# N249US: 1982 Boeing 737-201, registration cancelled 2003-09-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 26, 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-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22756
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 8, 1982
- Certificate issued: May 2, 2002
- Last registry action: January 10, 2003
- Mode S code: A25341
- 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/N249US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=249US
- Page: https://openairdocs.org/deregistered/N249US-2003-09-26

From the FAA registry file of October 29, 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 (78, newest 50)

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

- [SDR USAASB01328](https://openairdocs.org/sdr/USAASB01328), Nov 28, 2001: CHARGER. FAILED. LGA - THE MID CABIN AISLE EMERGENCY EXIT SIGN FLICKERED ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN CHARGER. (M)
- [SDR USAA011027](https://openairdocs.org/sdr/USAA011027), Aug 7, 2001: CREASE BEAM. CRACKED. CLT - FOUND CREASE BEAM CRACKED .750 INCH, BS 520 LBL 64. EXTRUDED SECTION REPAIR, SPLICE REPLACEMENT PER SRM 51-40-4 FIG 1. (M)
- [SDR USAA011026](https://openairdocs.org/sdr/USAA011026), Aug 7, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED .125 INCH, BS 178 BULKHEAD AT WL 234 AT RBL 10. INSTALLED DOUBLER PER SRM 53-10-11 FIG 1, 53-10-1. (M)
- [SDR USAA011029](https://openairdocs.org/sdr/USAA011029), Aug 7, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3.5 INCHES, BS 294.5 LBL 1.5 TO RBL 1.5. CORROSION LEVEL 1, TASK NR C53-107-01. UPPER T-CHORD REPAIRED PER TR 53-10-0
- [SDR USAASB01149](https://openairdocs.org/sdr/USAASB01149), May 29, 2001: LIGHT. INOPERATIVE. IAD - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL 
- [SDR USAA010448](https://openairdocs.org/sdr/USAA010448), Apr 25, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 707, AFT SIDE OF STRINGER 11R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-01, INSTALLED FREEZE PLUG REPAIR PER EA 691
- [SDR USAA010447](https://openairdocs.org/sdr/USAA010447), Apr 25, 2001: PRESSURE PANEL. CRACKED. CLT - FOUND PRESSURE DECK WEB 2 INCH, BS 663-676, RBL 20 TO RBL 50. INSTALLED DOUBLED, STIFFENERS, CHORD SEGMENT, FILLERS, WEB PER EA''S 69129, 69125, 69183. (M
- [SDR USAA010354](https://openairdocs.org/sdr/USAA010354), Apr 4, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKS, TWO CRACKS .4 INCHES, TWO CRACKS AT .7 INCH, STATION 380 AND 397 BETWEEN STRINGER 19R AND 20R. INSTALLED DOUBLER PER EA 69250. (M)
- [SDR USAA010353](https://openairdocs.org/sdr/USAA010353), Apr 4, 2001: SUPPORT. DAMAGED. CLT - FOUND WEB SUPPORT WITH .5 INCH BULGE, HORIZ STAB JACKSCREW LOWER WEB SUPPORT, STATION 1088, LBL 4. INSTALLED WEB DOUBLER AND FILLER PER EA 69281. (M)
- [SDR USAA010352](https://openairdocs.org/sdr/USAA010352), Apr 4, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED 2 INCHES, STATION 670-672 RBL 25 MWW CEILING. INSTALLED SPLICE PLATE, STIFFENERS, ANGLES WEB REPAIR PER EA 69183. (M)
- [SDR USAA010355](https://openairdocs.org/sdr/USAA010355), Apr 4, 2001: FRAME. CHAFED. CLT - FOUND FRAME CHAFED 2.5 INCH, STATIN 1040 FRAME CUTOUT OF APU DUCT STRINGER 22L-26L. INSTALLED DOUBLER, TRIPLER AND SHEAR TIES. INSTALLED DOUBLER, TRIPLER 
- [SDR USAA010347](https://openairdocs.org/sdr/USAA010347), Mar 26, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 5 INCHES, STATION 727A PLUS 16 INCHES ABOVE STRINGER 17L. INSTALLED FILLER AND DOUBLER PER EA 69166. (M)
- [SDR USAA010299](https://openairdocs.org/sdr/USAA010299), Mar 20, 2001: STIFFENER. CORRODED. CLT - FOUND CORROSION ON CHANNEL STIFFENER 6 FEET, FORWARD LOWER SIDE AFT BULKHEAD AFT STATION 1016, BL 0. INSTALLED DOUBLER AND REPAIR ANGLES PER EA 69123. (M)
- [SDR USAA010298](https://openairdocs.org/sdr/USAA010298), Mar 20, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, TIE CLIP STATION 663, STRINGER 10L. REPLACED WITH NEW PART PER SRM 51-10-1. (M)
