# N248US: 1982 Boeing 737-201, registration cancelled 2003-12-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 18, 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: 22755
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 17, 1982
- Certificate issued: May 2, 2002
- Last registry action: January 10, 2003
- Mode S code: A24F8A
- 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/N248US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=248US
- Page: https://openairdocs.org/deregistered/N248US-2003-12-18

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 (120, newest 50)

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

- [SDR USAASB01216](https://openairdocs.org/sdr/USAASB01216), Jul 30, 2001: BATTERY. DISCHARGED. BWI - THE EMERGENCY EXIT SIGN AT SEAT ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY. (M)
- [SDR USAASB0108](https://openairdocs.org/sdr/USAASB0108), Mar 18, 2001: CONNECTOR. DAMAGED. LGA-PBI - FLT 2693 - DURING A DESCENDING TURN THE CONTROL COLUMN SEIZED. NEITHER THE CAPT NOR THE F O COULD MOVE THE CONTROL COLUMN FOR SEVERAL SECONDS. AFTER A
- [SDR USAASB01080](https://openairdocs.org/sdr/USAASB01080), Mar 18, 2001: CONTROL COLUMN. SEIZED. LGA-PBI - FLT 2693 - DURING A DESCENDING TURN THE CONTROL COLUMN SEIZED. NEITHER THE CAPTAIN NOR THE FIRST OFFICER COULD MOVE THE CONTROL COLUMN FOR SEVERAL SEC
- [SDR USAASB01051](https://openairdocs.org/sdr/USAASB01051), Feb 20, 2001: DUCT. FAILED. BWI - FLT 2639 - ON CLIMB-OUT FROM BWI, AT FL120, THE NR 2 ENG OVERHEAT LIGHT ILLUMINATED. CREW REDUCED POWER ON NR 2 ENG TO IDLE AND LIGHT EXTINGUISHED. CREW D
- [SDR USAASB00366](https://openairdocs.org/sdr/USAASB00366), Dec 31, 2000: DUCT. CRACKED. BWI - FLT 2631 - EN ROUTE FROM FLL TO LGA, THE RIGHT WING-TO-BODY OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND CONTINUED FL
- [SDR USAASB00365](https://openairdocs.org/sdr/USAASB00365), Dec 30, 2000: BATTERY PACK. DISCHARGED. BWI - MAINTENANCE FOUND THE FORWARD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE FORWARD ENTRY
- [SDR USAA001962](https://openairdocs.org/sdr/USAA001962), Nov 17, 2000: SKIN. CRACKED. CRACKS NR 5 SLAT INBD TRACK IN SLAT LWR SKIN AT SPAR. INSTALLED DOUBLER PER EA 68377
- [SDR USAA001961](https://openairdocs.org/sdr/USAA001961), Nov 17, 2000: FRAME. CRACKED. CRACK STA 663 BULKHD UPPER CHORD RBL 25, WBL 201.5. INSTALLED NEW CHORD SEGMENT & SPLICE ANGLES PER EA 68487
- [SDR USAA001972](https://openairdocs.org/sdr/USAA001972), Nov 17, 2000: FLOORBEAM. CRACKED. FLOORBEAM CRACKED. INSTALLED DOUBLER AND RADIUS BLOCKS INSTALLED PER EA68253
- [SDR USAA001971](https://openairdocs.org/sdr/USAA001971), Nov 17, 2000: FLOORBEAM. CRACKED. FLOORBEAM CRACKED. DOUBLER INSTALLED PER EA68253
- [SDR USAA001970](https://openairdocs.org/sdr/USAA001970), Nov 17, 2000: SEAT TRACK. CRACKED. SEAT TRACK CRACKED. INSTALLED SEAT TRACK AND FLOOR SUPPORTS
- [SDR USAA0001969](https://openairdocs.org/sdr/USAA0001969), Nov 17, 2000: STRINGER CLIP. CRACKED. TEXTDRACKCORRECTIVE ACTION: DEFECTIVE PART REPLACED WITH IDENT. PART #
- [SDR USAA001968](https://openairdocs.org/sdr/USAA001968), Nov 17, 2000: FRAME. CRACKED. FRAME CRACKED. CORRECTIVE ACTION: INSTALLED REPAIR ANGLE PER SRM 51-40-3
- [SDR USAA001967](https://openairdocs.org/sdr/USAA001967), Nov 17, 2000: FASTENER. CRACKED. FASTENER CRACKED. CORRECTIVE ACTION:DEFECTIVE PART REPLACED WITH IDENT PART.
- [SDR USAA001966](https://openairdocs.org/sdr/USAA001966), Nov 17, 2000: FLOORBEAM. CRACKED. FLOORBEAM CRACKED. STOP DRILLED CRACK, HFEC VERIFIED CRACK REMOVED, INSTALLED REPAIR DBLRS PER EA 68328
- [SDR USAA001965](https://openairdocs.org/sdr/USAA001965), Nov 17, 2000: STRINGER CLIP. CRACKED. STRINGER CLIP IS CRACKED. DEFECTIVE PART REPLACED WITH IDENT. PART
