE PER SRM 51-10-1 AND SRM 51-30-2. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980546Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .03125 INCH CRACK AT LOWER AFT CORNERS FORWARD ENTRY DOOR STATION 342 WL 208.1 SKIN FUSELAGE. CUT OUT CRACKED AREA FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER PER BOEING DRAWING 65C27257 AND EAOct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980545Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 7R TIE CLIP. INSTALLED NEW STRINGER TIE CLIP PER PCI 1093, EO 5393G227. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980544Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION FOUND A .25 INCH CRACK BS 727A STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PER PCI 1093, EO 5393G227. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980543Web · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND A CRACK BL 0 BS 706, .6 INCH CRACK BS 708 .25 INCH CRACK BS 709 .6 INCH CRACK BS 710 .2 INCH CRACK BS 712 .15 INCH CRACK ON WEB. INSTALLED DOUBELR PER EA 62724A. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980534Skin · crackedCLT - DURING Q-CHECK VISUAL INSPECTION, FOUND A .20 INCH CRACK LEFT AFT ENTRY DOORWAY FORWARD LOWER CORNER BS 961, 2 INCHES ABOVE STRINGER 17L OF SKIN. INSTALLED TRIPLER PER REPAIR DOCUMENT 53-30-3 FIG 24. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980524Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 11 CORRODED AREAS BS 986.5 LBL 18 TO RBL 43 WL 208.1 OF FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED REPAIR T-CAP PER SRM 53-10-9 FIG 2. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA980518Stringer · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 927 STRINGER 25L. REPAIRED AREA PER SRM 53-10-1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA980517Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 1R TIE CLIP. REMOVED AND REPLACED PER EO 5393G227 REV 'A'. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980516Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 807 STRINGER 9R TIE CLIP. INSTALLED IDENTICAL PART PER EO 5393G227 REV 'A'. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980515Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 2R TIE CLIP. INSTALLED IDENTICAL PART PER EO 5393G227 REV 'A'. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980513Sill · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 294.5 WL 208.10 RBBL 53 FORWARD SERVICE ENTRY DOOR LOWER SILL INBOARD CHORD DOUBLER ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980512Skin · dentedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 1.5 INCH BY .062 INCH DENT 11 INCH AFT OF REAR ENTRY AND 18 INCH ABOVE LOWER DOOR SILL OF SKIN. INSTALLED DOUBLER PER SERM 53-30-3. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980511Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 767 STRINGER 19R OF SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980510Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 597 STRINGER 9R. INSTALLED MODIFIED PART PAR EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980509Clip · crackedCLT - DURIGN Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 8R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980508Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 5R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980507Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 685 STRINGER 4R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980506Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 747 STRINGER 9L TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980505Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 639 STRINGER 4L TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980504Clip · crackedCLT - DURING Q-5 CHECK VIAUL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 2R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980503Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 1R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980502Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 9R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAASB98214Battery Pack · dischargedCMH - PILOT REPORTED THE LEFT AFT SERVICE DOOR EMERGENCY EXIT LIGHT FLICKERS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Aug 19, 1998 · N268AU · Boeing 7372B7 · Emergency LightingSDR USAASB98170Anti-Ice Duct · blownPHL - FLT 993 - AFTER TAKEOFF FROM PHL, CREW OBSERVED A RAPID RISE IN THE NR 2 ENGINE CSD OIL TEMPERATURE FOLLOWED BY A NR 2 ENGINE OVERHEAT LIGHT. CREW REDUCED THRUST ON ENGINE AND OVERHEAT LIGHT WENT OUT. AIRCRAFT WAS AT FL 080 WHEN CREW MADE DECISION TO RJul 6, 1998 · N268AU · Boeing 7372B7 · Air Intake Anti/De-Ice SystemSDR USAASB98091Fuel Pump · defectiveBWI - FL 2197 - AFTER TAKEOFF AT 1,000 FEET, CAPTAIN THOUGHT HE HAD AN ENGINE FAILURE. THE NR 1 ENGINE FAILED TO RESPOND TO THRUST LEVER MOVEMENT. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT BWI WHERE THE FLIGHT LANDED WITHOUT INCIDENT. AN EApr 7, 1998 · N268AU · Boeing 7372B7 · Engine Fuel PumpSDR 98ZZZX1641Fuel Control · defectiveBWI - FL 2197 - AFTER TAKEOFF AT 1,000 FEET, CAPTAIN THOUGHT HE HAD AN ENGINE FAILURE. THE NR 1 ENGINE FAILED TO RESPOND TO THRUST LEVER MOVEMENT. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT BWI WHERE THE FLIGHT LANDED WITHOUT INCIDENT. AN EApr 7, 1998 · N268AU · Boeing 7372B7 · Fuel Control/Turbine EnginesSDR USAASB97281Battery Pack · dischargedSYR - MAINTENANCE FOUND THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT PANEL FAILS TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK NORMAL. (X)Sep 30, 1997 · N268AU · Boeing 7372B7 · Emergency LightingSDR USAASB97195Battery Pack · dischargedPHL - MAINTENANCE FOUND THE AFT ROW OF EMERGENCY ESCAPE PATH LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Jul 16, 1997 · N268AU · Boeing 7372B7 · Emergency LightingSDR 97ZZZM769Battery Pack · dischargedPHL - MAINTENANCE FOUND THE AFT ROW OF EMERGENCY ESCAPE PATH LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Jul 16, 1997 · N268AU · Boeing 7372B7 · Emergency LightingSDR USAASB97193Rod Assy · failedPHL - FL244 - DURING CLIMB-OUT FROM PHL AT APPROXIMATELY 21,000 FT, THE CABIN WAS AT 4 PSI DIFFERENTIAL WHEN THE AFT ENTRY DOOR WARNING LIGHT ILLUMINATED. FLIGHT ATTENDANT REPORTED THE AFT ENTRY DOOR HANDLE HAD POPPED UP. TRIED TO STOW IT BUT HANDLE WOULD NOJul 15, 1997 · N268AU · Boeing 7372B7 · Passenger/Crew DoorsSDR USAASB97085Battery Pack · dischargedCLT - FL 1499 - DURING FLIGHT, THE CENTER AISLE CEILING EMERGENCY LIGHTS IN THE MID CABIN FLICKER OFF AND ON. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND BATTERY CHARGER FOR THE CENTER AISLE CEILING EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. (M)Mar 20, 1997 · N268AU · Boeing 7372B7 · Emergency LightingSDR 97ZZZM475Battery Charger · failedCLT - FL 1499 - DURING FLIGHT, THE CENTER AISLE CEILING EMERGENCY LIGHTS IN THE MID CABIN FLICKER OFF AND ON. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND BATTERY CHARGER FOR THE CENTER AISLE CEILING EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. (M)Mar 20, 1997 · N268AU · Boeing 7372B7 · Emergency LightingSDR USAASB96259Battery Pack · dischargedROA - MAINTENANCE FOUND THE AFT LEFT AND RIGHT EXTERIOR EMERGENCY EXIT LGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT BATTERY PACKS LOCATED IN THE AFT CARGO COMPT. OPS CHECK GOOD. (M)Dec 14, 1996 · N268AU · Boeing 7372B7 · Emergency Lighting
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