# N14325: 1986 Boeing 737-3TO, registration cancelled 2013-03-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 21, 2013 - Status when cancelled: Third renewal notice - 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: 23455 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 16, 1986 - Certificate issued: May 21, 2008 - Last registry action: May 21, 2008 - Mode S code: A0B091 - Owner when cancelled: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC) - Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston) - Owner type: Corporation - Owner's area on the map: 29.7568° N, 95.3657° W: Placed by OpenAirDocs at the center of ZIP code 77002, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14325 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14325 - Page: https://openairdocs.org/deregistered/N14325-2013-03-21 From the FAA registry file of November 5, 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 CALA0800843](https://openairdocs.org/sdr/CALA0800843), Aug 31, 2008: WIRE. PINCHED. EMERGENCY PATH LIGHTING AT ROW 24 FOUND WIRE PINCHED BETWEEN SEAT TRACK COVER AND TRACK. REMOVED AND REPLACED SEAT HARNESS EMERGENCY SEAT LIGHTS ROW 24. ALL LIG - [SDR CALA0700596](https://openairdocs.org/sdr/CALA0700596), Oct 19, 2007: SERVICE PANEL. CORRODED. INSPECTION FOUND CORROSION AND 3 POPPED RIVETS AT FORWARD EDGE OF LAV SERVICE PANEL, STA 986.5, RBL 25. A REPAIR WAS INSTALLED IAW ECRA 5331-01355. - [SDR CALA0700586](https://openairdocs.org/sdr/CALA0700586), Oct 15, 2007: SKIN. CORRODED. FWD CARGO FUSELAGE SKIN HAS CORROSION AT STA 500C+18 LBL-17. SKIN REPAIR PER SRM 53-00-01 REPAIR 31 FIG 201. - [SDR CALA0700584](https://openairdocs.org/sdr/CALA0700584), Oct 15, 2007: STRINGER. CORRODED. AFT BAG BIN STA 867 STRINGER 26 RT HAS CORROSION. INSTALLED REPAIR PER SRM 53-00-03 FIG 201. - [SDR CALA0700585](https://openairdocs.org/sdr/CALA0700585), Oct 14, 2007: STRINGER. CORRODED. FWD CARGO STA 500C S26L CORROSION. INSTALLED REPAIR AT S26L STA 500C IN FWD CARGO IAW SRM 53-00-03 REPAIR 1. - [SDR CALA0700581](https://openairdocs.org/sdr/CALA0700581), Oct 12, 2007: FRAME. CORRODED. STA 227 LBL 5 TO RBL 5 FRAME CORRODED. REPAIR ACCOMP PER ECRA 5311-01366. - [SDR CALA0700580](https://openairdocs.org/sdr/CALA0700580), Oct 12, 2007: BRACKET. CRACKED. ANGLE BRACKET CRACKED STA 348-351 STR 16L. REMOVED & REPLACED BRACKET PER ECRA 5311-01364. - [SDR CALA0700579](https://openairdocs.org/sdr/CALA0700579), Oct 12, 2007: BRACKET. CRACKED. ANGLE BRACKET CRACKED STA 351 STR 16L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01364. - [SDR CALA0700578](https://openairdocs.org/sdr/CALA0700578), Oct 12, 2007: ANGLE. CRACKED. ANGLE CRACKED STA 348-350 STR 16L. REMOVED & REPLACED ANGLE PER ECRA 5311-01364. - [SDR CALA0700577](https://openairdocs.org/sdr/CALA0700577), Oct 12, 2007: SKIN. CRACKED. NR 1 ENG PYLON CRACKED AT ACCESS PANEL 5727. INSTALLED DOUBLER PER ECRA 5430-01230. - [SDR 0700573](https://openairdocs.org/sdr/0700573), Oct 10, 2007: DOOR FRAME. CRACKED. C-1 DOOR CUTOUT FED FRAME CRACKED AT LWR