# N17328: 1986 Boeing 737-3TO, registration cancelled 2010-06-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 14, 2010 - Exported to: Mexico - 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: 23458 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 10, 1986 - Certificate issued: May 13, 2010 - Last registry action: May 13, 2010 - Mode S code: A12711 - Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N17328 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17328 - Page: https://openairdocs.org/deregistered/N17328-2010-06-14 From the FAA registry file of October 31, 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 (63, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA2009082400460](https://openairdocs.org/sdr/CALA2009082400460), Aug 19, 2009: POWER SUPPLY. DISCHARGED. AFT GALLEY EMERGENCY EXIT LIGHTS WILL NOT GO OUT. REMOVED AND REPLACED AFT GALLEY LEFT EMERGENCY EXIT POWER SUPPLY PER MM 33-51-51. OPS CHECKS GOOD. - [SDR CALA2009080400429](https://openairdocs.org/sdr/CALA2009080400429), Aug 4, 2009: SWITCH. OUT OF POSITION. IN FLIGHT THE AFT CENTER AND R2 EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY. FOUND AFT FLIGHT ATTENDANT TEST SWITCH NOT FULLY SECURED IN THE OFF POSITION. SECU - [SDR CALA2009062300323](https://openairdocs.org/sdr/CALA2009062300323), Jun 21, 2009: RECTIFIER. UNSERVICEABLE. ON FINAL APPROACH, LOST T/R'S NR 2 AND 3. REMOVED AND REPLACED 2 T/R UNIT IAW AMM 24-21-31. TESTED NR 2 AND NR 3 T/R UNITS IAW AMM 24-21-31. OPS CKS NORMAL. ROT - [SDR CALA2009040900188](https://openairdocs.org/sdr/CALA2009040900188), Apr 9, 2009: PROXIMITY SENSOR. INOPERATIVE. ON GEAR RETRACTION UNSAFE INDICATION ON RIGHT MAIN GEAR IN UP POSITION. QRH CHECK LIST COMPLETED AND RETURNED TO IAH. REMOVED AND REPLACED RT MAIN LANDING GEAR - [SDR CALA2009012800066](https://openairdocs.org/sdr/CALA2009012800066), Jan 27, 2009: SKIN. CRACKED. CRACK IN FUSELAGE APPROXIMATELY 1.5 IN LONG, LOCATED AT APPROXIMATELY STATION 727, BELOW STRINGER 18R. INSTALLED REPAIR DOUBLER PER SRM 53-0001, REPAIR 31, DETA - [SDR CALA0800017](https://openairdocs.org/sdr/CALA0800017), Jan 10, 2008: CLAMP. LOOSE. AT FL340 APPROX 70 MILES SOUTH OF DFW GOT CABIN WARNING HORN, SAW CABIN AT 10,500 WENT TO STBY NO HELP. EMERGENCY DESCENT TO LANDING IN DFW DUE TIME CONSTRAINTS - [SDR CALA0700520](https://openairdocs.org/sdr/CALA0700520), Sep 14, 2007: SKIN. CRACKED. INSPECTION FOUND A 0.3 INCH CRACK IN AFT CARGO DOOR SKIN AT LIGHTENING HOLE 7.5 INCHES FROM THE FORWARD EDGE OF THE DOOR AND 21.5 INCHES FROM UPPER EDGE OF THE - [SDR CALA0700519](https://openairdocs.org/sdr/CALA0700519), Sep 14, 2007: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR INNER SKIN AROUND LIGHTENING HOLE LIP 13.5 INCHES FROM THE LOWER EDGE OF DOOR AND 4.5 INCHES FROM THE FORWARD EDGE - [SDR CALA0700518](https://openairdocs.org/sdr/CALA0700518), Sep 14, 2007: SKIN. CRACKED. INSPECTION FOUND A 0.2 INCH CRACK IN FUSELAGE SKIN TO FRAME SHEAR TIE AT STA 727, S14L. REPAIRED IAW ECRA 5310-04656. - [SDR CALA0700515](https://openairdocs.org/sdr/CALA0700515), Sep 12, 2007: STRINGER SPLICE. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN STRINGER SPLICE AT STA 360, S15L. THE STRINGER SPLICE WAS REPAIRED IAW ECRA 5311-01356. - [SDR CALA0700514](https://openairdocs.org/sdr/CALA0700514), Sep 12, 2007: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 294, 12L. THE INTERCOSTAL WAS REPLACED IAW ECRA 5311-01356. - [SDR CALA0700509](https://openairdocs.org/sdr/CALA0700509), Sep 8, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25L CORRODED AT STA 986.5. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, FIGURE 201, PAGE 206. - [SDR CALA0700508](https://openairdocs.org/sdr/CALA0700508), Sep 8, 2007: SKIN. CORRODED. INSPECTION FOUND INNER SKIN CORRODED AT STA 970-990 UNDER S25L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 201, PAGE 235, DETAIL XIII. - [SDR CALA0700505](https://openairdocs.org/sdr/CALA0700505), Sep 7, 2007: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF R-1 DOOR CUTOUT, STA 328-344, S16R TO S17R. THE SKIN WAS REPAIRED IAW SRM 53-10-01. - [SDR CALA0700501](https://openairdocs.org/sdr/CALA0700501), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 847, S9L. REPAIRED IAW ECRA 5310-04651. - [SDR CALA0700500](https://openairdocs.org/sdr/CALA0700500), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 807, S9R. REPAIRED IAW ECRA 5310-04651. - [SDR CALA0700499](https://openairdocs.org/sdr/CALA0700499), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 500A BETWEEN STRINGERS 8 & 9R. REPAIRED IAW ECRA 5310-04651. - [SDR CALA0700498](https://openairdocs.org/sdr/CALA0700498), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 480 BETWEEN STRINGERS 8 AND 9L. REPAIRED IAW ECRA 5310-04651. - [SDR CALA0700497](https://openairdocs.org/sdr/CALA0700497), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 807, S9L. REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700496](https://openairdocs.org/sdr/CALA0700496), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 907, S9L. REPAIRED IAW ECRA 5310-04651. - [SDR CALA0700495](https://openairdocs.org/sdr/CALA0700495), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 867, S9L. A REPAIR WAS INSTALLED IAW ECRA 5310-04651. - [SDR CALA0700494](https://openairdocs.org/sdr/CALA0700494), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 827, S9L. REPAIR ANGLES WERE INSTALLED IAW ECRA 5310-04651. - [SDR CALA0700493](https://openairdocs.org/sdr/CALA0700493), Sep 2, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 480 BETWEEN STRINGERS 8 AND 9R. A REPAIR WAS INSTALLED IAW ECRA 5310-04651. - [SDR CALA0700486](https://openairdocs.org/sdr/CALA0700486), Sep 2, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT STA 1016, RBL 6 TO RBL 20. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851. - [SDR CALA0700480](https://openairdocs.org/sdr/CALA0700480), Aug 30, 2007: SEAT TRACK. CORRODED. INSPECTION FOUND LT I/B SEAT TRACK CORRODED FROM STA 767-907, LBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. - [SDR CALA0700475](https://openairdocs.org/sdr/CALA0700475), Aug 30, 2007: SEAT TRACK. CORRODED. INSPECTION FOUND LT O/B SEAT TRACK CORRODED FROM STA 767-907, LBL 45. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, PAGE 201. - [SDR CALA0700460](https://openairdocs.org/sdr/CALA0700460), Aug 28, 2007: SEAT TRACK. CORRODED. INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT STA 480-540, RBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-00. - [SDR CALA0700221](https://openairdocs.org/sdr/CALA0700221), Apr 22, 2007: SKIN. CRACKED. INSPECTION FOUND A 2.125" CRACK IN LT FUSELAGE SKIN AT STA 727E, S24L, AFT OF EMERGENCY LIGHT. REPAIRED IAW SRM 53-00-01, REPAIR 31. - [SDR CALA0400651](https://openairdocs.org/sdr/CALA0400651), Sep 29, 2004: BEARING. WORN. THE HORIZONTAL STABILIZER TRIM STARTED GRINDING ON APPROACH TO MSP WITH THE AUTOPILOT ENGAGED. THE AUTOPILOT WAS TURNED OFF AND THE YOKE SWITCHES WERE ACTUATED. - [SDR CALA0300576](https://openairdocs.org/sdr/CALA0300576), Oct 3, 2003: SKIN. DAMAGED. THE FORWARD CARGO DOOR INNER SKIN WAS FOUND WITH THREE EXISTING REPAIRS AND ADDITIONAL DAMAGE TO THE INNER SKIN WHILE AIRCRAFT WAS IN 4C CHECK AT HOU. THE THREE - [SDR CALA0300564](https://openairdocs.org/sdr/CALA0300564), Sep 26, 2003: GATE. CORRODED. INSPECTION FOUND CORROSION ON INTERIOR OF R-1 DOOR LOWER GATE. THE GATE WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. - [SDR CALA0300563](https://openairdocs.org/sdr/CALA0300563), Sep 26, 2003: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN UPPER HINGE SKIN CUTOUT ON R-1 DOOR. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW ECRA 5241-01013. - [SDR CALA0300559](https://openairdocs.org/sdr/CALA0300559), Sep 25, 2003: STRAP. CORRODED. INSPECTION FOUND STRESS WEB UPPER STRAP CORRODED AT STA 1028, RBL 18. THE CORRODED STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02 - [SDR CALA0300558](https://openairdocs.org/sdr/CALA0300558), Sep 25, 2003: STRAP. CORRODED. INSPECTION FOUND STRESS WEB UPPER STRAP CORRODED AT STA 1006-1022, RBL 28. THE CORRODED STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02 AND 51- - [SDR CALA0300557](https://openairdocs.org/sdr/CALA0300557), Sep 25, 2003: PAN. CORRODED. INSPECTION FOUND RT AFT LAV PAN CORRODED AT STA 1028, RBL 18. A NEW LAV PAN WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. - [SDR CALA0300556](https://openairdocs.org/sdr/CALA0300556), Sep 25, 2003: PAN. CORRODED. INSPECTION FOUND CORROSION ON LT AFT LAV FLOOR PAN AT DUMP CHUTE, STA 1006, LBL 10. A NEW LAV PAN WAS INSTALLED IAW SRM 51-20-07 AND 51-10-02. - [SDR CALA0300555](https://openairdocs.org/sdr/CALA0300555), Sep 25, 2003: SKIN. DENTED. INSPECTION FOUND TWO DENTS IN AFT FUSELAGE SKIN FROM STA 934-943 BETWEEN S23L AND S24L. A REPAIR WAS INSTALLED IAW SRM 53-00-01. - [SDR CALA0300554](https://openairdocs.org/sdr/CALA0300554), Sep 23, 2003: SUPPORT. CORRODED. INSPECTION FOUND RT AFT LAV WALL SUPPORT CORRODED AT STA 994, RBL 14 TO RBL 38. THE SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-10-02 AND 51-40-0 - [SDR CALA0300553](https://openairdocs.org/sdr/CALA0300553), Sep 23, 2003: PAN. CORRODED. INSPECTION FOUND RT AFT LAV FLOOR PAN CORRODED AT SERVICE WATER FITTING. THE PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. - [SDR CALA0300550](https://openairdocs.org/sdr/CALA0300550), Sep 21, 2003: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A .2500 INCH CRACK IN FLOOR SUPPORT ANGLE AT STA 500D-520, BL 0. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0300549](https://openairdocs.org/sdr/CALA0300549), Sep 21, 2003: STIFFENER. CORRODED. INSPECTION FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED BELOW FLOOR ON LEFT HAND SIDE AT BL 0. REPAIRED STIFFENER IAW SRM 53-80-08 AND DRAWING PL NR 65C28106. - [SDR CALA0300547](https://openairdocs.org/sdr/CALA0300547), Sep 21, 2003: ANGLE. CORRODED. INSPECTION FOUND ZEE ANGLE CORRODED AROUND FASTENER AT L-2 DOOR, STA 947-986. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0300545](https://openairdocs.org/sdr/CALA0300545), Sep 20, 2003: FRAME. CORRODED. INSPECTION FOUND BELTFRAME CORRODED AT STA 500, S28R TO S28L. A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07. - [SDR CALA0300544](https://openairdocs.org/sdr/CALA0300544), Sep 20, 2003: FRAME. CRACKED. INSPECTION FOUND A .7500 INCH CRACK IN LT FRAME AT STA 616 JUST BELOW MAIN DECK FLOOR. A REPAIR WAS INSTALLED IAW ECRA 5311-01158. - [SDR CALA0300543](https://openairdocs.org/sdr/CALA0300543), Sep 20, 2003: GATE. CORRODED. INSPECTION FOUND R-1 DOOR UPPER GATE CORRODED. THE UPPER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0300540](https://openairdocs.org/sdr/CALA0300540), Sep 19, 2003: SKIN. WORN. INSPECTION FOUND FUSELAGE SKIN WORN TO BARE METAL BELOW FORWARD END OF DORSAL FIN AT STA 867-907. THE WORN AREA OF SKIN WAS REMOVED AND FILLER AND DOUBLER WERE - [SDR CALA0300538](https://openairdocs.org/sdr/CALA0300538), Sep 19, 2003: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 328-360, RBL 22. A SEAT TRACK REPAIR SECTION WAS INSTALLED IAW SRM 53-00-52. - [SDR CALA0300533](https://openairdocs.org/sdr/CALA0300533), Sep 17, 2003: INTERCOSTAL. CRACKED. INSPECTION FOUND AN 8 INCH CRACK IN INTERCOSTAL AT STA 380-400, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200003](https://openairdocs.org/sdr/CALA0200003), Jan 5, 2002: SKIN. CRACKED. INSPECTION FOUND A 1/2" CRACK IN FORWARD BAG BIN DOOR CUTOUT BETWEEN STRINGERS 24-25. REPAIRED IAW ECRA 5310-04013. - [SDR CALA0000108](https://openairdocs.org/sdr/CALA0000108), Jan 30, 2000: CIRCUIT BREAKER. TRIPPED. BOTH MLG GREEN INDICATION LIGHTS DID NOT ILLUMINATE WHEN LG WAS EXTENDED ON APPROACH. THE AIR/GROUND RELAY AND LIGHTS CB WAS FOUND TRIPPED DURING GO-AROUND. THE All 63: https://openairdocs.org/deregistered/N17328-2010-06-14/reports.md ## FAA accident and incident reports (3) 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 20080109000289I](https://openairdocs.org/incident/20080109000289I), Jan 9, 2008: Boeing 7373TO (N17328), TX, No damage. (-23) At FL340, 70 miles southwest of dfw, cabin altitude warning horn sounded (10,500 ft)- went to stby system - no help - O2 masks did not deploy - emerg.… - [Incident 19940722031469I](https://openairdocs.org/incident/19940722031469I), Jul 22, 1994: Boeing 737300 (N17328), Houston, TX, Minor damage. Narrative: on July 22, 1994, a Continental airlines, Boeing 737-300, flight 1607, departed atl enroute to iah at approximately 0930 am EST. During flight,… - [Incident 19911119055429I](https://openairdocs.org/incident/19911119055429I), Nov 19, 1991: Boeing 7373T0 (N17328), Kansas City, MO. Gear unsafe light on approach. Reset circuit breaker. Indications. Indications normal. Landed without incident. ## Other aircraft with N17328 - [Registered now](https://openairdocs.org/aircraft/N17328): Boeing 737-8, S/N 67583, built 2023 - [Cancelled 1937-05-03](https://openairdocs.org/deregistered/N17328-1937-05-03): Vultee V-11, S/N 32. Exported to Russia. Owner: [Carp Export & Import Corp](https://openairdocs.org/faa-owner/CARP%20EXPORT%20%26%20IMPORT%20CORP), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) --- 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.