# N351US: 1987 Boeing 737-301, registration cancelled 2004-10-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 21, 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: 23554
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 1987
- Certificate issued: May 11, 2004
- Last registry action: May 11, 2004
- Mode S code: A3EA57
- 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/N351US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=351US
- Page: https://openairdocs.org/deregistered/N351US-2004-10-21

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 (45)

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

- [SDR USAASB01287](https://openairdocs.org/sdr/USAASB01287), Oct 8, 2001: UPLOCK SENSOR. DEFECTIVE. PHL - FLT 8959 - AFTER TAKEOFF AND GEAR RETRACTION FROM MCO, EN ROUTE TO PHL, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED STEADY, THEN INTERMITTENTL
- [SDR USAASB01234](https://openairdocs.org/sdr/USAASB01234), Aug 18, 2001: BOLT. WORN. DCA - FLT 360 - ON CLIMB-OUT FROM DCA, EN ROUTE TO ROC, CREW FELT A RUMBLE/AIRFRAME VIBRATION THROUGHOUT THE CABIN. DUE TO PREVIOUS FILGHT SEGMENT EXPERIENCING 
- [SDR USAASB01222](https://openairdocs.org/sdr/USAASB01222), Aug 4, 2001: TRANSMITTER. FAULTY. ORD - FLT 537 - A TRAILING EDGE FLAP ASYMMETRY OCCURRED ON APPROACH TO ORD FROM CLT. LEFT FLAP INDICATED 1 UNIT WHILE RIGHT FLAP INDICATED 1.5 UNITS. CREW DECLA
- [SDR USAASB01005](https://openairdocs.org/sdr/USAASB01005), Jan 13, 2001: DOOR. NOT CLOSED. PHL - FLT 1228 - ON CLIMB-OUT FROM PHL, EN ROUTE TO CLT, CAPTAIN REPORTED THAT THE AIRCRAFT CABIN PRESSURE CONTINUED TO CLIMB ALONG WITH OUTSIDE PRESSURE. MIX V
- [SDR USAASB01002](https://openairdocs.org/sdr/USAASB01002), Jan 2, 2001: INDICATOR. FAILED. PIT - FLT 1950 - ON DESCENT TO PIT, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. AS CREW POSITIONED FLAPS TO ONE DEGREE FLAPS, THE LEFT FLAP INDICATOR STOPPED AT O
- [SDR USAASB00236](https://openairdocs.org/sdr/USAASB00236), Aug 30, 2000: SENSOR. FAILED. SAV - FLT 2382 - EN ROUTE FROM CLT TO SAV, AT FL220, THE CABIN BEGAN TO LOSE PRESS AND THE A/C EXPERIENCED SEVERAL INFLIGHT PROBLEMS WHICH SEEMED TO INDICATE AN
- [SDR USAA000654](https://openairdocs.org/sdr/USAA000654), May 1, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .25 INCH, AFT UPPER RADIUS EXIT HANDLE CLOSEOUT. INSTALLED REPAIRED DOUBLER PER SRM 52-00-01 PAGE 203. (M)
- [SDR USAA000601](https://openairdocs.org/sdr/USAA000601), Apr 26, 2000: FRAME. CORRODED. CLT - FOUND CHORD CORRODED 2 INCHES BY 4 INCHES, STATION 500 AND 500A CHORD ANGLE AT STRINGER 26R. INSTALLED REPAIR ANGLE PER EA 67007 AND SRM 51-70-12. CORROSI
- [SDR USAA000602](https://openairdocs.org/sdr/USAA000602), Apr 26, 2000: WEB. CORRODED. CLT - FOUND WEB CORRODED 2 INCHES BY 4 INCHES, STATION 500 AND 500A WEB ADJACENT TO STRINGER 26R. REPAIRED PER SRM 51-10-02. CORROSION LEVEL 2. (M)
- [SDR USAA000603](https://openairdocs.org/sdr/USAA000603), Apr 26, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 344, LBL 42 - RBL 9 TOP OF FLOORBEAM. INSTALLED NEW SECTION PER SRM 51-40-02. (M)
- [SDR USAA000604](https://openairdocs.org/sdr/USAA000604), Apr 26, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 328, RBL TO SERV DOOR SILL. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)
- [SDR USAA000605](https://openairdocs.org/sdr/USAA000605), Apr 26, 2000: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, STATION 500 AND 500A END OF STRINGER 26R. STRINGER REPAIR PER EA 67007 AND SRM 51-70-12. (M)
- [SDR USAA000606](https://openairdocs.org/sdr/USAA000606), Apr 26, 2000: FITTING. CRACKED. CLT - FOUND FITTING/STABILIZER CRACKED 4.5 INCH, HORIZ STABILIZER CENTER SECTION AFT JACK SCREW. REMOVED AND REPLACED FITTING/STABILIZER PER SRM 51-10-02. (M)
