# N354US: 1987 Boeing 737-301, registration cancelled 2007-08-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 29, 2007
- Exported to: Bermuda
- 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: 23557
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 4, 1987
- Certificate issued: July 7, 2006
- Last registry action: July 7, 2006
- Mode S code: A3F57C
- 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/N354US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=354US
- Page: https://openairdocs.org/deregistered/N354US-2007-08-29

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 (62, newest 50)

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

- [SDR USAA050768](https://openairdocs.org/sdr/USAA050768), Jun 16, 2005: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 4 INCHES, STATION 727D, S23R. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229 DETAIL XI. (M)
- [SDR USAA050767](https://openairdocs.org/sdr/USAA050767), Jun 16, 2005: SKIN. PUNCTURED. CLT - FOUND SKIN PUNCTURED 1 INCH BY 2.5 INCH, BS 312-322 AT S23R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M)
- [SDR USAA050221](https://openairdocs.org/sdr/USAA050221), Feb 1, 2005: PLATE. CRACKED. PIT - FOUND HINGE DOUBLER PLATE CRACKED .3750, MED TOP FORWARD HINGE CUTOUT INSIDE BOTTOM FORWARD CORNER. INSTALLED WEB PER SRM 51-40-02 AND DWG 65-17684. (M)
- [SDR USAA040065](https://openairdocs.org/sdr/USAA040065), Mar 27, 2004: FLOOR SUPPORT. CRACKED. FOUND FLANGE CRACKED 1.5 INCH FLOOR SUPPORT STATION 937 BL 0. REMOVED TOP FLANGE OF FLOOR SUPPORT, REPLACED WITH NEW PART EPN 1138864 PER SRM 51-40-00. (M)
- [SDR USAA040064](https://openairdocs.org/sdr/USAA040064), Mar 27, 2004: SHEAR WEB. CORRODED. FOUND SHEAR WEB CORRODED 3 INCHES BY 10 INCHES, TOP AND LOWER SURFACE OF FLOOR PAN AT AFT PRESS BULKHEAD, RBL 0-15. DEFECTIVE PART REPLACED WITH IDENTICAL PART 
- [SDR USAA040063](https://openairdocs.org/sdr/USAA040063), Mar 27, 2004: FLOOR PANEL. GOUGED. FOUND FLOOR PANEL GOUGED 4 INCHES, STATION 992 RBL 39. MANUFACTURED OUT OF 2024 T3 020 PER SRM 51-40-02. (M)
- [SDR USAA040120](https://openairdocs.org/sdr/USAA040120), Mar 24, 2004: KEELBEAM. CORRODED. FOUND KEELBEAM CORRODED AND PITTING 1 INCH BY 4 INCH AREA, RT KEELBEAM LOWER SURFACE STATION 663.75 TO 727. INSTALLED REPAIR STRAP PER EA 78097. LEVEL 1 TASK NR
- [SDR USAA040095](https://openairdocs.org/sdr/USAA040095), Jan 13, 2004: SKIN. CRACKED. FOUND SKIN WITH 3 INCH STRESS CRACK, FORWARD OF AFT BAGGAGE PIT DOOR BS 727E S18R. STRESS CRACK REPAIR PER SRM 53-00-01 FIG 201, AND OM-7 NR 27801. (M)
- [SDR USAA030169](https://openairdocs.org/sdr/USAA030169), Jul 27, 2003: SUPPORT. CORRODED. FOUND UPPER SUPPORT CORRODED .004 INCH TOP AND BOTTOM TOTAL OF .008 INCH, NLG UPPER SUPPORT. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA030152](https://openairdocs.org/sdr/USAA030152), Jul 27, 2003: SUPPORT. CORRODED. PHL - FOUND UPPER SUPPORT CORRODED TOP AND BOTTOM, .004 INCH TOP AND BOTTOM TOTAL OF .008 INCH. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAASB01288](https://openairdocs.org/sdr/USAASB01288), Oct 8, 2001: INDICATOR. FAULTY. BUF - FLT 1157 - AFTER TAKEOFF FROM BUF, EN ROUTE TO CLT, CREW EXPERIENCED A FLAP ASYMMETRY PROBLEM DURING FLAP RETRACTION. ONE FLAP WAS IN THE 5 DEGREE POSITIO
