# N578US: 1986 Boeing 737-301, registration cancelled 2004-03-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 11, 2004
- Exported to: Malaysia
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R)
- Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 23257
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: None
- Certificate issued: May 2, 2001
- Last registry action: November 7, 2002
- Mode S code: A76DF4
- 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/N578US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=578US
- Page: https://openairdocs.org/deregistered/N578US-2004-03-11

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

## Service difficulty reports (156, newest 50)

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

- [SDR F3LA200300152](https://openairdocs.org/sdr/F3LA200300152), Oct 20, 2003: SUPPORT. CRACKED. DURING C-5 CHECK, INSPECTION REPORTED ATTACH ANGLE CRACKED AT LOWER AFT END OF NR 1 PYLON. REPLACED DAMAGED SUPPORT IAW SRM 51-40-02.
- [SDR F3LA200300151](https://openairdocs.org/sdr/F3LA200300151), Oct 20, 2003: CHANNEL. CRACKED. DURING C-5 CHECK, INSPECTION REPORTED NR 1 ENGINE CHANNEL CRACKED OUTBOARD LOWER AFT END LT PYLON AT STA 320. REPLACED CHANNEL PER SRM 51-40-02.
- [SDR F3LA200300150](https://openairdocs.org/sdr/F3LA200300150), Oct 20, 2003: FRAME. CRACKED. DURING C-5 CHECK, INSPECTION REPORTED AFT LOWER END OF NR 1 ENGINE PYLON AT STA. 363 CRACKED. REPLACED NR 1 ENGINE AFT LOWER END "A" FRAME IAW SRM 51-40-02.
- [SDR F3LA200200359](https://openairdocs.org/sdr/F3LA200200359), Oct 21, 2002: SILL. CORRODED. DURING C 4 CHECK, CORROSION WAS FOUND ON THE R1 DOOR MOP SILL. INSPECTION, IAW SRM 53-10-15 FOUND THE SILL OUT OF TOLERANCE. NEW SILL WAS INSTALLED IAW SRM 53-1
- [SDR F3LA200200358](https://openairdocs.org/sdr/F3LA200200358), Oct 21, 2002: HOUSING. WORN. DURING C 4 CHECK, TRACK HOUSING WAS FOUND TO HAVE A HOLE WORN THROUGH IT CAUSING FUEL LEAK. HOUSING IS LOCATED INSIDE THE WING TANK FOR NR 5 OUT BOARD SLAT TRAC
- [SDR F3LA200200354](https://openairdocs.org/sdr/F3LA200200354), Oct 18, 2002: SKIN. CORRODED. DURING C 4 CHECK, CORROSION WAS FOUND ON THE INTERIOR FUSELAGE SKIN AT BS 500 AND STR 26L. FUSELAGE SKIN WAS ROUTED OUT AND REPAIRED IN ACCORDANCE WITH ENGINEER
- [SDR F3LA20020053](https://openairdocs.org/sdr/F3LA20020053), Oct 18, 2002: SKIN. CORRODED. DURING C 4 CHECK, CORROSION WAS FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN AT BS 500, STR 26L. CORRODED AREA WAS ROUTED OUT AND REPAIRED IAW EA 53-737-185, SRM 
- [SDR F3LA200200352](https://openairdocs.org/sdr/F3LA200200352), Oct 16, 2002: INTERCOSTAL. CORRODED. DURING C 4 CHECK, CORROSION WAS FOUND AROUND NUT PLATES ON INTERCOSTAL BETWEEN BS 847 AND BS 867, STRINGERS 25R AND 24R. REPAIR WAS PERFORMED IN ACCORDANCE WITH
- [SDR F3LA200200347](https://openairdocs.org/sdr/F3LA200200347), Oct 14, 2002: SHEAR TIE. CORRODED. CORROSION FOUND ON FRAME AND SHEAR TIE FORWARD AND AFT SIDES AT BS 500D, LBL 9 TO 22
- [SDR F3LA200200361](https://openairdocs.org/sdr/F3LA200200361), Oct 8, 2002: INTERCOSTAL. CRACKED. DURING C 4 CHECK, THE UPPER FLANGE OF FLOOR INTERCOSTAL WAS FOUND CRACKED AT BS 344 TO BS 360. REMOVED INTERCOSTAL. FABRICATED UPPER FLANGE OF THE INTERCOSTAL I
- [SDR F3LA200200360](https://openairdocs.org/sdr/F3LA200200360), Oct 8, 2002: INTERCOSTAL. CORRODED. DURING C 4 CHECK, CORROSION WAS FOUND ON THE INTERCOSTAL LOCATED AT BS 867 TO BS 887. INSPECTION REVEALED THE INTERCOSTAL WAS OUT OF LIMITS IAW THE REQUIREMENTS
- [SDR F3LA200200356](https://openairdocs.org/sdr/F3LA200200356), Oct 8, 2002: PANEL. CORRODED. DURING C 4 CHECK, AFT CARGO COMPARTMENT TRANSITION PANEL WAS FOUND TO HAVE CORROSION. INSPECTION OF THE TRANSITION PANEL, IAW THE REQUIREMENTS OF SRM 53-60-53, 
- [SDR F3LA200200329](https://openairdocs.org/sdr/F3LA200200329), Oct 6, 2002: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR BEAM UPPER CHORD, BS 344. REPAIRED FLOORBEAM PER SRM 53-10-51 AND EA 53-737-184.