- [SDR USAA000583](https://openairdocs.org/sdr/USAA000583), Apr 24, 2000: STIFFENER. CRACKED. CLT - FOUND STIFFENER WITH TWO CRACKS 2 INCHES AND .5 INCHES, STATION 312 AND 314, RBL 32. REPLACED STIFFENER PER SRM 51-10-02. (M)
- [SDR USAA000584](https://openairdocs.org/sdr/USAA000584), Apr 24, 2000: SUPPORT FITTING. CRACKED. CLT - FOUND SUPPORT FITTING CRACKED .250 INCH, MLG BEAM SUPPORT FITTING OUTBOARD BOLT HOLE RT WING. REPAIRED PER TR 57-40-13. (M)
- [SDR USAA000585](https://openairdocs.org/sdr/USAA000585), Apr 24, 2000: WEB. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, AFT INBOARD RIVET IN WEB S 18AR SHELF STA 726, LBL 53. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000586](https://openairdocs.org/sdr/USAA000586), Apr 24, 2000: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, AFT INBOARD RIVET IN WEB S 18AR SHELF, STATION 726, RBL 53. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000587](https://openairdocs.org/sdr/USAA000587), Apr 24, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 663, STRINGER 10L. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000588](https://openairdocs.org/sdr/USAA000588), Apr 24, 2000: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .125 INCH, BS 663, STRINGER 10R CLIP. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000589](https://openairdocs.org/sdr/USAA000589), Apr 24, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH, STATION 664, LBL 31. INSTALLED REPAIR PER TR 53-60-04. (M)
- [SDR USAA000590](https://openairdocs.org/sdr/USAA000590), Apr 24, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, LHG FUSE FRAME STATION 827 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000591](https://openairdocs.org/sdr/USAA000591), Apr 24, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED 1 INCH, STATION 294.5, JUST ABOVE ZEE FORWARD SERVICE DOOR. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA000592](https://openairdocs.org/sdr/USAA000592), Apr 24, 2000: SUPPORT FITTING. CRACKED. CLT - FOUND SUPPORT FITTING CRACKED .25 INCH, LEFT MLG BEAM SUPPORT FITTING. REPAIRED PER TR 57-40-13. (M)
- [SDR USAA000593](https://openairdocs.org/sdr/USAA000593), Apr 24, 2000: STRAP. CRACKED. CLT - FOUND STABILIZER STRAP CRACKED 2 INCHES, STATION 312, RBL 46 BOTTOM OF FLOORBEAM. INSTALLED DOUBLER PER SRM 51-10-02. (M)
- [SDR USAA000594](https://openairdocs.org/sdr/USAA000594), Apr 24, 2000: FLOORBEAM. CRACKED. CLT - FOUND LOWER FLOORBEAM 1 INCH CRACKED, BL 0, STATION 312-328 LOWER FLOORBEAM SUPPORT. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000564](https://openairdocs.org/sdr/USAA000564), Apr 17, 2000: BULKHEAD. CRACKED. CLT - FOUND SKIN CRACKED 1.5 INCHES, FORWARD BULKHEAD AT STATION 178.6, RBL 5. INSTALLED DOUBLER PER TR 53-10-07. (M)
- [SDR USAA000565](https://openairdocs.org/sdr/USAA000565), Apr 17, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, FORWARD UPPER SERVICE DOOR CUTOUT. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000566](https://openairdocs.org/sdr/USAA000566), Apr 17, 2000: BULKHEAD. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH, BL 0, WL 187, BULKHEAD 178. INSTALLED FILLER AND DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000567](https://openairdocs.org/sdr/USAA000567), Apr 17, 2000: BULKHEAD. CRACKED. CLT - FOUND WEB FOR BULKHEAD CRACKED 1 INCH, STATION 178 LBL 5, 9 INCHES BELOW FLOOR LEVEL. INSTALLED DOUBLER PER TR 53-10-07. (M)
- [SDR USAA000568](https://openairdocs.org/sdr/USAA000568), Apr 17, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, STATION 480 BETWEEN STRINGER 8L AND 9L LEFT FUSELAGE. REPAIR DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000570](https://openairdocs.org/sdr/USAA000570), Apr 17, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, STATION 827 BETWEEN STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)
