# N59302: 1985 Boeing 737-3TO, registration cancelled 2009-04-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 15, 2009 - Status when cancelled: Valid registration - Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 23353 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 19, 1985 - Certificate issued: April 15, 2009 - Last registry action: April 15, 2009 - Mode S code: A7AAFF - 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/N59302 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=59302 - Page: https://openairdocs.org/deregistered/N59302-2009-04-15 From the FAA registry file of November 4, 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md ## Service difficulty reports (64, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0700742](https://openairdocs.org/sdr/CALA0700742), Dec 11, 2007: SKIN. CRACKED. ON WALK AROUND FOUND 2 INCH CRACK IN FUSELAGE SKIN BETWEEN RT SIDE BETWEEN STA 747 AND 767 ON STR 19R. REPAIRED PER SRM 53-00-01 REPAIR 31 DETAIL 10. - [SDR CALA0700346](https://openairdocs.org/sdr/CALA0700346), Jul 11, 2007: SKIN. CRACKED. INSPECTION FOUND A CRACK AT LIGHTENING HOLE IN THE INNER SKIN OF THE FORWARD CARGO DOOR. THE DOOR SKIN WAS REPAIRED IAW ECRA 5230-01797. - [SDR CALA0600475](https://openairdocs.org/sdr/CALA0600475), Nov 14, 2006: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED AT STA 747, LBL 4. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A NEW SHEAR TIE WAS INSTALLED IAW SRM 53-00-07, REPAIR - [SDR CALA0600469](https://openairdocs.org/sdr/CALA0600469), Nov 12, 2006: KEELBEAM. CORRODED. INSPECTION FOUND LT KEELBEAM CORRODED AT STA 520, S28L. THE KEELBEAM SECTION WAS REPLACED IAW SRM 53-60-12. - [SDR CALA0600465](https://openairdocs.org/sdr/CALA0600465), Nov 11, 2006: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO CUTOUT AFT FRAME LOWER DOOR STOP AT STA 847, S18R TO S27R. THE FRAME WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0600466](https://openairdocs.org/sdr/CALA0600466), Nov 10, 2006: KEELBEAM. CORRODED. INSPECTION FOUND RT KEEL BEAM CORRODED ON INBOARD SIDE JUST AFT OF BULKHEAD AT STA 536. THE KEEL BEAM SECTION WAS REPLACED IAW SRM 53-60-12. - [SDR CALA0600460](https://openairdocs.org/sdr/CALA0600460), Nov 10, 2006: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN ANGLE THAT ATTACHES STRINGER TO WEB AT STA 360, S14L. THE ANGLE WAS REPLACED IAW ECRA 5311-01277. - [SDR CALA0600454](https://openairdocs.org/sdr/CALA0600454), Nov 10, 2006: FRAME. CORRODED. INSPECTION FOUND LOWER FRAME CORRODED AT STA 227.8, RBL 3 TO LBL 3, S1L TO S1R. A REPAIR WAS INSTALLED IAW ECRA 5311-01275. - [SDR CALA0600452](https://openairdocs.org/sdr/CALA0600452), Nov 9, 2006: STRINGER. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R CORRODED AT STA 864. THE STRINGER WAS REPLACED IAW SRM 53-00-03. - [SDR CALA0600496](https://openairdocs.org/sdr/CALA0600496), Nov 3, 2006: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN PANEL CORRODED AT STA 727 + 4.00 AND CENTERED OVER THE LT KEEL BEAM AT S27L. THE SKIN WAS REPAIRED IAW ECRA 5331-01274. - [SDR CALA0600449](https://openairdocs.org/sdr/CALA0600449), Nov 2, 2006: SHEAR TIE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LOWER SHEAR TIE FOR FUSELAGE FRAME AT STA 360, S13L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0600444](https://openairdocs.org/sdr/CALA0600444), Oct 30, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND RT OB SEAT TRACK CORRODED AT STA 897-927, RBL 45.