# Service difficulty reports: N269AU, cancelled Jun 18, 2004 A list on [N269AU, cancelled Jun 18, 2004](https://openairdocs.org/deregistered/N269AU-2004-06-18.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 · 60 reports - [SDR USAA010865](https://openairdocs.org/sdr/USAA010865.md): Skin · cracked · Jul 7, 2001 · N269AU · Boeing 7372B7 · Fuselage Structure (General) > CLT - FOUND FUSELAGE SKIN CRACKED, AFT END OF AIRSTAIR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-03. (M) - [SDR USAASB01160](https://openairdocs.org/sdr/USAASB01160.md): Flap · jammed · Jun 4, 2001 · N269AU · Boeing 7372B7 · Trailing Edge Flap Control System > EWR - FLT 2671 - DURING DESCENT, AIRCRAFT ENCOUNTERED TRAILING EDGE FLAP ASYMMETRY. CAPTAIN REQUESTED TO LAND AT EWR INSTEAD OF LGA DUE TO THE HIGHER LANDING SPEEDS FOR THIS TYPE OF FAILURE. AFTER LANDING AT EWR, WITHOUT INCIDENT, CAPTAIN REPORTED THAT THE L - [SDR USAA010296](https://openairdocs.org/sdr/USAA010296.md): Skin · cracked · Mar 20, 2001 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > TPA - FOUND SKIN CRACKED.75 INCH, LOWER HINGE BETWEEN STRINGER 9 AND 10 RT AFT STATION 947. INSTALLED DOUBLER PER SRM 53-30-3 FIG 33. (M) - [SDR USAA010187](https://openairdocs.org/sdr/USAA010187.md): Skin · cracked · Feb 28, 2001 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > TPA - FOUND SKIN CRACKED.75 INCH, LOWER HINGE CUTOUT BETWEEN STRINGER 9 AND 10R AFT STATION 947. INSTALLED DOUBLER PER SRM 53-30-3 FIG 33N AND TR 53-30-11. (M) - [SDR USAASB01048](https://openairdocs.org/sdr/USAASB01048.md): Engine · failed · Feb 15, 2001 · N269AU · Boeing 7372B7 · Engine (Turbine/Turboprop) > MCO - FLT 2727 - ON CLIMB-OUT FROM FLL, EN ROUTE TO LGA, CAPTAIN REPORTED THAT THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND METAL IN THE TAILPIPE OF - [SDR USAASB00338](https://openairdocs.org/sdr/USAASB00338.md): Indicator · faulty · Nov 30, 2000 · N269AU · Boeing 7372B7 · Hydraulic Quantity Indicator > CLT - FLT 2700 - EN ROUTE FROM BWI-MSY, THE CREW OBSERVED HYDRAULIC QTY DECREASING BELOW 1.8 GALLON VALUE IN FLIGHT. DURING INITIAL CONFIGURATION, QUANTITY WAS OBSERVED BELOW 1.4 GALLON VALUE. INITIAL QUANTITY LEAVING BWI WAS AT 3.2 GALLONS ON INDICATOR. FL - [SDR USAASB00229](https://openairdocs.org/sdr/USAASB00229.md): Power Supply · failed · Aug 17, 2000 · N269AU · Boeing 7372B7 · Emergency Lighting > IAD - MAINTENANCE FOUND THE OUTBOARD EXTERIOR EMERGENCY LIGHT FOR THE RIGHT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY. OPERATIONAL CHECK NORMAL. (M) - [SDR USAA000452](https://openairdocs.org/sdr/USAA000452.md): Skin · cracked · Mar 23, 2000 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - FOUND FUSELAGE SKIN CRACKED 1.125 INCH, AFT END OF E/E COOLING DUCT OUTLET. INSTALLED DOUBLER PER TR 53-30-04 AND DWG 65C33930. (M) - [SDR USAA000385](https://openairdocs.org/sdr/USAA000385.md): Skin · cracked · Mar 20, 2000 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > TPA - FOUND FUSELAGE SKIN 2.24 INCH CRACKED, STATION 767, STRINGER 19R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) - [SDR USAASB99260](https://openairdocs.org/sdr/USAASB99260.md): Acm · weak · Oct 27, 1999 · N269AU · Boeing 7372B7 · Cabin Cooling System > BWI - FLT 2741 - FLT ON MX DELAY IN BDL, WHEREAS MX PLACED THE RT PACK ON MEL. FLT DEPARTED BDL AND WHILE FLYING OVER PHL, THE LT PACK WOULD ONLY HOLD CABIN PRESSURE TO 9,500 FT. CAPT ELECTED TO DIVERT TO BWI WHERE THE FLT LANDED W/O FURTHER INCIDENT. NO EM - [SDR USAASB99159](https://openairdocs.org/sdr/USAASB99159.md): Fire Loop · failed · Jun 30, 1999 · N269AU · Boeing 7372B7 · Fire Detection > MCO-BWI - FLT 2662, AT APPROX FL330, CREW RECEIVED AND APU FIRE DETECTION LIGHT. CREW SHUTDOWN THE APU. WITH A/C BEING DOWN TO ONE SOURCE OF ELECT POWER, CREW DIVERTED FLIGHT TO THE NEAREST SUITABLE AIRPORT AT RDU. FLIGHT LANDED WITHOUT FURTHER INCIDENT. N - [SDR USAASB99075](https://openairdocs.org/sdr/USAASB99075.md): Battery Pack · discharged · Mar 18, 1999 · N269AU · Boeing 7372B7 · Emergency Lighting > CLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M572, RIGHT SIDE, AND THE POWER SUPP - [SDR 99ZZZM244](https://openairdocs.org/sdr/99ZZZM244.md): Power Supply · failed · Mar 18, 1999 · N269AU · Boeing 7372B7 · Emergency Lighting > CLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M572, RIGHT SIDE, AND THE POWER SUPP - [SDR USAASB99074](https://openairdocs.org/sdr/USAASB99074.md): Battery Pack · discharged · Mar 14, 1999 · N269AU · Boeing 7372B7 · Emergency Lighting > ALB - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB99046](https://openairdocs.org/sdr/USAASB99046.md): Battery Pack · discharged · Feb 20, 1999 · N269AU · Boeing 7372B7 · Emergency Lighting > BWI - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB99018](https://openairdocs.org/sdr/USAASB99018.md): Fire Light · illuminated · Jan 23, 1999 · N269AU · Boeing 7372B7 · Fire Detection > ILM - FLT 439 - ON DESCENT INTO ILM, THE CREW REPORTED THAT THE APU FIRE WARNIG LIGHT ILLUMINATD WITH THE APU ON MEL AND SHUTDOWN. THE APU IS SCHEDULED FOR REPLACEMENT DUE TO PERFORMANCE. CAPTAIN STATED THAT THE FLIGHT WAS AT 12,000 FEET WHEN THE FIRE WARNIN - [SDR USAASB98340](https://openairdocs.org/sdr/USAASB98340.md): Wire · broken · Dec 29, 1998 · N269AU · Boeing 7372B7 · Light System Wiring > PIT - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT FAULT TO THE M192 BATTERY PACK CANNON PLUG D1494, PIN 5. REPAIRED GROUND WIRE FROM PIN NR 5 ON CANNON PLUG D1494. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB98258](https://openairdocs.org/sdr/USAASB98258.md): Supply Duct · failed · Oct 1, 1998 · N269AU · Boeing 7372B7 · Air Distribution System > LGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LG - [SDR 98ZZZM890](https://openairdocs.org/sdr/98ZZZM890.md): Pack Control Vlv · failed · Oct 1, 1998 · N269AU · Boeing 7372B7 · Air Distribution System > LGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LG - [SDR 98ZZZM889](https://openairdocs.org/sdr/98ZZZM889.md): Press Regulator · failed · Oct 1, 1998 · N269AU · Boeing 7372B7 · Air Distribution System > LGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LG - [SDR 98ZZZM888](https://openairdocs.org/sdr/98ZZZM888.md): Mix Chamber Duct · failed · Oct 1, 1998 · N269AU · Boeing 7372B7 · Air Distribution System > LGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS HEARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT LG - [SDR USAA980468](https://openairdocs.org/sdr/USAA980468.md): Angle · corroded · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT LWR THRESHOLD SUPPORT ZEE AREA FWD SERVICE DOOR STATION 300 TO 340 ZEE ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-1. (M) - [SDR USAA980467](https://openairdocs.org/sdr/USAA980467.md): Frame · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A CRACK OUTBOARD FRAME CHORD BS 727 STRINGER 15L. INSTALLED DOUBLERS, FILLERS AND STRAPS PER EA 62502. (M) - [SDR USAA980466](https://openairdocs.org/sdr/USAA980466.md): Angle · corroded · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND.5 INCH BY 6 INCH AREA OF CORROSION LBL 54 STATION 887 TO STATION 1016. CORROSION TASK NR C53-107-02. REPLACED WITH IDENTICAL PART PER SRM 53-10-01. (M) - [SDR USAA980464](https://openairdocs.org/sdr/USAA980464.md): Floorbeam · corroded · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY.5 INCH BY 24 INCH AREA OF CORROSION CLIP NUT HOLES BS 1016 BETWEEN LBL 12 AND LBL 36 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-9. (M) - [SDR USAA980463](https://openairdocs.org/sdr/USAA980463.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 767 STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980462](https://openairdocs.org/sdr/USAA980462.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 727A STRINGER 6R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980461](https://openairdocs.org/sdr/USAA980461.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 747 STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980460](https://openairdocs.org/sdr/USAA980460.md): Floorbeam · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK BS 663 BBL.07 UPPER CHORD LONGITUDINAL FLOORBEAM. INSTALLED SPLICE ANGLES, STRAPS AND REINFORCED ANGLES PER EA 62511 AND BOEING S/B737-57-1210. (M) - [SDR USAA980459](https://openairdocs.org/sdr/USAA980459.md): Web · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK BS 230.5 WL 187 BL 0 RETRACT ACT FITTING SUPPORT WEB NLG. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1, BOEING 737-200. (M) - [SDR USAA980458](https://openairdocs.org/sdr/USAA980458.md): Floorbeam · corroded · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SEVERAL SCREW HOLES ON FLOORBEAM STATION 947.5. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP TO FLOORBEAM PER SRM 53-10-9. (M) - [SDR USAA980457](https://openairdocs.org/sdr/USAA980457.