- [SDR USAA000571](https://openairdocs.org/sdr/USAA000571), Apr 17, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, STATION 480 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000569](https://openairdocs.org/sdr/USAA000569), Apr 17, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOOR FRAME CORRODED 1 INCH, STATION 312, BL 0, RBL 8, RBL 36. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)
- [SDR USAA000557](https://openairdocs.org/sdr/USAA000557), Apr 14, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .500 INCH, AFT ENTRY DOOR UPPER HINGE FITTING. INSTALLED DOUBLER PER TR 53-10-11. (M)
- [SDR USAA000530](https://openairdocs.org/sdr/USAA000530), Apr 7, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED .5 INCH, STATION 1016, LBL 15 FLOORBEAM. INSTALLED REPAIR PER SRM 53-00-51 FIG 203. (M)
- [SDR USAASB99245](https://openairdocs.org/sdr/USAASB99245), Oct 9, 1999: HARNESS. FAILED. ORD - FLT 1817 - EN ROUTE FROM PHL/MSP, CAPTAIN REPORTED THE NR 2 AND NR 3 TRANSFORMER RECTIFIERS HAD TRIPPED AND THE CAPTAIN'S WINDOW OVERHEAT LIGHT WAS ON. CA
- [SDR USAASB98177](https://openairdocs.org/sdr/USAASB98177), Jul 10, 1998: VALVE. FAILED. CLT - FLT 1065 - AFTER TAKEOFF FROM CLT, THE AUTO PRESSURIZATION SYSTEM FAILED. CREW WAS UNABLE TO PRESSURIZE AIRCRAFT OR CONTROL CABIN IN STANDBY OR MANUAL OPE
- [SDR USAA980273](https://openairdocs.org/sdr/USAA980273), Jun 8, 1998: SKIN. CRACKED. TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK IN THE SKIN AFT OF THE EQUIPMENT EXHAUST AT STATION 380 BETWEEN STRINGER 28L AND BL 0. INSTAL
- [SDR USAASB98047](https://openairdocs.org/sdr/USAASB98047), Feb 24, 1998: LIGHT. INOPERATIVE. ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EME
- [SDR 98ZZZM321](https://openairdocs.org/sdr/98ZZZM321), Feb 24, 1998: CHARGER. FAILED. ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EME
- [SDR 98ZZZM320](https://openairdocs.org/sdr/98ZZZM320), Feb 24, 1998: BATTERY PACK. DISCHARGED. ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EME
- [SDR 98ZZZM319](https://openairdocs.org/sdr/98ZZZM319), Feb 24, 1998: SIGN. INOPERATIVE. ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EME
- [SDR USAASB97275](https://openairdocs.org/sdr/USAASB97275), Oct 5, 1997: OVEN. DIRTY. MIA - FLT 2182 - AFTER TAKEOFF, THERE WAS A STRONG SMELL FOLLOWED BY VISIBLE BLACK SMOKE THAT CAME OUT OF THE COCKPIT DUCT VENTS. THE COCKPIT FILLED WITH ENOUGH
- [SDR USAASB97253](https://openairdocs.org/sdr/USAASB97253), Sep 14, 1997: BATTERY PACK. DISCHARGED. ALB - FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT POSITIONS 1, 2 AND 4. OPERATIONAL CHECKED OK. (M)
- [SDR USAA960474](https://openairdocs.org/sdr/USAA960474), Jun 14, 1996: FLOOR BEAM. CORROSION. CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION ON TOP OF FLOORBEAM LOCATED AT STATION 986.5 RBL 12 AND RBL 14. INSTALLED NEW CHORD AND REPAIR ANGLES AS PER T

## 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 19930520018339I](https://openairdocs.org/incident/19930520018339I), May 20, 1993: Boeing 737301 (N351US), Washington, DC. Fumes in cockpit. Went on oxygen. Landed safely. Found excessive amount of lps lubricant on pilots seat rails.

## Other aircraft with N351US

- [Registered now](https://openairdocs.org/aircraft/N351US): Costruzioni Aeronautiche Tecna P2010 TDI, S/N 351/US, built 2025
- [Cancelled 2019-05-06](https://openairdocs.org/deregistered/N351US-2019-05-06): DJI MAVIC PRO PLATINUM, S/N 08QCF5QP122N8B. Assigned, pending cancellation
- [Cancelled 1971-06-30](https://openairdocs.org/deregistered/N351US-1971-06-30): Boeing 707-351B, S/N 18584. Owner: [Northwest Airlines Inc](https://openairdocs.org/faa-owner/NORTHWEST%20AIRLINES%20INC), [St Paul, MN](https://openairdocs.org/faa-place/MN/St%20Paul)

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