- [SDR USAA010265](https://openairdocs.org/sdr/USAA010265), Mar 7, 2001: BULKHEAD. CRACKED. CLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, RBL 5.7. REMOVED CRACKED AREA, INSTALLED DOUBLER. (M)
- [SDR USAA010261](https://openairdocs.org/sdr/USAA010261), Mar 5, 2001: BULKHEAD. CRACKED. CLT - FOUND BULKHEAD WEB CRACKED .125 INCH, BS 178, RBL 5, WL 189, 190 AND 191.5. REMOVED DAMAGE INSTALLED DOUBLER PER EA 69132. (M)
- [SDR USAA010264](https://openairdocs.org/sdr/USAA010264), Mar 2, 2001: BULKHEAD. CRACKED. CLT - FOUND BULKHEAD CRACKED 1 INCH, STATION 178 LBL 7, WL 213.5. REMOVED DAMAGE, INSTALLED DOUBLER. (M)
- [SDR USAA010263](https://openairdocs.org/sdr/USAA010263), Mar 2, 2001: BULKHEAD. CRACKED. CLT - FOUND BULKHEAD CRACKED .25 INCH, STATION 178, RBL 10.5, WL 234. REMOVED DAMAGE, INSTALLED DOUBLER. (M)
- [SDR USAA010188](https://openairdocs.org/sdr/USAA010188), Feb 28, 2001: WEB. CRACKED. CLT - FOUND DOOR WEB CRACKED .5 INCH, AFT SERVICE DOOR TORQUE BOX WEB BS 947 BELOW STRINGER 11R. INSTALLED DOUBLER PER TR 53-30-07A. (M)
- [SDR USAA010223](https://openairdocs.org/sdr/USAA010223), Feb 20, 2001: FRAME. CRACKED. CLT - FOUND VERTICAL CHORD CRACKED 1 INCH OUTBOARD RADIUS AND 1.8 INCH INBOARD, BS 178 BULKHEAD, LBL 5-7, WL 184. INSTALLED VERTICAL CHORD REPAIR PARTS PER EA 6
- [SDR USAA010222](https://openairdocs.org/sdr/USAA010222), Feb 20, 2001: FRAME. CRACKED. CLT - FOUND CHORD VERTICAL CRACKED .9 INCH IN INBOARD RADIUS, RBL 5-7, WL 184, BS 178 BULKHEAD. INSTALLED VERTICAL CHORD REPAIR PARTS PER EA 68935/EO5300V155. (
- [SDR 20010426AP004](https://openairdocs.org/sdr/20010426AP004), Feb 20, 2001: TIE CLIP. CRACKED. CLT - FOUND STRINGER AND TIE CLIP CRACKED .250 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED TIE CLIP AND INSTALLED STRINGER 18 INCH SECTION PER SRM 53-10-03,
- [SDR USAA010224](https://openairdocs.org/sdr/USAA010224), Feb 20, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER AND TIE CLIP CRACKED .250 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED TIE CLIP AND INSTALLED STRINGER 18 INCH SECTION PER SRM 53-10-03,
- [SDR USAA010237](https://openairdocs.org/sdr/USAA010237), Feb 19, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH, BS 380 AT E/E EQUIPMENT COOLING DUCT OUTLET. INSTALLED INTERIOR SKIN DOUBLER PER T/R 53-30-04. (M)
- [SDR USAA010236](https://openairdocs.org/sdr/USAA010236), Feb 19, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED 2 INCHES, FS 767 AT STRINGER 13L. INSTALLED REPAIR DOUBLERS PART 1 AND 2 IAW SRM 53-10-4. (M)
- [SDR USAA010235](https://openairdocs.org/sdr/USAA010235), Feb 19, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, FRAME 807 STRINGER 13L. REMOVED DAMAGE AND INSTALLED DOUBLERS PART 1 AND 2 IAW SRM 53-10-4. (M)
- [SDR USAA010234](https://openairdocs.org/sdr/USAA010234), Feb 19, 2001: SKIN. CRACKED. CLT - FOUND SKIN DOUBLER CRACKED 8 INCHES BY 11 INCHES, 727 PLUS 16 S 27R. INSTALLED DOUBLER PER SRM 53-30-03. (M)
- [SDR USAA010254](https://openairdocs.org/sdr/USAA010254), Feb 15, 2001: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .125 INCH, STATION 616 STRINGER 3 LEFT. MODIFIED PART NR INSTALLED. (M)
- [SDR USAA010253](https://openairdocs.org/sdr/USAA010253), Feb 15, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616 STRINGER 1. MODIFIED PART NR INSTALLED. (M)
- [SDR USAA010252](https://openairdocs.org/sdr/USAA010252), Feb 15, 2001: SHEAR TIE. CRACKED. CLT - FOUND SHEAR TIE CRACKED .5 INCH, BS 967 AT STRINGER 7L. FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-10-4 FIG 8. (M)
- [SDR USAA010255](https://openairdocs.org/sdr/USAA010255), Feb 14, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 15L BS 520-540. REPLACED STRINGER SECTION IAW SRM 53-10-3. (M)
- [SDR USAA010157](https://openairdocs.org/sdr/USAA010157), Feb 13, 2001: ANGLE. CRACKED. CLT - FOUND CREASEBEAM ANGLE .5 INCH, BS 630, RBL 45. FABRICATED NEW ANGLE PER SRM 51-10-1 AND DWG 65 47973. (M)
- [SDR USAA010156](https://openairdocs.org/sdr/USAA010156), Feb 13, 2001: CREASE BEAM. CRACKED. CLT - FOUND CREASEBEAM WEB CRACKED 1 INCH, AFT OUTBOARD CORNER AT STATION 638. SPLICED IN NEW SECTION PER SRM 51-10-1 AND 51-40-4. (M)
