# N267AU: 1982 Boeing 737-2B7, registration cancelled 2004-08-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 24, 2004
- Exported to: Philippines
- 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: 22879
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 19, 1982
- Certificate issued: May 2, 2002
- Last registry action: January 10, 2003
- Mode S code: A29911
- 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/N267AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=267AU
- Page: https://openairdocs.org/deregistered/N267AU-2004-08-24

From the FAA registry file of November 3, 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 (56, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR USAA010452](https://openairdocs.org/sdr/USAA010452), Apr 25, 2001: DOUBLER. CRACKED. CLT - FOUND SKIN DOUBLER CRACKED .09375, BS 178, 12 OCLOCK POSITION, STRINGER 1L. ROUTED OUT DAMAGE (TIME LIMITED REPAIR) PER EA 69533. (M)
- [SDR USAA010451](https://openairdocs.org/sdr/USAA010451), Apr 25, 2001: FRAME. CRACKED. CLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178 WL 207 LEFT SIDE. REMOVED DAMAGED SECTION, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)
- [SDR USAA010450](https://openairdocs.org/sdr/USAA010450), Apr 25, 2001: FRAME. CRACKED. CLT - FOUND SIDE CHORD CRACKED, BS 178 WL 207 RIGHT SIDE CHORD. DAMAGED SECTION CUTOUT, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)
- [SDR USAASB00355](https://openairdocs.org/sdr/USAASB00355), Dec 24, 2000: BATTERY PACK. DISCHARGED. BWI - DURING THE OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD EMERGENCY EXIT SIGN, AT SEAT ROW 2, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PA
- [SDR USAASB00285](https://openairdocs.org/sdr/USAASB00285), Oct 4, 2000: WINDSHIELD. CRACKED. BDL - FLT 2612 - EN ROUTE FROM MHT TO BWI, THE FIRST OFFICERS WINDSHIELD CRACKED IN FLIGHT. COCKPIT VISION WAS AFFECTED. CREW DECLARED AN EMERGENCY AND DIVERTED
- [SDR USAASB00171](https://openairdocs.org/sdr/USAASB00171), Jun 18, 2000: DUCT. RUPTURED. TPA - FLT 2704 - ON CLIMB-OUT FROM TPA, AT 6,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES. WHEN T
- [SDR USAASB99246](https://openairdocs.org/sdr/USAASB99246), Oct 10, 1999: CSD. FAILED. MCO - FLT 2646 - FLIGHT DEPARTED MIA WITH THE NR 1 GENERATOR ON MEL. DURING CRUISE, THE NR 2 GENERATOR LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE
- [SDR USAASB99235](https://openairdocs.org/sdr/USAASB99235), Sep 22, 1999: VALVE. FAILED. ORD - FLT 2704 - AFTER TAKEOFF FROM BWI, THE INBOARD ANTI-SKID LIGHT ILLUMINATED AND DID NOT EXTINGUISH AFTER GEAR RETRACTION. FLIGHT DIVERTED TO ORD FOR MAINTE
- [SDR USAASB99226](https://openairdocs.org/sdr/USAASB99226), Sep 4, 1999: POWER SUPPLY. INOPERATIVE. BOS - MAINTENANCE FOUND THE AFT EMERGENCY LIGHT INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB99161](https://openairdocs.org/sdr/USAASB99161), Jul 3, 1999: LIGHT. INOPERABLE. BWI - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT ASSEMBLY INOPERABLE AND THE FORWARD ESCAPE SLIDE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND FORWARD SERVICE D
- [SDR 99ZZZX2823](https://openairdocs.org/sdr/99ZZZX2823), Jul 3, 1999: BATTERY PACK. DISCHARGED. BWI - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT ASSEMBLY INOPERABLE AND THE FORWARD ESCAPE SLIDE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND FORWARD SERVICE D
