# N921WA: 1983 Boeing 737-2Y5, registration cancelled 2004-05-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 11, 2004
- Exported to: Honduras
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-2Y5](https://openairdocs.org/model/boeing-737-2y5) (registry code 1384554)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 23039
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 14, 1998
- Certificate issued: November 20, 2003
- Last registry action: November 20, 2003
- Mode S code: ACC3D6
- 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/N921WA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=921WA
- Page: https://openairdocs.org/deregistered/N921WA-2004-05-11

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 737-2Y5: https://openairdocs.org/model/boeing-737-2y5.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 F3LA200300114](https://openairdocs.org/sdr/F3LA200300114), Mar 10, 2003: FITTING. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED RT. HORIZONTAL STAB CENTER SECTION, AFT UPPER ATTACH CLEVIS, AFT LUG, CORRODED. REPAIRED PER EA 55-737-077.
- [SDR F3LA200300113](https://openairdocs.org/sdr/F3LA200300113), Mar 10, 2003: DOOR FRAME. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED R-2 DOOR FRAME ON FUSELAGE CORRODED ON AFT SEALING SURFACE BETWEEN BOTTOM TO SECOND FROM BOTTOM STOP PAD FITTINGS. BLENDED
- [SDR F3LA200300094](https://openairdocs.org/sdr/F3LA200300094), Mar 2, 2003: PANEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED AFT LAVATORY SERVICE PANEL CORRODED AT FWD HINGE. FOUND TO BE OUT OF LIMITS PER SRM 51-30-02. FABRICATED REPLACEMENT PANEL
- [SDR F3LA200300092](https://openairdocs.org/sdr/F3LA200300092), Feb 26, 2003: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED LOWER WEB FROM LAVATORY FLOOR TO FUSELAGE ON LT. SIDE OF FUSELAGE CORRODED AROUND CUTOUTS, STA. 277 TO STA. 294.5. FABRICA
- [SDR F3LA200300091](https://openairdocs.org/sdr/F3LA200300091), Feb 25, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR BEAM AT STA. 772, LBL 12, AT FLOOR PANEL SPLICE STRIP, BOTTOM SIDE OF UPPER FLANGE. CUT OUT DAMAG
- [SDR F3LA200300090](https://openairdocs.org/sdr/F3LA200300090), Feb 25, 2003: MOUNT BRACKET. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED FWD FUSELAGE VHF 2 ANTENNA MOUNT BRACKET CRACKED AT STA. 500, RBL 2. REPLACED BRACKET PER SRM 51-10-1 AND 51-30-2.
- [SDR F3LA200300089](https://openairdocs.org/sdr/F3LA200300089), Feb 25, 2003: SILL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED R-2 DOOR RT. MOP SILL CORRODED AT VARIOUS POINTS ALONG ENTIRE LENGTH OF MOP SILL. REPLACED DAMAGED MOP SILL PER SRM 51-30-
- [SDR F3LA200300088](https://openairdocs.org/sdr/F3LA200300088), Feb 25, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT/INTERCOSTAL (WEB STRAP)FROM STA. 1006 BACK, LBL 2, CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB
- [SDR F3LA200300087](https://openairdocs.org/sdr/F3LA200300087), Feb 20, 2003: SILL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, FIG. 1, SHEET 4, DETAIL I. RE
- [SDR F3LA200300086](https://openairdocs.org/sdr/F3LA200300086), Feb 20, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA. 927 AND STA. 947.5 ON RT. SIDE OF AIRCRAFT CENTERLINE CORRODED. REMOVED CORROSION AND INTERCOSTAL
- [SDR F3LA200300085](https://openairdocs.org/sdr/F3LA200300085), Feb 20, 2003: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO FLOOR SUPPORT CORRODED ON LOWER FLANGE AT STA. 859, RBL 8. INSTALLED REPAIR PER SRM 53-10-5 AND MM 51-21-99.
