# N246US: 1982 Boeing 737-201, registration cancelled 2002-03-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 25, 2002 - Exported to: Mexico - Status when cancelled: Triennial form not returned - 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: 22753 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 26, 1982 - Certificate issued: August 15, 1989 - Last registry action: April 18, 2000 - Mode S code: A2481C - Owner when cancelled: [US Airways Inc](https://openairdocs.org/faa-owner/US%20AIRWAYS%20INC) - Location: [Arlington, VA](https://openairdocs.org/faa-place/VA/Arlington) - Owner type: Corporation - Owner's area on the map: 38.8783° N, 77.1007° W: Placed by OpenAirDocs: center of Arlington, VA, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N246US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=246US - Page: https://openairdocs.org/deregistered/N246US-2002-03-25 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 (79, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA010396](https://openairdocs.org/sdr/USAA010396), Apr 16, 2001: SKIN. CRACKED. TPA - FOUND SKIN CRACKED BS 727A PLUS 1 INCH BELOW STRINGER 17L, BS 727A PLUS 18 INCHES ABOVE STRINGER 18L. REMOVED EXISTING REPAIR, INSTALLED REPAIR DOUBLER AN - [SDR USAA010394](https://openairdocs.org/sdr/USAA010394), Apr 16, 2001: SKIN. CRACKED. TPA - FOUND SKIN CRACKED 1.5 INCH, BS 727B PLUS 12 INCHES, STRINGER 17L. INSTALLED REPAIR DOUBLE, SRM 53-30-3, FIG 1. (M) - [SDR USAASB01098](https://openairdocs.org/sdr/USAASB01098), Apr 7, 2001: POWER SUPPLY. INOPERATIVE. CLE - THE AFT SERVICE DOOR AND AFT ENTRY DOOR EMERGENCY EXIT SIGNS AND ENTRY DOOR LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY - [SDR USAA010395](https://openairdocs.org/sdr/USAA010395), Apr 1, 2001: SKIN. CRACKED. TPA - FOUND SKIN CRACKED 4 INCHES, BS 747 PLUS 3 INCHES, STRINGER 18R. INSTALLED REPAIR DOUBLER, SRM 53-30-3 FIG 1. (M) - [SDR USAA010164](https://openairdocs.org/sdr/USAA010164), Jan 16, 2001: SKIN. CRACKED. BOS - FOUND SKIN CRACKED 2 INCHES, BS 727A STRINGER 15L. INSTALLED DOUBLER PER SRM 53-30-3 PP 2E, FIG 1. (M) - [SDR USAASB00260](https://openairdocs.org/sdr/USAASB00260), Sep 17, 2000: CONTROL UNIT. FAILED. FLL - FLT 2995 - EN ROUTE FROM LGA-FLL, AT FL310, THE PASSENGERS OXYGEN DROPPED TO ZERO PSI. CREW ACCOMPLISHED PROCEDURES AND DESCENDED TO FL100. BEFORE LANDING - [SDR USAA000736](https://openairdocs.org/sdr/USAA000736), May 24, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 30 INCHES, STATION 328, LBL 28, AND RBL 20 - RBL 50. T-CAP REPLACEMENT PER SRM 53-10-2. (M) - [SDR USAA000735](https://openairdocs.org/sdr/USAA000735), May 24, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED, 1 INCH BY 8 INCH, BS 259 FLOORBEAM. INSTALLED DOUBLER AND NEW T-CAP PER TR 53-10-16 AND EA 67170. CORROSION LEVEL 2. (M) - [SDR USAA000726](https://openairdocs.org/sdr/USAA000726), May 23, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 344 UPPER CHORD LBL 15 TO LBL 50. REPAIRED T-CAP PER TR 53-10-13. (M) - [SDR USAA000725](https://openairdocs.org/sdr/USAA000725), May 23, 2000: FITTING. CRACKED. CLT - FOUND .5 INCH CRACK IN FITTING, OUTBOARD SUPPORT FITTING MLG BEAM AT CUTOUT, REMOVED AND REPLACED. (M) - [SDR USAA000715](https://openairdocs.org/sdr/USAA000715), May 16, 2000: FITTING. CRACKED. CLT - Q-1, EXPANSION BEAM FITTING CRACKED 1.5 INCHES, BS 520, RBL 25. INSTALLED DOUBLER AND NEW CHANNEL PER EA 67143. (X) - [SDR USAA000711](https://openairdocs.org/sdr/USAA000711), May 15, 2000: BEAM. CRACKED. CLT - Q-1, BEAM WEB HAD 2 EACH .75 INCH CRACKS, BL ZERO, STA 706 TO STA 713, WL 203 BEAM WEB. INSTALLED DOUBLER PER EA 67224. (X) - [SDR USAA000710](https://openairdocs.org/sdr/USAA000710), May 15, 2000: FITTING. CRACKED. CLT - Q-1, EXPANSION BEAM FITTING HAD .50 INCH CRACK, STA 520, LBL 25 EXPANSION BEAM FITTING . INSTALLED DOUBLER AND REPAIR ANGLES PER EA 67143. (X) - [SDR