STOP PAD MOUNT. REMOVED AND REPLACED PER SRM 51-40-02. - [SDR 0700572](https://openairdocs.org/sdr/0700572), Oct 10, 2007: STRINGER. CORRODED. FWD CARGO STRINGER 27L HAS CORROSION ON IT AT STA 500C+18 LBL. REPAIRED STRINGER PER SRM 53-00-03. - [SDR 0700571](https://openairdocs.org/sdr/0700571), Oct 10, 2007: FRAME. CRACKED. FWD CARGO LWR FRAME HAS CORROSION ON FED SIDE AT STA 500D LBL 16 TO LBL 21. REPLACED FWD CARGO LWR FRAME PER SRM 53-00-07. - [SDR 0700569](https://openairdocs.org/sdr/0700569), Oct 9, 2007: DOOR FRAME. CRACKED. C-2 DOOR CUTOUT FWD FRAME HAS CRACK. REPLACED FWD FRAME PER SRM 51-40-02 BOEING DRAWING 65-47959. - [SDR 0700568](https://openairdocs.org/sdr/0700568), Oct 8, 2007: FRAME. CRACKED. UPPER FRAME SECTION STA 440 STR 17R-14R HAS CRACK AT FASTENER HOLE. REPLACED UPPER FRAME AT STA 440 IAW SRM 51-40-02. - [SDR CALA0700562](https://openairdocs.org/sdr/CALA0700562), Oct 3, 2007: SHEAR TIE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LEFT FRAME SHEAR TIE AT STA 500D BETWEEN STRINGERS 10L AND 11L. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS INSTALLED - [SDR CALA0700488](https://openairdocs.org/sdr/CALA0700488), Sep 2, 2007: CHARGER. INOPERATIVE. INSPECTION FOUND THE LAST 4 SEAT MOUNTED EMERGENCY LIGHTS OUT. THREE BATTERY CHARGERS IN THE AFT GALLEY WERE REMOVED AND REPLACED IAW AMM 33-51-51. THE EMERGENC - [SDR CALA0700272](https://openairdocs.org/sdr/CALA0700272), May 27, 2007: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN RT FUSELAGE SKIN AT STA 727D-727E, S22R-24R, AT AFT EMERGENCY LIGHT. THE SKIN WAS REPAIRED IAW ECRA 5330-03682. - [SDR CALA0700260](https://openairdocs.org/sdr/CALA0700260), May 24, 2007: SIGN. INOPERATIVE. THE RIGHT OVERWING ESCAPE DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED IAW REFERENCE TO SWP 20-13-12 AND BRUCE WDM 33- - [SDR CALA0600289](https://openairdocs.org/sdr/CALA0600289), Aug 1, 2006: SKIN. CRACKED. INSPECTION FOUND A 3" CRACK IN FUSELAGE SKIN BELOW EMERGENCY LIGHT AT STA 727D-727E, S22L TO S24L. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03560 AND A DIP - [SDR CALA0600092](https://openairdocs.org/sdr/CALA0600092), Mar 20, 2006: SKIN. CRACKED. INSPECTION FOUND A 3.375 INCH CRACK IN FUSELAGE SKIN AFT OF AFT CARGO DOOR AT STA 867, S23R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, DETAIL X, FIGURE 2 - [SDR CALA0500378](https://openairdocs.org/sdr/CALA0500378), Oct 28, 2005: ACTUATOR. INOPERATIVE. WHEN THE GEAR HANDLE WAS PLACED DOWN ON FINAL APPROACH, THE NLG DID NOT EXTEND. THE CHECKLIST WAS RUN AND THE GEAR WAS EXTENDED MANUALLY WITH THREE GREEN LIGHTS - [SDR CALA0500336](https://openairdocs.org/sdr/CALA0500336), Oct 7, 2005: SKIN. CRACKED. CRACK IN FUSELAGE SKIN AT STA 727E, STRINGER 18, 2.5 IN. REPAIRED CRACK PER SRM 53-00-01, FIG 201. - [SDR CALA0500183](https://openairdocs.org/sdr/CALA0500183), Jun 2, 2005: DOOR FRAME. CORRODED. INSPECTION FOUND SKIN BULGED AND RIVET HEADS STRESSED AT STA 360 AND S28L. THE E&E DOOR CUTOUT BEAM LOWER T-CHORD WAS FOUND CORRODED. THE T-CHORD WAS REPAIRED