# N47332: 1986 Boeing 737-3TO, registration cancelled 2009-01-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 30, 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: 23570 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 21, 1986 - Certificate issued: June 20, 2007 - Last registry action: June 20, 2007 - Mode S code: A5CF1B - 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/N47332 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=47332 - Page: https://openairdocs.org/deregistered/N47332-2009-01-30 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md ## Service difficulty reports (66, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0800740](https://openairdocs.org/sdr/CALA0800740), Jul 18, 2008: HEATER. SHORTED. DURING TAXI AND SHORTLY AFTER TURNING ON WINDOW HEAT, A SPARK WAS NOTED COMING FROM THE 1R WINDOW WHICH THEN CRACKED. REMOVED AND REPLACED R-1 WINDOW PER MM 56- - [SDR CALA0800084](https://openairdocs.org/sdr/CALA0800084), Jan 29, 2008: BELTFRAME. CRACKED. FUSELAGE CROWN INTERIOR BELT FRAME HAS CRACK AROUND FASTENER OF OVERHEAD GRILL MOUNTING BRACKET JUST ABOVE STRINGER S9R AT STA 480. - [SDR CALA0700787](https://openairdocs.org/sdr/CALA0700787), Dec 9, 2007: SHEAR TIE. CORRODED. SHEAR TIE CORRODED BEHIND AFT PIT AFT BULKHEAD 1 FRAME AFT OF POT WATER PANEL IN CENTER OF AC BELLY SKIN. PERFORMED REPAIR STA 967 STRINGER 27L AND 27R PER ECRA - [SDR CALA0700786](https://openairdocs.org/sdr/CALA0700786), Dec 9, 2007: STRAP. CORRODED. PAN STRAP CORRODED AT STA 967 BETWEEN S-27L AND S-27R. REPAIRED PER ECRA 5330-03760. - [SDR CALA0700038](https://openairdocs.org/sdr/CALA0700038), Jan 22, 2007: STIFFENER. CRACKED. INSPECTION FOUND A CRACK IN THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT RBL 6.15. THE STIFFENER WAS REPAIRED IAW ECRA 5714-01019. - [SDR CALA0700024](https://openairdocs.org/sdr/CALA0700024), Jan 21, 2007: SUPPORT ANGLE. CORRODED. INSPECTION FOUND RT WHEEL WELL BLADE SEAL RING SUPPORT ANGLE CORRODED AT AFT AREA. THE BLADE SEAL RING SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02. - [SDR CALA0700021](https://openairdocs.org/sdr/CALA0700021), Jan 19, 2007: SKIN. BUCKLED. INSPECTION FOUND FUSELAGE SKIN BUCKLED WITH STRESSED RIVETS AT BS 500D + 10, S28R, RBL 10. A REPAIR WAS INSTALLED IAW SRM 53-30-12. - [SDR CALA0600039](https://openairdocs.org/sdr/CALA0600039), Jan 22, 2006: STIFFENER. CRACKED. INSPECTION FOUND THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER CRACKED AT LBL 6.15. A REPAIR WAS INSTALLED IAW ECRA 5714-01014. A DIP WAS ISSUED TO REINS - [SDR CALA0500136](https://openairdocs.org/sdr/CALA0500136), Apr 27, 2005: HINGE. LACK OF LUBE. MAIN CABIN DOOR WILL NOT CLOSE. CLEANED AND LUBRICATED TRACKS AND HINGE. - [SDR CALA0400715](https://openairdocs.org/sdr/CALA0400715), Nov 11, 2004: SKIN. CRACKED. INSPECTION FOUND A 0.2 INCH CRACK IN LT FUSELAGE SKIN 5.6 INCH AFT OF STA 727D AT STRINGER 22L TO 23L. REPAIRED IAW ECRA 5331-01167. - [SDR CALA0400705](https://openairdocs.org/sdr/CALA0400705), Nov 9, 2004: INTERCOSTAL. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT UPPER FORWARD CORNER OF FORWARD ENTRY DOOR SURROUND STRUCTURE BETWEEN STA 309 AND 312, S4L. THE INTERCOSTAL WA - [SDR CALA0400701](https://openairdocs.org/sdr/CALA0400701), Nov 4, 2004: STRINGER. CORRODED. INSPECTION FOUND STRINGER 23L CORRODED APPROXIMATELY 2 INCHES AFT OF STA 887 FRAME. A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. - [SDR CALA0400700](https://openairdocs.org/sdr/CALA0400700), Nov 3, 2004: STRAP. