# N264AU: 1983 Boeing 737-201, registration cancelled 2003-04-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 28, 2003
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-201](https://openairdocs.org/model/boeing-737-201) (registry code 1384454)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22961
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 30, 1983
- Certificate issued: May 2, 2002
- Last registry action: January 10, 2003
- Mode S code: A28DEC
- 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/N264AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=264AU
- Page: https://openairdocs.org/deregistered/N264AU-2003-04-28

From the FAA registry file of October 31, 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 737-201: https://openairdocs.org/model/boeing-737-201.md

## Service difficulty reports (89, newest 50)

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

- [SDR USAASB01261](https://openairdocs.org/sdr/USAASB01261), Sep 19, 2001: POWERPACK. FAILED. BWI - THE FORWARD RIGHT EMERGENCY EVACUATION SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
- [SDR USAA011207](https://openairdocs.org/sdr/USAA011207), Sep 5, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, BS 360 STRINGER 11L. INSTALLED REPAIR DOUBLER PER SRM 53-1-2. (M)
- [SDR USAA011206](https://openairdocs.org/sdr/USAA011206), Sep 5, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER SHELF 18A CRACKED .375 INCH, BS 727 AT STRINGER 18R. INSTALLED NON SHELF PER EA 85230. INSTALLED NON SHELF PER EA 85230. (M)
- [SDR USAA011205](https://openairdocs.org/sdr/USAA011205), Sep 5, 2001: KEELBEAM. CHAFED. CLT - FOUND KEEL BEAM CHAFED 1 INCH BY 27 INCHES, LEFT KEEL BEAM BS 700-727 LOWER CHORD. INSTALLED REPAIR WASHERS AND REPAIR STRAP PER EA 85306A. (M)
- [SDR USAA011204](https://openairdocs.org/sdr/USAA011204), Sep 5, 2001: KEELBEAM. CHAFED. CLT - FOUND KEEL BEAM CHAFED 1 INCH BY 64 INCHES, RT KEEL BEAM, BS 663-727. INSTALLED REPAIR WASHERS AND REPAIR STRAP PER EA 85306A. (M)
- [SDR USAA011203](https://openairdocs.org/sdr/USAA011203), Sep 4, 2001: BULKHEAD. DAMAGED. CLT - FOUND WEB SKIN DAMAGED 10 SQUARE INCHES, BS 178, WL 196 TO WL 205, LBL 10.5 TO RBL 10.5. C/O DAMAGE VERIF, NO DAMAGE AT PERIM INSU CUT .100 MORE, INSTALLE
- [SDR USAA011202](https://openairdocs.org/sdr/USAA011202), Sep 4, 2001: FRAME. CORRODED. CLT - FOUND FRAME CORRODED 5 INCHES, BS 415 STRINGER 25R. REMOVED DAMAGED SECTION OF STRINGER 25R, ADD STRINGER SPLICE J CHANNEL DOUBLER AND CENTER U-CHANNEL EA
- [SDR USAA011201](https://openairdocs.org/sdr/USAA011201), Sep 4, 2001: FITTING. CORRODED. CLT - FOUND CORROSION ON CLEVIS LUG .019 INCH BY 2 INCH, LEFT HORIZONTAL CENTER, UP REAR SPAR AFT LUG, AFT FACE. SPOT FACED AFFECTED AREA AND INSTALLED NEW BUSH
- [SDR USAA011200](https://openairdocs.org/sdr/USAA011200), Sep 4, 2001: FITTING. CORRODED. CLT - FOUND CORROSION ON CLEVIS LUG .020 INCH BY 2 INCH, LEFT HORIZONTAL, STAB CENTER SECTION UP REAR SPAR FORWARD LUG. SPOT FACED AFFECTED AREA AND INSTALLED N
- [SDR USAA011196](https://openairdocs.org/sdr/USAA011196), Sep 4, 2001: SKIN. CORRODED. CLT - FOUND SKIN CORRODED 1 INCH BY 2 INCH, BS 1016. CORROSION LEVEL 2. INSTALLED DOUBLER PER EA 85159 AND EA 85231. (M)
