# N17326: 1986 Boeing 737-3TO, registration cancelled 2011-05-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 11, 2011 - 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: 23456 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 20, 1986 - Certificate issued: June 13, 2008 - Last registry action: December 15, 2010 - Mode S code: A1270F - 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/N17326 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17326 - Page: https://openairdocs.org/deregistered/N17326-2011-05-11 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md ## Service difficulty reports (68, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0700670](https://openairdocs.org/sdr/CALA0700670), Nov 11, 2007: SKIN. CRACKED. INSPECTION FOUND A 4.7 INCH CRACK IN FUSELAGE SKIN AT EMERGENCY LIGHT, STA 727C TO 727E, S21R TO S24R. THE SKIN WAS REPAIRED IAW ECRA 5331-01362. - [SDR CALA0700522](https://openairdocs.org/sdr/CALA0700522), Sep 16, 2007: SKIN. CORRODED. INSPECTION FOUND SKIN CORRODED AT STA 492 BETWEEN S27R AND S28R. THE SKIN WAS REPAIRED IAW ECRA 5330-03720. - [SDR CALA0700521](https://openairdocs.org/sdr/CALA0700521), Sep 15, 2007: KEELBEAM. CORRODED. INSPECTION FOUND KEEL BEAM CORRODED AT STA 500D, S29R. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, REPAIR NR 3. - [SDR CALA0700511](https://openairdocs.org/sdr/CALA0700511), Sep 10, 2007: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE R-2 DOOR LOWER HINGE CUTOUT AT STA 947.5-967, S14R TO S15R. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS - [SDR CALA0700510](https://openairdocs.org/sdr/CALA0700510), Sep 4, 2007: FRAME. CRACKED. INSPECTION FOUND A 1.2 INCH CRACK IN LOWER SECTION OF LEFT FRAME INNER CHORD AT STA 616, S17L TO S18L. THE FRAME CHORD WAS REPAIRED IAW ECRA 5311-01158. - [SDR CALA0500301](https://openairdocs.org/sdr/CALA0500301), Sep 5, 2005: SKIN. CRACKED. A WALKAROUND FOUND A 4 INCH CRACK IN RT FUSELAGE SKIN AT BS 747, S19R. REPAIRED IAW SRM 53-00-01, FIGURE 229. - [SDR CALA0500137](https://openairdocs.org/sdr/CALA0500137), Apr 8, 2005: SKIN. WORN. INNER SKIN WEAR AT THE AFT EDGE OF THE FORWARD MIDDLE ROW LIGHTNING HOLE OF THE AFT CARGO DOOR. INSTALLED DOUBLER PER ECRA 5232-01059. - [SDR CALA0500099](https://openairdocs.org/sdr/CALA0500099), Apr 8, 2005: BEAM. CORRODED. INSPECTION FOUND TOP AFT MID SECTION OF LT HORIZONTAL STABILIZER CORRODED AT AFT T/E STRAP AROUND SUPPORT RETAINER HOLES AT STAB STA 176.4 ON TOP SIDE OF T/E BE - [SDR CALA0500095](https://openairdocs.org/sdr/CALA0500095), Apr 2, 2005: SUPPORT BRACKET. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK IN ANTENNA SUPPORT BRACKET AT STA 727D + 5 INCH. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0500094](https://openairdocs.org/sdr/CALA0500094), Apr 2, 2005: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 916, LBL 24.75. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00-52. - [SDR CALA0500092](https://openairdocs.org/sdr/CALA0500092), Mar 31, 2005: FLOOR SUPPORT. CORRODED. INSPECTION FOUND G-1 I/B SUPPORT MOUNT BETWEEN FLOORBEAMS CORRODED AROUND SCREW HOLES AT STA 277-294, RBL 14. A NEW SUPPORT MOUNT WAS INSTALLED IAW SRM 51-40-2. - [SDR CALA0400729](https://openairdocs.org/sdr/CALA0400729), Nov 30, 2004: SKIN. CRACKED. INSPECTION FOUND TWO 2 INCH CRACKS IN FUSELAGE SKIN AT BS 727E, S22R AND S23R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. - [SDR CALA0400268](https://openairdocs.org/sdr/CALA0400268), Mar 22, 2004: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN LEFT FUSELAGE SKIN AT STA 727C. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. - [SDR CALA0400233](https://openairdocs.org/sdr/CALA0400233), Mar 10, 2004: CIRCUIT CARD. FAILED. THE LANDING GEAR DID NOT RETRACT INITIALLY AFTER TAKEOFF FROM HAV. QRH WAS FOLLOWED AND LOCK OVERRIDE WAS USED TO RETRACT GEAR. THE FLIGHT WAS CONTINUED TO MIA - [SDR CALA0300441](https://openairdocs.org/sdr/CALA0300441), May 6, 2003: STIFFENER. CORRODED. INSPECTION FOUND AFT PRESSURE BULKHEAD SIDE, TWO EACH CENTER CHANNEL STIFFENERS CORRODED ON BOTH SIDES AT STA 1016. A STIFFENER REPAIR WAS INSTALLED IAW DRAWING - [SDR CALA0100626](https://openairdocs.org/sdr/CALA0100626), Jul 1, 2001: SKIN. GOUGED. INSPECTION FOUND FUSELAGE SKIN BETWEEN FORWARD