# N244US: 1982 Boeing 737-201, registration cancelled 2002-10-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 1, 2002 - 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-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22752 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 2, 1982 - Certificate issued: May 2, 2002 - Last registry action: May 2, 2002 - Mode S code: A240AE - 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/N244US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=244US - Page: https://openairdocs.org/deregistered/N244US-2002-10-01 From the FAA registry file of October 28, 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 (84, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAASB01232](https://openairdocs.org/sdr/USAASB01232), Aug 16, 2001: LIGHT. INOPERATIVE. ALB - PILOT REPORTED THAT THE COCKPIT EVACUATION LIGHT WOULD NOT ILLUMINATE WITH COCKPIT SWITCH IN THE ON POSITION. MAINTENANCE REMOVED AND REPLACED THE LIGHT A - [SDR USAASB01084](https://openairdocs.org/sdr/USAASB01084), Mar 22, 2001: HARNESS. FAILED. BOS - FLT 2993 - ON CLIMB-OUT FROM BOS, EN ROUTE TO FLL, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED. CREW TRIED TO RESET GENERATOR WITH NO HELP. THE APU WAS A - [SDR USAA000954](https://openairdocs.org/sdr/USAA000954), Jul 6, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, BS 986.5, LBL 38. INSTALLED NEW FLOOR SUPPORT PER SRM 51-10-1. (M) - [SDR USAA000953](https://openairdocs.org/sdr/USAA000953), Jul 6, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 787, STRINGER 20R. INSTALLED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000950](https://openairdocs.org/sdr/USAA000950), Jul 3, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 3 INCHES AND 2 INCHES BY 2 INCHES, BS 986.5 4 INCHES, RBL AND 4 INCHES THROUGH 12 INCHES LBL. FABRICATED NEW T-CAP AN - [SDR USAA000949](https://openairdocs.org/sdr/USAA000949), Jul 3, 2000: STRAP. CRACKED. CLT - FOUND STRAP CRACKED .750 INCH, S-5A STRAP STATION 1138 LT SIDE. INSTALLED INTERIM REPAIR PER EA 67518 AND SRM 53-00-01 FIG 221. (M) - [SDR USAA000948](https://openairdocs.org/sdr/USAA000948), Jul 3, 2000: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED 3 INCHES, STATION 1006 TO 1009, STRINGER 27R. REPAIRED PER BOEING DWG 65-46558. (M) - [SDR USAA000947](https://openairdocs.org/sdr/USAA000947), Jul 3, 2000: SKIN. CRACKED. CLT - FOUND AFT SKIN CRACKED .350 INCH, BS 951 AFT GALLEY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR USAA000946](https://openairdocs.org/sdr/USAA000946), Jul 3, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .3 INCHES, STATION 948 SKIN UPPER END SERVICE DOOR HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR USAA000945](https://openairdocs.org/sdr/USAA000945), Jul 3, 2000: FRAME. CRACKED. CLT - FOUND FRAME .125 INCH CRACKED, STATION 887, STRINGER 19L. REMOVED AND INSTALLED DOUBLER PER SRM 53-10-4 FIG 9. (M) - [SDR USAA000944](https://openairdocs.org/sdr/USAA000944), Jul 3, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 787, STRINGER 3R. INSTALED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA000943](https://openairdocs.org/sdr/USAA000943), Jul 3, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .5 INCH, BS 764.5 AT STRINGER 19L. INSTALLED FILLER AND DOUBLER PER 53-30-3 FIG 6. (M) - [SDR USAA000942](https://openairdocs.org/sdr/USAA000942), Jul 3, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .5 INCH, BS 727A PLUS 17 INCHES STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M) - [SDR USAA000941](https://openairdocs.org/sdr/USAA000941), Jul 3, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727A PLUS 8 INCHES STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M) - [SDR USAA000940](https://openairdocs.org/sdr/USAA000940), Jul 3, 2000: STRINGER CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 706, STRINGER 3R. REMOVED AND REPLACED