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 639 STRINGER 4L STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980456](https://openairdocs.org/sdr/USAA980456.md): Floorbeam · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-4 CHECK HFEC INSPECTION, FOUND A 1.5 INCH CRACK BS 520 WL 208 LBL 24 FLOORBEAM. INSTALLED REPAIR ANGLE PER EA 62449 SB 737-53-1120 REV 1 PART VI. (M) - [SDR USAA980455](https://openairdocs.org/sdr/USAA980455.md): Floorbeam · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-4 CHECK HFEC INSPECTION, FOUND A 1.5 INCH CRACK BS 520 WL 208 RBL 24 FLOORBEAM. INSTALLED REPAIR ANGLES PER EA 62449 SB 737-53-1120 REV 1. (M) - [SDR USAA980454](https://openairdocs.org/sdr/USAA980454.md): Floorbeam · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK HFEC INSPECTION, FOUND.25 INCH CRACK BS 520 RBL 45 FLOORBEAM 'T' CAP RADIUS. INSTALLED REPAIR ANGLES PER EA 62449 BOEING SB 737-53-1120 REV 1. (M) - [SDR USAA980453](https://openairdocs.org/sdr/USAA980453.md): Floorbeam · corroded · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND CLIP NUT HOLES STATION 344 FLOORBEAM BL 0 TO LBBL 42. REPAIRED 'T' CAP SPLICED DOUBLER PER SRM 53-10-13. (M) - [SDR USAA980452](https://openairdocs.org/sdr/USAA980452.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 807 STRINGER 10R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980451](https://openairdocs.org/sdr/USAA980451.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 727B STRINGER 8R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980450](https://openairdocs.org/sdr/USAA980450.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 727B STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980449](https://openairdocs.org/sdr/USAA980449.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 727A STRINGER 2R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980448](https://openairdocs.org/sdr/USAA980448.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 727A STRINGER 2R, STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980447](https://openairdocs.org/sdr/USAA980447.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 747 STRINGER 7L STRINGER TIE CLIP. REPAIRED PER EO 5939G227 REV 'A'. (M) - [SDR USAA980446](https://openairdocs.org/sdr/USAA980446.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 706 STRINGER 9L. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980445](https://openairdocs.org/sdr/USAA980445.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK STATION 500B STRINGER 10L STRINGER TIE CLIP. REPAIRED PER SRM 51-10-1 AND EO 5393G227 REV 'A'. (M) - [SDR USAA980444](https://openairdocs.org/sdr/USAA980444.md): Clip · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STRINGER TIE CLIP STATION 616 S 1. REPAIRED PER EO 5393G227 REV 'A'. (M) - [SDR USAA980439](https://openairdocs.org/sdr/USAA980439.md): Angle · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN RADIUS SUPPORT BRACKET FOR NLG AT BEAM VERT FLANGE STATION 259 WL 192 ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-1. (M) - [SDR USAA980438](https://openairdocs.org/sdr/USAA980438.md): Skin · cracked · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURING Q-1 CHECK EDDY CURRENT INSPECTION, FOUND A.25 INCH CRACK LOWER FORWARD CORNER LEFT AFT ENTRY DOOR CUTOUT STATION 962 WL 208 SKIN. INSTALLED TRIPLER PER SRM 53-30-03 FIG 24. (M) - [SDR USAA980437](https://openairdocs.org/sdr/USAA980437.md): Skin · dented · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH LONG.875 INCH WIDE AND.09375 INCH DEEP DENT BETWEEN STATION 987.5 AND STATION 1006 STRINGER 17L SKIN. FABRICATED DOUBLER PER SRM 53-30-3 FIG 61. (M) - [SDR USA980469](https://openairdocs.org/sdr/USA980469.md): Floorbeam · corroded · Sep 30, 1998 · N269AU · Boeing 7372B7 · Fuselage Main, Floor Beam > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT CLIP NUTS STATION 344 FLOORBEAM BL 0 LBL 42. CORROSION TASK NR C53-107-01. FABRICATED REPAIR PER TR 53-10-13 'T' CAP. (M) - [SDR USAASB98158](https://openairdocs.org/sdr/USAASB98158.md): Duct · cracked · Jun 26, 1998 · N269AU · Boeing 7372B7 · Air Intake Anti/De-Ice System > TPA - FLT 940 - DURING CLIMB-OUT FROM TPA AT FL200, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPTAIN RETARDED THROTTLE ON THE NR 1 ENGINE TO IDLE AND THE LIGHT EXTINGUISHED. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD AT TPA. FLT LANDED WITHOUT IN Next page: https://openairdocs.org/deregistered/N269AU-2004-06-18/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 = 'N269AU' AND deregistration_id = 'N269AU-2004-06-18' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N269AU-2004-06-18/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.