N263AU, cancelled Aug 21, 2002

Service difficulty reports · 81

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 = 'N263AU' AND deregistration_id = 'N263AU-2002-08-21'
  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 USAASB01278Wire · damagedLGA - THE FLOOR PATH EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 7. MAINTENANCE REPAIRED A WIRE UNDER THE SEAT ASSEMBLY. (M)Oct 2, 2001 · N263AU · Boeing 737201 · Light System WiringSDR USAASB01255Ballast · failedBWI-MDW - FLT 2735 - DURING CRUISE, SMOKE WAS REPORTED IN THE AFT GALLEY. THE AFT GALLEY CIRCUIT BREAKER WAS PULLED AND THE SMOKE SUBSIDED. THE FLIGHT CREW DECIDED TO DIVERT TO PIT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AFT GALLEY WORK LIGHT WAS PLACSep 10, 2001 · N263AU · Boeing 737201 · Lighting SystemSDR USASB01255Light · faultyBWI-MDW - FLT 2735 - DURING CRUISE, SMOKE WAS REPORTED IN THE AFT GALLEY. THE AFT GALLEY CIRCUIT BREAKER WAS PULLED AND THE SMOKE SUBSIDED. THE FLIGHT CREW DECIDED TO DIVERT TO PIT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AFT GALLEY WORK LIGHT WAS PLACSep 10, 2001 · N263AU · Boeing 737201 · Passenger Compartment LightingSDR USAASB01026Duct · leakingFLL - FLT 2626 - ON CLIMB-OUT FROM FLL, AT 6,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED PROCEDURES, REDUCED POWER TO IDLE AND LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT FLL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY Jan 28, 2001 · N263AU · Boeing 737201 · Air Intake Anti/De-Ice SystemSDR USAA002091Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, FORWARD FASTENER, LBL 28, WL 195 STATION 179. REPAIRED PER SRM 53-10-11 FIG 7. (M)Dec 11, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002090Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, FORWARD FASTENER, RBL 28, WL 195 STATION 179. REPAIRED PER SRM 53-10-11 FIG 7. (M)Dec 11, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002085Bulkhead · crackedCLT - FOUND WEB CRACKED .125 INCH, BS 178, WL 234, RBL 10. INSTALLED DOUBLER PER SRM 53-10-11 FIG 1. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002084Bulkhead · crackedCLT - FOUND WEB CRACKED TWO PLACES .5 INCH EACH, BS 178, WL 218, RBL 11 AND RBL 13. INSTALLED DOUBLER PER EA 68609A. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002083Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, FORWARD FASTENER RBL 28, WL 207, STATION 179. INSTALLED NEW WEB SECTION PER SRM 51-10-01 AND 51-30-0. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002082Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, FORWARD FASTENER LBL 28, WL 207, STATION 179. INSTALLED NEW WEB SECTION PER SRM 51-30-0 AND 51-10-01. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002081Bulkhead · crackedCLT - FOUND WEB CRACKED TWO PLACES .5 INCH, BS 178, WL 207, LBL 1 AND RBL 1. INSTALLED DOUBLER PER EA 68609A. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002080Structure · crackedCLT - FOUND SIDE CHORD .75 INCH, BS 178, WL 207, LBL 24. SPLICED IN NEW PART PER EO 5300V157 AND EA 68604. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002079Structure · crackedCLT - FOUND SIDE CHORD CRACKED .75 INCH, BS 178, WL 195, LBL 24. SPLICED IN NEW PART PER EO 5300V157 AND EA 68604. (M)Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002056Bulkhead · crackedCRACK BS178 WL234 LBL 13.25. CORRECTIVE ACTION: REMOVED DAMAGE & INSTALLED DOUBLER PER SRM 53-10-11 FIG 1Dec 4, 2000 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAASB00264Light · failedATL - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHT ABOVE THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Sep 20, 2000 · N263AU · Boeing 737201 · Emergency LightingSDR USAASB00161Generator · failedORF - FLT 1297 - A FEW MINUTES AFTER TAKEOFF FROM ORF, THE FILGHT LOST THE NR 2 GENERATOR WHICH CAUSED THE GASPER FAN AND NR 2 AND NR 3 TRANSFORMER RECTIFIER CIRCUIT BREAKERS TO POP. CREW TRIED TO RESET CIRCUIT BREAKERS BUT THEY WOULD NOT RESET. THE GENERATOJun 9, 2000 · N263AU · Boeing 737201 · AC Generator-AlternatorSDR USAASB00116Downlock Sensor · out of adjORD - FLT 2287 - ON APPROACH INTO ORD, WITH THE LANDING GEAR LOWERED, ALL THREE GEAR GREEN LIGHTS WERE ILLUMINATED. SUDDENLY, THE RIGHT MAIN LANIDNG GEAR RED LIGHT ILLUMINATED. CAPTAIN ACCOMPLISHED CHECKLIST AND DECLARED AN EMERGENCY. AS A PRECAUTION, CAPTAApr 17, 2000 · N263AU · Boeing 737201 · Landing Gear Position and WarningSDR USAASB00093Separator · dirtyCLT - FLT 1282 - ON DESCENT INTO CLT, AN ODOR WAS NOTED IN THE FLIGHT COMPARTMENT LIKE THAT OF DIRTY GYM SOCKS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WATER SEPARATOR BAGS PER MM. OPERATIONAL CHECK AND LEAK CHECK GOOD. Mar 30, 2000 · N263AU · Boeing 737201 · Humidity Control SystemSDR USAASB00064Battery Pack · failedCLE - MAINTENANCE FOUND THE OVERWING EMERGENCY EXIT SIGNS BLINKING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Mar 6, 2000 · N263AU · Boeing 737201 · Emergency LightingSDR USAA991500Skin · crackedCLT - DURING Q-1 CHECK EDDY CURRENT AND VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 330, STRINGER 17R LOWER FORWARD CORNER OF FORWARD SERVICE DOOR. INSTALLED DOUBLER, TRIPLER AND QUADRUPLER PER SRM 53-30-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA991493Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH AREA OF CORROSION AT BS 328, RBL 19 FLOORBEAM. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-9. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991492Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 178 BULKHEAD AFT SIDE LBL 5 VERTICAL ANGLE. INSTALLED REPAIR ANGLE PER SRM 53-10-11. