# Service difficulty reports: N276AU, cancelled Oct 30, 2003 A list on [N276AU, cancelled Oct 30, 2003](https://openairdocs.org/deregistered/N276AU-2003-10-30.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 · 73 reports - [SDR USAA002219](https://openairdocs.org/sdr/USAA002219.md): Structure · cracked · Dec 29, 2000 · N276AU · Boeing 7372B7 · Fuselage Main, Bulkhead > CLT - FOUND VERTICAL CHORD CRACKED.5 INCH, BS 178 BULKHEAD AFT SIDE LBL 5.7, WL 184. REPAIRED PER SRM 53-10-11 FIG 8 AND EA 68672. (M) - [SDR USAA002216](https://openairdocs.org/sdr/USAA002216.md): Intercostal · cracked · Dec 28, 2000 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND 178 BULKHEAD INTERCOSTAL 3 INCHES CRACKED, WL 195 INTERCOSTAL AFT OF STATION 18 BULKHEAD RBL 24. REPAIRED PER EO 5300V157. (M) - [SDR USAA002215](https://openairdocs.org/sdr/USAA002215.md): Intercostal · cracked · Dec 28, 2000 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND 178 BULKHEAD INTERCOSTAL CRACKED 3 INCHES, WL 195, INTERCOSTAL JUST AFT STATION 178 BULKHEAD LBL 24. REPAIRED PER EO 5300V157. (M) - [SDR USAA002211](https://openairdocs.org/sdr/USAA002211.md): Bulkhead · cracked · Dec 27, 2000 · N276AU · Boeing 7372B7 · Fuselage Main, Bulkhead > CLT - FOUND BULKHEAD WEB CRACKED.25 INCH, BS 178, WL 234, RBL 10. INSTALLED DOUBLER PER SRM 53-10-11. (M) - [SDR USAA002048](https://openairdocs.org/sdr/USAA002048.md): Channel · corroded · Nov 30, 2000 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CORROSION LEVEL 2 AFT DRAIN MAST SUPPORT CHANNEL. CORRECTIVE ACTION: INSTALLED NEW PART PER SRM 51-10-1 STEP 6 - [SDR USAA991344](https://openairdocs.org/sdr/USAA991344.md): Floorbeam · corroded · Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM APPROX 6 FT FORWARD CABIN STATION 328 - RBL 51. CORROSION LEVEL. INSTALLED DOUBLER PER TR 53-10-13. (M) - [SDR USAA991294](https://openairdocs.org/sdr/USAA991294.md): Skin · cracked · Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND A 2.25 INCH CRACK AT BS 324 STRINGER 17R SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 26. (M) - [SDR USAA991293](https://openairdocs.org/sdr/USAA991293.md): Skin · cracked · Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A..250 INCH CRACK AT BS 806 STRINGER 13L LOWER HINGE CUTOUT SKIN. INSTALLED FILLER AND DOUBLER PER SRM 53-30-03. (M) - [SDR USAA991292](https://openairdocs.org/sdr/USAA991292.md): Tie Clip · cracked · Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A..25 INCH CRACK AT BS 727B STRINGER 2-23 TIE CLIP. REMOVED AND REPLACED PER SRM 51-10-1. (M) - [SDR USAA991291](https://openairdocs.org/sdr/USAA991291.md): Skin · cracked · Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK AT RIGHT AFT SERVICE DOOR UPPER HINGE CUTOUT SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR USAA991290](https://openairdocs.org/sdr/USAA991290.md): Fitting · corroded · Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT BS 1016, STRINGER 20R TIE FITTING. CORROSION LEVEL 1. REMOVED CORROSION AND PRIMED PER SRM 51-10-06. (M) - [SDR USAA991289](https://openairdocs.org/sdr/USAA991289.md): Floorbeam · corroded · Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 20 INCH BY 2 FT AT STATION 344, LBL 10 RBL 10 T-CAP. CORROSION LEVEL 2. FABRICATED NEW T-CAP PER TR 53-10-13. (M) - [SDR USAA991284](https://openairdocs.org/sdr/USAA991284.md): Skin · corroded · Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURNG Q-6 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY4 INCH AREA OF CORROSION AT STATION 500B STRINGER 27R SKIN. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR USAASB99217](https://openairdocs.org/sdr/USAASB99217.md): Light · inoperative · Aug 8, 1999 · N276AU · Boeing 7372B7 · Emergency Lighting > CLT - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT IN THE COCKPIT REMAINS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AS PER THE MM. OPERATIONAL CHECK GOOD. (M) - [SDR USAA990626](https://openairdocs.org/sdr/USAA990626.md): Skin · cracked · Jun 28, 1999 · N276AU · Boeing 7372B7 · Service Doors > TPA - DURING CX-3 VISUAL INSPECTION, FOUND TWO CRACKS, ONE CRACK.125 INCH AND ONE CRACK.25 INCH LOWER HINGE CUTOUT AT FORWARD SERVICE DOOR SKIN. INSTALLED FILLER, DOUBLER AND FASTENERS PER TR 52-10-01A. (M) - [SDR USAASB98173](https://openairdocs.org/sdr/USAASB98173.md): Outflow Valve · failed · Jul 7, 1998 · N276AU · Boeing 7372B7 · Pressure Regulator/Outflow Valve > PHL - FLT 221 - AIRCRAFT DEPARTED PHL WITH THE RIGHT AIR CONDITIONING PACK ON MEL. AFTER TAKEOFF, CREW COULD NOT GET THE LEFT PACK TO PRESSURIZE AIRCRAFT. DECISION WAS MADE TO RETURN TO FIELD AT PHL. FLT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. - [SDR USAA980301](https://openairdocs.org/sdr/USAA980301.md): Skin · crack · Jul 3, 1998 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURING CX-2 CHECK EDDY CURRENT, FOUND A.25 INCH CRACK IN SKIN RT AFT SERVICE DOOR LOWER HINGE CUT-OUT ON SKIN. INSTALLED DOUBLER AND TRIPPLER PER SRM 53-30-3 FIG 33. (X) - [SDR USAA980296](https://openairdocs.org/sdr/USAA980296.md): Skin · cracked · Jul 3, 1998 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURING A DROP-IN VISUAL INSPECTION, FOUND A CRACK AT FORWARD ENTRY DOOR SKIN AT LOWER AFT CUT-OUT. INSTALLED DOUBLER/TRIPLER PER EA 41616. (X) - [SDR USAA980295](https://openairdocs.org/sdr/USAA980295.md): Skin · cracked · Jul 3, 1998 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURING CX-2 CHECK EDDY CURRENT, FOUND A.25 INCH CRACK IN SKIN RIGHT AFT SERVICE DOOR LOWER HINGE CUT-OUT. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 33. (X) - [SDR USAASB98082](https://openairdocs.org/sdr/USAASB98082.md): Power Supply · inoperative · Mar 28, 1998 · N276AU · Boeing 7372B7 · Emergency Lighting > CMH - MAINTENANCE FOUND ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. MAINTENANCE FOUND ALL EMERGENCY LIGHT BATTERIES DEAD. CHARGED ALL BATTERIES FOR FIVE HOURS, THEN REMOVED AND REPLACED BATTERY PACKS FOR THE INTERIOR LIGHTS ABOVE THE MAIN ENTRANCE DOOR - [SDR USAASB98029](https://openairdocs.org/sdr/USAASB98029.md): Power Supply · inoperative · Jan 27, 1998 · N276AU · Boeing 7372B7 · Emergency Lighting > ROA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD. (M) - [SDR 98ZZZM290](https://openairdocs.org/sdr/98ZZZM290.md): Battery Pack · discharged · Jan 27, 1998 · N276AU · Boeing 7372B7 · Emergency Lighting > ROA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD. (M) - [SDR USAASB97353](https://openairdocs.org/sdr/USAASB97353.md): Anti-Ice Duct · cracked · Dec 29, 1997 · N276AU · Boeing 7372B7 · Air Intake Anti/De-Ice System > PIT - FL 1223 - DURING CLIMB-OUT OF PIT AT APPROX 12,9000 FT, THE START VALVE OPEN LIGHT ILLUMINATED ON THE NR 2 ENGINE. CREW FOLLOWED CHECKLIST AND SHUT DOWN THE NR 2 ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT PIT WHERE IT LANDED - [SDR USAASB97350](https://openairdocs.org/sdr/USAASB97350.md): Shutoff Vlv · failed · Dec 28, 1997 · N276AU · Boeing 7372B7 · Engine Start Valves/Controls > PIT - FLT 1090 - FLT DIVERTED TO PIT DUE TO A NR 2 ENGINE START VALVE INDICATOR LIGHT ILLUMINATING. CREW SHUT DOWN THE NR 2 ENGINE IN FLIGHT AND DECLARED AND EMERGENCY. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. - [SDR 98ZZZM142](https://openairdocs.org/sdr/98ZZZM142.md): Switch · failed · Dec 28, 1997 · N276AU · Boeing 7372B7 · Engine Start Valves/Controls > PIT - FLT 1090 - FLT DIVERTED TO PIT DUE TO A NR 2 ENGINE START VALVE INDICATOR LIGHT ILLUMINATING. CREW SHUT DOWN THE NR 2 ENGINE IN FLIGHT AND DECLARED AND EMERGENCY. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. - [SDR 98ZZZM141](https://openairdocs.org/sdr/98ZZZM141.md): Shutoff Vlv · failed · Dec 28, 1997 · N276AU · Boeing 7372B7 · Engine Start Valves/Controls > PIT - FLT 1090 - FLT DIVERTED TO PIT DUE TO A NR 2 ENGINE START VALVE INDICATOR LIGHT ILLUMINATING. CREW SHUT DOWN THE NR 2 ENGINE IN FLIGHT AND DECLARED AND EMERGENCY. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. - [SDR USAASB97263](https://openairdocs.org/sdr/USAASB97263.md): Oil Filter Stud · stripped · Sep 23, 1997 · N276AU · Boeing 7372B7 · Turbine Engine Oil System > ORF - FLT 1721 - DURING CLIMB-OUT FL230 TO FL350 THE CREW NOTICED THE OIL PRESSURE LIGHT ON AND THE OIL QUANTITY RAPIDLY DECREASING ON THE LEFT ENGINE. THE LEFT ENGINE WAS SHUT DOWN AS A PRECAUTIONARY WHEN THE OIL PRESSURE REACHED 20 PSI. AN EMERGENCY WAS DE - [SDR USAASB97261](https://openairdocs.org/sdr/USAASB97261.md): Battery · discharged · Sep 21, 1997 · N276AU · Boeing 7372B7 · Emergency Lighting > BOS - LEFT AND RIGHT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB97149](https://openairdocs.org/sdr/USAASB97149.md): Light · inoperative · May 16, 1997 · N276AU · Boeing 7372B7 · Emergency Lighting > ORD - MAINTENANCE FOUND THE EMERGENCY FLOOR TRACK LIGHT INOP AT SEAT 19D. MAINTENANCE REPLACED SOCKET ASSEMBLY, REPAIRED WIRING AND RELAMPED. OPS CHECK NORMAL. (M) - [SDR USAASB97111](https://openairdocs.org/sdr/USAASB97111.md): Hydraulic Pump · failed · Apr 22, 1997 · N276AU · Boeing 7372B7 · Hydraulic Pump (Electric/Engine), Main > GSO - FLT 1046 - EN ROUTE MCO TO LGA, A-HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. HYD SYSTEM QTY WENT FROM 4 TO 1.5 GALLONS. DECLARED EMERGENCY AND DIVERTED TO GSO LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED NR 2 ENG DRIVEN HYD PUMP, REPLACED CA - [SDR USAA960666](https://openairdocs.org/sdr/USAA960666.md): Skin · cracked · Oct 7, 1996 · N276AU · Boeing 7372B7 · Emergency Lighting > ROA - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND.25 INCH CRACK FORWARD ENTRY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN, BONDED DOUBLER AND BEAR STRAP. INSTALLED STRAPS, REPAIRED PER EA 41616 INTERIM REPAIR. (M) - [SDR USAASB96129](https://openairdocs.org/sdr/USAASB96129.md): Fuel Hose · failed · Jul 15, 1996 · N276AU · Boeing 7372B7 · Aircraft Fuel Distribution System > BWI - FLT 1176 - EN ROUTE FROM MCO TO BDL, CAPTAIN NOTICED WHAT APPEARED TO BE A FUEL LOSS AND SUSPECTED A FUEL LEAK. CAPTAIN DECLARED AN EMERENCY AND THE FLIGHT DIVERTED TO BWI. AFTER LANDING SAFELY AND EXITING RUNWAY, FIRE DEPARTMENT TOLD CREW A BAD FUEL L - [SDR USAASB96056](https://openairdocs.org/sdr/USAASB96056.md): Oil System · over serviced · Mar 27, 1996 · N276AU · Boeing 7372B7 · Turbine Engine Oil System > MIA FL - 652 - AFTER TAKEOFF, CREW NOTED OIL PRESSURE RISE ON LEFT ENGINE. CREW REDUCED POWER ON ENGINE AND NOTED OIL TEMPERATURE RISE. CREW SECURED THE LEFT ENGINE. FLIGHT RETURNED TO MIA AND LANDED WITH NO FURTHER INCIDENT. SET - 12 MINUTES. MAINTENANCE - [SDR USAASB96055](https://openairdocs.org/sdr/USAASB96055.md): Engine · failed · Mar 24, 1996 · N276AU · Boeing 7372B7 · Engine (Turbine/Turboprop) > FLT NR 571 - CLT - NR 1 ENGINE WAS SHUT DOWN IN FLIGHT. LOUD BANG WAS HEARD AND SHORTLY THERE AFTER THE ENGINE FAILED. NO FIRE WARNING OR OTHER INDICATIONS WERE NOTED. TOTAL SINGLE ENGINE TIME WAS APPROXIMATELY 30 MINUTES. MAINTENANCE REPLACED NR 1 ENGINE - [SDR USAA960054](https://openairdocs.org/sdr/USAA960054.md): Intercostal · corrosion · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREA ON INTERCOSTAL.5 INCH BY.25 INCH AT BS 986 TO BS 1006 APPROXIMATELY LBL 18 INCHES. REPLACED WITH IDENTICAL PART NR 1121963. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROS - [SDR USAA960053](https://openairdocs.org/sdr/USAA960053.md): Floor Beam · corrosion · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Floor Beam > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 21 INCHES CORRODED AREA AT FLOOR BEAM BS 947 RBL 10 TO LBL 11. REPAIRED T-CAP. REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02. CORROSION LEVEL 1. (M) - [SDR USAA960052](https://openairdocs.org/sdr/USAA960052.md): Floor Beam · corrosion · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Floor Beam > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 38 INCHES IN LENGTH UPPER FLANGE CABIN FLOOR BEAM BS 967 LBL 10-RBL 28. INSTALLED T-CAP REPAIR. REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) - [SDR