PER SRM 51-10-1. (M) - [SDR USAA000939](https://openairdocs.org/sdr/USAA000939), Jul 3, 2000: FLOORBEAM. CRACKED. CLT - FOUND 2 CRACKS IN FLOORBEAM .100 INCH, BS 663, WL 208 UPPER T-CAP. INSTALLED REPAIR PER TR 57-10-04. (M) - [SDR USAA000938](https://openairdocs.org/sdr/USAA000938), Jul 3, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED .250 INCH, STATION 520, RBL 45 UPPER CHORD RADIUS. INSTALLED REPAIR PER EA 67455. (M) - [SDR USAA000937](https://openairdocs.org/sdr/USAA000937), Jul 3, 2000: FLOORBEAM. CRACKED. CLT - FOUND BEAM CRACKED 3 INCHES, BS 520, RBL 24, WL 208. INSTALLED REPAIR ANGLE PER EA 67455. (M) - [SDR USAA000936](https://openairdocs.org/sdr/USAA000936), Jul 3, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED, BS 520, LBL 45 UPPER CHORD AFT RADIUS. INSTALLED DOUBLER PER EA 67455. (M) - [SDR USAA000935](https://openairdocs.org/sdr/USAA000935), Jul 3, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED .500 INCH, BS 520, LBL 24 UPPER CHORD AFT RADIUS. REPAIRED PER EA 67455. (M) - [SDR USAA000934](https://openairdocs.org/sdr/USAA000934), Jul 3, 2000: STRINGER CLIP. CRACKED. CLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 520, STRINGER 19L. INSTALLED DOUBLER PER SRM 51-40-03. (M) - [SDR USAA000933](https://openairdocs.org/sdr/USAA000933), Jul 3, 2000: WEB. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, STRINGER 10L SUPPORT WEB BS 350. REPLACED WEB PER SRM 51-10-02. (M) - [SDR USAA000932](https://openairdocs.org/sdr/USAA000932), Jul 3, 2000: ANGLE. CRACKED. CLT - FOUND ANGLE CRACKED 1.5 INCHES, BS 350, STRINGER 16L. REPLACED SUPPORT ANGLE PER SRM 51-10-2. (M) - [SDR USAA000931](https://openairdocs.org/sdr/USAA000931), Jul 3, 2000: ANGLE. CRACKED. CLT - FOUND ANGLE CRACKED 2 INCHES, BS 350, STRINGER 15L. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND SRM 51-40-02. (M) - [SDR USAA000930](https://openairdocs.org/sdr/USAA000930), Jul 3, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED 1.5 INCH, BS 350, AT STRINGER 15L DOOR STOP FITTING. REPAIRED PER SRM 51-10-2. (M) - [SDR USAA000929](https://openairdocs.org/sdr/USAA000929), Jul 3, 2000: SKIN. CRACKED. CLT - FOUND OUTER SKIN CRACKED 3 INCHES, AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER STATION 947. INSTALLED EXTERNAL SKIN TRIPLER PER SRM 53-30-3. (M) - [SDR USAA000928](https://openairdocs.org/sdr/USAA000928), Jul 3, 2000: SKIN. CRACKED. CLT - FOUND INNER SKIN PLATE CRACKED 1 INCH, AFT SERVICE DOOR FUSE. CUTOUT TORQUE BOX INBOARD SIDE. INSTALLED DOUBLER AND FILLER PER TR 53-30-07A. (M) - [SDR USAA000927](https://openairdocs.org/sdr/USAA000927), Jul 3, 2000: SUPPORT FITTING. CRACKED. CLT - FOUND SUPPORT FITTING CRACKED .200 INCH, RT WING LANDING GEAR BEAM. ACCOMPLISHED PART A PER TR 57-40-10. (M) - [SDR USAA000951](https://openairdocs.org/sdr/USAA000951), Jul 3, 2000: ANGLE. CORRODED. CLT - FOUND Z-ANGLE CORRODED 24 INCHES BY 1 INCH, AFT SERVICE DOOR BS 947 TO BS 986 RT. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M) - [SDR USAA000879](https://openairdocs.org/sdr/USAA000879), Jun 20, 2000: ANGLE. CORRODED. CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 1 INCH, AFT ENTRY DOOR SILL Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-10-1 AND 51-30-0. CORROSION LEVEL 1. (M) - [SDR USAA000873](https://openairdocs.org/sdr/USAA000873), Jun 19, 2000: STRINGER. CORRODED. CLT - FOUND STRINGER CORRODED 2 INCHES, STATION 947 STRINGER 27L. REMOVED AND REPLACED PER SRM 53-10-03. (M) - [SDR USAA000872](https://openairdocs.org/sdr/USAA000872), Jun 19, 2000: FITTING. CRACKED. CLT - FOUND BULKHEAD FITTING CRACKED .750 AND .375 INCH, BS 663.75 BULKHEAD FITTING RT SIDE WL 191.5 POCKET. REMOVED AND REPLACED BULKHEAD FITTING PER EA 67452, - [SDR USAA000854](https://openairdocs.org/sdr/USAA000854), Jun 15, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 12 INCHES BY 1 INCH, 3 AREAS AT STATION 344, LBL 8 THROUGH