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52. - [SDR CALA0600439](https://openairdocs.org/sdr/CALA0600439), Oct 29, 2006: ATTACH FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE TO BELTFRAME CLIP AT STA 616, S7L TO S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0600438](https://openairdocs.org/sdr/CALA0600438), Oct 29, 2006: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 907-1006, LBL 34 TO LBL 60. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0600437](https://openairdocs.org/sdr/CALA0600437), Oct 29, 2006: BELTFRAME. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME AT STA 616, S7L. REPAIRED IAW SRM 53-00-07. - [SDR CALA0600436](https://openairdocs.org/sdr/CALA0600436), Oct 29, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 907-938, BL 0. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-02, REPAIR 3. - [SDR CALA0600430](https://openairdocs.org/sdr/CALA0600430), Oct 26, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 50 TO RBL 25. DOUBLERS AND A SECTION OF T-CHORD WERE INSTALLED IAW SRM 53-10-51. - [SDR CALA0600429](https://openairdocs.org/sdr/CALA0600429), Oct 25, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 907-947.5, LBL 24.75. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. - [SDR CALA0600428](https://openairdocs.org/sdr/CALA0600428), Oct 24, 2006: FRAME. CRACKED. INSPECTION FOUND A 1/2" CRACK IN MAIN FRAME AT STA 616 JUST BELOW FLOOR, S18R. REPAIRED IAW ECRA 5311-01158. - [SDR CALA0600427](https://openairdocs.org/sdr/CALA0600427), Oct 24, 2006: FRAME. CRACKED. INSPECTION FOUND A 0.6" CRACK IN MAIN FRAME AT STA 616 JUST BELOW FLOOR, S17L. REPAIRED IAW ECRA 5311-01158. - [SDR CALA0600424](https://openairdocs.org/sdr/CALA0600424), Oct 23, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R IN AFT CARGO COMPARTMENT CORRODED FROM STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-80-03 AND BOEING DRAWING 65 - [SDR CALA0600419](https://openairdocs.org/sdr/CALA0600419), Oct 18, 2006: FLOORBEAM. CORRODED. CORRODED AFT ENTRY FLOORBEAM AT STA 986.5. REPAIRED IAW ECRA 5310-03851. - [SDR CALA0600411](https://openairdocs.org/sdr/CALA0600411), Oct 16, 2006: FLOORBEAM. CORRODED. CORRODED FLOORBEAM 312 RBL 35. REPAIRED IAW SRM 53-10-51, REPAIR 5, FIG 201. - [SDR CALA0600280](https://openairdocs.org/sdr/CALA0600280), Jul 30, 2006: DOOR FRAME. CRACKED. INSPECTION FOUND A 1" CRACK IN AFT CARGO DOOR AT PULLEY ATTACHMENT. THE AFT CARGO DOOR FORWARD UPPER AND LOWER CORNER ASSEMBLY (FRAME) WAS REMOVED AND REPLACED - [SDR CALA0600279](https://openairdocs.org/sdr/CALA0600279), Jul 30, 2006: FRAME. CORRODED. INSPECTION FOUND AFT PIT FORWARD FLOOR FRAME UNDER CAMPLATE CORRODED THROUGH FRAME AT STA 787-807, S2R TO S17R. THE CORRODED SECTION OF FRAME WAS REMOVED AND RE - [SDR ZN3R543100](https://openairdocs.org/sdr/ZN3R543100), Dec 12, 2005: PLENUM. RUPTURED. TURBINE PLENUM OF APU RUPTURED AT A PREVIOUSLY REPAIRED WELD SEAM. - [SDR CALA0500133](https://openairdocs.org/sdr/CALA0500133), Apr 