- [SDR USAASB00231](https://openairdocs.org/sdr/USAASB00231), Aug 26, 2000: WIRE. BROKEN. PIT - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT BEHIND THE LEFT WING INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SPLICE JUST ABOVE EMERGENCY LIGHT IN A
- [SDR USAA001122](https://openairdocs.org/sdr/USAA001122), Aug 1, 2000: BUSHING. CORRODED. CLT - FOUND LUG AND BUSHING CORRODED .25 INCH, LEFT HORIZONTAL STAB LOWER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1 C-53-701-02. REMOVED CORROSION PER SRM 55-10
- [SDR USAA001121](https://openairdocs.org/sdr/USAA001121), Aug 1, 2000: BUSHING. CORRODED. CLT - FOUND LUG AND BUSHING CORRODED .25 INCH, LEFT HORIZ STAB UPPER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1. REMOVED CORROSION PER SRM 55-10-10. (M)
- [SDR USAA001125](https://openairdocs.org/sdr/USAA001125), Aug 1, 2000: PRESSURE PANEL. CRACKED. CLT - FOUND PRESSURE DECK WITH TWO CRACKS .5 INCH AND 1 INCH, PRESS DECK MLG WHEEL WELL STRINGER 663, LBL 30. REMOVED DAMAGE INSTALLED REPAIR DOUBLER AND FILLER
- [SDR USAA001124](https://openairdocs.org/sdr/USAA001124), Aug 1, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM T-CAP CORRODED 2 INCHES, STATION 328, LBL 49. CORROSION LEVEL 1, C53-107-01. REMOVED CORROSION AND INSTALLED NEW T-CAP PER SRM 51-70-12 FI
- [SDR USAA001123](https://openairdocs.org/sdr/USAA001123), Aug 1, 2000: BEAM. CRACKED. CLT - FOUND SUPPORT BEAM CRACKED .375 INCH, LEFT MLG SUPPORT BEAM. ACCOMPLISHED INTERMIN REPAIR PER EA 67644 AND TR 57-40-13. (M)
- [SDR USAA001085](https://openairdocs.org/sdr/USAA001085), Jul 31, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCH AREA, STATION 294.5, RBL 45. REMOVED AND INSTALLED FABRICATED ANGLE PER SRM 53-10-08 AND 51-40-02. (M)
- [SDR USAA001090](https://openairdocs.org/sdr/USAA001090), Jul 31, 2000: SPLICE. CRACKED. CLT - FOUND STRINGER SPLICE CRACKED .25 INCH, STRINGER 4R SPLICE STATION 907. REMOVED DAMAGE AND INSTALLED PER SRM 51-10-02. (M)
- [SDR USAA001089](https://openairdocs.org/sdr/USAA001089), Jul 31, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .025 INCH, AFT SIDE FRAME 847 AT TWO RIVETS JUST ABOVE STRINGER 9L. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-00-07 FIG 201 AND T
- [SDR USAA001088](https://openairdocs.org/sdr/USAA001088), Jul 31, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .375 INCH, FUSE SKIN AT LOWER AFT CORNER OF DOOR CUTOUT. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-10-01 FIG 202. (M)
- [SDR USAA001087](https://openairdocs.org/sdr/USAA001087), Jul 31, 2000: DOOR FRAME. CRACKED. CLT - FOUND FRAME CRACKED .125 INCH, FORWARD SERVICE DOOR JAMB FORWARD FRAME AT LOWER OUTBOARD CORNER. REMOVED AND REPLACED PER SRM 51-40-02 AND BOEING DWG 65 4
- [SDR USAA001086](https://openairdocs.org/sdr/USAA001086), Jul 31, 2000: ATTACH ANGLE. CRACKED. CLT - FOUND ATTACH ANGLE CRACKED 1 INCH, HORIZ STAB CENTER BOX LOWER CHORD TO WEB. INSTALLED NEW ANGE PER TR 51-10-02. (M)
- [SDR USAA001010](https://openairdocs.org/sdr/USAA001010), Jul 20, 2000: SUPPORT BRACKET. CRACKED. CLT - FOUND DOOR SUPPORT CRACKED .25 INCH, STATION 294.5, FRAME AT STRINGER 14L. FABRICATED NEW WEB AND INSTALLED PER SRM 51-70-11. (M)