- [SDR F3LA200300084](https://openairdocs.org/sdr/F3LA200300084), Feb 20, 2003: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED WEB BETWEEN STA. 332 AND STA. 344, AFT OF R-1 DOOR, CORRODED ON BOTTOM SIDE. REMOVED DAMAGE ON WEB, FABRICATED AND INSTALL
- [SDR F3LA200300083](https://openairdocs.org/sdr/F3LA200300083), Feb 20, 2003: CHANNEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION IN SCREW HOLES OF FWD LAVATORY AFT BULKHEAD ATTACH ANGLE, HAT SECTION, STA. 312, LBL 12 TO LBL 42. REMOVED HAT S
- [SDR F3LA200300082](https://openairdocs.org/sdr/F3LA200300082), Feb 19, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SHORT INTERCOSTAL AT CENTERLINE BETWEEN STA. 1006 AND STA. 1016 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL
- [SDR F3LA200300081](https://openairdocs.org/sdr/F3LA200300081), Feb 19, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED LT. INTERCOSTAL BETWEEN STA. 967 AND STA. 986.5 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-1
- [SDR F3LA200300080](https://openairdocs.org/sdr/F3LA200300080), Feb 19, 2003: SEAT TRACK. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND SCREW HOLES AT SEAT TRACK BETWEEN STA. 328 AND STA. 344, RBL 54. FABRICATED AND INSTALLED REPLACEM
- [SDR F3LA200300078](https://openairdocs.org/sdr/F3LA200300078), Feb 19, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON AFT GALLEY FLOOR INTERCOSTAL AT STA. 957, LBL 18.75 THRU LBL 40.5. FOUND CORROSION TO BE OUT OF LIMIT
- [SDR F3LA200300077](https://openairdocs.org/sdr/F3LA200300077), Feb 19, 2003: SEAT TRACK. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK CORRODED AT NUTCLIP HOLES, RT. SIDE BETWEEN FLOORBEAM AT STA. 986.5 TO STA. 1016. REPLACED SEAT TRACK PER SRM 5
- [SDR F3LA200300075](https://openairdocs.org/sdr/F3LA200300075), Feb 19, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP AT STA. 312, LBL 13 TO RBL 10. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-01
- [SDR F3LA200300076](https://openairdocs.org/sdr/F3LA200300076), Feb 19, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT SCREW HOLE, STA. 328, LBL 29. REMOVED TOP CAP REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGL
- [SDR F3LA200300074](https://openairdocs.org/sdr/F3LA200300074), Feb 18, 2003: STRINGER. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON STRINGER 18-R AT STA. 727B + 16. REPAIRED DAMAGED SECTION OF STRINGER PER SRM 53-10-1, PAGE 6, DETAIL
- [SDR F3LA200300073](https://openairdocs.org/sdr/F3LA200300073), Feb 18, 2003: ANGLE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON BULKHEAD ANGLE AT STA. 947.5 LOWER ANGLE. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-1, 53-20-0
- [SDR F3LA200300072](https://openairdocs.org/sdr/F3LA200300072), Feb 18, 2003: PANEL. PUNCTURED. DURING C-4 CHECK, INSPECTION REPORTED SMALL PUNCTURE IN TRANSITION PANEL BETWEEN STA. 767 AND 794. REPAIRED PANEL PER SRM 53-10-13 AND SOPM 20-4-02.
- [SDR F3LA200300071](https://openairdocs.org/sdr/F3LA200300071), Feb 18, 2003: SEAT TRACK. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK CORRODED AT STA 290, RBL 16. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-2 AND 53-10-2.