- [SDR USAASB99114](https://openairdocs.org/sdr/USAASB99114), Apr 28, 1999: CONNECTOR. LOOSE. BWI - FLT 2681 - DURING CLIMB-OUT FROM BWI, THE NR 2 ENGINE FUEL HEAT LIGHT ILLUMINATED. THE NR 2 ENGIN OIL TEMP BEGAN TO EXCEED LIMITS. CREW TRIED DIFFERENT PO
- [SDR USAA990423](https://openairdocs.org/sdr/USAA990423), Apr 23, 1999: STRINGER. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT TERMINAL END STRINGER 26R AT STATION 540. INSTALLED NEW END FITTING PER SRM 51-10-
- [SDR USAA990391](https://openairdocs.org/sdr/USAA990391), Apr 23, 1999: WEB. CRACKED. CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND A 2 INCH CRACK AT STATION 259 BL 0 CEILING ON NWW VERT STIFFENER WEB. REPAIRED PER SRM 51-10-01 PAGE 5. (M)
- [SDR USAA990390](https://openairdocs.org/sdr/USAA990390), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING A Q-2 CHECK, VISUAL INSPECTION FOUND A 1 INCH AREA OF CORROSION AT STATION 312 LBL 12 FLOORBEAM. INSTALLED NEW 'T' CAP WITH SPLICES AND REPAIR STRA
- [SDR USAA990382](https://openairdocs.org/sdr/USAA990382), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING A Q-2 CHECK, VISUAL INSPECTION FOUND A 1 INCH AREA OF CORROSION AT STATION 312 LBL 1 FLOORBEAM. INSTALLED NEW 'T' CAP WITH SPLICES AND REPAIR STRAP
- [SDR USAA990364](https://openairdocs.org/sdr/USAA990364), Apr 23, 1999: FRAME. CRACKED. CLT - DURING A Q-C CHECK, VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 727 LEFT STRINGER 18A OUTER CHORD FRAME. INSTALLED NEW CHORD PER EO 5394G068 AND EO 5
- [SDR USAA990363](https://openairdocs.org/sdr/USAA990363), Apr 23, 1999: ANGLE. CRACKED. CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND SEVERAL 1 INCH CRACKS AT BS 727 BETWEEN STRINGER 24R AND 25R CHORD ANGLE. REPAIRED PER EA 64377, 64403 AND EO
- [SDR USAA990353](https://openairdocs.org/sdr/USAA990353), Apr 23, 1999: STRINGER. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2.5 INCH CORRODED AREA AT STRINGER 20L AND STATION 911 AFT CARGO. INSTALLED J ANGLE, U CHANNEL, SHIM
- [SDR USAA990314](https://openairdocs.org/sdr/USAA990314), Apr 23, 1999: SKIN. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR LOWER AFT CORNER SKIN. INSTALLED EXTERNAL DOUBLER PER T/R 53-10-19 REV A 
- [SDR USAA990313](https://openairdocs.org/sdr/USAA990313), Apr 23, 1999: SKIN. CRACKED. CLT - DURING Q-2 CHECK HFEC INSPECTION, FOUND A .09375 INCH CRACK IN FORWARD ENTRY DOOR LOWER HINGE CUTOUT FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND FILLER PE
- [SDR USAA990312](https://openairdocs.org/sdr/USAA990312), Apr 23, 1999: ANGLE. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FLOORBEAM TO FUSELAGE ATTACH ANGLE AT BS 597, RBL 70.85 AND WL 204-208. INSTALLED ANGLE REPAI
- [SDR USAA990309](https://openairdocs.org/sdr/USAA990309), Apr 23, 1999: CREASEBEAM. CORRODED. CLT - DURING VISUAL CHECK INSPECTION, FOUND SEVERAL AREAS OF CORROSION AT BS 270 TO BS 360 STRINGER 17L CREASEBEAM INNER CHORD ANGLE. REPAIRED PER BOEING DRAWIN
- [SDR USAA990303](https://openairdocs.org/sdr/USAA990303), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 947 RBL 6 FLOORBEAM. INSTALLED REPAIR ANGLES AND FILLERS PER SRM 53-10-09 PAGE 
- [SDR USAA990302](https://openairdocs.org/sdr/USAA990302), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 986.5. SPLICED IN NEW SECTION OF FLOORBEAM 'T' CAP PER TR 53-60-01 AND EA 64288. 