USAA000704](https://openairdocs.org/sdr/USAA000704), May 11, 2000: FLOORBEAM. CORRODED. CLT - FLOORBEAM HAD LEVEL 2 CORROSION, 3 INCHES BY 15 INCHES, BS 986.5 LBL 14 TO RBL 16. INSTALLED T-CAP PER TR 53-60-1. (X) - [SDR USAA000694](https://openairdocs.org/sdr/USAA000694), May 11, 2000: BELTFRAME. CORRODED. CLT - BELT FRAME HAD LEVEL 2 CORROSION, .250 INCH BY .250 INCH, BS 727B, RBL 04. INSTALLED DOUBLER PER SRM 53-10-4. (X) - [SDR USAA000692](https://openairdocs.org/sdr/USAA000692), May 11, 2000: FLOORBEAM. CORRODED. CLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 1 INCH, BS 986.5 LBL 43. INSTALLED T-CAP PER TR 53-60-01. (X) - [SDR USAA000690](https://openairdocs.org/sdr/USAA000690), May 11, 2000: FLOORBEAM. CORRODED. CLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 6 INCH, AT BS 986.5, RBL 27, RBL 33. INSTALLED T-CAP PER TR 53-60-1. (X) - [SDR USAA000688](https://openairdocs.org/sdr/USAA000688), May 11, 2000: FLOORBEAM. CORRODED. CLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 2 INCH, BS 986.5, RBL 40 TO RBL 42. INSTALLED T-CAP PER TR 53-60-1. (X) - [SDR USAA000687](https://openairdocs.org/sdr/USAA000687), May 11, 2000: SKIN. CRACKED. CLT - SKIN CRACKED 2.7 INCHES, STR 19L, STA 726 - STA 765, STR 18L 765-780. REPAIRED FILLER AND DOUBLER PER SRM 53-30-03 FIGURE 17. (X) - [SDR USAA000686](https://openairdocs.org/sdr/USAA000686), May 11, 2000: FLOORBEAM. CRACKED. CLT - FLOORBEAM CRACKED .50 INCH, UPPER FLANGE STA 520, LBL 45. INSTALLED DOUBLER AND PIVOT LINK PER EA 67143. (X) - [SDR USAA000685](https://openairdocs.org/sdr/USAA000685), May 11, 2000: ATTACH ANGLE. CRACKED. CLT - ATTACH ANGLE CRACKED 1.50 INCHES, AT FRAME TO STRINGER ATTACH ANGLE STA 360, STR 20R. INSTALLED DOUBLER PER SRM 51-40-3. (X) - [SDR USAA000684](https://openairdocs.org/sdr/USAA000684), May 11, 2000: FRAME. CRACKED. CLT - FRAME HAD A 4 INCH CRACK AT STA 360, JUST ABOVE STR 20R. INSTALLED DOUBLER PER SRM 51-40-3. (X) - [SDR USAA000683](https://openairdocs.org/sdr/USAA000683), May 11, 2000: FLOORBEAM. CORRODED. CLT- FLOORBEAM HAD LEVEL 1 CORROSION, .250 INCH BY .250 INCH, BS 312, LBL 08 TO RBL 08. INSTALLED NEW T-CAP PER TR 53-10-13. (X) - [SDR USAA000682](https://openairdocs.org/sdr/USAA000682), May 11, 2000: FLOORBEAM. CORRODED. CLT- FLOORBEAM HAS LEVEL 1 CORROSION, 1 INCH BY 2 INCH, BS 986.5, RBL 37 TO RBL 45. INSTALLED T-CAP PER TR 53-60-1. (X) - [SDR USAA000681](https://openairdocs.org/sdr/USAA000681), May 11, 2000: FLOORBEAM. CORRODED. CLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BL 1006, LBL 19. REPAIRED ANGLE, INSTALLED PER EA67218 AND SRM 51-10-6. (X) - [SDR USAA000679](https://openairdocs.org/sdr/USAA000679), May 9, 2000: ANGLE. CRACKED. CLT - WEB AND ANGLE HAD 6 EACH CRACKS, 4 EACH AT .50 INCH AND 2 EACH AT .1250 INCH, BL ZERO FROM BS 927 TO BS 947. FABRICATED AND INSTALLED NEW ANGLE PER DWG 69 - [SDR USAA000678](https://openairdocs.org/sdr/USAA000678), May 8, 2000: FLOORBEAM. CORRODED. CLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BS 947, LBL 18. REPLACED T-CAP PER SRM 53-10-2. (X) - [SDR USAA000677](https://openairdocs.org/sdr/USAA000677), May 8, 2000: FLOORBEAM. CORRODED. CLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BS 947, LBL 14. REPLACED T-CAP PER SRM 53-10-2. (X) - [SDR USAA000676](https://openairdocs.org/sdr/USAA000676), May 8, 2000: FLOORBEAM. CORRODED. CLT - FLOORBEAM HAD LEVEL 1 CORROSION, 2 INCHES BY 3 INCHES, BS 947, LBL 4.5, RBL 5. REPLACED T-CAP PER SRM 53-10-2. (X) - [SDR USAA000675](https://openairdocs.org/sdr/USAA000675), May 8, 2000: BEAM. CRACKED. CLT - WEB CRACKED 1 INCH, AT LT SIDE CREASE BEAM, STA 663.75. (X) - [SDR USAA000673](https://openairdocs.org/sdr/USAA000673), May 8, 2000: TIE CLIP. CRACKED. CLT - TIE CLIP CRACKED 0.500 INCH, BS 986.5, STR 25R. INSTALLED TIE CLIP PER SRM 51-10-01. (X) - [SDR USAA000672](https://openairdocs.org/sdr/USAA000672), May 8, 2000: BEAM. CRACKED. CLT - LEFT CREASE BEAM WEB HAD .50 