- [SDR F3LA200300070](https://openairdocs.org/sdr/F3LA200300070), Feb 18, 2003: CLIP. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED TIE CLIP AND ATTACHING HARDWARE CORRODED AT AFT END OF RT MOP SILL BEHIND R-2 DOOR. REPLACED CLIP HARDWARE PER SRM 51-30-2
- [SDR F3LA200300069](https://openairdocs.org/sdr/F3LA200300069), Feb 18, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM BETWEEN STA 727 AND 727A, LBL 3, AT NUT PLATE ON UNDERSIDE OF FLANGE. FABRICATED AND INSTALLE
- [SDR F3LA200300068](https://openairdocs.org/sdr/F3LA200300068), Feb 18, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM BETWEEN STA 727 AND 727A, RBL 3, AT NUT PLATE ON UNDERSIDE OF UPPER FLANGE. FABRICATED AND IN
- [SDR F3LA200300067](https://openairdocs.org/sdr/F3LA200300067), Feb 18, 2003: SUPPORT ANGLE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR/LAVATORY SUPPORT BEAM BETWEEN STA 986.5 AND STA 1006 CORRODED. REMOVED SUPPORT ANGLE AND HAT CHANNEL PER SRM 51-30-0
- [SDR F3LA200300066](https://openairdocs.org/sdr/F3LA200300066), Feb 18, 2003: STRINGER. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED HEAVY CORROSION AT STR 27-L BETWEEN STA 945 AND STA 953.5. REPLACED STRINGER FROM STA 945 TO STA 967.5, LBL 3, STR 27-L, P
- [SDR F3LA200300065](https://openairdocs.org/sdr/F3LA200300065), Feb 18, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP AT STA 344, LBL 60 - RBL 14. REMOVED DAMAGE ON WEB BETWEEN STA 332 AND STA 344 AFT OF R-1 DOOR 
- [SDR F3LA200300064](https://openairdocs.org/sdr/F3LA200300064), Feb 17, 2003: ATTACH ANGLE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED RT RAM AIR DUCT ANGLE ATTACH POINT FOR CROSS BRACE UNDER WING BLEED AIR DUCT CORRODED AT STA 540, STR 22R. REMOVED DAMAGED
- [SDR F3LA200300063](https://openairdocs.org/sdr/F3LA200300063), Feb 17, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CAP CORRODED AT STA 290, RBL 15. FABRICATED AND INSTALLED REPLACEMENT CAP STRIP PER SRM 53-10-2 AND 53-10-9.
- [SDR F3LA200300062](https://openairdocs.org/sdr/F3LA200300062), Feb 14, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CAP AT STA 1006 CORRODED IN VARIOUS AREAS FROM CENTERLINE EXTENDING TO LEFT SIDE. REPAIRED PER SRM 53-10-9, FIG 
- [SDR F3LA200300061](https://openairdocs.org/sdr/F3LA200300061), Feb 13, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM AT NUT PLATE ON UNDERSIDE OF UPPER FLANGE, STA 794, LBL 8. FOUND CORROSION TO BE OUT OF LIMIT
- [SDR F3LA200200397](https://openairdocs.org/sdr/F3LA200200397), Dec 23, 2002: TRUNNION. CORRODED. DURING NOSE GEAR CHANGE, INSPECTED REPORTED LT NOSE GEAR TRUNNION BOSS CORRODED. REPLACED NOSE GEAR TRUNNION BOSS.
- [SDR F3LA200100113](https://openairdocs.org/sdr/F3LA200100113), Oct 21, 2001: DUCT. BROKEN. ENROUTE FROM SAN TO DEN, FLIGHT CREW REPORTED CABIN SIDEWALL AT ROW 7 EXTREMELY HOT TO THE TOUCH AND AN OVERHEAT ODOR. AN EMERGENCY WAS DECLARED AND AIRCRAFT DI
- [SDR F3LA200100111](https://openairdocs.org/sdr/F3LA200100111), Sep 26, 2001: DOOR FRAME. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED CRACK IN LOWER AFT CORNER OF C1 DOOR. DOOR WAS REPAIRED AT VENDOR AND RETURNED IN SERVICEABLE CONDITION.
- [SDR F3LA200100110](https://openairdocs.org/sdr/F3LA200100110), Sep 24, 2001: DOOR FRAME. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LT SIDE OF E&E DOOR CUTOUT BETWEEN CHORD AND SKIN. REMOVED DOOR FITTINGS, CORRODED WEBS, SKIN AND CHORDS. INS
- [SDR F3LA200100109](https://openairdocs.org/sdr/F3LA200100109), Sep 24, 2001: DOOR FRAME. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DOOR FRAME CRACKED AT LOWER SET OF BACK FASTENERS. REPAIRED PER SRM 51-40-04.
- [SDR F3LA200100106](https://openairdocs.org/sdr/F3LA200100106), Sep 15, 2001: SKIN. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED CRACK IN L-2 DOOR CUTOUT, LOWER FWD CORNER, BS 947.5, S-18L, APPROXIMATELY 3.5 INCHES LONG. REPAIRED CRACK PER SRM 53-30-3
- [SDR F3LA200100064](https://openairdocs.org/sdr/F3LA200100064), May 13, 2001: OIL FILTER. DIRTY. FLIGHT CREW REPORTED NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT CRUISE. NR 1 ENGINE WAS SHUT DOWN IN FLIGHT AND AN EMERGENCY WAS DECLARED. AIRCRAFT DIVE
- [SDR F3LA200100050](https://openairdocs.org/sdr/F3LA200100050), Mar 27, 2001: ATTACH FITTING. BROKEN. DURING A-CHECK, MAINTENANCE REPORTED LT WING OTBD FOREFLAP OTBD ATTACH LINK BROKEN. REPLACED LT WING OTBD FOREFLAP.