14, 2005: SKIN. CORRODED. FUSELAGE SKIN CORRODED AT NR 3 VHF ANTENNA SUPPORT. INSTALLED CHANNEL PER ECRA 5331-01179. - [SDR CALA0500084](https://openairdocs.org/sdr/CALA0500084), Mar 22, 2005: SKIN. CORRODED. INSPECTION FOUND THE FUSELAGE SKIN UNDER NR 3 VHF ANTENNA CORRODED, STA 727D, S29L TO S29R. INSTALLED REPAIR IAW ECRA 5331-01179. - [SDR CALA0500083](https://openairdocs.org/sdr/CALA0500083), Mar 22, 2005: STRINGER. CORRODED. INSPECTION FOUND SKIN BULGING AT STA 360 MINUS 6 INCHES TO 360 WITH CORROSION ON STRINGER 25L. REPAIRED STRINGER IAW ECRA 5311-01219. - [SDR CALA0500014](https://openairdocs.org/sdr/CALA0500014), Jan 19, 2005: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN EIGHT INCHES FORWARD OF STA 727E AND BELOW STRINGER 22L. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5330-03410. - [SDR CALA0500008](https://openairdocs.org/sdr/CALA0500008), Jan 14, 2005: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN SKIN AFT OF RT WING TO BODY FAIRING, 10 INCHES AFT OF EMERGENCY LIGHT (JUST 2 INCHES FORWARD OF BS 727E AT S23R). INSTALLED - [SDR CALA0200493](https://openairdocs.org/sdr/CALA0200493), Oct 11, 2002: SKIN. CRACKED. INSPECTION FOUND AN 8" CRACK IN R/H WING FIXED L/E SKIN PANEL ABOVE #4 SLAT ACTUATOR. THE SKIN PANEL WAS REMOVED AND REPLACED IAW ECRA 5720-01894. - [SDR CALA0200488](https://openairdocs.org/sdr/CALA0200488), Oct 7, 2002: STRINGER. CORRODED. INSPECTION FOUND STRINGER 23L CORRODED AT STA 375 IN FORWARD CARGO PIT. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A NEW SECTION OF STRINGER WAS SPLICED I - [SDR CALA0200487](https://openairdocs.org/sdr/CALA0200487), Oct 5, 2002: FLOORBEAM. CRACKED. INSPECTION FOUND FLOORBEAM CRACKED ON UPPER ANGLE AT STA 328, LBL 12. THE CRACKED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA0200481](https://openairdocs.org/sdr/CALA0200481), Oct 1, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 990 FROM LBL 14 TO LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0200479](https://openairdocs.org/sdr/CALA0200479), Sep 29, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 270 AND 294.5, RBL 43 UNDER G-1 GALLEY. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 AND 51-10-02. - [SDR CALA0200112](https://openairdocs.org/sdr/CALA0200112), Feb 28, 2002: OVEN. MALFUNCTIONED. A STRONG TOXIC ODOR WAS OBSERVED IN THE CABIN WHILE EN ROUTE FROM MSY TO EWR. THE CABIN CREW AND PASSENGERS COMPLAINED OF THE ODOR. THE FLIGHT WAS DIVERTED TO A - [SDR CALA0100652](https://openairdocs.org/sdr/CALA0100652), Jul 12, 2001: AILERON. CRUSHED. INSPECTION FOUND LEADING EDGE I/B CORNER OF L/H AILERON CRUSHED. THE AILERON WAS REPAIRED IAW ECRA 5761-01026. - [SDR CALA0100651](https://openairdocs.org/sdr/CALA0100651), Jul 11, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL SKIN OF E&E DOOR DENTED. THE E&E DOOR OUTER SKIN WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0100649](https://openairdocs.org/sdr/CALA0100649), Jul 11, 2001: LIGHT. INOPERATIVE. THE AFT RIGHT SERVICE DOOR EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-11 AND OPERATION CHECKED GOO - [SDR CALA0100648](https://openairdocs.org/sdr/CALA0100648), Jul 11, 2001: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN AFT BAGGAGE BIN FLOOR SUPPORT AT STA 767, RBL 14. A REPAIR WAS INSTALLED IAW SRM 53-00-53. - [SDR CALA0100634](https://openairdocs.org/sdr/CALA0100634), Jul 6, 2001: FRAME. CRACKED. INSPECTION FOUND A 1" CRACK IN L-1 WINDOW FRAME AT UPPER O/B CORNER. THE WINDOW FRAME WAS REPAIRED IAW SRM 53-10-01. - [SDR CALA0100633](https://openairdocs.org/sdr/CALA0100633), Jul 5, 2001: SKIN. CRACKED. A PERMANENT REPAIR WAS INSTALLED WHERE AN INTERIM REPAIR HAD PREVIOUSLY BEEN DONE FOR 4 EACH CRACKS AT LIGHTENING HOLES IN AFT CARGO DOOR INNER SKIN. THE INTERI - [SDR CALA0100487](https://openairdocs.org/sdr/CALA0100487), May 21, 2001: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN SKIN OF AFT CUTOUT FOR THE E&E COMPARTMENT COOLING EXHAUST AT STA 373. AN INTERNAL DOUBLER WAS INSTALLED IAW ECRA 5330-02894 - [SDR CALA9900073](https://openairdocs.org/sdr/CALA9900073), Jan 24, 1999: SKIN. CRACKED. INSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN FUSELAGE SKIN AT FORWARD LOWER CORNER OF C-2 AFT CARGO DOOR CUTOUT. REPAIRED IAW ECRA 5330-02763. - [SDR CALA9900072](https://openairdocs.org/sdr/CALA9900072), Jan 23, 1999: BATTERY PACK. DISCHARGED. THE BATTERY CHARGER ASSEMBLY AND BATTERY FAILED SYSTEM FUNCTIONAL CHECK, PACK M1135, STA 629R (28 VDC PRESENT AT PIN 2 OF PLUG POWER SUPPLY). REMOVED AND REPLAC - [SDR CALA9900071](https://openairdocs.org/sdr/CALA9900071), Jan 22, 1999: KEEL BEAM. CORRODED. INSPECTION FOUND KEEL BEAM CORRODED AT STA 727, STRINGER 27L. A REPAIR WAS INSTALLED IAW ECRA 5310-03814. - [SDR CALA9900009](https://openairdocs.org/sdr/CALA9900009), Jan 13, 1999: FLOORBEAM. CORRODED. FLOOR SUPPORT BEAM HAS SURFACE CORROSION AROUND FASTENER HOLES STA 986.5. INSTALLED NEW FLOORBEAM PER EC/RA 5310-03450. - [SDR CALA9900059](https://openairdocs.org/sdr/CALA9900059), Jan 11, 1999: FLOORBEAM. CORRODED. FORWARD GALLEY CORROSION IN HOLES UPPER AND LOWER SURFACE ON FLOORBEAM STA 328 BL 0 TO R1 Z ANGLE. CUT OUT DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED NE - [SDR CALA9801969](https://openairdocs.org/sdr/CALA9801969), Oct 17, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT NUTPLATES LOCATED IN E/E COMPARTMENT AT STA 312, RBL 3.5 TO 17. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 51-70-12, All 64: https://openairdocs.org/deregistered/N59302-2009-04-15/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 19930605026149I](https://openairdocs.org/incident/19930605026149I), Jun 5, 1993: Boeing 737300 (N59302), Denver, CO, Minor damage. On landing rollout either left main tire blew or brakeline failed. Found lower torque link had failed. - [Incident 19860830056479I](https://openairdocs.org/incident/19860830056479I), Aug 30, 1986: Boeing 7373TO (N59302), Omaha, NE. Diverted after overheat light came on as power lever was advanced. Overheat detector unit replaced. ## Other aircraft with N59302 - [Cancelled 1955-10-26](https://openairdocs.org/deregistered/N59302-1955-10-26): Cessna T-50, S/N 5958. Owner: [Foote Lou/DBA Lou Foote Flying Service](https://openairdocs.org/faa-owner/FOOTE%20LOU%2FDBA%20LOU%20FOOTE%20FLYING%20SERVICE), [Lancaster, TX](https://openairdocs.org/faa-place/TX/Lancaster) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.