# N349US: 1987 Boeing 737-301, registration cancelled 2004-11-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 8, 2004
- Exported to: Malaysia
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 23552
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 11, 1987
- Certificate issued: March 16, 2004
- Last registry action: March 16, 2004
- Mode S code: A3E090
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N349US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=349US
- Page: https://openairdocs.org/deregistered/N349US-2004-11-08

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 737-301: https://openairdocs.org/model/boeing-737-301.md

## Service difficulty reports (25)

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

- [SDR USA2001F00007](https://openairdocs.org/sdr/USA2001F00007), Dec 12, 2001: SOCKET. DEFECTIVE. PIT MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR USAASB00204](https://openairdocs.org/sdr/USAASB00204), Aug 1, 2000: DUCT. SEVERED. BOS - FLT 6507 - FLIGHT RETURNED TO FIELD AT BOS DUE TO AN ELECTRICAL SMELL THROUGHOUT THE CABIN. CAPTAIN ELECTED TO RETURN TO BOS AFTER NUMEROUS COMPLAINTS FRO
- [SDR USAASB00187](https://openairdocs.org/sdr/USAASB00187), Jul 9, 2000: SENSOR. FAILED. BOS - FLT 6527 - AFTER TAKEOFF, THE LANDING GEAR LEVER WOULD NOT MOVE UP TO THE RETRACT POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETU
- [SDR USAA991031](https://openairdocs.org/sdr/USAA991031), Oct 13, 1999: ANGLE. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 59 INCH AREA OF CORROSION AT STATION 285-344, WL 208.1 Z-ANGLE. CORROSION LEVEL 2. REMOVED AND REPLACED Z-ANGL
- [SDR USAA991032](https://openairdocs.org/sdr/USAA991032), Oct 13, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ALONG UPPER T-CAP AT NUTPLATE HOLES 10 INCH AT BS 294.5, LBL 22 TO RBL 22, BEAM CAP. CORROSION LEVEL 2
- [SDR USAA991022](https://openairdocs.org/sdr/USAA991022), Oct 13, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM UPPER CHORD STATION 986 FROM BL 3.5 TO RBL 9.5, CORROSION LEVEL 1. INSTALLE
- [SDR USAA991023](https://openairdocs.org/sdr/USAA991023), Oct 13, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION FLOORBEAM BETWEEN STATION 986.5 BY 1016 DIAGONALLY FROM RBL 19 TO RBL 5. CORROSION LE
- [SDR USAA991002](https://openairdocs.org/sdr/USAA991002), Oct 13, 1999: FLOORBEAM. CORRODED. CLT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH AREA OF CORROSION FLOORBEAM 967 UPPER CHORD AT LBL 27.5, CORROSION LEVEL 1. REPAIRED DOUBLER PER SRM 53
- [SDR USAA991102](https://openairdocs.org/sdr/USAA991102), Oct 13, 1999: ANGLE. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT HORIZONTAL STAB CENTER SECTION THRUST BEAM ATTACH ANGLE. REPLACED ANGLE PER REPAIR DOCUMENT 51
- [SDR USAA991090](https://openairdocs.org/sdr/USAA991090), Oct 13, 1999: SKIN. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 EACH .50 INCH CRACKS AT BS 5332, RBBL 60, WL 21.5 SKIN ASSEMBLY. INSTALLED REPAIR PLATES PER SRM 53-10-01 FIG 
- [SDR USAA991081](https://openairdocs.org/sdr/USAA991081), Oct 13, 1999: FITTING. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT FORWARD SERVICE DOOR LOWER AFT DOOR STOP FITTING ASSEMBLY. REPLACED WITH IDENTICAL PART PER SR
- [SDR USAA991057](https://openairdocs.org/sdr/USAA991057), Oct 13, 1999: KEEL BEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CORRODED AREA KEEL BEAM AT BS 500C PLUS 9.5 INCH LBL 5. CORROSION LEVEL 2. INSTALLED REPAIR DOUBLER PER
- [SDR USAA991047](https://openairdocs.org/sdr/USAA991047), Oct 13, 1999: KEEL BEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION .75 INCH BY 5 INCH AT STATIN 532, RLB 6.5 STRINGER 28R KEEL BEAM. CORROSION LEVEL 2. CORROSION TASK NR
