# Service difficulty reports: N268AU, cancelled Dec 9, 2003 A list on [N268AU, cancelled Dec 9, 2003](https://openairdocs.org/deregistered/N268AU-2003-12-09.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 · 56 reports - [SDR USAASB01321](https://openairdocs.org/sdr/USAASB01321.md): Wire · broken · Nov 20, 2001 · N268AU · Boeing 7372B7 · Light System Wiring > PVD - THE EMERGENCY LIGHT AT SEAT 12 WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. (M) - [SDR USAA010622](https://openairdocs.org/sdr/USAA010622.md): Skin · cracked · Jun 8, 2001 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAASB0279](https://openairdocs.org/sdr/USAASB0279.md): Fuel Control · failed · Sep 30, 2000 · N268AU · Boeing 7372B7 · Fuel Control/Turbine Engines > BWI - 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. F - [SDR USAA001138](https://openairdocs.org/sdr/USAA001138.md): Frame · corroded · Aug 1, 2000 · N268AU · Boeing 7372B7 · Fuselage Main, Frame > TPA - 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) - [SDR USAASB00190](https://openairdocs.org/sdr/USAASB00190.md): Structure · vibration · Jul 16, 2000 · N268AU · Boeing 7372B7 · Fuselage Main, Structure > PVD - 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 DIV - [SDR USAASB00153](https://openairdocs.org/sdr/USAASB00153.md): Flap · jammed · Jun 1, 2000 · N268AU · Boeing 7372B7 · Trailing Edge Flap Control System > TPA - 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 WIT - [SDR USAASB00134](https://openairdocs.org/sdr/USAASB00134.md): Hose · failed · May 6, 2000 · N268AU · Boeing 7372B7 · Hydraulic System, Main > IAD - 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 - [SDR USAASB00131](https://openairdocs.org/sdr/USAASB00131.md): Start Valve · failed · May 3, 2000 · N268AU · Boeing 7372B7 · Engine Start Valves/Controls > TPA - 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 FU - [SDR USAASB00121](https://openairdocs.org/sdr/USAASB00121.md): Actuator · failed · Apr 23, 2000 · N268AU · Boeing 7372B7 · Leading Edge Slat Actuator > ATL - 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 RE - [SDR USAASB99199](https://openairdocs.org/sdr/USAASB99199.md): Compressor · stalled · Aug 11, 1999 · N268AU · Boeing 7372B7 · Turbine Engine Compressor Section > BOS - 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 PREPPED - [SDR USAASB99150](https://openairdocs.org/sdr/USAASB99150.md): Wire Harness · failed · Jun 20, 1999 · N268AU · Boeing 7372B7 · Fuel System Wiring > RDU - 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 GA - [SDR USAASB98304](https://openairdocs.org/sdr/USAASB98304.md): Battery Pack · discharged · Nov 13, 1998 · N268AU · Boeing 7372B7 · Emergency Lighting > PHL - MAINTENANCE FOUND THE AFT CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) - [SDR USAA980554](https://openairdocs.org/sdr/USAA980554.md): Skin · creased · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA980553](https://openairdocs.org/sdr/USAA980553.md): Skin · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA980552](https://openairdocs.org/sdr/USAA980552.md): Stringer · corroded · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer > CLT - 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) - [SDR USAA980551](https://openairdocs.org/sdr/USAA980551.md): Angle · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > DURING 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) - [SDR USAA980550](https://openairdocs.org/sdr/USAA980550.md): Sill · corroded · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980546](https://openairdocs.org/sdr/USAA980546.md): Skin · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - 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 EA - [SDR USAA980545](https://openairdocs.org/sdr/USAA980545.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980544](https://openairdocs.org/sdr/USAA980544.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980543](https://openairdocs.org/sdr/USAA980543.md): Web · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980534](https://openairdocs.org/sdr/USAA980534.md): Skin · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA980524](https://openairdocs.org/sdr/USAA980524.md): Floorbeam · corroded · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA980518](https://openairdocs.org/sdr/USAA980518.md): Stringer · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 927 STRINGER 25L. REPAIRED AREA PER SRM 53-10-1. (M) - [SDR USAA980517](https://openairdocs.org/sdr/USAA980517.