INCH CRACK. REPLACED WEB PER TR 53-10-02. (X) - [SDR USAA000671](https://openairdocs.org/sdr/USAA000671), May 8, 2000: WEB. CRACKED. CLT - WEB CRACKED, 1 INCH, STR 25R, BS 847. INSTALLED NEW WEB PER SRM 51-10-02. (X) - [SDR USAA000670](https://openairdocs.org/sdr/USAA000670), May 8, 2000: FLOORBEAM. CRACKED. CLT - FLOORBEAM CRACKED0 .500 INCH BY 2 INCH, BS 967, RBL 17.5, CORROSION LEVEL 1. REPLACED ANGLE PER EA67156. (X) - [SDR USAA000669](https://openairdocs.org/sdr/USAA000669), May 8, 2000: SKIN. CRACKED. CLT - SKIN CRACKED .250 INCH, FORWARD SERVICE DOOR CUT OUT AFT CORNER. REPAIRED FILLER AND DOUBLER PER SRM 53-30-3. (X) - [SDR USAA000653](https://openairdocs.org/sdr/USAA000653), May 1, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 597, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO5393G227. (M) - [SDR USAA000652](https://openairdocs.org/sdr/USAA000652), May 1, 2000: BEAM. CRACKED. CLT - FOUND BEAM WEB CRACKED .5 INCH, RIGHT CREASE BEAM WEB STATIN 647. REPLACED WEB PER TR 53-10-02. (M) - [SDR USAA000651](https://openairdocs.org/sdr/USAA000651), May 1, 2000: BEAM. CRACKED. CLT - FOUND BEAM WEB CRACKED .375 INCH, FRAME 663.75 RT CREASE BEAM FORWARD WEB. REPLACED WEB PER TR 53-10-02. (M) - [SDR USAA000650](https://openairdocs.org/sdr/USAA000650), May 1, 2000: BEAM. CRACKED. CLT - FOUND BEAM WEB CRACKED .5 INCH, STATION 616 RIGHT CREASE BEAM WEB. REPLACED NEW WEB PER TR 53-10-02. (M) - [SDR USAA000641](https://openairdocs.org/sdr/USAA000641), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 767, STRINGER 5 LEFT. REMOVED AND REPLACED PER EO 5393G227. (M) - [SDR USAA000640](https://openairdocs.org/sdr/USAA000640), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 747, STRINGER 10 RIGHT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000639](https://openairdocs.org/sdr/USAA000639), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 747, STRINGER 7 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000638](https://openairdocs.org/sdr/USAA000638), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .500 INCH, BS 747, STRINGER 5 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000637](https://openairdocs.org/sdr/USAA000637), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .500 INCH, BS 727B, STRINGER 5 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000636](https://openairdocs.org/sdr/USAA000636), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 727B, STRINGER 8 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000635](https://openairdocs.org/sdr/USAA000635), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .50 INCH, BS 727B, STRINGER 6 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000634](https://openairdocs.org/sdr/USAA000634), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 727A, STRINGER 5R. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000633](https://openairdocs.org/sdr/USAA000633), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED, BS 706, STRINGER 10 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA000632](https://openairdocs.org/sdr/USAA000632), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED, .250 INCH, BS 706 STRINGER 3 RIGHT. REPAIRED PER EO 5393G227. (M) - [SDR USAA000631](https://openairdocs.org/sdr/USAA000631), Apr 28, 2000: CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 706, STRINGER 2 RIGHT. REPAIRED PER EO 5393G227. (M) All 79: https://openairdocs.org/deregistered/N246US-2002-03-25/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 19911113058949I](https://openairdocs.org/incident/19911113058949I), Nov 13, 1991: Boeing 737201 (N246US), Atlanta, GA. TCAS resolution advisory at cruise altitude. Pilot initiated climb. Traffic was a lear jet climbing to FL281 ## Other aircraft with N246US - [Registered now](https://openairdocs.org/aircraft/N246US): DJI AGRAS T20P, S/N 1581F574B23830010093 --- 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.