- [SDR F3LA200200328](https://openairdocs.org/sdr/F3LA200200328), Oct 6, 2002: FLOOR SUPPORT. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 328 TO 344, RBL 11. REPLACED FLOOR SUPPORT PER SRM 53-10-01, FIG. 101, 51-40-02 AND EA 53-7
- [SDR F3LA200200327](https://openairdocs.org/sdr/F3LA200200327), Oct 6, 2002: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 312 TO 328, LBL 12. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 51-40-02, 51
- [SDR F3LA200200326](https://openairdocs.org/sdr/F3LA200200326), Oct 6, 2002: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 328 TO 344, LBL 12. REPLACED FLOOR SUPPORT PER SRM 53-10-51, 51-40-02 AND EA 53-737-181.
- [SDR F3LA200200325](https://openairdocs.org/sdr/F3LA200200325), Oct 6, 2002: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 294.5 TO 312, LBL 12. REPLACED FLOOR SUPPORT PER SRM 53-10-51, 51-40-02 AND EA 53-737-181.
- [SDR F3LA200200355](https://openairdocs.org/sdr/F3LA200200355), Oct 4, 2002: FLOOR SUPPORT. CORRODED. DURING C 4 CHECK, USING INSPECTION CRITERIA IN SRM 53-60-53, CORROSION WAS FOUND AROUND THE NUT PLATE ON THE FLOOR SUPPORT CHANNEL AT RBL 3 AT BS 887. REMOVED A
- [SDR F3LA200200351](https://openairdocs.org/sdr/F3LA200200351), Oct 4, 2002: FLOOR SUPPORT. CORRODED. DURING C 4 CHECK, CORROSION WAS FOUND ON THE FLOOR SUPPORT CHANNEL AT BS 897 AROUND THE NUT PLATE HOLE. REMOVED AND REPLACED SECTION OF FLOOR SUPPORT CHANNEL FR
- [SDR F3LA200200350](https://openairdocs.org/sdr/F3LA200200350), Oct 4, 2002: CARGO TRACK. CORRODED. DURING C 4 CHECK, CORROSION WAS FOUND ON CARGO TRACK AT BS 947, RBL 14 AT THE TIE DOWN SOCKET. CARGO TRACK SECTION WAS REPLACED IN ACCORDANCE WITH SRM 53-00-53,
- [SDR F3LA200200317](https://openairdocs.org/sdr/F3LA200200317), Oct 4, 2002: CHANNEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CHANNEL CORRODED AT BBL 8.1 BETWEEN BS 867 AND 847. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53, 55-00-
- [SDR F3LA200200316](https://openairdocs.org/sdr/F3LA200200316), Oct 4, 2002: FRAME. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED LT FUSELAGE FORMER AT FWD OTBD CORNER OF OUTER AIR CONDITIONING DUCT BAY DOOR CRACKED APPROXIMATELY 4 INCHES. DRILLED AND 
- [SDR F3LA200200315](https://openairdocs.org/sdr/F3LA200200315), Oct 4, 2002: THRESHOLD. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SILL PLATE IN FRONT OF C2 DOOR CORRODED. REPLACED THRESHOLD WEB PER SRM 51-40-02 AND 51-30-01.