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980516](https://openairdocs.org/sdr/USAA980516.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980515](https://openairdocs.org/sdr/USAA980515.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980513](https://openairdocs.org/sdr/USAA980513.md): Sill · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980512](https://openairdocs.org/sdr/USAA980512.md): Skin · dented · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA980511](https://openairdocs.org/sdr/USAA980511.md): Skin · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA980510](https://openairdocs.org/sdr/USAA980510.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980509](https://openairdocs.org/sdr/USAA980509.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980508](https://openairdocs.org/sdr/USAA980508.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980507](https://openairdocs.org/sdr/USAA980507.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980506](https://openairdocs.org/sdr/USAA980506.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980505](https://openairdocs.org/sdr/USAA980505.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980504](https://openairdocs.org/sdr/USAA980504.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980503](https://openairdocs.org/sdr/USAA980503.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA980502](https://openairdocs.org/sdr/USAA980502.md): Clip · cracked · Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAASB98214](https://openairdocs.org/sdr/USAASB98214.md): Battery Pack · discharged · Aug 19, 1998 · N268AU · Boeing 7372B7 · Emergency Lighting > CMH - PILOT REPORTED THE LEFT AFT SERVICE DOOR EMERGENCY EXIT LIGHT FLICKERS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB98170](https://openairdocs.org/sdr/USAASB98170.md): Anti-Ice Duct · blown · Jul 6, 1998 · N268AU · Boeing 7372B7 · Air Intake Anti/De-Ice System > PHL - 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 R - [SDR USAASB98091](https://openairdocs.org/sdr/USAASB98091.md): Fuel Pump · defective · Apr 7, 1998 · N268AU · Boeing 7372B7 · Engine Fuel Pump > BWI - 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 E - [SDR 98ZZZX1641](https://openairdocs.org/sdr/98ZZZX1641.md): Fuel Control · defective · Apr 7, 1998 · N268AU · Boeing 7372B7 · Fuel Control/Turbine Engines > BWI - 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 E - [SDR USAASB97281](https://openairdocs.org/sdr/USAASB97281.md): Battery Pack · discharged · Sep 30, 1997 · N268AU · Boeing 7372B7 · Emergency Lighting > SYR - MAINTENANCE FOUND THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT PANEL FAILS TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK NORMAL. (X) - [SDR USAASB97195](https://openairdocs.org/sdr/USAASB97195.md): Battery Pack · discharged · Jul 16, 1997 · N268AU · Boeing 7372B7 · Emergency Lighting > PHL - 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) - [SDR 97ZZZM769](https://openairdocs.org/sdr/97ZZZM769.md): Battery Pack · discharged · Jul 16, 1997 · N268AU · Boeing 7372B7 · Emergency Lighting > PHL - 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) - [SDR USAASB97193](https://openairdocs.org/sdr/USAASB97193.md): Rod Assy · failed · Jul 15, 1997 · N268AU · Boeing 7372B7 · Passenger/Crew Doors > PHL - 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 NO - [SDR USAASB97085](https://openairdocs.org/sdr/USAASB97085.md): Battery Pack · discharged · Mar 20, 1997 · N268AU · Boeing 7372B7 · Emergency Lighting > CLT - 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) - [SDR 97ZZZM475](https://openairdocs.org/sdr/97ZZZM475.md): Battery Charger · failed · Mar 20, 1997 · N268AU · Boeing 7372B7 · Emergency Lighting > CLT - 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) - [SDR USAASB96259](https://openairdocs.org/sdr/USAASB96259.md): Battery Pack · discharged · Dec 14, 1996 · N268AU · Boeing 7372B7 · Emergency Lighting > ROA - 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) Next page: https://openairdocs.org/deregistered/N268AU-2003-12-09/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 = 'N268AU' AND deregistration_id = 'N268AU-2003-12-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N268AU-2003-12-09/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.