- [SDR USAA011189](https://openairdocs.org/sdr/USAA011189), Aug 31, 2001: BEAR STRAP. CORRODED. CLT - FOUND DOOR C/O BEARSTRAP CORRODED 3 INCHES BY 5 INCHES, BS 485 AND BS 440 AND BS 420. INSTALLED FILLER AND DOUBLER AND 2 TRIPLERS PER EA NR 85292. (M)
- [SDR USAA011188](https://openairdocs.org/sdr/USAA011188), Aug 31, 2001: FRAME. CRACKED. CLT - FOUND CHORD ANGLE CRACKED 1 INCH, BS 178 BULKHEAD RIGHT SIDE RADIUS WL 195. REMOVED AND REPLACED CHORD SECTION, INSTALLED INT DOUBLER ANGLE AND EX DOUBLER
- [SDR USAA011171](https://openairdocs.org/sdr/USAA011171), Aug 30, 2001: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 3 INCH, BS 663 BL 0. INSTALLED DOUBLER, SPLICE PLATES AND STIFFENERS, PER T/R 57-10-04 AND EA 69909. (M)
- [SDR USAA011170](https://openairdocs.org/sdr/USAA011170), Aug 30, 2001: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM WEB CRACKED .5 INCH, BS 663 BL0. INSTALLED DOUBLER SPLICE PLATES AND STIFFENERS, PER TT 57-10-04 AND EA 69909. (M)
- [SDR USAA011169](https://openairdocs.org/sdr/USAA011169), Aug 29, 2001: FRAME. CORRODED. CLT - FOUND FRAME CORRODED, BS 807 STRINGER 17R TO STRINGER 27R, CORROSION LEVEL 1 TASK NR C53-100-01. (M)
- [SDR USAA011157](https://openairdocs.org/sdr/USAA011157), Aug 28, 2001: STRINGER. CRACKED. CLT - FOUND SHELF WEB CRACKED 3 INCHES, RIGHT 18A SHELF. REPLACED WITH NEW PART PER SRM 51-10-1 AND EO 85230. (M)
- [SDR USAA011156](https://openairdocs.org/sdr/USAA011156), Aug 28, 2001: FRAME. CORRODED. CLT - FOUND FRAME CORRODED 2 INCHES BY 5 INCHES, BS 500 BL0. CORROSION LEVEL 1, TASK NR 90-25-01. CUT OUT DAMAGE ON FRM, HFEC INSPECTION FMD PARTS, HT TREAT/INS
- [SDR USAA011152](https://openairdocs.org/sdr/USAA011152), Aug 24, 2001: BULKHEAD. CRACKED. CLT - FOUND WEB SKIN CRACKED .500 INCH, BS 178 BULKHEAD, LBL 1,WL 206. REMOVED DAMAGE, HFEC INSPECTION. CUT .100 MORE, INSTALLED DOUBLER PER EO 5300V153, EA 699
- [SDR USAA011150](https://openairdocs.org/sdr/USAA011150), Aug 24, 2001: BULKHEAD. CRACKED. CLT - FOUND WEB SKIN CRACKED .500 INCH, BS 178 BULKHEAD, RBL 1, WL 206. REMOVED DAMAGED HFEC INSPECTION, CUT .100 MORE, INSTALLED DOUBLER PER EO 5300V153 EA 699
- [SDR USAA011149](https://openairdocs.org/sdr/USAA011149), Aug 24, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED 1 INCH, BS 178 BULKHEAD AT WL 207.5 AT RBL 1 TO 2. INSTALLED DOUBLER DAMAGE. REMOVED HFEC DONE. PER EO 5300V153 EA 69902, SRM 53-10-08 F
- [SDR USAA011142](https://openairdocs.org/sdr/USAA011142), Aug 22, 2001: BULKHEAD. GOUGED. CLT - FOUND PRESSURE AFT BULKHEAD WITH 3 GOUGES APPROXIMATELY .125 INCH, LBL 3 BS 1016. INSTALLED DOUBLER, TRIPLER, FILLER OF REPAIR PER EA 85254. (M)
- [SDR USAA011141](https://openairdocs.org/sdr/USAA011141), Aug 22, 2001: FLOORBEAM. CORRODED. CLT - FOUND INTERCOSTAL CORRODED 2 INCHES BY 2.5 INCHES, BS 312, FLOORBEAM LBL 8.5 TO RBL 11 UPPER SURFACE. CORROSION TASK NR C53-107-01. REMOVED AND REPLACED F
- [SDR USAA011140](https://openairdocs.org/sdr/USAA011140), Aug 22, 2001: FRAME. CRACKED. CLT - FOUND CHORD ANGLE CRACKED 1 INCH, RIGHT SIDE CHORD BS 178 AT WL 207. INSTALLED REPAIR, SIDE CHORD, PER EO 5300V157. (M)
