# N274US: 1983 Boeing 737-2B7, registration cancelled 2003-09-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 25, 2003
- Exported to: Philippines
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-2B7](https://openairdocs.org/model/boeing-737-2b7) (registry code 138447C)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 22886
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 14, 1983
- Certificate issued: May 2, 2002
- Last registry action: January 10, 2003
- Mode S code: A2B72B
- 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/N274US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=274US
- Page: https://openairdocs.org/deregistered/N274US-2003-09-25

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 737-2B7: https://openairdocs.org/model/boeing-737-2b7.md

## Service difficulty reports (46)

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

- [SDR USAA990826](https://openairdocs.org/sdr/USAA990826), Aug 7, 1999: SKIN. CRACKED. TPA - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK ABOVE RIVET .125 INCH CRACK BELOW RIVET STRINGER 17R, WL STATION 344 SKIN. IN
- [SDR USAASB99014](https://openairdocs.org/sdr/USAASB99014), Jan 15, 1999: COALESCER. DIRTY. FWA - FLT 1177 - EN ROUTE FROM BWI TO ORD AT FL310, ONE OF THE FLIGHT ATTENDANTS ADVISED THE COCKPIT CREW THAT THERE WERE FUMES IN THE CABIN AND THE FUMES WERE 
- [SDR USAA980523](https://openairdocs.org/sdr/USAA980523), Oct 15, 1998: SKIN. CRACKED. PIT - FOUND RON, FOUND 3 INCH CRACK IN SKIN AT STATION 767 .5 INCH ABOVE STRINGER NR 20. INSTALLED DOUBLER PER SRM 53-30-03. (M)
- [SDR USAA980339](https://openairdocs.org/sdr/USAA980339), Aug 7, 1998: SKIN. CRACKED. TPA - DURING CX-5 CHECK EDDY CURRENT, FOUND A .125 INCH CRACK IN OUTER SKIN AT LOWER CORNER OF AFT ENTRY DOOR, LOWER HINGE CUTOUT STATION 950.5 2.5 INCHES BELOW
- [SDR USAA980338](https://openairdocs.org/sdr/USAA980338), Aug 7, 1998: SKIN. CRACKED. TPA - DURING CX-5 CHECK EDDY CURRENT INSPECTION, FOUND A .5 INCH CRACK IN OUTER SKIN OF AFT ENTRY DOOR, LOWER AFT CORNER OF UPPER HINGE CUTOUT. ROUTED DAMAGE AN
- [SDR USAA980337](https://openairdocs.org/sdr/USAA980337), Aug 7, 1998: ANGLE. CRACKED. TPA - DURING CX-5 VISUAL INSPECTION, FOUND A 1 INCH CRACK IN ANGLE AT STATION 727 COMPRESSION CHORD RBL 25. INSTALLED DOUBLER PER TYPICAL REPAIR NR 53-10-03A PA
- [SDR USAASB98200](https://openairdocs.org/sdr/USAASB98200), Jul 28, 1998: LIGHT. INOPERATIVE. PHL - WHILE TESTING EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 9A WITHOUT A LENSE AND SMOKING. MAINTENANCE REMOVED AND RE
- [SDR USAASB98111](https://openairdocs.org/sdr/USAASB98111), May 11, 1998: BATTERY PACK. DISCHARGED. ALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN AT THE CENTER AISLE CEILING BETWEEN THE EXIT HATCHES INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PA
- [SDR USAA960757](https://openairdocs.org/sdr/USAA960757), Nov 27, 1996: SKIN. CRACKED. ROA - DURING CX-3 CHECK, EDDY CURRENT INSPECTION FOUND .25 INCH CRACK IN A/C SKIN AT LOWER HINGE CUT OUT FORWARD ENTRY DOOR. BODY STA 302 - JUST ABOVE STR 13L. 
- [SDR USAASB96214](https://openairdocs.org/sdr/USAASB96214), Oct 21, 1996: FUEL CONTROL. MALFUNCTIONED. EVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFEC
- [SDR 96ZZZM1487](https://openairdocs.org/sdr/96ZZZM1487), Oct 21, 1996: FUEL PUMP. MALFUNCTIONED. EVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFEC
- [SDR USAASB96039](https://openairdocs.org/sdr/USAASB96039), Mar 2, 1996: FILTER BYPASS SW. INTERMITTENT. FLT NR 797 - MCO - FIVE MINUTES AFTER TAKEOFF, 'OIL FILTER BYPASS' LIGHT FOR NR 1 ENGINE CAME ON. RETARDED THROTTLES, NO HELP. SHUT DOWN ENGINE AND RETURNED TO 
- [SDR USAA960240](https://openairdocs.org/sdr/USAA960240), Feb 7, 1996: FITTING. CRACKED. INT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A R
- [SDR USAA960239](https://openairdocs.org/sdr/USAA960239), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 4 INCH CORRODED WEB AFT ENTRY DOOR Z-ANGLE THRESHOLD WEB. FABRICATED NEW WEB, REPAIRED PER SRM 51-10-1