- [SDR USAA991029](https://openairdocs.org/sdr/USAA991029), Oct 13, 1999: TIE CLIP. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT BS 907, STR 9L STRINGER TIE CLIP. REPAIRED WITH IDENTICAL PART PER SRM 51-10-2. (X)
- [SDR USAA991021](https://openairdocs.org/sdr/USAA991021), Oct 13, 1999: FRAME. CRACKED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 480, BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER ANGLE PER EA 65618 AND SRM 53-00-
- [SDR USAA991020](https://openairdocs.org/sdr/USAA991020), Oct 13, 1999: FRAME. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 887, BETWEEN STR 8L AND STR 9L FRAME. INTALLED DOUBLER ANGLE PER EA 65618. (X)
- [SDR USAA990795](https://openairdocs.org/sdr/USAA990795), Aug 12, 1999: STRINGER. CRACKED. CLT - ON PARKED, OUT OF TIME AIRCRAFT, FOUND 1.5 INCH CRACK AT STR 22R, STA 809. INSTALLED DOUBLER PER SRM 53-00-01. (X)
- [SDR USAASB99169](https://openairdocs.org/sdr/USAASB99169), Jul 9, 1999: BATTERY PACK. DISCHARGED. IAH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)
- [SDR USAASB97286](https://openairdocs.org/sdr/USAASB97286), Oct 18, 1997: BATTERY PACK. DISCHARGED. PIT - EMERGENCY EXIT SIGN ROW 10 BROKEN AND BATTERY PACK ABOVE ROW 9D INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY (10-1262-3), NO HELP. FOUND BROKEN WIRE U
- [SDR USAASB97192](https://openairdocs.org/sdr/USAASB97192), Jul 15, 1997: POSITION IND. FAILED. PHL - FL2191 - IN THE PROCESS OF CONFIGURING THE A/C FOR LANDING. CAPTAIN DID NOT RECEIVE LEADING OR TRAILING EDGE FLAP INDICATION. ADVISED PHL TOWER OF THE PRO
- [SDR USAA951034](https://openairdocs.org/sdr/USAA951034), Sep 19, 1995: SKIN. MIS MFG. CLT - VISUALLY INSPECTED EXISTING REPAIR, LARGE RIVET IN SKIN BAY LOCATED AT STATION 390 ABOVE STRINGER 11L. INSTALLED PROTRUDING HEAD RIVET 211TT3. (M)
- [SDR USAA951033](https://openairdocs.org/sdr/USAA951033), Sep 19, 1995: DOUBLER. DAMAGED. CLT - PREVIOUS 14 INCH BY 10 INCH REPAIR (EXT DOUBLER) INSTALLED LOCATED STATION 867 BETWEEN STRINGER 21R AND STRINGER 22R. VISUALLY INSPECTED. PREVIOUS REPAIR 
- [SDR USAA951032](https://openairdocs.org/sdr/USAA951032), Sep 19, 1995: DOUBLER. DAMAGED. CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 8 INCH BY 8 INCH REPAIR INSTALLED LOCATED AT STATION 430 STRINGER 10L. PREVIOUS REPAIR DOUBLER INSTALLED. (
- [SDR USAA951031](https://openairdocs.org/sdr/USAA951031), Sep 19, 1995: DOUBLER. DAMAGED. CLT - DURING A Q3-CHECK INSPECTION, A 16 INCH BY 10 INCH REPAIR INSTALLED LOCATED AT STATION 365, STRINGER 11L WAS VISUALLY FOUND. EXISTING REPAIR DOUBLER INSTA
- [SDR USAA951030](https://openairdocs.org/sdr/USAA951030), Sep 19, 1995: DOUBLER. DAMAGED. CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH HOLE REPAIR LOCATED AT STATION 344, STRINGER 18L. EXISTING REPAIR, DOUBLER INSTALLED. (M)

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA01LA146](https://openairdocs.org/ntsb/MIA01LA146), May 28, 2001: Boeing 737-301 (N349US), Toccoa, GA, no damage. Probable cause: An in-flight encounter with unforecasted weather (turbulence) during an enroute climb resulting in one flight attendant sustaining serious injury.

## 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.

- [Accident 20010528011649A](https://openairdocs.org/incident/20010528011649A), May 28, 2001: Boeing 737301 (N349US), Toccoa, GA, No damage. (-23)This is preliminary information and will be amended when final NTSB report is completed. On mzy 28 2001, at about 0940 EDT, a Boeing 737-301, N349US,…

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