- [SDR F3LA200200314](https://openairdocs.org/sdr/F3LA200200314), Oct 4, 2002: SKIN. DENTED. DURING C-4 CHECK, INSPECTION REPORTED L/E OF LT OTBD MID T/E FLAP DENTED AND GOUGED AT OTBD ACTUATOR. FABRICATED AND INSTALLED DOUBLER PER SRM 57-53-01, SOPM 20
- [SDR F3LA200200313](https://openairdocs.org/sdr/F3LA200200313), Oct 4, 2002: ANGLE. LOOSE. DURING C-4 CHECK, INSPECTION REPORTED RT WING INBD TE PLATE LOOSE FASTENERS ON MID FLAP. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-01, FIGURE 7 A
- [SDR F3LA200200312](https://openairdocs.org/sdr/F3LA200200312), Oct 4, 2002: DOUBLER. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RADIO ALTIMETER ANTENNA INTERNAL DOUBLER BETWEEN BS 440 AND 460. REPLACED RADIO ALTIMETER ANTENNA INTERNAL DO
- [SDR F3LA200200311](https://openairdocs.org/sdr/F3LA200200311), Oct 2, 2002: BEAR STRAP. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON C-1 DOOR BEAR STRAP AT BS 441, RBL 7.5. FABRICATED AND INSTALLED REPAIR PER PER EA 53-737-180.
- [SDR F3LA200200310](https://openairdocs.org/sdr/F3LA200200310), Oct 2, 2002: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON 312 FLOOR BEAM UPPER CHORD. FABRICATED AND INSTALLED REPLACEMENT UPPER CHORD PER SRM 51-40-02, 51-40-06 AND S
- [SDR F3LA200200308](https://openairdocs.org/sdr/F3LA200200308), Oct 2, 2002: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON DIAGONAL FLOOR SUPPORT BETWEEN BS 1006 AND 1016, RT. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER S
- [SDR F3LA200200309](https://openairdocs.org/sdr/F3LA200200309), Oct 2, 2002: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON DIAGONAL FLOOR SUPPORT BETWEEN BS 1006 AND 1016, L/H. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER 
- [SDR F3LA200200307](https://openairdocs.org/sdr/F3LA200200307), Oct 2, 2002: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR BEAM UPPER CHORD AT BS 294.5. FABRICATED REPLACEMENT PARTS AND INSTALLED REPAIR PER SRM 53-10-51, SRM 5
- [SDR F3LA200200306](https://openairdocs.org/sdr/F3LA200200306), Oct 2, 2002: CHANNEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR CHANNEL CORRODED AT BS 727D ABOVE STRINGER 28L. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. FA
- [SDR F3LA200200305](https://openairdocs.org/sdr/F3LA200200305), Oct 2, 2002: ANGLE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO BULKHEAD ANGLE AT BS 947. REPLACED BULKHEAD ANGLE PER SRM 53-30-53 AND 51-40-03.
- [SDR F3LA200200304](https://openairdocs.org/sdr/F3LA200200304), Oct 2, 2002: STRAP. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRAP BETWEEN BS 1006 AND BS 1016, RBL 18. FABRICATED AND INSTALLED REPLACEMENT FLOOR STRAP PER BOEING 
- [SDR F3LA200200303](https://openairdocs.org/sdr/F3LA200200303), Oct 2, 2002: STRAP. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRAP AT BS 1016. FABRICATED AND INSTALLED REPLACEMENT FLOOR STRAP PER SRM 53-30-01 AND BOEING DRAWING 
- [SDR F3LA200200302](https://openairdocs.org/sdr/F3LA200200302), Oct 2, 2002: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB AT BS 1016. FABRICATED AN INSTALLED REPLACEMENT WEB PER BOEING DRAWING 65-46812-109 AND SRM 53-30-0
- [SDR F3LA200200301](https://openairdocs.org/sdr/F3LA200200301), Oct 2, 2002: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL IN FWD CARGO COMPARTMENT BETWEEN BS 500B AND 500C, ABOVE STR 25L. FABRICATED AND INSTALLED REPLAC
- [SDR F3LA200200300](https://openairdocs.org/sdr/F3LA200200300), Oct 2, 2002: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL BETWEEN BS 294.5 AND BS 312, RBL 1 AND CRACKED ON AFT END. REMOVED DAMAGED INTERCOSTAL PER SRM 51
- [SDR F3LA200200299](https://openairdocs.org/sdr/F3LA200200299), Oct 2, 2002: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL IN FWD CARGO COMPARTMENT BETWEEN BS 500 AND 500A, ABOVE STR 25L. FABRICATED AND INSTALLED REPLACE
- [SDR F3LA200200298](https://openairdocs.org/sdr/F3LA200200298), Oct 2, 2002: STRINGER. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON STR 25L AT BS 500B+6. REPAIRED PER SRM 53-00-03, DETAIL VII.