- [SDR USAA990301](https://openairdocs.org/sdr/USAA990301), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND CORROSION ALONG TOP SURFACE OF FLOORBEAM AT STATION 967, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP
- [SDR USAA990300](https://openairdocs.org/sdr/USAA990300), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 328 LBL 12 AND RBL 1. INSTALLED NEW 'T' CAP REPAIR ANGLES AND STRAPS PER TR 53-10
- [SDR USAA990299](https://openairdocs.org/sdr/USAA990299), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 294.5 BL 0. SPLICED IN NEW 'T' CAP PER TR 53-10-04B. (M)
- [SDR USAA990298](https://openairdocs.org/sdr/USAA990298), Apr 23, 1999: CAP. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH AREA OF CORROSION AT BS 344 LBL 6 AND LBL 10 FLOOR 'T' CAP, CORROSION TASK NR C53-107-01. INSTALLED NEW
- [SDR USAA990297](https://openairdocs.org/sdr/USAA990297), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND SEVERAL 1 INCH AREAS OF CORROSION AT STATION 967 BETWEEN LBL 10 AND RBL 50 FLOORBEAM. SPLICED IN NEW 'T' CAP 
- [SDR USAA990296](https://openairdocs.org/sdr/USAA990296), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON SURFACE TOP OF FLOORBEAM STATION 1006, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP PER SRM
- [SDR USAA990291](https://openairdocs.org/sdr/USAA990291), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT STATION 947 RBL 6 ON FLOORBEAM, CORROSION TASK NR C53-107-02. INSTALLE
- [SDR USAA990290](https://openairdocs.org/sdr/USAA990290), Apr 23, 1999: ANGLE. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY 20 INCH AREA OF CORROSION AT STATION 947 TO STATION 1016 LBL 53 INNER CHORD ANGLE, CORROSION TASK N
- [SDR USAA990289](https://openairdocs.org/sdr/USAA990289), Apr 23, 1999: FLOORBEAM. CORRODED. CLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION ON FLOORBEAM AT STATION 328 LBL 12 AND RBL 1, CORROSION TASK NR C53-107-02. SPLICED I
- [SDR USAA990259](https://openairdocs.org/sdr/USAA990259), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 16R TIE CLIP. REPAIRED PER SRM 51-10-01. (M)
- [SDR USAA990220](https://openairdocs.org/sdr/USAA990220), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 847 STRINGER 1 TIE CLIP. INSTALLED NEW TIE CLIP PER EO NR 5393G227. (M)
- [SDR USAA990214](https://openairdocs.org/sdr/USAA990214), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 10R TIE CLIP. REPLACED PART. (M)
- [SDR USAA990213](https://openairdocs.org/sdr/USAA990213), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRCK BS 787 STRINGER 10L TIE CLIP. REPLACED PART. (M)
- [SDR USAA990212](https://openairdocs.org/sdr/USAA990212), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727 STRINGER 8L TIE CLIP. REPLACED PART. (M)
- [SDR USAA990211](https://openairdocs.org/sdr/USAA990211), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 727A STRINGER 1 TIE CLIP. REPLACED PART. (M)
- [SDR USAA990210](https://openairdocs.org/sdr/USAA990210), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 8R TIE CIP. REPLACED PART. (M)
- [SDR USAA990209](https://openairdocs.org/sdr/USAA990209), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 15R TIE CLIP. REMOVED ORIGINAL CLIP AND HFEC PART AND STRINGER, NO CRACK FOUND
- [SDR USAA990208](https://openairdocs.org/sdr/USAA990208), Apr 23, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 5R TIE CLIP. REPLACED PART. (M)
- [SDR USAASB99047](https://openairdocs.org/sdr/USAASB99047), Feb 20, 1999: POWER SUPPLY. INOPERATIVE. CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND 
- [SDR 99ZZZM195](https://openairdocs.org/sdr/99ZZZM195), Feb 20, 1999: BATTERY. DISCHARGED. CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND 
- [SDR 99ZZZM194](https://openairdocs.org/sdr/99ZZZM194), Feb 20, 1999: BATTERY PACK. DISCHARGED. CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND 
- [SDR USAA970090](https://openairdocs.org/sdr/USAA970090), Mar 12, 1997: SKIN. CRACKED. GSO - DURING TRANSIT CHECK VISUAL, VERIFIED BY EDDY CURRENT INSPECTION, FOUND TWO .25 INCH CRACKS LEFT FORWARD SERVICE DOOR, SKIN AT AFT CORNERS OF LOWER HINGE 
- [SDR USAA970089](https://openairdocs.org/sdr/USAA970089), Mar 12, 1997: SKIN. CRACKED. GSO - DURING TRANSIT CHECK VISUAL, VERIFIED WITH EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK IN SKIN FUSELAGE RIGHT SIDE, STATION 764, STRINGER 19R. INSTALLED
- [SDR USAA960784](https://openairdocs.org/sdr/USAA960784), Dec 7, 1996: STRINGER. CORROSION. ROA - DURING CX-4 CHECK, VISUAL INSPECTION FOUND 2 INCH BY 12 INCH CORROSION, STR 27L, BS 967. REMOVED CORROSION AND INSTALLED DOUBLER AND SPLICED, REPAIRED PER
- [SDR USAASB96197](https://openairdocs.org/sdr/USAASB96197), Sep 19, 1996: FUEL HEAT VLV. STUCK OPEN. CMH - FL 1183 - DURING CLIMB AT FL 280, CAPTAIN SHUT DOWN THE NR 1 ENGINE DUE TO HIGH OIL TEMPERATURE. THE OIL TEMPERATURE WAS IN THE YELLOW BAND FOR APPROX 15 

All 56: https://openairdocs.org/deregistered/N267AU-2004-08-24/reports.md

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