- [SDR F3LA200100009](https://openairdocs.org/sdr/F3LA200100009), Jan 19, 2001: CHARGER. INOPERATIVE. L-1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED L-1 DOOR SLIDE LIGHT ASSY, BATTERY AND CHARGER PER MM 33-51-71.
- [SDR F3LA200000248](https://openairdocs.org/sdr/F3LA200000248), Oct 3, 2000: STRINGER. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON STR 21-R, STA 847 TO 867, AND CORROSION ON INTERCOSTAL BETWEEN STR 21-R AND 22-R, STA 847 TO 867. MAINTENANCE
- [SDR F3LA200000247](https://openairdocs.org/sdr/F3LA200000247), Sep 29, 2000: DOOR FRAME. CRACKED. DURING C-2 CHECK, INSPECTION REPORTED CRACK IN R-1 DOOR CUTOUT UNDER SCUFF PLATE AT LOWER AFT CORNER. MAINTENANCE VERIFIED CRACK BY ACCOMPLISHING AN NDT INSPECT
- [SDR F3LA200000246](https://openairdocs.org/sdr/F3LA200000246), Sep 25, 2000: STRINGER. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON INSIDE SURFACE OF STRINGER 25L, STA 1006, AROUND FASTENER. MAINTENANCE BLENDED CORROSION AND FOUND TO BE OUT 
- [SDR F3LA00240](https://openairdocs.org/sdr/F3LA00240), Sep 13, 2000: SKIN. CHAFED. DEN - DURING C-2 CHECK INSPECTION, REPORTED CHAFING ON LEFT LEADING EDGE ABOVE NR 1 ENGINE PYLON. MAINTENANCE REPLACED WING LEADING EDGE SECTION ABOVE NR 1 ENGI
- [SDR F3LA00241](https://openairdocs.org/sdr/F3LA00241), Sep 12, 2000: STRINGER. CORRODED. DEN - DURING C-2 CHECK INSPECTION, REPORT CORROSION ON STRINGER 23R FROM STATION 259 TO STATION 312. MAINTENANCE FABRICATED AND INSTALLED NEW STRINGER PER SRM 5
- [SDR F3LA00235](https://openairdocs.org/sdr/F3LA00235), Sep 7, 2000: STRUCTURE. CRACKED. DURING C-2 CHECK, INSPECTION REPORTED CRACK IN FORWARD PRESSURE BULKHEAD FLOOR STRUCTURE NEXT TO INTERCOSTAL WL 207, RBL 27. MAINTENANCE INSTALLED NEW WEB PER S
- [SDR F3LA00234](https://openairdocs.org/sdr/F3LA00234), Sep 7, 2000: STRUCTURE. CRACKED. DEN - DURING C-2 CHECK, INSPECTION REPORTED CRACK IN FORWARD PRESSURE BULKHEAD FLOOR STRUCTURE NEXT TO INTERCOSTAL, WL 207, LBL 27. MAINTENANCE INSTALLED NEW WE

All 79: https://openairdocs.org/deregistered/N921WA-2004-05-11/reports.md

## FAA accident and incident reports (2)

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 20010513012979I](https://openairdocs.org/incident/20010513012979I), May 13, 2001: Boeing 7372Y5 (N921WA), Kansas City, MO. (-23)On may 13, 2001 at approximately 2200 hours, a frontier airlines B737-2Y5, flight 546, enroute from den to mdw, declared an emergency and diverted to mci,…
- [Incident 19990413018009I](https://openairdocs.org/incident/19990413018009I), Apr 13, 1999: Boeing 7372Y5 (N921WA), Long Beach, CA. (-5) During climb capt. observed APU fire warning light illuminated. Executed memory items and discharged one bottle. Returned to Long Beach airport after…

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