# N14342: 1987 Boeing 737-3TO, registration cancelled 2009-07-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 21, 2009 - 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: 23580 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 22, 1987 - Certificate issued: April 17, 2007 - Last registry action: April 17, 2007 - Mode S code: A0B0D4 - 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/N14342 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14342 - Page: https://openairdocs.org/deregistered/N14342-2009-07-21 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 (48) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0800414](https://openairdocs.org/sdr/CALA0800414), May 6, 2008: CHANNEL. CRACKED. DURING REMOVAL AND REPLACEMENT OF THE NR 3 VHF ANTENNA TWO CRACKS WERE FOUND ON THE ANTENNA MOUNTING CHANNEL LOCATED IN THE AFT CARGO COMPARTMENT. CHANNEL AT ST - [SDR CALA0700321](https://openairdocs.org/sdr/CALA0700321), Jun 24, 2007: WIRE. BROKEN. THE APU FIRE LIGHT ILLUMINATED ACCOMPANIED BY ACTIVATION OF THE FIRE BELL WHILE AT CRUISE ENROUTE FROM SFO TO IAH. THE APU DETECTOR INOP LIGHT ALSO ILLUMINATED. - [SDR CALA0600195](https://openairdocs.org/sdr/CALA0600195), Jun 1, 2006: FLOORBEAM. CRACKED. INSPECTION FOUND A 0.7 INCH CRACK IN FORWARD CABIN FLOORBEAM WEB AT STA 328, LBL 46. THE WEB WAS REPAIRED IAW ECRA 5321-01367. - [SDR CALA0600178](https://openairdocs.org/sdr/CALA0600178), May 21, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0600177](https://openairdocs.org/sdr/CALA0600177), May 21, 2006: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED AT STA 1006, S26R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0600173](https://openairdocs.org/sdr/CALA0600173), May 20, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND AFT CABIN FLOORBEAM CORRODED I/B OF LT Z-ANGLE AT STA 986.5, LBL 26-52. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW ECRA 5310-03851. - [SDR CALA0600169](https://openairdocs.org/sdr/CALA0600169), May 18, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND AFT CABIN INTERIOR RIGHT I/B FLOOR SEAT TRACK CORRODED FROM STA 907-936, RBL 15. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52. - [SDR CALA0600243](https://openairdocs.org/sdr/CALA0600243), May 17, 2006: STRINGER. CORRODED. INSPECTION FOUND E&E COMPARTMENT STA 312-323.7 STRINGER 28R CORRODED ON BOTH SIDES AND ALONG TOP LEFT UPPER EDGE. THE STRINGER WAS REMOVED AND REPLACED IAW SRM - [SDR CALA0300424](https://openairdocs.org/sdr/CALA0300424), Jul 20, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED UNDER LAV-A AT STA 294.5, LBL 24.67. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 5 - [SDR CALA0300398](https://openairdocs.org/sdr/CALA0300398), Jul 19, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE DECK AT BS 663, LBL 31. THE CRACKED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-60-51. - [SDR CALA0300396](https://openairdocs.org/sdr/CALA0300396), Jul 19, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT L-2 DOOR AFT GIRT BAR ATTACH POINT, STA 986. A REPAIR WAS ACCOMPLISHED ON UPPER CHORD OF FLOORBEAM IAW ECRA 5310-03851. - [SDR CALA0300045](https://openairdocs.org/sdr/CALA0300045), Feb 12, 2003: SOLENOID. INOPERATIVE. THE CREW WAS UNABLE TO RAISE THE GEAR HANDLE PAST THE OFF POSITION AFTER TAKEOFF. THE GEAR OVERRIDE TRIGGER WAS USED TO RAISE GEAR. MAINTENANCE REPLACED THE LAN - [SDR CALA2000257](https://openairdocs.org/sdr/CALA2000257), May 3, 2002: ANGLE. CORRODED. CORROSION ON L-ANGLE AT STA 500D, STRINGER 26L F/B/B. REMOVED AND REPLACED ANGLE REF SRM 51-70-12. - [SDR CALA0200255](https://openairdocs.org/sdr/CALA0200255), May 2, 2002: FITTING. CORRODED. R/H MLG FITTING INNER BUSHING CORROSION ON THE BOSS. REPAIRED FITTING HOLE AND INSTALLED OVER SIZE BUSHING PER ECRA 5711-01039. - [SDR CALA0200254](https://openairdocs.org/sdr/CALA0200254), Apr 29, 2002: SKIN. CRACKED. INSPECTION FOUND A 1/2" CRACK IN #2 ENGINE UPPER PYLON SKIN AT ACCESS PANEL 5827R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230. - [SDR CALA0200250](https://openairdocs.org/sdr/CALA0200250), Apr 29, 2002: SKIN. CRACKED. INSPECTION FOUND A 1/2" CRACK IN FUSELAGE SKIN AT TWO SCREW HOLES AFT OF C/L OF AIRCRAFT STA 380. A DOUBLER WAS INSTALLED IAW ECRA 5330-02849. - [SDR CALA0200249](https://openairdocs.org/sdr/CALA0200249), Apr 27, 2002: ANGLE. CHAFED. INSPECTION FOUND UPPER SURFACE OF FUSELAGE KEEL BEAM RIGHT AND LEFT LOWER ANGLES HAD WASHERS WEARING INTO THE ANGLES AT STA 710-727. THE KEEL BEAM ANGLES WERE R - [SDR CALA0200246](https://openairdocs.org/sdr/CALA0200246), Apr 26, 2002: SPAR. CRACKED. INSPECTION FOUND THE RT AND LT WING REAR SPARS HAD A 0.050 INCH CRACK INDICATION AT HOLE AT MLG BEAM ATTACH FITTINGS. - [SDR CALA0200244](https://openairdocs.org/sdr/CALA0200244), Apr 26, 2002: CARGO TRACK. CORRODED. INSPECTION FOUND RT TIE DOWN RAIL CORRODED ON UPPER SIDE FRONT IN AFT BAGGAGE BIN AT STA 807-840. A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53, PAGE 204-2 - [SDR CALA0200241](https://openairdocs.org/sdr/CALA0200241), Apr 25, 2002: STRINGER. CORRODED. INSPECTION FOUND STRINGER 22L CORRODED AT STA 867-887. A REPAIR STRINGER WAS INSTALLED IAW SRM 53-00-03, PAGE 201 AND 204. - [SDR CALA0200240](https://openairdocs.org/sdr/CALA0200240), Apr 25, 2002: STRINGER. CRACKED. INSPECTION FOUND A 1" CRACK IN STRINGER 16R AND 16L AT STA 500C + 5". THE CRACKED AREA OF EACH STRINGER WAS REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-00-03. - [SDR CALA0200236](https://openairdocs.org/sdr/CALA0200236), Apr 23, 2002: BELTFRAME. CRACKED. INSPECTION FOUND A 1/4" CRACK IN L/H BELTFRAME ANGLE AT STA 616 JUST ABOVE CENTER TANK. THE CRACKED AREA WAS TRIMMED OUT. AN ANGLE DOUBLER AND FILLER WERE INSTA - [SDR CALA0200235](https://openairdocs.org/sdr/CALA0200235), Apr 22, 2002: SKIN. CRACKED. INSPECTION FOUND A 3/4" CRACK IN FUSELAGE SKIN FORWARD OF L-2 DOOR FUSELAGE TORQUE TUBE ACCESS PANEL AT STA 947 BETWEEN STRINGER 10 AND 11L. THE CRACKED AREA WA - [SDR CALA0200234](https://openairdocs.org/sdr/CALA0200234), Apr 22, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND L/H O/B SEAT TRACK HAD PITTING CORROSION AT STA 727-767. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGURE 204. - [SDR CALA0200227](https://openairdocs.org/sdr/CALA0200227), Apr 21, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND R/H SEAT TRACK HAD PITTING CORROSION AT STA 847-907. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52. - [SDR CALA0200215](https://openairdocs.org/sdr/CALA0200215), Apr 17, 2002: STRINGER. CORRODED. INSPECTION FOUND CENTER STRINGER ON LOWER FLOOR SIDE OF AFT PRESSURE BULKHEAD AT STA 1016 CORRODED ON LOWER END. THE STRINGER WAS REPAIRED IAW SRM 51-70-11, PAG - [SDR CALA0200209](https://openairdocs.org/sdr/CALA0200209), Apr 16, 2002: FITTING. CORRODED. INSPECTION FOUND RT HORIZONTAL STABILIZER FORWARD UPPER LUG CORRODED. THE CORROSION WAS REMOVED FROM LUG IAW SRM 55-10-10. - [SDR CALA0200208](https://openairdocs.org/sdr/CALA0200208), Apr 16, 2002: SPLICE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN STRINGER SPLICE AT STA 907, S4L. A NEW SPLICE WAS INSTALLED IAW SRM 51-40-00. - [SDR CALA0200197](https://openairdocs.org/sdr/CALA0200197), Apr 12, 2002: WEB. CRACKED. INSPECTION FOUND A 4" CRACK IN WEB AT STA 303.9, STRINGER 4L. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0200196](https://openairdocs.org/sdr/CALA0200196), Apr 11, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 360. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52. - [SDR CALA0000895](https://openairdocs.org/sdr/CALA0000895), Jun 13, 2000: SKIN. CRACKED. INSPECTION FOUND INNER SKIN OF C-1 DOOR CRACKED IN THREE PLACES AT LIGHTENING HOLES. THE CRACKS WERE 1 INCH LONG. A REPAIR WAS INSTALLED IAW ECRA 5230-01555. - [SDR CALA0000851](https://openairdocs.org/sdr/CALA0000851), Jun 8, 2000: SKIN. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS IN NR 1 ENGINE PYLON I/B SIDE ACCESS DOOR PANEL NR 5724L CUTOUT. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204. - [SDR CALA0000818](https://openairdocs.org/sdr/CALA0000818), Jun 3, 2000: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT LOWER SKIN AT ACTUATOR AREA. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02586. - [SDR CALA9900850](https://openairdocs.org/sdr/CALA9900850), Jul 22, 1999: RELAY. INOP. THE GEAR HANDLE TRIGGER HAD TO BE PULLED TO RAISE LANDING GEAR PAST THE OFF POSITION AFTER TAKEOFF. THE FLIGHT CONTINUED TO LAX WHERE IT LANDED WITHOUT INCIDENT - [SDR CALA9801418](https://openairdocs.org/sdr/CALA9801418), Aug 9, 1998: SENSOR. INOPERATIVE. THE LANDING GEAR WOULD NOT RETRACT; THE LEVER WOULD NOT GO ABOVE THE OFF POSITION AFTER TAKEOFF FROM SFO. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHO - [SDR CALA9801384](https://openairdocs.org/sdr/CALA9801384), Aug 2, 1998: LOGIC CARDS. INOPERATIVE. THE LANDING GEAR HANDLE WOULD NOT MOVE ABOVE THE OFF POSITION AFTER TAKEOFF. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE GEAR HANDLE RAISED. MAINTENANCE REMO - [SDR CALA9801187](https://openairdocs.org/sdr/CALA9801187), Jun 27, 1998: WIRE. DAMAGED. INSPECTION FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 6ABC TO 12AB. TROUBLESHOOTING FOUND A CRUSHED WIRE UNDER SEAT AT ROW 9ABC. THE WIRE WAS REPAIR - [SDR CALA9801062](https://openairdocs.org/sdr/CALA9801062), Jun 12, 1998: SKIN. DENTED. INSPECTION FOUND SMALL DENTS IN RT FUSELAGE SKIN JUST FORWARD OF STA 360 BETWEEN STRINGERS 18R AND 19R. REPAIRED IAW ECRA 5331-01024. - [SDR CALA9801037](https://openairdocs.org/sdr/CALA9801037), Jun 10, 1998: HINGE. GOUGED. INSPECTION FOUND NR 