# N269AU: 1982 Boeing 737-2B7, registration cancelled 2004-06-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 18, 2004 - Exported to: Nigeria - Status when cancelled: Valid registration - Airframe: [Boeing 737-2B7](https://openairdocs.org/model/boeing-737-2b7) (registry code 138447C) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22881 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 16, 1982 - Certificate issued: May 2, 2002 - Last registry action: January 10, 2003 - Mode S code: A2A07F - Owner when cancelled: [Alameda Corp Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORP%20TRUSTEE) - Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio) - Owner type: Corporation - Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N269AU - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=269AU - Page: https://openairdocs.org/deregistered/N269AU-2004-06-18 From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-2B7: https://openairdocs.org/model/boeing-737-2b7.md ## Service difficulty reports (60, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA010865](https://openairdocs.org/sdr/USAA010865), Jul 7, 2001: SKIN. CRACKED. 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), Jun 4, 2001: FLAP. JAMMED. 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 SP - [SDR USAA010296](https://openairdocs.org/sdr/USAA010296), Mar 20, 2001: SKIN. CRACKED. 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), Feb 28, 2001: SKIN. CRACKED. 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), Feb 15, 2001: ENGINE. FAILED. 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 - [SDR USAASB00338](https://openairdocs.org/sdr/USAASB00338), Nov 30, 2000: INDICATOR. FAULTY. 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 - [SDR USAASB00229](https://openairdocs.org/sdr/USAASB00229), Aug 17, 2000: POWER SUPPLY. FAILED. IAD - MAINTENANCE FOUND THE OUTBOARD EXTERIOR EMERGENCY LIGHT FOR THE RIGHT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT BATTERY PACK ( - [SDR USAA000452](https://openairdocs.org/sdr/USAA000452), Mar 23, 2000: SKIN. CRACKED. 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), Mar 20, 2000: SKIN. CRACKED. 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), Oct 27, 1999: ACM. WEAK. 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 PRE - [SDR USAASB99159](https://openairdocs.org/sdr/USAASB99159), Jun 30, 1999: FIRE LOOP. FAILED. 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 D - [SDR USAASB99075](https://openairdocs.org/sdr/USAASB99075), Mar 18, 1999: BATTERY PACK. DISCHARGED. CLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS - [SDR 99ZZZM244](https://openairdocs.org/sdr/99ZZZM244), Mar 18, 1999: POWER SUPPLY. FAILED. CLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS - [SDR USAASB99074](https://openairdocs.org/sdr/USAASB99074), Mar 14, 1999: BATTERY PACK. DISCHARGED. ALB - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT, LEFT - [SDR USAASB99046](https://openairdocs.org/sdr/USAASB99046), Feb 20, 1999: BATTERY PACK. DISCHARGED. 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), Jan 23, 1999: FIRE LIGHT. ILLUMINATED. 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 REPL - [SDR USAASB98340](https://openairdocs.org/sdr/USAASB98340), Dec 29, 1998: WIRE. BROKEN. PIT - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT FAULT TO THE M192 BATTERY PACK CANNON PLUG D1494, - [SDR USAASB98258](https://openairdocs.org/sdr/USAASB98258), Oct 1, 1998: SUPPLY DUCT. FAILED. 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 A - [SDR 98ZZZM890](https://openairdocs.org/sdr/98ZZZM890), Oct 1, 1998: PACK CONTROL VLV. FAILED. 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 A - [SDR 98ZZZM889](https://openairdocs.org/sdr/98ZZZM889), Oct 1, 1998: PRESS REGULATOR. FAILED. 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 A - [SDR 98ZZZM888](https://openairdocs.org/sdr/98ZZZM888), Oct 1, 1998: MIX CHAMBER DUCT. FAILED. 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 A - [SDR USAA980468](https://openairdocs.org/sdr/USAA980468), Sep 30, 1998: ANGLE. CORRODED. 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 IDENTIC - [SDR USAA980467](https://openairdocs.org/sdr/USAA980467), Sep 30, 1998: FRAME. CRACKED. 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 - [SDR USAA980466](https://openairdocs.org/sdr/USAA980466), Sep 30, 1998: ANGLE. CORRODED. 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 W - [SDR USAA980464](https://openairdocs.org/sdr/USAA980464), Sep 30, 1998: FLOORBEAM. CORRODED. 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 UPP - [SDR USAA980463](https://openairdocs.org/sdr/USAA980463), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: FLOORBEAM. CRACKED. 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 - [SDR USAA980459](https://openairdocs.org/sdr/USAA980459), Sep 30, 1998: WEB. CRACKED. 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 - [SDR USAA980458](https://openairdocs.org/sdr/USAA980458), Sep 30, 1998: FLOORBEAM. CORRODED. 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-C - [SDR USAA980457](https://openairdocs.org/sdr/USAA980457), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: FLOORBEAM. CRACKED. 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. - [SDR USAA980455](https://openairdocs.org/sdr/USAA980455), Sep 30, 1998: FLOORBEAM. CRACKED. 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), Sep 30, 1998: FLOORBEAM. CRACKED. 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 - [SDR USAA980453](https://openairdocs.org/sdr/USAA980453), Sep 30, 1998: FLOORBEAM. CORRODED. 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 - [SDR USAA980452](https://openairdocs.org/sdr/USAA980452), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: CLIP. CRACKED. 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'. - [SDR USAA980444](https://openairdocs.org/sdr/USAA980444), Sep 30, 1998: CLIP. CRACKED. 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), Sep 30, 1998: ANGLE. CRACKED. 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 IDE - [SDR USAA980438](https://openairdocs.org/sdr/USAA980438), Sep 30, 1998: SKIN. CRACKED. 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 TRIPLE - [SDR USAA980437](https://openairdocs.org/sdr/USAA980437), Sep 30, 1998: SKIN. DENTED. 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. - [SDR USA980469](https://openairdocs.org/sdr/USA980469), Sep 30, 1998: FLOORBEAM. CORRODED. 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. FABRICA - [SDR USAASB98158](https://openairdocs.org/sdr/USAASB98158), Jun 26, 1998: DUCT. CRACKED. 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 LIG All 60: https://openairdocs.org/deregistered/N269AU-2004-06-18/reports.md --- 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.