- [SDR USAA960238](https://openairdocs.org/sdr/USAA960238), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH CORROSION Z-ANGLE AFT ENTRY DOOR. REPLACED WITH IDENTICAL PART NR 65-52878-533, REPAIRED PER S
- [SDR USAA960237](https://openairdocs.org/sdr/USAA960237), Feb 7, 1996: FLOOR BEAM. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED NUT PLATE HOLES 3 FLOOR BEAM, STATION 986.5 RBL 36, LBL 5, RBL 5. INSTALLED DOUBLERS,
- [SDR USAA960236](https://openairdocs.org/sdr/USAA960236), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE AT STATIO N967 TO 947 RBL 20. REPAIRED PER SRM 51-10-1. REPLACED
- [SDR USAA960235](https://openairdocs.org/sdr/USAA960235), Feb 7, 1996: FLOOR BEAM. GOUGED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND GOUGE APPROXIMATELY 22 INCHES FLOOR BEAM BS 312, LBL 12 INCHES TO RBL 10 INCHES. CUT OUT DAMAGED AREA AND INSTAL
- [SDR USAA960234](https://openairdocs.org/sdr/USAA960234), Feb 7, 1996: STRINGER. CORRODED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORRODED AREA ON SIDE OF STRINGER BS 351.2 - BS 380, STRINGER 28L. REPLACED STRINGER SECTION RE
- [SDR USAA960233](https://openairdocs.org/sdr/USAA960233), Feb 7, 1996: FLOOR BEAM. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM UPPER T-CAP BS 1016 LBL 3 INCHES. INSTALLED T-CAP, REPAIR PLUS 2.6 LB 
- [SDR USAA960232](https://openairdocs.org/sdr/USAA960232), Feb 7, 1996: SEAT TRACK. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR SEAT TRACK BETWEEN STATION 1016 AND STATION 986.5. INSTALLED NEW SEAT TRACK SEC
- [SDR USAA960231](https://openairdocs.org/sdr/USAA960231), Feb 7, 1996: FLOOR SUPPORT. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION 8 INCH FLOOR SUPPORT INTERCOSTAL STATION 986.5 LNL 15 INCHES. REPLACED WITH IDENTICAL
- [SDR USAA960230](https://openairdocs.org/sdr/USAA960230), Feb 7, 1996: FLOOR BEAM. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR BEAM STATION 1006, LBL 11 INCHES. SPLICED IN NEW SECTION OF FLOOR BEAM, REPAIRE
- [SDR USAA960229](https://openairdocs.org/sdr/USAA960229), Feb 7, 1996: INTERCOSTAL. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION INTERCOSTAL STATION 1006 - 986.5 '0' BL. REPLACED WITH INDENTICAL PART NR 65-46812-17
- [SDR USAA960228](https://openairdocs.org/sdr/USAA960228), Feb 7, 1996: INTERCOSTAL. CORROSION. INT - DURING Q-6 CHCK VISUAL INSPECTION, FOUND TWO CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH, INTERCOSTAL LBL 10 INCHES BETWEEN BS 328 AND BS 344. REPLACED 
- [SDR USAA960227](https://openairdocs.org/sdr/USAA960227), Feb 7, 1996: INTERCOSTAL. CORRODED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA INTERCOSTAL LBL 11 INCHES BETWEEN BS 312 AND BS 328. REPLACED WITH IDENTICAL PAR
- [SDR USAA960226](https://openairdocs.org/sdr/USAA960226), Feb 7, 1996: INTERCOSTAL. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREAS, APPROXIMATELY 1 INCH BY 1 INCH AT INTERCOSTAL, RBL 10 INCH BETWEEN BS 312 AND BS 328. REPL
- [SDR USAA960225](https://openairdocs.org/sdr/USAA960225), Feb 7, 1996: FLOOR BEAM. CORRODED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM 'T' CAP CABIN BS 294.5 LBL 10 INCHES, RBL 20. CUT AND REPLACED T-CAP, 
- [SDR USAA960224](https://openairdocs.org/sdr/USAA960224), Feb 7, 1996: INTERCOSTAL. CORRODED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 CORRODED AREAS APPROXIMATELY 2 INCHES BY 2 INCHES INTERCOSTAL, BS 297 AND BS 303 LBL 12. INSTALLED NEW INTERCO
- [SDR USAA960223](https://openairdocs.org/sdr/USAA960223), Feb 7, 1996: INTERCOSTAL. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA 4 PLACES INTERCOSTAL, BS 344 TO BS 360 RBL 11. REPAIRED PER SRM 51-10-1. CORROSIO
- [SDR USAA960222](https://openairdocs.org/sdr/USAA960222), Feb 7, 1996: INTERCOSTAL. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA AT INTERCOSTAL BS 292 LBL 12 INCHES. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10
- [SDR USAA960221](https://openairdocs.org/sdr/USAA960221), Feb 7, 1996: INTERCOSTAL. CORRODED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH ON INTERCOSTAL, RBL 10 INCHES BETWEEN BS 294.5 AND BS 312. REPLA