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN H-STRAP LEFT L1 UPPER HINGE CUTOUT AT STA 312. THE H-STRAP WAS REMOVED AND A NEW H-STRAP WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0400695](https://openairdocs.org/sdr/CALA0400695), Nov 1, 2004: WEB. CORRODED. INSPECTION FOUND LOWER SIDE OF WEB CORRODED BELOW S17L, JUST FORWARD OF STA 1016. INSTALLED DOUBLER IAW SRM 51-70-130, FIGURE 1. - [SDR CALA0400694](https://openairdocs.org/sdr/CALA0400694), Nov 1, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 277 - 294.5. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10- - [SDR CALA0400693](https://openairdocs.org/sdr/CALA0400693), Oct 31, 2004: FLOORBEAM. CORRODED. INSPECTION FOUND UPPER AND LOWER SURFACES OF FLOORBEAM UPPER CAP CORRODED AT STA 344, RBL 10-LBL 20. THE FLOORBEAM CHORD WAS REPAIRED IAW SRM 53-10-51, FIGURE 2 - [SDR CALA0400692](https://openairdocs.org/sdr/CALA0400692), Oct 31, 2004: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R CORRODED IN E&E COMPARTMENT AT STA 319 - 322.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. - [SDR CALA0400691](https://openairdocs.org/sdr/CALA0400691), Oct 30, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-00-52 AND 51-40-02. - [SDR CALA0400195](https://openairdocs.org/sdr/CALA0400195), Mar 1, 2004: SKIN. DENTED. INSPECTION FOUND LT HORIZONTAL STABILIZER LOWER SKIN DENTED 57 INCHES FROM I/B EDGE AND 33 INCHES BACK FROM T/E. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-10-01 - [SDR CALA0400194](https://openairdocs.org/sdr/CALA0400194), Mar 1, 2004: RIB. CRACKED. INSPECTION FOUND TWO LT HORIZONTAL STABILIZER L/E RIBS CRACKED AT DENTED AREA 72 INCHES TO 78 INCHES FROM I/B. THE CRACKS WERE 1 INCH LONG. THE RIBS WERE REMOVE - [SDR CALA0400190](https://openairdocs.org/sdr/CALA0400190), Feb 29, 2004: SKIN. PUNCTURED. INSPECTION FOUND LT HORIZONTAL STABILIZER LOWER TRAILING EDGE SKIN PANEL PUNCTURED JUST OUTBOARD OF ELEVATOR, BL 215.28. THE PANEL WAS REPAIRED IAW SRM 51-70-05 - [SDR CALA0300726](https://openairdocs.org/sdr/CALA0300726), Dec 31, 2003: SKIN. CRACKED. A 3 INCH CRACK WAS FOUND IN LT FUSELAGE SKIN AT STA 727D, S23L DURING A WALKAROUND INSPECTION. THE SKIN WAS REPAIRED IAW ECRA 5330-03090. - [SDR CALA0300401](https://openairdocs.org/sdr/CALA0300401), Jul 21, 2003: BATTERY PACK. INOPERATIVE. THE EMERGENCY EXIT LIGHTS AT ROWS 21-25 AND THE LEFT, CENTER, AND RIGHT AFT EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REMOVED AND REPLACED M9101 EMERGENCY LIGHT - [SDR CALA0300258](https://openairdocs.org/sdr/CALA0300258), May 20, 2003: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 1 I/B PYLON SKIN AT FORWARD UPPER CORNER OF PANEL 5724. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW - [SDR CALA0300257](https://openairdocs.org/sdr/CALA0300257), May 20, 2003: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON UPPER SURFACE PANEL 5727L CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230. - [SDR CALA0200313](https://openairdocs.org/sdr/CALA0200313), May 22, 2002: SKIN. CRACKED. SKIN CRACK AT EXHAUST COOLING FAN OUTLET 6 OCLOCK POSITION. INSTALLED REPAIR DOUBLER PER EC/RA 5330-02894. - [SDR CALA0100240](https://openairdocs.org/sdr/CALA0100240), Mar 21, 2001: BELTFRAME. CRACKED. INSPECTION FOUND A 1.125 INCH CRACK IN BELTFRAME LOWER SECTION AT STA 807, S28R. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-07, FIGURE 201. - [SDR CALA0100233](https://openairdocs.org/sdr/CALA0100233), Mar 16, 2001: STIFFENER. CORRODED. INSPECTION FOUND FORWARD FACE LOWER RADIAL STIFFENER CORRODED AT AFT PRESSURE BULKHEAD. THE STIFFENER WAS REMOVED AND REPLACED. - [SDR CALA0100232](https://openairdocs.org/sdr/CALA0100232), Mar 16, 2001: SKIN. CORRODED. INSPECTION FOUND SKIN CORRODED AT AFT PRESSURE BULKHEAD BETWEEN STRINGER 29L AND 29R. THE CORRODED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED. - [SDR CALA0100229](https://openairdocs.org/sdr/CALA0100229), Mar 14, 2001: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L AND 16R AT STA 500C. STRINGER REPAIRS WERE INSTALLED. - [SDR CALA0100228](https://openairdocs.org/sdr/CALA0100228), Mar 14, 2001: PAN. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO DOOR PAN AT LOWER FORWARD STOP AND AFT LOWER PAN WAS GOUGED. THE FORWARD LOWER AND AFT LOWER DOOR PANS WERE REP - [SDR CALA0100227](https://openairdocs.org/sdr/CALA0100227), Mar 14, 2001: STRUCTURE. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LOWER T-CHORD OF C-1 DOOR. THE T-CHORD WAS REPLACED IAW SRM 51-30-2. - [SDR CALA0100226](https://openairdocs.org/sdr/CALA0100226), Mar 14, 2001: WEB. CRACKED. INSPECTION FOUND A 3 INCHES CRACK IN C-1 DOOR WEB INSIDE FORWARD OF LOWER AFT DOOR STOP. A NEW DOOR WEB WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0100221](https://openairdocs.org/sdr/CALA0100221), Mar 12, 2001: PANEL. CORRODED. INSPECTION FOUND AFT CARGO RIGHT TRANSITION PANEL CORRODED FROM STA 727-747. THE TRANSITION PANEL WAS REPLACED. - [SDR CALA0100220](https://openairdocs.org/sdr/CALA0100220), Mar 12, 2001: STRAP. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN CARGO DOOR JAMB METAL STRAP CORRODED ALONG SCREW HOLES AT LOWER JAMB AREA BETWEEN BS 787-867, S25R. THE STRAP WAS REMOVED AND A - [SDR CALA0100216](https://openairdocs.org/sdr/CALA0100216), Mar 11, 2001: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED IN AFT BAGGAGE BIN AT STA 847 - 867, S25R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-40-02. - [SDR CALA0100206](https://openairdocs.org/sdr/CALA0100206), Mar 5, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LAV WALL LOWER FLOOR SUPPORT CORRODED AT STA 990, RBL 16-45. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0100202](https://openairdocs.org/sdr/CALA0100202), Mar 3, 2001: ANGLE. CORRODED. INSPECTION FOUND LT SIDE Z-ANGLE CORRODED AT STA 312 - 360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9901062](https://openairdocs.org/sdr/CALA9901062), Aug 15, 1999: FIRELOOP. SHORTED. THE APU FIRE DETECT LIGHT ILLUMINATED WHILE ON CLIMBOUT OF EWR. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTINGUISHED. THE APU FIRE LIGHT CAME BACK ON A - [SDR CALA9900694](https://openairdocs.org/sdr/CALA9900694), Jun 15, 1999: FIRE LOOP. MALFUNCTIONED. THE APU FIRE DETECTION LIGHT ILLUMINATED AT FL 350 WHILE EN ROUTE FROM IAH TO SEA. EMERGENCY PROCEDURES WERE FOLLOWED AND THE FIRE BOTTLE WAS DISCHARGED. THE AI - [SDR CALA9800673](https://openairdocs.org/sdr/CALA9800673), Apr 18, 1998: SENSOR. OUT OF ADJUST. THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. WHEN OFF POSITION WAS SELECTED, BOTH RED AND GREEN LIGHTS WERE ILLUMINATED. - [SDR CALA9700471](https://openairdocs.org/sdr/CALA9700471), Mar 22, 1997: BEAM. CORRODED. INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT STA 328 FROM RBL 20 TO RIGHT OUTBOARD WALL. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53- - [SDR CALA9700470](https://openairdocs.org/sdr/CALA9700470), Mar 22, 1997: SUPPORT. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT STA 328-344, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW ECRA 5310-03447. - [SDR CALA9700469](https://openairdocs.org/sdr/CALA9700469), Mar 22, 1997: TEE FITTING. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT T-FITTING CORRODED BETWEEN STA 303 AND 312 AT RBL 25. THE T-FITTING WAS REMOVED AND REPLACED IAW ECRA 5310-03447. - [SDR CALA9700468](https://openairdocs.org/sdr/CALA9700468), Mar 22, 1997: TEE FITTING. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT T-FITTING CORRODED AT STA 312-328, RBL 24. THE T-FITTING WAS REMOVED AND REPLACED IAW ECRA 5310-03447. - [SDR CALA9700466](https://openairdocs.org/sdr/CALA9700466), Mar 21, 1997: EXTRUSION. CORRODED. INSPECTION FOUND FLOOR EXTRUSION CORRODED AT STA 967-986.5, LBL 16. THE AREA WAS REPAIRED IAW SRM 51-10-02. - [SDR CALA9700474](https://openairdocs.org/sdr/CALA9700474), Mar 20, 1997: ANGLE. CORRODED. INSPECTION FOUND R-1 DOOR THRESHOLD SUPPORT ANGLE CORRODED. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-2. - [SDR CALA9700472](https://openairdocs.org/sdr/CALA9700472), Mar 17, 1997: SUPPORT. CORRODED. INSPECTION FOUND CENTER FLOOR LEFT SIDE SUPPORT CORRODED AT STA 727-847 ABOVE STRINGER 25L. THE CORROSION WAS BURNISHED OFF FROM STA 747-847. THE SECTION FROM S - [SDR CALA9700467](https://openairdocs.org/sdr/CALA9700467), Mar 16, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 950 RBL 24 TO RBL 48 AND LBL 12 TO LBL 50. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-02 AND ECRA 5310-03447. - [SDR CALA9700465](https://openairdocs.org/sdr/CALA9700465), Mar 16, 1997: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED FROM BS 947 TO 967, RBL 15 AND LBL 15. THE AREAS WERE REPAIRED IAW SRM 51-10-2 AND ECRA 5310-03447. All 66: https://openairdocs.org/deregistered/N47332-2009-01-30/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 19980407013839I](https://openairdocs.org/incident/19980407013839I), Apr 7, 1998: Boeing 7373T0 (N47332), Seattle, WA, Minor damage. Narrative: on takeoff roll for this 121 CFR flight from sea to iah the right MLG outboard tire tread separated from the main tire carcass. Flying tread damaged… ## Other aircraft with N47332 - [Registered now](https://openairdocs.org/aircraft/N47332): Boeing 737-8, S/N 67586, built 2024 - [Cancelled 1972-03-31](https://openairdocs.org/deregistered/N47332-1972-03-31): Boeing 707-324C, S/N 19870. Exported to Brazil. Owner: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC) - [Cancelled 1955-11-18](https://openairdocs.org/deregistered/N47332-1955-11-18): Taylorcraft DCO-65, S/N L-4627. Owner: [Campbell Allen & Kenneth Heft](https://openairdocs.org/faa-owner/CAMPBELL%20ALLEN%20%26%20KENNETH%20HEFT) --- 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.