- [SDR USAA010152](https://openairdocs.org/sdr/USAA010152), Feb 12, 2001: TORQUE BOX. CRACKED. CLT - FOUND TORQUE BOX WEB CRACKED .5 INCH, BS 947 JUST BELOW STRINGER 11L. REMOVED AND REPLACED DOUBLER AND FILLER PER TR 53-30-07 REV A. (M)
- [SDR USAA01043](https://openairdocs.org/sdr/USAA01043), Feb 12, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 707, STRINGER 10R. INSTALLED NEW TIE CLIP PER SRM 51-10-1 AND 51-30-2. (M)
- [SDR USAA010142](https://openairdocs.org/sdr/USAA010142), Feb 12, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 706, STRINGER 6L. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA010141](https://openairdocs.org/sdr/USAA010141), Feb 12, 2001: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .125 INCH, STATION 639, STRINGER 3L. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010140](https://openairdocs.org/sdr/USAA010140), Feb 12, 2001: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .125 INCH, STATION 616, STRINGER 2R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010139](https://openairdocs.org/sdr/USAA010139), Feb 12, 2001: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .125 INCH, STATION 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA010138](https://openairdocs.org/sdr/USAA010138), Feb 12, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 328, LBL 54. CORROSION LEVEL 1. INSTALLED UPPER SECTION PER TR 53-10-13 AND SRM 51-10-6. (M)
- [SDR USAA010148](https://openairdocs.org/sdr/USAA010148), Feb 12, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 807, STRINGER 11L. REPLACED TIE CLIP PER SRM 51-10-01 AND DWG 69-45156. (M)
- [SDR USAA010147](https://openairdocs.org/sdr/USAA010147), Feb 12, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 807, STRINGER 10L. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010146](https://openairdocs.org/sdr/USAA010146), Feb 12, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 747, STRINGER 7R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010145](https://openairdocs.org/sdr/USAA010145), Feb 12, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED, STATION 747, STRINGER 4R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010144](https://openairdocs.org/sdr/USAA010144), Feb 12, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .5 INCH, FUSELAGE SKIN STATION 727A PLUS 8 JUST ABOVE STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-03. (M)
- [SDR USAA010262](https://openairdocs.org/sdr/USAA010262), Feb 4, 2001: BULKHEAD. CRACKED. CLT - FOUND PRESSURE BULKHEAD CRACKED 6.5 INCHES, BS 1016 PLUS 1 AT STRINGER 6L. INSTALLED FILLER, DOUBLER AND SHIMS. (M)
- [SDR USAA001393](https://openairdocs.org/sdr/USAA001393), Aug 30, 2000: BEAM. CORRODED. TPA - FOUND BEAMS AND ANGLES CORRODED 12 INCHES, AFT LAV AREA FS 986 TO 1016. CORROSION LEVEL 1. REMOVED AND REPLACED BEAMS AND ANGLES PER SRM 51-10-1. (M)
- [SDR USAA000774](https://openairdocs.org/sdr/USAA000774), May 29, 2000: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 1.5 INCHES, STATION 767, STRINGER 19L. PREVIOUS REPAIR TOO CLOSE TO DAMAGE. REMOVED IT AND INSTALLED LARGE REPAIR PER SRM 53-30-3 FIG 6
- [SDR USAASB00009](https://openairdocs.org/sdr/USAASB00009), Jan 10, 2000: ENGINE. FAILED. TPA - FLT 2746 - ON CLIMB-OUT FROM TPA, AT FL150, CREW REPORTED THE NR 1 ENGINE OIL PRESSURE WENT TO RED LINE WITH ENGINE TEMPERATURE FOLLOWING SHORTLY THEREAFT
- [SDR USAASB98154](https://openairdocs.org/sdr/USAASB98154), Jun 24, 1998: BATTERY PACK. DISCHARGED. CMH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

All 78: https://openairdocs.org/deregistered/N249US-2003-09-26/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 19900103044979I](https://openairdocs.org/incident/19900103044979I), Jan 3, 1990: Boeing 737201 (N249US), Jacksonville, FL, Minor damage. Left wing tip struck a jetway while turning to start taxiing. Signal man directing aircraft.

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