- [SDR USAA001009](https://openairdocs.org/sdr/USAA001009), Jul 20, 2000: DOOR FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, STATION 294.5, STRINGER 7L. REPAIRED PER SRM 53-10-15. (M)
- [SDR USAA001008](https://openairdocs.org/sdr/USAA001008), Jul 20, 2000: DOOR FRAME. CRACKED. CLT - FOUND FRAME CRACKED 2.5 INCHES, STATION 294.5, FORWARD SERVICE DOOR FRAME WL 208. REMOVED DAMAGED AREA INSTALLED REPAIR DOUBLER PER SRM 50-70-11. (M)
- [SDR USAA001007](https://openairdocs.org/sdr/USAA001007), Jul 20, 2000: WEB. CRACKED. CLT - FOUND WEB CRACKED .500 INCH, STRINGER 14R, WEB INNER CHORD ANGLE STATION 278. FABRICATED NEW WEB AND INSTALLED PER SRM 51-40-00 AND DWG 6 45807. (M)
- [SDR USAA001006](https://openairdocs.org/sdr/USAA001006), Jul 20, 2000: BULKHEAD. CRACKED. CLT - FOUND WEB CRACKED TWO PLACES .25 INCH AND 1.5 INCH, STATION 178 BULKHEAD, WEB RBL 6.75, WL 201. FABRICATE REPAIR DOUBLER PER SRM 53-10-08 DETAIL 111. (M)
- [SDR USAA001005](https://openairdocs.org/sdr/USAA001005), Jul 20, 2000: ANGLE. CRACKED. CLT - FOUND CHORD ANGLE CRACKED .5 INCH, LBL 5.7 VERT CHORD L/B FLANGE STATION 178, WL 184. INSTALLED REPAIR ANGLE AND STRAPS PER SRM 53-10-08. (M)
- [SDR USAA001004](https://openairdocs.org/sdr/USAA001004), Jul 20, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 36. FABRICATED T-CAP PER REPAIR DOCUMENT 53-10-51. (M)
- [SDR USAA001003](https://openairdocs.org/sdr/USAA001003), Jul 20, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 28. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. CORROSION LEVEL 1. (M)
- [SDR USAA001002](https://openairdocs.org/sdr/USAA001002), Jul 20, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 14. CORROSION LEVEL 1. FABRICATED T-CAP PER SRM 53-10-51. (M)
- [SDR USAA001001](https://openairdocs.org/sdr/USAA001001), Jul 20, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, LBL 12. REMOVED DAMAGED T-CAP PER SRM 53-10-51 FIG 205. (M)
- [SDR USAA001022](https://openairdocs.org/sdr/USAA001022), Jul 20, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 328, LBL 28. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND INSTALLED PER REPAIR 51-70-12. (M)
- [SDR USAA001021](https://openairdocs.org/sdr/USAA001021), Jul 20, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 312, BL 0. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND SPLICE ANGLE PER SRM 53-10-51. (M)
- [SDR USAA001020](https://openairdocs.org/sdr/USAA001020), Jul 20, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, RBL 36. FABRICATED NEW T-CAP AND SPLICE ANGLE PER SRM 53-10-51. CORROSION LEVEL 1. (M)
- [SDR USAA000891](https://openairdocs.org/sdr/USAA000891), Jul 3, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344 STRINGER 11R. FABRICATED CLIP PER BOEING DWG 6938939. (M)
- [SDR USAA000892](https://openairdocs.org/sdr/USAA000892), Jul 3, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STRINGER 1 BS 380. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA000893](https://openairdocs.org/sdr/USAA000893), Jul 3, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 380, STRINGER 2L. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA000894](https://openairdocs.org/sdr/USAA000894), Jul 3, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .0625 INCH, BS 616, STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-2. (M)
