# Service difficulty reports: N263AU, cancelled Aug 21, 2002 A list on [N263AU, cancelled Aug 21, 2002](https://openairdocs.org/deregistered/N263AU-2002-08-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 81 reports - [SDR USAASB01278](https://openairdocs.org/sdr/USAASB01278.md): Wire · damaged · Oct 2, 2001 · N263AU · Boeing 737201 · Light System Wiring > LGA - THE FLOOR PATH EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 7. MAINTENANCE REPAIRED A WIRE UNDER THE SEAT ASSEMBLY. (M) - [SDR USAASB01255](https://openairdocs.org/sdr/USAASB01255.md): Ballast · failed · Sep 10, 2001 · N263AU · Boeing 737201 · Lighting System > BWI-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 PLAC - [SDR USASB01255](https://openairdocs.org/sdr/USASB01255.md): Light · faulty · Sep 10, 2001 · N263AU · Boeing 737201 · Passenger Compartment Lighting > BWI-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 PLAC - [SDR USAASB01026](https://openairdocs.org/sdr/USAASB01026.md): Duct · leaking · Jan 28, 2001 · N263AU · Boeing 737201 · Air Intake Anti/De-Ice System > FLL - 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 - [SDR USAA002091](https://openairdocs.org/sdr/USAA002091.md): Intercostal · cracked · Dec 11, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND INTERCOSTAL CRACKED.5 INCH, FORWARD FASTENER, LBL 28, WL 195 STATION 179. REPAIRED PER SRM 53-10-11 FIG 7. (M) - [SDR USAA002090](https://openairdocs.org/sdr/USAA002090.md): Intercostal · cracked · Dec 11, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND INTERCOSTAL CRACKED.5 INCH, FORWARD FASTENER, RBL 28, WL 195 STATION 179. REPAIRED PER SRM 53-10-11 FIG 7. (M) - [SDR USAA002085](https://openairdocs.org/sdr/USAA002085.md): Bulkhead · cracked · Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, Bulkhead > CLT - FOUND WEB CRACKED.125 INCH, BS 178, WL 234, RBL 10. INSTALLED DOUBLER PER SRM 53-10-11 FIG 1. (M) - [SDR USAA002084](https://openairdocs.org/sdr/USAA002084.md): Bulkhead · cracked · Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, Bulkhead > CLT - FOUND WEB CRACKED TWO PLACES.5 INCH EACH, BS 178, WL 218, RBL 11 AND RBL 13. INSTALLED DOUBLER PER EA 68609A. (M) - [SDR USAA002083](https://openairdocs.org/sdr/USAA002083.md): Bulkhead · cracked · Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, Bulkhead > CLT - 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) - [SDR USAA002082](https://openairdocs.org/sdr/USAA002082.md): Intercostal · cracked · Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA002081](https://openairdocs.org/sdr/USAA002081.md): Bulkhead · cracked · Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Main, Bulkhead > CLT - FOUND WEB CRACKED TWO PLACES.5 INCH, BS 178, WL 207, LBL 1 AND RBL 1. INSTALLED DOUBLER PER EA 68609A. (M) - [SDR USAA002080](https://openairdocs.org/sdr/USAA002080.md): Structure · cracked · Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND SIDE CHORD.75 INCH, BS 178, WL 207, LBL 24. SPLICED IN NEW PART PER EO 5300V157 AND EA 68604. (M) - [SDR USAA002079](https://openairdocs.org/sdr/USAA002079.md): Structure · cracked · Dec 8, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND SIDE CHORD CRACKED.75 INCH, BS 178, WL 195, LBL 24. SPLICED IN NEW PART PER EO 5300V157 AND EA 68604. (M) - [SDR USAA002056](https://openairdocs.org/sdr/USAA002056.md): Bulkhead · cracked · Dec 4, 2000 · N263AU · Boeing 737201 · Fuselage Main, Bulkhead > CRACK BS178 WL234 LBL 13.25. CORRECTIVE ACTION: REMOVED DAMAGE & INSTALLED DOUBLER PER SRM 53-10-11 FIG 1 - [SDR USAASB00264](https://openairdocs.org/sdr/USAASB00264.md): Light · failed · Sep 20, 2000 · N263AU · Boeing 737201 · Emergency Lighting > ATL - 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) - [SDR USAASB00161](https://openairdocs.org/sdr/USAASB00161.md): Generator · failed · Jun 9, 2000 · N263AU · Boeing 737201 · AC Generator-Alternator > ORF - 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 GENERATO - [SDR USAASB00116](https://openairdocs.org/sdr/USAASB00116.md): Downlock Sensor · out of adj · Apr 17, 2000 · N263AU · Boeing 737201 · Landing Gear Position and Warning > ORD - 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, CAPTA - [SDR USAASB00093](https://openairdocs.org/sdr/USAASB00093.md): Separator · dirty · Mar 30, 2000 · N263AU · Boeing 737201 · Humidity Control System > CLT - 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. - [SDR USAASB00064](https://openairdocs.org/sdr/USAASB00064.md): Battery Pack · failed · Mar 6, 2000 · N263AU · Boeing 737201 · Emergency Lighting > CLE - MAINTENANCE FOUND THE OVERWING EMERGENCY EXIT SIGNS BLINKING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAA991500](https://openairdocs.org/sdr/USAA991500.md): Skin · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA991493](https://openairdocs.org/sdr/USAA991493.md): Floorbeam · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA991492](https://openairdocs.org/sdr/USAA991492.md): Angle · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991491](https://openairdocs.org/sdr/USAA991491.md): Web · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK BS 360, STRINGER 16L WEB. INSTALLED DOUBLER PER EA 66284. (M) - [SDR USAA991490](https://openairdocs.org/sdr/USAA991490.md): Doubler · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA991489](https://openairdocs.org/sdr/USAA991489.md): Frame · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Frame > CLT - 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) - [SDR USAA991488](https://openairdocs.org/sdr/USAA991488.md): Web · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991487](https://openairdocs.org/sdr/USAA991487.md): Floorbeam · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor Beam > CLT - DURNG Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 663, BL 0 FLOORBEAM. INSTALLED DOUBLER PER TR 57-10-04. (M) - [SDR USAA991486](https://openairdocs.org/sdr/USAA991486.md): Angle · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991485](https://openairdocs.org/sdr/USAA991485.md): Floorbeam · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA991484](https://openairdocs.org/sdr/USAA991484.md): Floorbeam · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA991483](https://openairdocs.org/sdr/USAA991483.md): Mount · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · VHF Communications System > CLT - 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) - [SDR USAA991482](https://openairdocs.org/sdr/USAA991482.md): Stringer · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - 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) - [SDR USAA991481](https://openairdocs.org/sdr/USAA991481.md): Angle · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991474](https://openairdocs.org/sdr/USAA991474.md): Floorbeam · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA991473](https://openairdocs.org/sdr/USAA991473.md): Angle · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991472](https://openairdocs.org/sdr/USAA991472.md): Fitting · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991471](https://openairdocs.org/sdr/USAA991471.md): Bracket · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991470](https://openairdocs.org/sdr/USAA991470.md): Bracket · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991469](https://openairdocs.org/sdr/USAA991469.md): Frame · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Frame > CLT - 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) - [SDR USAA991464](https://openairdocs.org/sdr/USAA991464.md): Floorbeam · corroded · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA991463](https://openairdocs.org/sdr/USAA991463.md): Shear Beam · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991455](https://openairdocs.org/sdr/USAA991455.md): Shear Tie · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991454](https://openairdocs.org/sdr/USAA991454.md): Bracket · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.50 INCH CRACK STATION 360 LEFT BRACKET. REMOVED AND REPLACED PER SRM 51-10-1. (M) - [SDR USAA991453](https://openairdocs.org/sdr/USAA991453.md): Skin · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA991407](https://openairdocs.org/sdr/USAA991407.md): Tie Clip · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991406](https://openairdocs.org/sdr/USAA991406.md): Tie Clip · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991405](https://openairdocs.org/sdr/USAA991405.md): Tie Clip · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991404](https://openairdocs.org/sdr/USAA991404.md): Tie Clip · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991403](https://openairdocs.org/sdr/USAA991403.md): Tie Clip · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA991402](https://openairdocs.org/sdr/USAA991402.md): Tie Clip · cracked · Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) Next page: https://openairdocs.org/deregistered/N263AU-2002-08-21/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N263AU-2002-08-21/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.