LBL 18. REPAIRED T-CAP PER TR 53-10-13. CORROSION LEVEL 2. (M) - [SDR USAA000852](https://openairdocs.org/sdr/USAA000852), Jun 15, 2000: FRAME. CORRODED. CLT - FOUND FRAME CORRODED 2.5 INCHES, BS 967, STRINGER 26R AT SKIN ATTACH POINT. INSTALLED DOUBLER FRAME REPAIR PER SRM 53-10-4. CORROSION LEVEL 2, C53-208-01. - [SDR USAA000836](https://openairdocs.org/sdr/USAA000836), Jun 13, 2000: WEB. CRACKED. CLT - FOUND WEB/STIFFENER CRACKED 6 INCHES, STATION 727, LBL 13 BETWEEN VERT SUPPORT BEAMS. REPLACED PART PER SRM 51-10-1. (M) - [SDR USAA000837](https://openairdocs.org/sdr/USAA000837), Jun 13, 2000: ANGLE. CRACKED. CLT - FOUND ANGLE CRACKED 4 INCHES, STATION 727B LBL 40. REPLACED PER SRM 51-10-1. (M) - [SDR USAA000839](https://openairdocs.org/sdr/USAA000839), Jun 13, 2000: STRINGER. CRACKED. CLT - FOUND SEVERAL CRACKS .125 INCH OR LESS, INSIDE CHANNEL STRINGER 15L, BETWEEN STATION 520 AND 540. INSTALLED STRINGER REPAIR SECTION PER SRM 53-10-3. (M) - [SDR USAA000813](https://openairdocs.org/sdr/USAA000813), Jun 12, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 706, STRINGER 5R. REMOVED AND REPLACED PER SRM 51-10-1. (M) - [SDR USAA000808](https://openairdocs.org/sdr/USAA000808), Jun 8, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 787 STRINGER 7R. REPLACED TIE CLIP PER SRM 51-10-1. (M) - [SDR USAA000804](https://openairdocs.org/sdr/USAA000804), Jun 8, 2000: INTERCOSTAL. CRACKED. CLT - FOUND INTERCOSTAL CRACKED 1 INCH AND 2 INCHES, FLOOR SUPPORT BETWEEN STATION 380 TO 400 BL 0. REPAIRED PER SRM 51-10-01. (M) - [SDR USAA000797](https://openairdocs.org/sdr/USAA000797), Jun 5, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 767, STRINGER 11R. FABRICATED NEW CLIP PER SRM 51-10-1 AND DWG 6945156. (M) - [SDR USAA000798](https://openairdocs.org/sdr/USAA000798), Jun 5, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 663, STRINGER 10L. REPAIRED PER EO 5393G227. (M) - [SDR USAA000799](https://openairdocs.org/sdr/USAA000799), Jun 5, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 597, STRINGER 5R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-1. (M) - [SDR USAA000800](https://openairdocs.org/sdr/USAA000800), Jun 5, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 706, STRINGER 3R. REPAIRED PER EO 5393G227. (M) - [SDR USAA000775](https://openairdocs.org/sdr/USAA000775), Jun 2, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 685, STRINGER 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M) - [SDR USAA000776](https://openairdocs.org/sdr/USAA000776), Jun 2, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M) - [SDR USAA000777](https://openairdocs.org/sdr/USAA000777), Jun 2, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 3R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M) - [SDR USAA000778](https://openairdocs.org/sdr/USAA000778), Jun 2, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 5R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M) - [SDR USAA000779](https://openairdocs.org/sdr/USAA000779), Jun 2, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 7R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M) - [SDR USAA991341](https://openairdocs.org/sdr/USAA991341), Dec 6, 1999: KEEL BEAM. CORRODED. TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND MINOR CORROSION 4 INCH BY 6 INCH BOTTOM KEEL BEAM STATION 727 STRINGER 26L. CORROSION LEVEL 1. All 84: https://openairdocs.org/deregistered/N244US-2002-10-01/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 19901017055449I](https://openairdocs.org/incident/19901017055449I), Oct 17, 1990: Boeing 737201 (N244US), Charlotte, NC. Cabin pressure rose after departure. Descended and returned for landing. ## Other aircraft with N244US - [Registered now](https://openairdocs.org/aircraft/N244US): Costruzioni Aeronautiche Tecna P2012 TRAVELLER, S/N 044/US, built 2022 --- 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.