- [SDR F3LA200200297](https://openairdocs.org/sdr/F3LA200200297), Oct 2, 2002: STRINGER. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON STR 26R AT BS 380. REMOVED CORRODED SECTION OF STRINGER PER SRM 51-40-02. FABRICATED AND INSTALLED REPAIR PER
- [SDR F3LA200200296](https://openairdocs.org/sdr/F3LA200200296), Oct 2, 2002: SILL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON R2 MOP SILL. REPLACED MOP SILL PER SRM 51-40-02.
- [SDR F3LA200200295](https://openairdocs.org/sdr/F3LA200200295), Oct 2, 2002: SILL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR MOP SILL. REPLACED MOP SILL PER SRM 51-40-02.
- [SDR F3LA200200294](https://openairdocs.org/sdr/F3LA200200294), Oct 2, 2002: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947-967, LBL 45. REMOVED INTERCOSTAL PER SRM 51-40-02. FABRICATED AND INSTALLED REPLACEMENT
- [SDR F3LA200200293](https://openairdocs.org/sdr/F3LA200200293), Oct 2, 2002: ATTACH ANGLE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CLOSET ATTACH ANGLES AT BS 1015. FABRICATED AND INSTALLED REPLACEMENT ANGLES PER BOEING DRAWING 65-48812 AND 
- [SDR F3LA200200292](https://openairdocs.org/sdr/F3LA200200292), Oct 2, 2002: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED ON CORROSION ON FLOOR INTERCOSTAL AT STA 986.5 - 1006, RBL 37. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51
- [SDR F3LA200200291](https://openairdocs.org/sdr/F3LA200200291), Oct 2, 2002: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION STA 947-967 LBL 17 INTERCOSTAL. FABRICATED NEW INTERCOSTAL PART SRM 53-60-51 & MM 51-21-99. INSTALLED PART PER S
- [SDR F3LA200200290](https://openairdocs.org/sdr/F3LA200200290), Oct 2, 2002: CHANNEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO BIN LT FLOOR SUPPORT ZEE CHANNEL. FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. FABRICATED PARTS PER 
- [SDR F3LA200200289](https://openairdocs.org/sdr/F3LA200200289), Oct 2, 2002: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION STA 947-967 LBL 30-45 ON INTERCOSTAL. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-60-51, 51-40-0
- [SDR F3LA200200284](https://openairdocs.org/sdr/F3LA200200284), Oct 2, 2002: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947 - BS 967, LBL 8. REMOVED DAMAGED INTERCOSTAL PER SRM 51-40-02. FABRICATED AND INSTALLED

All 156: https://openairdocs.org/deregistered/N578US-2004-03-11/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 19980223005109I](https://openairdocs.org/incident/19980223005109I), Feb 23, 1998: Boeing 737301 (N578US), Salt Lake City, UT. Narrative: [privacy data omitted] when the box was removed by the maintenance personnel it showed signs of smoke (streaking) and had a strong smell of…
- [Incident 19901027061359I](https://openairdocs.org/incident/19901027061359I), Oct 27, 1990: Boeing 737301 (N578US), Rochester, NY. Aborted takeoff two times due to high EGT indication on left engine. Replaced the EGT harness.

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