- [SDR USAA011139](https://openairdocs.org/sdr/USAA011139), Aug 22, 2001: FRAME. CRACKED. CLT - FOUND CHORD ANGLE CRACKED 1 INCH, BS 178 SIDE CHORD AT WL 207, LEFT SIDE. INSTALLED REPAIR SIDE CHORD PER EO 5300V157. (M)
- [SDR USA011106](https://openairdocs.org/sdr/USA011106), Aug 20, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED, AFT ENTRY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 34. (M)
- [SDR USAA011104](https://openairdocs.org/sdr/USAA011104), Aug 20, 2001: STRINGER. CORRODED. CLT - FOUND STRINGER AND TIE CLIP CORRODED 1 INCH, BS 538, S26R. REMOVED AND REPLACED PART PER SRM 53-10-03. (M)
- [SDR USAA011103](https://openairdocs.org/sdr/USAA011103), Aug 20, 2001: TIE CLIP. CLT - FOUND TIE CLIP WITH WRONG TYPE CLIP INSTALLED, BS 596-S9L. INSTALLED NEW TIE CLIP PER EO NR 5393G227. (M)
- [SDR USAA011102](https://openairdocs.org/sdr/USAA011102), Aug 20, 2001: FRAME. CRACKED. CLT - FOUND FRAME OUTER CHORD CRACKED 1 INCH, BS 597, 6 INCHES BELOW S17L ON FORWARD SIDE OF FRAME. REMOVED AND REPLACED WITH PART NR 65-46538-33 PER SRM 51-30-
- [SDR USA011101](https://openairdocs.org/sdr/USA011101), Aug 20, 2001: FLOORBEAM. UNKNOWN. CLT - FOUND FLOORBEAM NO CRACKS PER NDT, BS 520 RBL 45. INSTALLED DOUBLER PER EA 85214. (M)
- [SDR USAA011100](https://openairdocs.org/sdr/USAA011100), Aug 20, 2001: WEB. CORRODED. CLT - FOUND FLOORBEAM WEB CORRODED, BS 344 FLOORBEAM, LBL 14.5 TO 21.5. CORROSION LEVEL 1, TASK NR C53-107-01. BLENDED OUT CORROSION, INSTALLED DOUBLER AND TRIP
- [SDR USAA011099](https://openairdocs.org/sdr/USAA011099), Aug 20, 2001: FRAME. CRACKED. CLT - FOUND CHORD CRACKED .250 INCH, BS 178, LBL 5.6, RBL 5.7, WL 184. INSTALLED REPAIR ANGLES PER EO 5300 US155 PER JC MC-90-93857. (M)
- [SDR USAA011098](https://openairdocs.org/sdr/USAA011098), Aug 20, 2001: FRAME. CRACKED. CLT - FOUND FRAME OUTER CHORD 1 INCH, BS 597, 6 INCHES BELOW 17L ON AFT SIDE OF FRAME. REMOVED AND REPLACED PART WITH PART NR 1126923 PER SRM 51-30-2. (M)
- [SDR USAA011097](https://openairdocs.org/sdr/USAA011097), Aug 20, 2001: FRAME. CRACKED. CLT - FOUND CHORD CRACKED 1 INCH, BS 178, LBL 5.8, WL 184. INSTALLED REPAIR ANGLES PER EO 5300V155 PER M2-90-93857. (M)
- [SDR USAA011089](https://openairdocs.org/sdr/USAA011089), Aug 14, 2001: SKIN. DENTED. CLT - FOUND SKIN DENTED AND GOUGED 1 INCH BY .070 INCH, BS 309 JUST BELOW BS 24R. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLERS PER SRM 53-30-3 FIG 42. (
- [SDR USAA011088](https://openairdocs.org/sdr/USAA011088), Aug 14, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 3 SQUARE INCHES, BS 1006 LBL 10. CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-10-9. (M)
- [SDR USAA011087](https://openairdocs.org/sdr/USAA011087), Aug 14, 2001: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 1.5 INCH, BS 520 LBL 45. INSTALLED DOUBLER PER EA 85214. (M)
- [SDR USAA011086](https://openairdocs.org/sdr/USAA011086), Aug 14, 2001: ANGLE. CRACKED. CLT - FOUND ANGLE CRACKED .5 INCH, BS 328 FLOORBEAM RBL 31.5 TO INTERCOSTAL. FABRICATED REPAIR DOUBLER PER SRM 53-10-02. (M)