- [SDR USAA001964](https://openairdocs.org/sdr/USAA001964), Nov 17, 2000: STRINGER CLIP. CRACKED. STINGER CLIP IS CRACKED. DRILLED IDENTICAL REPLACEMENT PART & INSTALLED PER EO 53936227
- [SDR USAA001963](https://openairdocs.org/sdr/USAA001963), Nov 17, 2000: STRINGER CLIP. CRACKED. STRINGER CLIP IS CRACKED. DEFECTIVE PART REPLACED WITH PART 693535214
- [SDR USAA001956](https://openairdocs.org/sdr/USAA001956), Nov 15, 2000: SKIN. CRACKED. CRACK FUSELAGE SKIN STA 727A FWD SIDE STR 16R. CORRECTIVE ACTION: INSTALLED DOUBLER PER SRM 53-30-3
- [SDR USAA001957](https://openairdocs.org/sdr/USAA001957), Nov 15, 2000: SKIN. CRACKED. CRACK FUSELAGE SKIN STA 727A FWD SIDE STR 16L. CORRECTIVE ACTION: INSTALLED DOUBLER PER SRM 53-30-3
- [SDR USAA001924](https://openairdocs.org/sdr/USAA001924), Nov 13, 2000: KEELBEAM. CORRODED. CLT - FOUND KEEL BEAM ANGLE .750 INCH BY 64 INCHES, LOWER KEEL BEAM RIGHT ANGLE STATION 727 TO 663. INSTALLED REPAIR STRAPS PER TR 53-10-22. (M)
- [SDR USAA001923](https://openairdocs.org/sdr/USAA001923), Nov 13, 2000: FRAME. CORRODED. CLT - FOUND CHORD CORRODED 5 INCHES, PRESSURE BULKHEAD RIGHT SIDE OF Y CHORD STATION 1016 BL 0. REPAIRED WEB PER EA 68373A AND SRM 51-30-0. (M)
- [SDR USAA001922](https://openairdocs.org/sdr/USAA001922), Nov 13, 2000: BULKHEAD. CRACKED. CLT - FOUND BULKHEAD WEB CRACKED .125, BS 1016 BETWEEN STRINGER 5L AND 6L. INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 15. (M)
- [SDR USAA001921](https://openairdocs.org/sdr/USAA001921), Nov 13, 2000: CROSSBEAM. CRACKED. CLT - FOUND BEAM CRACKED 2 INCHES, LOWER CROSS BEAM OF FORWARD CARGO DOOR. INSTALLED DOUBLER PER EA 68360. (M)
- [SDR USAA001916](https://openairdocs.org/sdr/USAA001916), Nov 9, 2000: SEAT TRACK. CRACKED. CLT - FOUND SEAT TRACK CRACKED TWO PLACES .25 INCH EACH, FORWARD OF STATION 520, BELOW LBL 45.5 SEAT TRACK. FABRICATED NEW WEB PER SRM 51-10-1. (M)
- [SDR USAA001915](https://openairdocs.org/sdr/USAA001915), Nov 9, 2000: FITTING. CRACKED. CLT - FOUND FITTING CRACKED .5 INCH, STATION 331.1 AFT SIDE STRINGER 8R. REMOVED AND INSTALLED PER SRM 51-10-01. (M)
- [SDR USAA001914](https://openairdocs.org/sdr/USAA001914), Nov 9, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, FORWARD FRAME OF FORWARD SERVICE DOOR STATION 328. INSTALLED DOUBLER PER SRM 51-40-2. (M)
- [SDR USAA001913](https://openairdocs.org/sdr/USAA001913), Nov 9, 2000: ATTACH ANGLE. CRACKED. CLT - FOUND ATTACH ANGLE CRACKED .25 INCH, STATION 290, STRINGER 10R. REPLACED PER SRM 51-30-0 AND 51-10-1. (M)
- [SDR USAA001912](https://openairdocs.org/sdr/USAA001912), Nov 9, 2000: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED 1 INCH, STATION 270, STRINGER 14R. FABRICATED NEW INTERCOSTAL PER SRM 53-10-2 FIG 1. (M)
- [SDR USAA001911](https://openairdocs.org/sdr/USAA001911), Nov 9, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 4 INCHES, BL 0 LONGITUDINAL UPPER CHORD WEB WL 208, STATION 663. REMOVED DAMAGE INSTALLED DOUBLER PER SRM 51-10-02. (M)
- [SDR USAA001908](https://openairdocs.org/sdr/USAA001908), Nov 8, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 1 INCH, BS 669, RBL 24 LONGITUDINAL UPPER CHORD. REPAIRED DOUBLER AND U-CHANNEL PER EA 68275. (M)
- [SDR USAA001907](https://openairdocs.org/sdr/USAA001907), Nov 8, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 1 INCH, BS 665, RBL 24 UPPER CHORD. REPAIRED DOUBLER AND U-CHANNEL PER EA 68275. (M)
- [SDR USAA001906](https://openairdocs.org/sdr/USAA001906), Nov 8, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED .5 INCH, BS 663, RBL 24 UPPER CHORD. REPAIRED DOUBLERS AND U-CHANNEL PER EA 68275. (M)
- [SDR USAA001905](https://openairdocs.org/sdr/USAA001905), Nov 7, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED .5 INCH, 360 AND RBBL 53. INSTALLED REPAIR DOUBLER PER EA 68400. (M)
- [SDR USAA001904](https://openairdocs.org/sdr/USAA001904), Nov 7, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH, STATION 986, LBL 30 TO RBL 45. INSTALLED T-CAP TR 53-60-01 REV A. (M)