I - [SDR CALA0500180](https://openairdocs.org/sdr/CALA0500180), Jun 2, 2005: SKIN. CRACKED. INSPECTION FOUND A 1.75 INCH CRACK IN C-1 DOOR INNER SKIN AT CENTER LIGHTENING HOLES. A DOUBLER WAS INSTALLED IAW ECRA 5232-01063. - [SDR CALA0500182](https://openairdocs.org/sdr/CALA0500182), May 27, 2005: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR OUTER SKIN. THE CRACK WAS LOCATED AT THE AFT UPPER CORNER OF C-2 DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED - [SDR CALA0500170](https://openairdocs.org/sdr/CALA0500170), May 26, 2005: DOOR FRAME. CORRODED. INSPECTION FOUND THE AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME CORRODED ON I/B SIDE AT STA 794, L26R TO L27R. THE CORRODED AREA WAS CUT OUT AND DOUBLER AN - [SDR CALA0500162](https://openairdocs.org/sdr/CALA0500162), May 23, 2005: DOOR FRAME. CORRODED. INSPECTION FOUND THE R-2 AFT DOOR FRAME CORRODED AT STA 996, RBL 48. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11. - [SDR CALA0500161](https://openairdocs.org/sdr/CALA0500161), May 23, 2005: GATE. CORRODED. INSPECTION FOUND THE R-2 DOOR LOWER GATE CORRODED ON INTERIOR AND EXTERIOR SURFACE. THE LOWER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0500158](https://openairdocs.org/sdr/CALA0500158), May 22, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 48 TO RBL 48. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA0400060](https://openairdocs.org/sdr/CALA0400060), Jan 25, 2004: SKIN. GOUGED. INSPECTION FOUND LT WING LEADING EDGE SKIN GOUGED AT CENTER AUX TRACK ICE DOOR CUTOUT (UNDER NR 1 SLAT). REPAIRED IAW SRM 51-70-16. - [SDR CALA0400055](https://openairdocs.org/sdr/CALA0400055), Jan 23, 2004: SKIN. CRACKED. INSPECTION FOUND FIVE 1 INCH CRACKS IN NR 5 SLAT SKIN LOWER SURFACE I/B OF AUX TRACK. A DOUBLER WAS INSTALLED IAW SRM 57-43-01. - [SDR CALA0400050](https://openairdocs.org/sdr/CALA0400050), Jan 21, 2004: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, RBL 2 AND AT LBL 2. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0300548](https://openairdocs.org/sdr/CALA0300548), Sep 21, 2003: BULKHEAD. CORRODED. INSPECTION FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT STA 1016 JUST LEFT OF BL 0. REPAIRED WEB IAW SRM 53-80-08 AND BOEING DRAWING 65C28106. - [SDR CALA0100760](https://openairdocs.org/sdr/CALA0100760), Aug 13, 2001: SKIN. DENTED. INSPECTION FOUND THREE DENTS IN C-2 DOOR SKIN AT TEN INCHES FROM AFT SIDE AND FROM FIVE INCHES ABOVE PAINT LINE TO THIRTEEN INCHES ABOVE PAINT LINE. THE DENTED - [SDR CALA0100748](https://openairdocs.org/sdr/CALA0100748), Aug 8, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN CENTER FLOOR SUPPORT CORRODED AT STA 727D, RBL 18. A NEW SUPPORT AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-20-01. - [SDR CALA0100732](https://openairdocs.org/sdr/CALA0100732), Aug 2, 2001: SPLICE. CRACKED. INSPECTION FOUND STRINGER 4L SPLICE CRACKED AT STA 907. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 203. - [SDR CALA0100729](https://openairdocs.org/sdr/CALA0100729), Jul 31, 2001: WEB. CRACKED. INSPECTION FOUND A 1/4" CRACK IN STRESS WEB AT FLOORBEAM ATTACH POINT, STA 312, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100727](https://openairdocs.org/sdr/CALA0100727), Jul 30, 2001: SKIN. GOUGED. INSPECTION FOUND FUSELAGE SKIN GOUGED AT FORWARD END ON DORSAL FIN MOUNT AREA. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01. - [SDR CALA0100726](https://openairdocs.org/sdr/CALA0100726), Jul 30, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-00. - [SDR CALA0100723](https://openairdocs.org/sdr/CALA0100723), Jul 30, 2001: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 944-991.5. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100722](https://openairdocs.org/sdr/CALA0100722), Jul 30, 2001: FITTING. CORRODED. INSPECTION FOUND GALLEY MOUNTS CORRODED AT STA 946.5, LBL 14 AND RBL 8. THE GALLEY MOUNTS WERE REMOVED AND REPLACED IAW SRM 53-10-03. - [SDR CALA0100721](https://openairdocs.org/sdr/CALA0100721), Jul 30, 2001: FITTING. CORRODED. INSPECTION FOUND L-1 DOOR AFT GIRT BAR LATCH MOUNT CORRODED. THE GIRT BAR LATCH MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-00. - [SDR CALA0100720](https://openairdocs.org/sdr/CALA0100720), Jul 30, 2001: ANGLE. CRACKED. INSPECTION FOUND A 1INCH CRACK IN WEB ANGLE AT STA 927-947.5, BL 0. THE WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100719](https://openairdocs.org/sdr/CALA0100719), Jul 30, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FASTENER HOLES, STA 294-312, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0100707](https://openairdocs.org/sdr/CALA0100707), Jul 27, 2001: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100706](https://openairdocs.org/sdr/CALA0100706), Jul 27, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 21 TO LBL 35. A CAP WAS INSTALLED ON BEAM IAW ECRA 5310-03851, REV A. - [SDR CALA0100691](https://openairdocs.org/sdr/CALA0100691), Jul 25, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM SECTIONS CORRODED AT STA 967, RBL 17.5 AND AT STA 986.5, RBL 16 TO LBL 46. THE FLOORBEAM SECTIONS WERE REMOVED AND REPLACED IAW ECRA - [SDR CALA0100681](https://openairdocs.org/sdr/CALA0100681), Jul 25, 2001: WEB. CORRODED. INSPECTION FOUND WEB CORRODED AT STA 1020, LBL 23 AND AT STA 1016, RBL 7 - LBL 16. A NEW WEB WAS INSTALLED ON LEFT OF CENTER BBL 0 TO LBL 38 AND A NEW WEB WAS I - [SDR CALA0100680](https://openairdocs.org/sdr/CALA0100680), Jul 25, 2001: SUPPORT. CORRODED. INSPECTION FOUND LT AFT LAV WALL SUPPORT CORRODED AT STA 1013, LBL 5 AND H STRAP CORRODED AT STA 1012, LBL 5, UNDER LAV WALL SUPPORT. THE SUPPORT AND STRAP WERE All 64: https://openairdocs.org/deregistered/N14325-2013-03-21/reports.md ## Other aircraft with N14325 - [Cancelled 1974-09-10](https://openairdocs.org/deregistered/N14325-1974-09-10): Piper PA-18-150, S/N 18-7409085. Exported to Brazil. Owner: [Aero Export International Inc](https://openairdocs.org/faa-owner/AERO%20EXPORT%20INTERNATIONAL%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) --- 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.