- [SDR USAA011085](https://openairdocs.org/sdr/USAA011085), Aug 14, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, BS 359 S11L. REMOVED AND REPLACED PART WITH PART NR 1126212 PER 51-10-1. (M)
- [SDR USAA011093](https://openairdocs.org/sdr/USAA011093), Aug 14, 2001: WEB. CORRODED. CLT - FOUND CREASE BEAM WEB CORRODED 10 SQUARE INCHES, LEFT SIDE BS 927-947. FABRICATED NEW WEB PER DRAWING 65-52878 AND INSTALLED PER SRM 51-30-2. (M)
- [SDR USAA011092](https://openairdocs.org/sdr/USAA011092), Aug 14, 2001: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED .5 INCHES, BS 520 TO RBL 24 AND LBL 24. INSTALLED DOUBLER PER EA 85215. (M)
- [SDR USAA011064](https://openairdocs.org/sdr/USAA011064), Aug 13, 2001: ANGLE. BENT. CLT - FOUND DRAG ANGLE BENT, RIGHT AFT VERTICAL STABILIZER MOUNT AREA. FABRICATED AND INSTALLED REPAIR STRAPS AND FILLERS PER EA 85186. (M)
- [SDR USAA01061](https://openairdocs.org/sdr/USAA01061), Aug 13, 2001: INTERCOSTAL. CRACKED. CLT - FOUND INTERCOSTAL CRACKED .75 INCH, BS 300.5 TO BS 301.5 S10L. INSTALLED NEW ANGLE PER SRM 51-10-1. (M)
- [SDR USAA011059](https://openairdocs.org/sdr/USAA011059), Aug 13, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED TWO PLACES .060 INCH, BULKHEAD WEB AT ATTACH TO 1016 Y CHORD. INSTALLED DOUBLER PER SRM 53-10-4 AND SRM 51-30-5. (M)
- [SDR USAA011058](https://openairdocs.org/sdr/USAA011058), Aug 13, 2001: FRAME. DENTED. CLT - FOUND FRAME DENTED .25 INCH, BS 827 AT S24L UPPER CHORD. INSTALLED FRAME DOUBLER PER SRM 53-10-4. (M)
- [SDR USAA011057](https://openairdocs.org/sdr/USAA011057), Aug 13, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, BS 359 S14L. REMOVED AND REPLACED WITH PART NR 1131272 PER SRM 51-10-01. (M)
- [SDR USAA011055](https://openairdocs.org/sdr/USAA011055), Aug 13, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .250 INCH, BS 380 STRINGER 26L. FABRICATED REPLACEMENT PART PER SRM 53-10-04. (M)
- [SDR USAA011056](https://openairdocs.org/sdr/USAA011056), Aug 13, 2001: ANGLE. CORRODED. CLT - FOUND Z-CHORD CORRODED 2 INCHES BY 10 INCHES, BS 947 TO BS 996. REMOVED AND REPLACED WITH NEW PART NR 1124774 PER SRM 51-10-1 AND SRM 51-30-02. (M)
- [SDR USAA011060](https://openairdocs.org/sdr/USAA011060), Aug 13, 2001: FLOORBEAM. CORRODED. CLT - FOUND TOP SURFACE OF T-CAP CORRODED, BS 947 RBL 22 THROUGH LBL 9. REPLACED T-CAP, INSTALLED PER EA 85177. (M)
- [SDR USAA011054](https://openairdocs.org/sdr/USAA011054), Aug 10, 2001: SKIN. DENTED. CLT - FOUND SKIN DENTED 2 INCHES BY 8 INCHES BY .250 INCH, BS 827 STRINGER 27L. PREVIOUS REPAIR, FOUND AT S27L, REPORT STATES S27R, PER SRM 53-30-3. (M)
- [SDR USAA011053](https://openairdocs.org/sdr/USAA011053), Aug 10, 2001: PRESSURE PANEL. DAMAGED. CLT - FOUND BEADS MISSING IN PRESSURE WEB, BS 662 TO BS 673 WL 203. INSTALLED ANGLE STIFFENERS PER EA 85189 REF SB 737-57-1234. (M)

All 89: https://openairdocs.org/deregistered/N264AU-2003-04-28/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19920421013799I](https://openairdocs.org/incident/19920421013799I), Apr 21, 1992: Boeing 737201 (N264AU), Rochester, NY. Flap extension problem on appraoch. Made go around. Landed safely. Replaced NR7 jackscrew ball nut assembly.

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