# N14346: 1987 Boeing 737-3TO, registration cancelled 2013-03-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 21, 2013 - Status when cancelled: Valid registration - Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G) - Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016) - Serial number: 23584 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 15, 1987 - Certificate issued: December 18, 2008 - Last registry action: January 23, 2013 - Mode S code: A0B0D8 - 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/N14346 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14346 - Page: https://openairdocs.org/deregistered/N14346-2013-03-21 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 (51, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0800303](https://openairdocs.org/sdr/CALA0800303), Apr 4, 2008: SKIN. MISREPAIRED. SKIN REPAIR AT STA 420 TO 440 BETWEEN STR 16L TO 20L MISSING FIELD FASTENERS. REMOVED EXISTING DOUBLER, FABRICATED AND INSTALLED NEW REPAIR IN REF TO SRM 53-00- - [SDR CALA0700340](https://openairdocs.org/sdr/CALA0700340), Jul 6, 2007: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN SKIN AT SCREW HOLE, STA 380, S28L TO 28R. REPAIRED IAW ECRA 5330-02894. - [SDR CALA0600133](https://openairdocs.org/sdr/CALA0600133), Apr 14, 2006: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM 967 LBL 5. INSTALLED REPAIR STRAP PER SRM 53-00-51, FIG 201. - [SDR CALA0600118](https://openairdocs.org/sdr/CALA0600118), Apr 10, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25R CORRODED ON SIDE FLANGE AT STA 986 IN AFT BILGE AREA. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, PAGE 201-207, FIGURE 201, DETAIL - [SDR CALA0600108](https://openairdocs.org/sdr/CALA0600108), Apr 8, 2006: SKIN. CRACKED. INSPECTION FOUND A 0.125 INCH CRACK AT FASTENER IN FUSELAGE SKIN JUST AFT OF STA 390, S21R. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5331-01229 AND A DIP WAS IN - [SDR CALA0600103](https://openairdocs.org/sdr/CALA0600103), Apr 3, 2006: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN STRINGER 15R, STA 500+10. A REPAIR WAS INSTALLED IAW SRM 53-00-03. - [SDR CALA0600101](https://openairdocs.org/sdr/CALA0600101), Apr 2, 2006: STRINGER. CRACKED. INSPECTION FOUND .25 INCH CRACKS (4 EACH) AROUND FASTENER HOLES IN STRINGER AT STA 428-486, S16R. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-30-53, FIGURE - [SDR CALA0600099](https://openairdocs.org/sdr/CALA0600099), Mar 29, 2006: KEELBEAM. CORRODED. INSPECTION FOUND LT KEEL BEAM CORRODED IN LT WHEEL WELL AT STA 727, S28L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, FIGURE 101, SHEET 4-13. - [SDR CALA0600111](https://openairdocs.org/sdr/CALA0600111), Mar 27, 2006: FRAME. CORRODED. INSPECTION FOUND CORROSION ON LOWER FRAME OF STA 227.8 BULKHEAD, LBL 6 TO RBL 6. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR IAW ECRA 5311-01252 WITHIN 6,000 - [SDR CALA0600097](https://openairdocs.org/sdr/CALA0600097), Mar 27, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FORWARD CARGO FLOORBEAM FORWARD FACE CORRODED AT STA 500D, LBL 14. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-07, PAGE 203, FIGURE 201. - [SDR CALA0600096](https://openairdocs.org/sdr/CALA0600096), Mar 26, 2006: STRIP. CORRODED. INSPECTION FOUND AFT CARGO FLOOR PANEL MOUNT STRIP UPPER SURFACE CORRODED AT STA 847, RBL 45. THE FLOOR PANEL MOUNT STRIP WAS REMOVED AND REPLACED IAW SRM 51-10 - [SDR CALA0600115](https://openairdocs.org/sdr/CALA0600115), Mar 25, 2006: SUPPORT FITTING. CORRODED. INSPECTION FOUND THE R-1 DOOR FUSELAGE TORQUE TUBE UPPER SUPPORT FITTING CORRODED AT STA 294.5, S10R TO S14R. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW E - [SDR CALA0600112](https://openairdocs.org/sdr/CALA0600112), Mar 25, 2006: FRAME. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN ABB DOOR CUTOUT FORWARD FRAME AT STA 794.3 ALONG UPPER THREE STOP PAD MOUNTS. THE FRAME WAS REPLACED IAW SRM 51-41-02. - [SDR CALA0600091](https://openairdocs.org/sdr/CALA0600091), Mar 20, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 328, RBL 12. THE CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA0600090](https://openairdocs.org/sdr/CALA0600090), Mar 19, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 344, LBL 9. A DOUBLER WAS INSTALLED IAW SRM 53-10-51. - [SDR CALA0600149](https://openairdocs.org/sdr/CALA0600149), Mar 15, 2006: ANGLE. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN THE R1 DOOR UPPER/FORWARD TORQUE BOX ATTACH INTERCOSTAL MOUNT ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AN - [SDR CALA0400595](https://openairdocs.org/sdr/CALA0400595), Aug 11, 2004: CHANNEL. CORRODED. INSPECTION FOUND HAT CHANNEL FOR VHF ANTENNA CORRODED AT STA 727D, BL 0. A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0400578](https://openairdocs.org/sdr/CALA0400578), Jul 16, 2004: BOLT. SHEARED. THE LEFT O/B ELEVATOR HINGE BOLT WAS FOUND MISSING AND SHEARED OFF DURING A WALKAROUND INSPECTION. THE BOLT OR HINGE HARDWARE WAS JAMMED BETWEEN THE STABILIZER - [SDR CALA0300470](https://openairdocs.org/sdr/CALA0300470), Aug 17, 2003: SKIN. BIRD STRIKE. INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN AND RIB AT STA 86.66 DAMAGED DUE TO A BIRD STRIKE. - [SDR CALA0200193](https://openairdocs.org/sdr/CALA0200193), Apr 9, 2002: TRUNNION. CORRODED. INSPECTION FOUND NLG LT AND RT MAIN TRUNNION SUPPORT FITTING BEARING SEATS CORRODED. THE CORROSION WAS REMOVED, THE AREAS WERE REWORKED AND BUSHINGS WERE INSTAL - [SDR CALA0200192](https://openairdocs.org/sdr/CALA0200192), Apr 9, 2002: SPAR. CRACKED. INSPECTION FOUND A .125 INCH CRACK IN RT WING REAR SPAR UPPER CHORD AT MLG BEAM ATTACH FITTING. THE CRACKED AREA WAS REMOVED AND A FREEZE PLUG WAS INSTALLED. - [SDR CALA0200190](https://openairdocs.org/sdr/CALA0200190), Apr 8, 2002: SKIN. CRACKED. INSPECTION FOUND A 1/4" CRACK IN UPPER PYLON SKIN PANEL #5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV. B. - [SDR CALA0200169](https://openairdocs.org/sdr/CALA0200169), Apr 3, 2002: FITTING. CORRODED. INSPECTION FOUND R/H MLG FITTING AFT SPAR CASTING HOLE AT FALSE SPAR O/B ATTACH PIN CORRODED. THE CORROSION WAS REMOVED IAW ECRA 5711-01038. - [SDR CALA0200161](https://openairdocs.org/sdr/CALA0200161), Mar 29, 2002: SKIN. DENTED. INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 887, S15R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. - [SDR CALA0200160](https://openairdocs.org/sdr/CALA0200160), Mar 29, 2002: BUSHING. CORRODED. INSPECTION FOUND THE L/H AND R/H MLG(WALKING BEAM) O/B ATTACH FITTING BUSHINGS CORRODED. THE CORROSION WAS REMOVED AND A NEW BUSHING WAS INSTALLED AT EACH LOCAT - [SDR CALA0200159](https://openairdocs.org/sdr/CALA0200159), Mar 28, 2002: STRINGER. CORRODED. INSPECTION FOUND APU COMPARTMENT STRINGER CORRODED AT CUTOUT JUST BELOW APU INLET. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0200157](https://openairdocs.org/sdr/CALA0200157), Mar 28, 2002: WEB. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN WEB AT DOORWAY CORRODED, STA 796-847. A NEW WEB WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0200150](https://openairdocs.org/sdr/CALA0200150), Mar 25, 2002: SEAT TRACK. CRACKED. INSPECTION FOUND A 2" CRACK AT HI-LOCK HOLE IN R/H O/B SEAT TRACK, STA 727B. THE CRACKED AREA WAS REMOVED AND A REPAIR STRAP AND FILLER WERE INSTALLED IAW ECRA - [SDR CALA0200140](https://openairdocs.org/sdr/CALA0200140), Mar 21, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 887-947.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0200139](https://openairdocs.org/sdr/CALA0200139), Mar 20, 2002: SKIN. CRACKED. INSPECTION FOUND A 3" CRACK IN UPPER FUSELAGE SKIN AT STA 178, WL 243, LBL 1.5. THE CRACKED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SOEING DRAWI - [SDR CALA0200135](https://openairdocs.org/sdr/CALA0200135), Mar 17, 2002: STRAP. CORRODED. INSPECTION FOUND RT AFT LAV ANGLE STRAP CORRODED BETWEEN STA 986 AND 1006. A NEW ANGLE STRAP WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0200134](https://openairdocs.org/sdr/CALA0200134), Mar 17, 2002: FITTING. CORRODED. INSPECTION FOUND TWO R/H FORWARD HORIZONTAL STABILIZER ATTACH FITTINGS HAD LOWER AFT AND FORWARD BUSHINGS CORRODED BETWEEN BUSHING AND LUG. AN OVERSIZED BUSHING - [SDR CALA0200133](https://openairdocs.org/sdr/CALA0200133), Mar 16, 2002: STRINGER. CRACKED. INSPECTION FOUND A 1/8" CRACK IN STRINGER 16L AND 16R AT FASTENER AREA FWD OF LIGHT ASSEMBLY STA 500C AFT. A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW S - [SDR CALA0200131](https://openairdocs.org/sdr/CALA0200131), Mar 15, 2002: SKIN. CRACKED. INSPECTION FOUND A 1.125" CRACK IN WHEEL WELL CENTER KEEL EXTERIOR SKIN PANEL. THE CRACK WAS LOCATED ALONG R/H SIDE BETWEEN STA 685 AND 706. A DOUBLER WAS INSTA - [SDR CALA0001059](https://openairdocs.org/sdr/CALA0001059), Jul 12, 2000: KEELBEAM. WORN. INSPECTION FOUND THE RIGHT O/B FLANGE OF THE KEEL BEAM WORN JUST FORWARD OF BS 727. THE WEAR WAS CAUSED BY LOOSE FAIRING ATTACH FASTENERS. THE WORN AREAS WERE S - [SDR CALA0000615](https://openairdocs.org/sdr/CALA0000615), Apr 27, 2000: ARM. WORN. L2 DOOR HARD TO OPEN AND CLOSE BOTH INTERNALLY AND EXTERNALLY. REPLACED SNUBBER AND GUIDE ARM PER MM 52-13-31. - [SDR CALA9801181](https://openairdocs.org/sdr/CALA9801181), Jun 28, 1998: ANGLE. CORRODED. INSPECTION FOUND ANGLE CORRODED AT R-1 DOOR, STA 290 TO 294 AND 344. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-00. - [SDR CALA9801180](https://openairdocs.org/sdr/CALA9801180), Jun 26, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 2. REPAIRED IAW SRM 53-10-51, FIGURE 205. - [SDR CALA9801179](https://openairdocs.org/sdr/CALA9801179), Jun 26, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 328 TO 344. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-00-52. - [SDR CALA9801178](https://openairdocs.org/sdr/CALA9801178), Jun 26, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND CORROSION AROUND FASTENER HOLES OF FLOORBEAM AT STA 967, RBL 40 TO 50. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 202. - [SDR CALA9801170](https://openairdocs.org/sdr/CALA9801170), Jun 26, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 986 FROM RBL 0 TO RBL 46. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03450. - [SDR CALA9801169](https://openairdocs.org/sdr/CALA9801169), Jun 26, 1998: ANGLE. CORRODED. INSPECTION FOUND CORROSION AROUND FASTENER HOLES OF R-2 DOOR THRESHOLD Z-ANGLE FROM STA 967 TO 996, LBL 48, WL 208.1. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10- - [SDR CALA9801168](https://openairdocs.org/sdr/CALA9801168), Jun 25, 1998: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE CORRODED AT FORWARD ENTRY, LT SIDE, STA 312-340. A NEW Z-ANGLE WAS INSTALLED IAW SRM 53-10-2. - [SDR CALA9801167](https://openairdocs.org/sdr/CALA9801167), Jun 25, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT FORWARD ENTRY, STA 312, RBL 21. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. - [SDR CALA9801166](https://openairdocs.org/sdr/CALA9801166), Jun 25, 1998: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT Z-ANGLE CORRODED AT STA 967, LBL 46, WL 208. THE Z-ANGLE WAS REPLACED IAW SRM 51-10-2. - [SDR CALA9801165](https://openairdocs.org/sdr/CALA9801165), Jun 25, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 907-937, RBL 24. A NEW SECTION OF SEAT TRACK WAS SPLICED IN IAW SRM 53-00-52, FIGURE 204. - [SDR CALA9801164](https://openairdocs.org/sdr/CALA9801164), Jun 24, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND LT INBOARD SEAT TRACK CORRODED AT STA 917, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204. - [SDR CALA9801159](https://openairdocs.org/sdr/CALA9801159), Jun 23, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND OUTBOARD SEAT TRACK CORRODED AT STA 927, RBL 48, WL 208.1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, FIGURE 204, SHEET 1-4 AND SRM 51-30-00 - [SDR CAL960595](https://openairdocs.org/sdr/CAL960595), May 13, 1996: LIGHT. LOOSE WIRE. IAH - FLT 1677 - INSPECTION FOUND EMERGENCY PATH LIGHTING AT FORWARD FIRST CLASS CLOSET INOPERATIVE. MAINTENANCE RECONNECTED LOOSE WIRE ON CONNECTOR TO LIGHT AS - [SDR CAL960327](https://openairdocs.org/sdr/CAL960327), Mar 17, 1996: UPLOCK SENSOR. OUT OF ADJUST. IAH - FLT 8954 - THE LT MLG RED LIGHT CAME BACK ON AFTER GEAR RETRACTION. CYCLING THE GEAR WAS NO HELP. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT All 51: https://openairdocs.org/deregistered/N14346-2013-03-21/reports.md ## Other aircraft with N14346 - [Cancelled 1972-11-03](https://openairdocs.org/deregistered/N14346-1972-11-03): Piper PA-23-250, S/N 277304927. Exported to United Kingdom. Owner: [Aviation Services International Inc](https://openairdocs.org/faa-owner/AVIATION%20SERVICES%20INTERNATIONAL%20INC), [Lock Haven, PA](https://openairdocs.org/faa-place/PA/Lock%20Haven) --- 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.