EQUIPMENT ACCESSORY DOOR AND NOSE GEAR WHEEL WELL GOUGED AT BS 219-227, BL 0. THE SKIN WAS REPAIRED IAW ECRA 5310 - [SDR CALA0100418](https://openairdocs.org/sdr/CALA0100418), Apr 25, 2001: FRAME. CRACKED. CRACK IN FRAME STATION 727 AT S 14L. REPAIRED PER EC/RA 5310-04133. - [SDR CALA0100417](https://openairdocs.org/sdr/CALA0100417), Apr 25, 2001: WEB. CRACKED. CRACK AT LIGHTENING HOLE ON VERTICAL WEB AT LBL 23 APPROX 6 INCHES AFT OF 178 BULKHEAD AND 10 INCHES BELOW COCKPIT FLOOR. REPAIRED PER EC/RA 5320-01671. - [SDR CALA0100400](https://openairdocs.org/sdr/CALA0100400), Apr 21, 2001: SKIN. DAMAGED. LEFT ELEVATOR UPPER SURFACE HAS SMALL DAMAGED AREA (.25 INCH HOLE). INSTALLED COMPOSITE REPAIR PER EC/RA 5523-01025 AND SRM 51-70-17. CALCULATED WEIGHT AND BALA - [SDR CALA0100396](https://openairdocs.org/sdr/CALA0100396), Apr 18, 2001: CHANNEL. CORRODED. INSPECTION FOUND SUPPORT CHANNEL CORRODED AT STA 727A - 727B. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100395](https://openairdocs.org/sdr/CALA0100395), Apr 18, 2001: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED AT STA 747 - 767, RT SIDE. REPLACED INTERCOSTAL IAW SRM 51-40-02. - [SDR CALA0100394](https://openairdocs.org/sdr/CALA0100394), Apr 18, 2001: STRAP. CORRODED. INSPECTION FOUND CORROSION IN LOWER STRAP DOUBLER FORWARD LOWER CORNER CARGO DOOR CUTOUT AT THRESHOLD PLATE AFT CARGO. THE STRAP DOUBLER WAS REMOVED AND REPLACE - [SDR CALA0100393](https://openairdocs.org/sdr/CALA0100393), Apr 18, 2001: WEB. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD WEB CORRODED ON UPPER SURFACE. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100391](https://openairdocs.org/sdr/CALA0100391), Apr 18, 2001: INTERCOSTAL. CRACKED. INSPECTION FOUND INTERCOSTAL CRACKED AT LOWER AFT CORNER OF AFT CARGO DOOR CUTOUT. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0100388](https://openairdocs.org/sdr/CALA0100388), Apr 17, 2001: ANGLE. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN RT SUPPORT Z-ANGLE CORRODED AT STA 727 - 767. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100387](https://openairdocs.org/sdr/CALA0100387), Apr 17, 2001: MOUNT BRACKET. CORRODED. INSPECTION FOUND AFT LEFT LAV FLOOR MOUNT BRACKET CORRODED AT STA 1016, LBL 6. THE FLOOR MOUNT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100361](https://openairdocs.org/sdr/CALA0100361), Apr 13, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 907-947. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204. - [SDR CALA0100321](https://openairdocs.org/sdr/CALA0100321), Apr 9, 2001: WEB. CORRODED. INSPECTION FOUND MAIN DECK SUBFLOOR CORRODED BETWEEN RUBBER SEAL OF APB, STA 1016, RBL 2. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100320](https://openairdocs.org/sdr/CALA0100320), Apr 9, 2001: FITTING. CORRODED. INSPECTION FOUND LT MLG STAB LINK AFT ATTACH FITTING ON GEAR BEAM CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW MM 51-40-04. - [SDR CALA0100319](https://openairdocs.org/sdr/CALA0100319), Apr 9, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1006 - 1016, LBL 4 - 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100318](https://openairdocs.org/sdr/CALA0100318), Apr 9, 2001: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE CORRODED AT R-2 DOOR ENTRY. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100316](https://openairdocs.org/sdr/CALA0100316), Apr 8, 2001: MOUNT. CORRODED. INSPECTION FOUND AFT GALLEY AFT I/B MOUNT CORRODED AT STA 967, LBL 14. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 51-10-02. - [SDR CALA0100315](https://openairdocs.org/sdr/CALA0100315), Apr 8, 2001: WEB. CORRODED. INSPECTION FOUND MAIN DECK SUBFLOOR CORRODED JUST FORWARD OF AFT PRESSURE BULKHEAD AT STA 1010, LBL 4. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100314](https://openairdocs.org/sdr/CALA0100314), Apr 8, 2001: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE CORRODED O/B OF AFT LAV AND GALLEY (L-2 DOOR AREA). THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0100312](https://openairdocs.org/sdr/CALA0100312), Apr 7, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND SCREW HOLES AT STA 967-986.5, LBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND ECRA 5310-0 - [SDR CALA0100311](https://openairdocs.org/sdr/CALA0100311), Apr 7, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT RIGHT LAV FLOOR SUPPORT CORRODED AT STA 1016, RBL 6. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100310](https://openairdocs.org/sdr/CALA0100310), Apr 7, 2001: ANGLE. CRACKED. INSPECTION FOUND A .0625 INCH CRACK AT FASTENER ON UNDER SIDE OF LEFT CREASE BEAM STIFFENER ANGLE AT STA 1000. THE CREASE BEAM STIFFENER ANGLE WAS REMOVED AND R - [SDR CALA0100309](https://openairdocs.org/sdr/CALA0100309), Apr 7, 2001: ATTACH FITTING. CORRODED. INSPECTION FOUND RIGHT MLG STAB LINK AFT ATTACH FITTING ON GEAR BEAM CORRODED. THE ATTACH FITTING WAS REMOVED AND A NEW ATTACH FITTING WAS INSTALLED IAW MM 57-1 - [SDR CALA0100308](https://openairdocs.org/sdr/CALA0100308), Apr 7, 2001: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE O/B LOWER PYLON ANGLE AT NAC STA 278. A DOUBLER WAS INSTALLED ON THE ANGLE IAW SRM 51-40-00. - [SDR CALA0100307](https://openairdocs.org/sdr/CALA0100307), Apr 6, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT RIGHT LAV FLOOR SUPPORTS CORRODED AROUND FASTENER HOLES AT STA 1006-1016, RBL 18 AND RBL 27. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED I - [SDR CALA0100306](https://openairdocs.org/sdr/CALA0100306), Apr 6, 2001: STRAP. CORRODED. INSPECTION FOUND METAL STRAP CORRODED BETWEEN STA 1006 AND APB, LBL 18. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100305](https://openairdocs.org/sdr/CALA0100305), Apr 6, 2001: STRAP. CORRODED. INSPECTION FOUND METAL STRAP CORRODED AT EYEBOLT AREA OF TANK HOLD DOWN ROD AT STA 1016, LBL 27. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100303](https://openairdocs.org/sdr/CALA0100303), Apr 6, 2001: WEB. CORRODED. INSPECTION FOUND LEFT O/B SUBFLOOR CORRODED AT STA 986-1016. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100302](https://openairdocs.org/sdr/CALA0100302), Apr 6, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT SCREW HOLES AT STA 1006-1016, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100301](https://openairdocs.org/sdr/CALA0100301), Apr 6, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 986.5-1006, LBL 10-20 AND AT STA 996-1006, LBL 36. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-40-02 - [SDR CALA0100300](https://openairdocs.org/sdr/CALA0100300), Apr 6, 2001: SUPPORT. CORRODED. INSPECTION FOUND FORWARD LOWER WALL SUPPORT OF AFT LT LAV CORRODED AT STA 996. THE WALL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100296](https://openairdocs.org/sdr/CALA0100296), Apr 6, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND DIAGONAL FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AT STA 986-1016 IN RT AFT LAV AREA. THE DIAGONAL FLOOR SUPPORT WAS REMOVED AND REPLACED I - [SDR CALA0100295](https://openairdocs.org/sdr/CALA0100295), Apr 6, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT RT LAV FLOOR SUPPORT BEAM CORRODED AROUND FASTENER HOLES AT STA 998-1016, RBL 36. THE FLOOR SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 5 - [SDR CALA0100294](https://openairdocs.org/sdr/CALA0100294), Apr 6, 2001: SUPPORT. CORRODED. INSPECTION FOUND AFT RT LAV FORWARD WALL SUPPORT CORRODED AT I/B END. THE WALL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100287](https://openairdocs.org/sdr/CALA0100287), Apr 6, 2001: ATTACH FITTING. CORRODED. INSPECTION FOUND RT UPPER FORWARD HORIZONTAL STABILIZER ATTACH FITTING FWD AND AFT BUSHINGS HAD CORROSION BETWEEN BUSHINGS AND FITTINGS. NEW OVERSIZED BUSHINGS All 68: https://openairdocs.org/deregistered/N17326-2011-05-11/reports.md ## Other aircraft with N17326 - [Registered now](https://openairdocs.org/aircraft/N17326): Boeing 737-8, S/N 67580, built 2023 - [Cancelled 1972-05-09](https://openairdocs.org/deregistered/N17326-1972-05-09): Boeing 707-324C, S/N 19178, built 1966. Exported to China. Owner: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC), [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles) - [Cancelled 1940-02-27](https://openairdocs.org/deregistered/N17326-1940-02-27): Vultee V-1A, S/N 26. Exported to China. Owner: [Intercontinent Corp](https://openairdocs.org/faa-owner/INTERCONTINENT%20CORP), [New York City, NY](https://openairdocs.org/faa-place/NY/New%20York%20City) --- 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.