- [SDR USAA000895](https://openairdocs.org/sdr/USAA000895), Jul 3, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CILP CRACKED .0625 INCH, BS 639, STRINGER 4L. INSTALLED CLIP PER SRM 51-10-2. (M)
- [SDR USAA000896](https://openairdocs.org/sdr/USAA000896), Jul 3, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, FORWARD SIDE FRAME 907, BELOW STRINGER 1. REPLACED TIE CLIP PER BOEING DWG 69-47869. (M)
- [SDR USAA000897](https://openairdocs.org/sdr/USAA000897), Jul 3, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED TWO PLACES .5 INCH, FS 663, STRINGER 10L. INSTALLED CLIP PER SRM 51-10-2. (M)
- [SDR USAASB00142](https://openairdocs.org/sdr/USAASB00142), May 11, 2000: LIGHT. FAILED. PHL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 12ABC INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBL
- [SDR USAASB99305](https://openairdocs.org/sdr/USAASB99305), Dec 27, 1999: FIRE LOOP. FAILED. MCI - FLT 328 - AFTER TAKEOFF FROM MCI, THE RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. THREE MINUTES LATER, THE LEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED
- [SDR USAASB99085](https://openairdocs.org/sdr/USAASB99085), Apr 1, 1999: SPLICE. DEFECTIVE. ROC - WHOLE ACCOMPLISHING OVERNIGHT CHECK, MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHT ON SEAT ROW 16 END BAY INOPERATIVE. MAINTENANCE REPLACED DEFECTIVE WI
- [SDR USAA980600](https://openairdocs.org/sdr/USAA980600), Nov 25, 1998: SKIN. CRACKED. TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC FOUND A .125 INCH CRACK UPPER HINGE CUTOUT ON FORWARD SERVICE DOOR SKIN. FABRICATED DOUBLER AND INS
- [SDR USAA980599](https://openairdocs.org/sdr/USAA980599), Nov 25, 1998: SKIN. CRACKED. TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC, FOUND A .375 INCH CRACK LOWER HINGE CUTOUT ON FORWARD SERVICE DOOR SKIN. FABRICATED DOUBLER AND IN
- [SDR USAA980598](https://openairdocs.org/sdr/USAA980598), Nov 25, 1998: SKIN. CRACKED. TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC, FOUND A .375 INCH CRACK LOWER HINGE CUTOUT ON FORWARD ENTRY DOOR SKIN. FABRICATED DOUBLER AND INST
- [SDR USAASB98233](https://openairdocs.org/sdr/USAASB98233), Sep 6, 1998: TRANSMITTER. INOPERATIVE. CLT - FLT 1080 - AT FL370, THE 'B' SYSTEM HYDRAULIC PRESSURE GAUGE WENT OT 750 PSI. SHORTLY THEREAFTER, THE 'B' SYSTEM HYDRAULIC QUANTITY RESERVOIR STARTED TO D

All 62: https://openairdocs.org/deregistered/N354US-2007-08-29/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 20011008028439I](https://openairdocs.org/incident/20011008028439I), Oct 8, 2001: Boeing 737301 (N354US), Buffalo, NY. (-23) On Monday, October 8, 2001, N354US, a B-737-301 operated by usairways, inc., after takeoff and during flap retraction, the flaps split and an assemetry…

## Other aircraft with N354US

- [Cancelled 1972-05-01](https://openairdocs.org/deregistered/N354US-1972-05-01): Boeing 707-351B, S/N 18693. Exported to Hong Kong. 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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