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991491Web · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK BS 360, STRINGER 16L WEB. INSTALLED DOUBLER PER EA 66284. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991490Doubler · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 1138, STRINGER 5R HORIZONTAL STAB CUTOUT DOUBLER.. INSTALLED FILLER AND DOUBLER PER EA 66420 AND SRM 53-00-01 FIG 201. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA991489Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 597 JUST BELOW STRINGER 17R FRAME. INSTALLED DOUBLER PER SRM 53-10-2 FIG 5 AND EA 66417. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, FrameSDR USAA991488Web · crackedCLT - DURNG Q-1 CHECK VISUAL INSPECTION, FOUND 5 CRACKS .25 INCH STATION 706-717, RBL 24, WL 202 WEB. INSTALLED FILLER AND DOUBLER PER SRM 51-40-2 FIG 1. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991487Floorbeam · crackedCLT - DURNG Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 663, BL 0 FLOORBEAM. INSTALLED DOUBLER PER TR 57-10-04. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991486Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .625 INCH CRACK UPPER CHORD BULKHEAD STATION 663, RBL 24, WL 202 ANGLE. INSTALLED REPAIR ANGLE PER TR 57-10-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991485Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 17 INCHES TOP OF FLOORBEAM STATION 986, RBL 7-11, CORROSION LEVEL 1. REPLACED T-CAP PER SRM 5. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991484Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION STATION 1006, LBL 29 FLOORBEAM, CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-10-09 FIG 7. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991483Mount · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION STATION 777, BL 0 VHF ANTENNA MOUNT. CORRSION LEVEL 1. REPLACED PART PER 51-10-01 AND 51-30-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · VHF Communications SystemSDR USAA991482Stringer · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION BS 993, STRINGER 20R, CORROSION LEVEL 1. SPLICED IN NEW SECTION PER SRM 53-10-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA991481Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION STATION 344, LBL 65 FORWARD ENTRY DOOR Z-ANGLE. CORROSON LEVEL 2. REPLACED Z-ANGLE PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991474Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 34 INCH AREA OF CORROSION STATION 294.5, LBL 13 TO RBL 21 FLOORBEAM, CORROSION LEVEL 2. REPAIRED PER TR 53-10-04B. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991473Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 16 INCH AREA OF CORROSION STATION 259, RBL 9 - LBL 8 SUPPORT ANGLE/FLOOR. CORROSION LEVEL 1. REPLACED CHORD ANGLES, FLOOR PANEL, FILLERS, SPLICE AND VERTICAL ANGLES PER TR 53-10-16. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991472Fitting · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 727, BL 0, WL 206 FITTING. INSTALLED REPLACEMENT FITTING AND MOD PER EO 5394G176. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991471Bracket · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 322.5, LBL 65 BRACKET. FABRICATED BRACKET PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991470Bracket · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK UNDER FORWARD ENTRY DOOR STATION 322 BRACKET. FABRICATED BRACKET PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991469Frame · crackedCLT - DURNG Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 663, WL 202, LBL 24 UPPER CHORD. INSTALLED DOUBLER PER TR 57-10-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, FrameSDR USAA991464Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 794.3, STRINGER 26R FLOOR SUPPORT BEAM, CORROSION LEVEL 2. INSTALLED NEW FLOOR SUPPORT SECTION PER SRM 53-10-05. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991463Shear Beam · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK INBOARD AFT EDGE 18A SHEAR BEAM LEFT SIDE. INSTALLED NEW PARTS PE REPAIR DOCUMENT 51-10-1. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991455Shear Tie · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 616 STRINGER 4R SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991454Bracket · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK STATION 360 LEFT BRACKET. REMOVED AND REPLACED PER SRM 51-10-1. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991453Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 CRACKS APPROX 1.5 INCH LONG AT BS 960 AFT SERVICE DOOR CUTOUT LOWER FORWARD CORNER SKIN. INSTALLED FILLER, DOUBLER AND TRIPLER PER SRM 53-30-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA991407Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 887, STRINGER 6L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991406Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 344, STRINGER 11R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991405Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B, STRINGER 6 TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991404Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 787, STRINGER 7R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991403Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 847, STRINGER 10L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991402Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867, STRINGER 4L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure
Back to N263AU, cancelled Aug 21, 2002