1 ENGINE INBOARD AND OUTBOARD THRUST REVERSER FORWARD HINGE POINT FORWARD LUGS GOUGED. THE HINGES WERE REPAIRED IAW ECRA 7832-01125. - [SDR CALA9800967](https://openairdocs.org/sdr/CALA9800967), Jun 4, 1998: DOOR. CRACKED. INSPECTION FOUND A 1 CRACK AT FORWARD LOWER CORNER (JUST BELOW HOLD OPEN HOOK) OF FORWARD BAGGAGE BIN DOOR. THE DOOR WAS REPAIRED IAW ECRA 5234-01004. - [SDR CALA9800951](https://openairdocs.org/sdr/CALA9800951), Jun 3, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND CORROSION AT FASTENER HOLES OF AFT LAV LT FLOORBEAM AT STA 1016 FROM CENTERLINE TO LBL 36. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTA - [SDR CALA9800915](https://openairdocs.org/sdr/CALA9800915), May 31, 1998: SKIN. CRACKED. INSPECTION FOUND THREE .25 CRACKS COMING FROM RIVETS IN NR 1 SLAT LOWER SKIN BETWEEN OUTBOARD MAIN TRACK AND OUTBOARD AUX TRACK. A REPAIR WAS INSTALLED IAW BOEI - [SDR CALA9800914](https://openairdocs.org/sdr/CALA9800914), May 29, 1998: ANGLE. CORRODED. INSPECTION FOUND ANGLE CORRODED AT AFT GALLEY NEAR L-2 DOOR THRESHOLD AREA, STA 947 TO 967. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2. - [SDR CALA9800913](https://openairdocs.org/sdr/CALA9800913), May 29, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND LT INBOARD SEAT TRACK IN AFT GALLEY AT STA 947.5 CORRODED. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52. - [SDR CALA9601816](https://openairdocs.org/sdr/CALA9601816), Dec 13, 1996: AXLE. CRACKED. WHILE TURNING ONTO THE RUNWAY FOR TAKEOFF, THE CREW FELT THE NOSE STRUT BOTTOM OUT. THE CREW IN AIRCRAFT BEHIND THEM REPORTED THAT THEY LOST A NOSE TIRE. THE AI - [SDR CALA9600685](https://openairdocs.org/sdr/CALA9600685), May 20, 1996: TRACK. WORN. INSPECTION FOUND A HOLE WORN THROUGH AFT CARGO FLOORBEAM TRACK ON LT SIDE. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA9600684](https://openairdocs.org/sdr/CALA9600684), May 20, 1996: SKIN. CRACKED. INSPECTION FOUND A 2.875 INCH CRACK IN NR 1 SLAT LOWER SKIN PANEL. A DOUBLER WAS INSTALLED IAW ECRA 5750-01159. - [SDR CAL960450](https://openairdocs.org/sdr/CAL960450), Apr 9, 1996: PIN. FAILED. THE FLIGHT CREW REPORTED AIRFRAME VIBRATION AFTER TAKEOFF FROM PHX. THE FLIGHT CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT INBOA ## 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 19971105041679I](https://openairdocs.org/incident/19971105041679I), Nov 5, 1997: Boeing 7373T0 (N14342), Cleveland, OH. Narrative: Continental airlines flight 1120 landed on runway 23R and was instructed to hold short of runway 23L on rollout. Coa 1120 turned left at taxiway k… ## Other aircraft with N14342 - [Cancelled 1973-01-10](https://openairdocs.org/deregistered/N14342-1973-01-10): Piper PA-23-250, S/N 27-7304923. Exported to South Africa. Owner: [International Aircraft Deliveries](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIRCRAFT%20DELIVERIES), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - [Cancelled 1948-07-27](https://openairdocs.org/deregistered/N14342-1948-07-27): Stinson SR-5A, S/N 9214, built 1934. Owner: [Blackwelder Cecil F](https://openairdocs.org/faa-owner/BLACKWELDER%20CECIL%20F) --- 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.