- [SDR USAA960220](https://openairdocs.org/sdr/USAA960220), Feb 7, 1996: ANGLE. CORRODED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES 'Z' ANGLE BS 294.5 TO BS 344 RBL 56. REPAIRED PER SRM 
- [SDR USAA960219](https://openairdocs.org/sdr/USAA960219), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 CORRODED AREAS AT CLIP NUT HOLES APPROXIMATELY 1 INCH BY 1 INCH BS 306 TO BS 345 LBL 48 'A' ANGLE LEFT ENTRANC
- [SDR USAA960218](https://openairdocs.org/sdr/USAA960218), Feb 7, 1996: INTERCOSTAL. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FOUR 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES BS 312 TO BS 328 RBL 11 INTERCOSTAL. REMOVED AND INSTALLE
- [SDR USAA960217](https://openairdocs.org/sdr/USAA960217), Feb 7, 1996: BLKHD FITTING. CRACKED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 727 BULKHEAD STIFFENER FITTING AT BL 0 WL 202.5. REMOVED CRACKED FITTING, INSTALLED NEW ON
- [SDR USAA960216](https://openairdocs.org/sdr/USAA960216), Feb 7, 1996: FRAME. CRACKED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK TOP FLANGE OF FRAME STATION 807 LEFT BETWEEN STRINGER 24 AND STRINGER 25. CUT OUT CRACK, FABRICATE
- [SDR USAA960213](https://openairdocs.org/sdr/USAA960213), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED FLOOR SUPPORT ANGLE STATION 986.5 TO 967 LBL 12. REPLACED ANGLE, REPAIRED PER SRM 51-
- [SDR USAA960212](https://openairdocs.org/sdr/USAA960212), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH FLOOR SUPPORT ANGLE CORROSION STATION 967 TO 947 RBL 6. REPAIRED PER SRM 51-10-1. REPLACED WIT
- [SDR USAA960211](https://openairdocs.org/sdr/USAA960211), Feb 7, 1996: FLOOR BEAM. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCH CORROSION FLOOR BEAM STATION 967 BL 0 TO LBL 45. INSTALLED ONE DUOBLER AT LBL 42, REPAIRED PER
- [SDR USAA960210](https://openairdocs.org/sdr/USAA960210), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 11 INCH BY 40 INCH CORROSION FLOOR SUPPORT ANGLE AT STATION 957 RBL 6 TO RBL 45. REPAIRED PER SRM 51-10-1. REPLA
- [SDR USAA960209](https://openairdocs.org/sdr/USAA960209), Feb 7, 1996: ANGLE. CRACKED. INT - DURING Q-6 CHECK VISUAL EDDY CURRENT INSPECTION, FOUND 1 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A LEFT. I
- [SDR USAA960208](https://openairdocs.org/sdr/USAA960208), Feb 7, 1996: FLOOR BEAM. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 2 INCH CORRODED FLOOR BEAM AREA AND AT ALL CLIPNUT HOLES BS 328 RBL 6 TO RBL 56. INSTALLED NEW T-CAP A
- [SDR USAA960207](https://openairdocs.org/sdr/USAA960207), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE, STATION 967 TO STATION 947 RBL 45, REPAIRED PER SRM 51-10-1. RE
- [SDR USAA960206](https://openairdocs.org/sdr/USAA960206), Feb 7, 1996: ANGLE. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION AT FLOOR BEAM SUPPORT ANGLE STATION 967 TO 947 LBL 12. REPLACED WITH IDENTICAL PART 
- [SDR USAA960205](https://openairdocs.org/sdr/USAA960205), Feb 7, 1996: FLOOR BEAM. CORROSION. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCHES CORROSION STATION 967 BL 0 TO RBL 45 FLOOR BEAM. CUTOFF TOP CAP, FABRICATED AND REPAIRED SPL

## 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 19990115008739I](https://openairdocs.org/incident/19990115008739I), Jan 15, 1999: Boeing 737* (N274US), Fort Wayne, IN. (-5) Usair flight 1177, B737, enroute from baltimore (bwi) to ord. At 31000', the pilot declared an emergency 25 miles s.e. of Fort Wayne, ind (fwa) at…

## Other aircraft with N274US

- [Registered now](https://openairdocs.org/aircraft/N274US): Rossi Randall A VANS RV-7, S/N 71710, built 2006
- [Cancelled 1975-01-02](https://openairdocs.org/deregistered/N274US-1975-01-02): Boeing 727-251, S/N 20296, built 1969. Owner: [Northwest Airlines Inc](https://openairdocs.org/faa-owner/NORTHWEST%20AIRLINES%20INC), [St Paul, MN](https://openairdocs.org/faa-place/MN/St%20Paul)

---
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.