USAA960051](https://openairdocs.org/sdr/USAA960051.md): Floor Beam · corrosion · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Floor Beam > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SPOTS OF CORROSION AT FLOOR BOARD BEAM ATTACH HOLES BS 986.5 LBL 18 TO RIGHT END. INSTALLED REPLACEMENT T-CAP. REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 1. (M) - [SDR USAA960050](https://openairdocs.org/sdr/USAA960050.md): Tie Clip · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK STATION 616, STRINGER 2L TIE CLIP. INSTALLED NEW TIE CLIP. REPAIRED PER EO 5393G227. (M) - [SDR USAA960049](https://openairdocs.org/sdr/USAA960049.md): Clip · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK IN STRINGER CLIP, AT BS 639 STRINGER 6R. REPLACED CLIP, REPAIRED PER EO 5393G227. (M) - [SDR USAA960048](https://openairdocs.org/sdr/USAA960048.md): Frame · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Frame > INT - DURING Q-5 CHECK, EDDY CURRENT FOUND.5 INCH CRACK AT BS 400 STRINGER 25L TO STRINGER 26L. INSTALLED DOUBLER, REPAIRED PER EA 40544. (M) - [SDR USAA960047](https://openairdocs.org/sdr/USAA960047.md): Frame · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Frame > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 597 RIGHT FRAME OUTBOARD FLANGE RADIUS JUST ABOVE CENTER WING. REMOVED AND REPLACED FRAME PER DRAWING 65-46538. NO WEIGHT CHANGE. (M) - [SDR USAA960046](https://openairdocs.org/sdr/USAA960046.md): Frame · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Frame > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK STATION 616 RIGHT FRAME INBOARD INNER CHORD ANGLE FIRST FASTENER ABOVE CENTER WING. INSTALLED FILLER AND REPAIR ANGLE. REPAIRED PER EA 40570. (M) - [SDR USAA960045](https://openairdocs.org/sdr/USAA960045.md): Floor Beam · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Floor Beam > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO.25 INCH CRACKS RBL 25 LONGITUDINAL FLOOR BEAM LOWER WEB STATION 707-708, WL 203 AT FASTENER HOLES. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) - [SDR USAA960044](https://openairdocs.org/sdr/USAA960044.md): Floor Beam · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Floor Beam > INT -DURING Q-5 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK BL 0 LONGITUDINAL FLOOR BEAM LOWER WEB STATION 707 WL 203 AT FASTENER HOLE. INSTALLED DOUBLER, REPAIRED PER BOEING REF DRAWING 65C34537. (M) - [SDR USAA960043](https://openairdocs.org/sdr/USAA960043.md): Inner Chord · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Main, Frame > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK STATION 616 LEFT FRAME INBOARD INNER CHORD ANGLE FIRST FASTENER ABOVE CENTER WING. INSTALLED FILLER AND ANGLE. REPAIRED PER EA 40570. (M) - [SDR USAA960042](https://openairdocs.org/sdr/USAA960042.md): Clip · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.1250 INCH CRACK IN STRINGER 5R TIE CLIP, BS 727 B. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M) - [SDR USAA960041](https://openairdocs.org/sdr/USAA960041.md): Clip · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.1250 INCH CRACK IN STRINGER 10R TIE CLIP AT BS 747. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M) - [SDR USAA960040](https://openairdocs.org/sdr/USAA960040.md): Clip · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > DURING Q-5 CHECK VISUAL INSPECTION, FOUND.1250 INCH CRACK IN STRINGER 3L, BS 747 AT STRINGER TIE CLIP. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M) - [SDR USAA960039](https://openairdocs.org/sdr/USAA960039.md): Clip · cracked · Jan 5, 1996 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.1250 INCH CRACK IN STRINGER 7R TIE CLIP, BS 727B. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M) Next page: https://openairdocs.org/deregistered/N276AU-2003-10-30/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 = 'N276AU' AND deregistration_id = 'N276AU-2003-10-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N276AU-2003-10-30/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.