- [SDR USAA001903](https://openairdocs.org/sdr/USAA001903), Nov 7, 2000: ANGLE. CORRODED. CLT - FOUND Z-ANGLE CORRODED 2 INCHES BY 1.5 INCHES, BS 957-1006. CORROSION LEVEL 1 C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-01. (M)
- [SDR USAA001901](https://openairdocs.org/sdr/USAA001901), Nov 7, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED 1 INCH BY 3 INCHES, STATION 767 FRAME BL 0. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 51-40-3. (M)
- [SDR USAA001900](https://openairdocs.org/sdr/USAA001900), Nov 7, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 500 AND STRINGER 21L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-4. (M)
- [SDR USAA001899](https://openairdocs.org/sdr/USAA001899), Nov 7, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 1 INCH, BL 0 LONGITUDINAL WEB STATION 706 TO 714, WL 203. INSTALLED REPAIR DOUBLER AND WEB PER EA 68300 AND SRM 53-60-51. (M)
- [SDR USAA001898](https://openairdocs.org/sdr/USAA001898), Nov 7, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED .25 INCH, LBL 25 LONGITUDINAL WEB STATION 706 TO 710, WL 203. INSTALLED WEB REPAIR PER EA 68300. (M)
- [SDR USAA001897](https://openairdocs.org/sdr/USAA001897), Nov 7, 2000: BEAM. CRACKED. CLT - FOUND BEAM CRACKED 3 INCHES, STATION 695 STUB BEAM WEB LBL 62, WL 206. FABRICATED STUB BEAM WEB AND INSTALLED PER SRM 51-10-1. (M)
- [SDR USAA001896](https://openairdocs.org/sdr/USAA001896), Nov 7, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 1.5 INCHES, LBL 24 LONGITUDINAL AT AILERON QUADRANT STATION 677. INSTALLED DOUBLER AND U-CHANNEL PER EO 5791G632. (M)
- [SDR USAA001895](https://openairdocs.org/sdr/USAA001895), Nov 7, 2000: ANGLE. CRACKED. CLT - FOUND FRAME CHORD ANGLE CRACKED .50 INCH, INBOARD CHORD ANGLE OF FRAME AT STATION 639 STRINGER 16L. REMOVED AND REPLACED PER SRM 51-10-1. (M)
- [SDR USAA001894](https://openairdocs.org/sdr/USAA001894), Nov 7, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 1.5 INCH, RBL 24 LONGITUDINAL FLOORBEAM STATION 677, WL 206. INSTALLED DOUBLER AND U-CHANNEL PER EA 68275. (M)
- [SDR USAA001893](https://openairdocs.org/sdr/USAA001893), Nov 7, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .5 INCH, STATION 322, FORWARD ENTRY DOOR SILL. EXTERIOR. INSTALLED REPAIR STRAP AND DOUBLER PER EA 68364. (M)
- [SDR USAA001876](https://openairdocs.org/sdr/USAA001876), Nov 3, 2000: STRINGER. CRACKED. CLT - FOUND SHELF 18A CRACKED .5 INCH, LEFT MOST INBOARD HOLE. INSTALLED NEW PART PER SRM 51-30-1. (M)
- [SDR USAA001871](https://openairdocs.org/sdr/USAA001871), Nov 2, 2000: WEB. CRACKED. CLT - FOUND WEB CRACKED .75 INCH, BS 178, WL 213, LBL 5. INSTALLED DOUBLER PER SRM 53-10-11 AND EA 68167. (M)
- [SDR USAA001870](https://openairdocs.org/sdr/USAA001870), Nov 2, 2000: WEB. CRACKED. CLT - FOUND WEB CRACKED 2 INCHES, BS 178 LBL 5, WL 201/197. INSTALLED DOUBLER PER SRM 53-10-11. (M)
- [SDR USAA001869](https://openairdocs.org/sdr/USAA001869), Nov 2, 2000: WEB. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, BS 178, WL 190, 194, 196 AT RBL 5. INSTALLED DOUBLER PER SRM 53-10-11 AND EA 68167. (M)
- [SDR USAA001868](https://openairdocs.org/sdr/USAA001868), Nov 2, 2000: WEB. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, BS 178, LBL 5, WL 190, 193, 194. INSTALLED DOUBLER PER EA 68167 AND SRM 53-10-11. (M)

All 120: https://openairdocs.org/deregistered/N248US-2003-12-18/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 19920107003639I](https://openairdocs.org/incident/19920107003639I), Jan 7, 1992: Boeing 737201 (N248US), Charlotte, NC, Minor damage. Noise on climbout. Engine indicators dropped to zero. Returned. Engine turbine failure and metal in tailpipe.

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