# N14308: 1985 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: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 23359 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 5, 1985 - Certificate issued: January 13, 2010 - Last registry action: January 13, 2010 - Mode S code: A0B04E - 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/N14308 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14308 - Page: https://openairdocs.org/deregistered/N14308-2013-03-21 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 (71, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA2009062300325](https://openairdocs.org/sdr/CALA2009062300325), Jun 22, 2009: HANDLE. LACK OF LUBE. AT FLAPS 10 AT 2000 FT ALL SELECTED GEAR DOWN, RECEIVED LIGHT INDICATION 3 GREEN AND 3 RED STEADY, NO HORN W/ FLAPS 30 AT APROX 400 FT AGL TOO LOW GEAR, WENT AR - [SDR CALA0700660](https://openairdocs.org/sdr/CALA0700660), Oct 24, 2007: SKIN. CRACKED. A WALKAROUND INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT STA 727D, S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03745. - [SDR CALA0700435](https://openairdocs.org/sdr/CALA0700435), Aug 13, 2007: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR SKIN AT AFT EDGE OF HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, REPAIR 3. - [SDR CALA0700434](https://openairdocs.org/sdr/CALA0700434), Aug 13, 2007: CHANNEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CHANNEL AT FORWARD LOWER STOP. REPAIRED IAW SRM 51-40-02. - [SDR CALA0700428](https://openairdocs.org/sdr/CALA0700428), Aug 12, 2007: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB UPPER HINGE INTERCOSTAL AT STA 294.5, S10L. A REPAIR WAS INSTALLED IAW ECRA 5311-01350. - [SDR CALA0700427](https://openairdocs.org/sdr/CALA0700427), Aug 12, 2007: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB LOWER HINGE INTERCOSTAL AT STA 294.5, S13L TO S14L. A REPAIR WAS INSTALLED IAW ECRA 5311-01349. - [SDR CALA0700426](https://openairdocs.org/sdr/CALA0700426), Aug 12, 2007: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FRAME AT DRAIN HOLE, STA 440, BL 0. A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201. - [SDR CALA0700424](https://openairdocs.org/sdr/CALA0700424), Aug 12, 2007: SKIN. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS IN R-1 DOOR SKIN CUTOUT AT STA 328, S16R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5331-01337. - [SDR CALA0700423](https://openairdocs.org/sdr/CALA0700423), Aug 11, 2007: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR INNER SKIN BETWEEN LIGHTENING HOLES ABOVE HANDLE. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01089. - [SDR CALA0700422](https://openairdocs.org/sdr/CALA0700422), Aug 11, 2007: SEAT TRACK. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, RBL 24.8. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-0149 - [SDR CALA0700421](https://openairdocs.org/sdr/CALA0700421), Aug 11, 2007: SEAT TRACK. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, LBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-01492 - [SDR CALA0700420](https://openairdocs.org/sdr/CALA0700420), Aug 11, 2007: SEAT TRACK. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK O/B MOUNT FLANGE AT STA 727B, RBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 55321-014 - [SDR CALA0700419](https://openairdocs.org/sdr/CALA0700419), Aug 11, 2007: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT TWO EACH HOLES IN I/B CHORD AT STA 639, S16R TO S17R. THE INNER CHORD WAS REPLACED AND A REPAIR WAS INSTALLED IAW ECRA 5311-0 - [SDR CALA0700418](https://openairdocs.org/sdr/CALA0700418), Aug 10, 2007: FRAME. CORRODED. INSPECTION FOUND FORWARD BAGGAGE BIN FRAME CORRODED AT STA 500B BETWEEN STRINGER 25R AND S26R. A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07, REPAIR 7. - [SDR CALA0700415](https://openairdocs.org/sdr/CALA0700415), Aug 9, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 947.5 BETWEEN S21L AND S21R, LBL 10 TO RBL 10. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0700452](https://openairdocs.org/sdr/CALA0700452), Aug 7, 2007: FLOORBEAM. CRACKED. INSPECTION FOUND CRACKS TO THE LONGITUDINAL FLOORBEAM FLANGES AT STA 727B, LBL 45.5, RBL 45.5 AND RBL 24.8. REPAIRS WERE PERFORMED IAW ECRA 5321-01492. - [SDR CALA0700411](https://openairdocs.org/sdr/CALA0700411), Aug 4, 2007: SKIN. DAMAGED. INSPECTION FOUND A HOLE IN FUSELAGE SKIN CAUSED BY A LIGHTNING STRIKE AT STA 375, S24R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. - [SDR CALA0700396](https://openairdocs.org/sdr/CALA0700396), Aug 3, 2007: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647. - [SDR CALA0700395](https://openairdocs.org/sdr/CALA0700395), Aug 3, 2007: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 827, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647. - [SDR CALA0700392](https://openairdocs.org/sdr/CALA0700392), Aug 2, 2007: STRAP. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN WEB STRAP JUST FORWARD OF L-2 DOOR AT STA 947.5, S10L TO S11L. A NEW WEB STRAP WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0700391](https://openairdocs.org/sdr/CALA0700391), Aug 1, 2007: KEELBEAM. CORRODED. INSPECTION FOUND LEFT KEEL BEAM CORRODED IN A/C DISTRIBUTION BAY AT STA 500D-520. THE KEEL BEAM WAS REPAIRED IAW SRM 53-30-12, FIGURE 201. - [SDR CALA0700387](https://openairdocs.org/sdr/CALA0700387), Aug 1, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R CORRODED AT STA 294-323. THE STRINGER WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0700441](https://openairdocs.org/sdr/CALA0700441), Jul 30, 2007: DOOR FRAME. CRACKED. INSPECTION FOUND A CRACK EMANATING FROM THE DOORSTOP CUTOUT IN THE AFT EDGE BEAM OF THE L-1 DOOR. THE EDGE BEAM WAS REPAIRED IAW ECRA 5210-01944. - [SDR CALA0700381](https://openairdocs.org/sdr/CALA0700381), Jul 29, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 1006 FROM S25R TO 26L. THE CORRODED SECTION OF FRAME WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIG - [SDR CALA0700377](https://openairdocs.org/sdr/CALA0700377), Jul 27, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25L CORRODED AT REPAIR CUTOUT AFT OF STA 1006. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 201, - [SDR CALA0700374](https://openairdocs.org/sdr/CALA0700374), Jul 24, 2007: SHEAR WEB. CRACKED. INSPECTION FOUND A 2.5 INCH CRACK IN LEFT SHEAR WEB FORWARD OF STA 639 FUSELAGE FRAME, LBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02 - [SDR CALA0700373](https://openairdocs.org/sdr/CALA0700373), Jul 24, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AROUND FASTENER HOLE AT STA 360, BL 0. THE CORRODED AREA WAS CUT OUT AND REPAIR ANGLES WERE INSTALLED IAW SRM 53- - [SDR CALA0600245](https://openairdocs.org/sdr/CALA0600245), Jun 16, 2006: CONTROLLER. INOPERATIVE. THE CREW REPORTED SMOKE IN THE CABIN WHILE EN ROUTE TO IAH. THE SMOKE REMOVAL CHECKLIST WAS COMPLETED AND AFTER TURNING OFF THE RECIRCULATION FAN THE SMOKE WENT - [SDR CALA0500429](https://openairdocs.org/sdr/CALA0500429), Dec 10, 2005: SHEAR TIE. CORRODED. INSPECTION FOUND FRAME/SHEAR TIE CORRODED AT STA 967 BETWEEN STRINGERS 27L-27R. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED - [SDR CALA0500428](https://openairdocs.org/sdr/CALA0500428), Dec 9, 2005: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON FRAME (HORSE COLLAR FITTING) AROUND LOCK FASTENER COLLAR. THE NR 2 PYLON HORSE COLLAR WAS REMOVED AND REPLACED IAW - [SDR CALA0500371](https://openairdocs.org/sdr/CALA0500371), Oct 20, 2005: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727E - 747 JUST BELOW S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, DETAIL X - [SDR CALA0300496](https://openairdocs.org/sdr/CALA0300496), Aug 26, 2003: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27L CORRODED AT STA 996. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. - [SDR CALA0300495](https://openairdocs.org/sdr/CALA0300495), Aug 25, 2003: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0300493](https://openairdocs.org/sdr/CALA0300493), Aug 25, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FORWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 500D BETWEEN S26L AND S27L, LOWER AREA. THE CORRODED AREA WAS CUT OUT AND FILLER, DOUBLER A - [SDR CALA0300490](https://openairdocs.org/sdr/CALA0300490), Aug 24, 2003: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 296, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-40352 AND SRM 51-40-02. - [SDR CALA0300489](https://openairdocs.org/sdr/CALA0300489), Aug 24, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294.5, RBL 41. THE FLOORBEAM UPPER CHORD SECTION WAS REMOVED AND A NEW UPPER CHORD WAS INSTALLED IAW SRM - [SDR CALA0300487](https://openairdocs.org/sdr/CALA0300487), Aug 24, 2003: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED FROM STA 947.5 TO 967 AT RBL 7 AND RBL 46. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-40-02 AND ECRA 5310-03585. - [SDR CALA0300486](https://openairdocs.org/sdr/CALA0300486), Aug 24, 2003: CHANNEL. CRACKED. INSPECTION FOUND THE LT WING T/E NR 3 FLAP TRACK FAIRING AFT END U-CHANNEL CRACKED IN TWO PLACES UNDER THE TRACK. THE CRACKS WERE .25 INCH LONG. THE CHANNEL WAS - [SDR CALA0300086](https://openairdocs.org/sdr/CALA0300086), Mar 2, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES OF UPPER CAP AT STA 1006 FROM BL 0 TO RBL 40. REMOVED AND REPLACED T-CAP IAW ECRA 5310-03851. - [SDR CALA0300085](https://openairdocs.org/sdr/CALA0300085), Mar 2, 2003: CHANNEL. CORRODED. INSPECTION FOUND CHANNEL CORRODED ON UPPER SURFACE AND AT NUTPLATES AT STA 1006-1016, LBL 5 TO LBL 9. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02. - [SDR CALA0300084](https://openairdocs.org/sdr/CALA0300084), Mar 2, 2003: ANGLE. CORRODED. INSPECTION FOUND CORROSION ON UPPER SURFACE OF ANGLE AT NUTPLATES, STA 1006, LBL 10. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0300083](https://openairdocs.org/sdr/CALA0300083), Mar 2, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED IN AFT GALLEY AREA AT STA 967, LBL 25. REPAIRED IAW ECRA 5320-01726. - [SDR CALA0300081](https://openairdocs.org/sdr/CALA0300081), Mar 1, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE OF CAP AND AT FASTENER HOLES AT STA 1006, BL 0 TO RBL 30. THE T-CAP WAS REMOVED AND REPLACED IAW - [SDR CALA0300068](https://openairdocs.org/sdr/CALA0300068), Feb 23, 2003: FRAME. CORRODED. INSPECTION FOUND R/H O/B FRAME CORRODED AT STA 986, RBL 40. REPAIRED IAW ECRA 5310-03851. - [SDR CALA0300054](https://openairdocs.org/sdr/CALA0300054), Feb 18, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN PRESSURE DECK AT BS 664 - 675, LBL 30 - 35. REPAIRED IAW SRM 53-60-51, PAGE 213-221. - [SDR CALA0300052](https://openairdocs.org/sdr/CALA0300052), Feb 17, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A 2.75 INCH CRACK IN RT WHEEL WELL PRESSURE DECK AT FS 663, RBL 35. REPAIRED IAW SRM 53-60-51, PAGE 213-231. - [SDR CALA0200028](https://openairdocs.org/sdr/CALA0200028), Jan 21, 2002: SKIN. CRACKED. INSPECTION FOUND A 3/4" CRACK AT LIGHTENING HOLE CUTOUT OF FORWARD CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01014. - [SDR CALA0200025](https://openairdocs.org/sdr/CALA0200025), Jan 17, 2002: SKIN. DELAMINATED. INSPECTION FOUND L/H WING LEADING EDGE SKIN DELAMINATED AND HILOCK PULLED THROUGH SKIN BEHIND #2 SLAT AT O/B END. REPAIRED IAW ECRA 5721-01048. - [SDR CALA0200024](https://openairdocs.org/sdr/CALA0200024), Jan 17, 2002: SKIN. DELAMINATED. INSPECTION FOUND R/H WING LEADING EDGE SKIN UNDER O/B EDGE OF #5 SLAT DELAMINATED. REPAIRED IAW ECRA 5721-01048. - [SDR CALA0200022](https://openairdocs.org/sdr/CALA0200022), Jan 17, 2002: ATTACH ANGLE. WORN. INSPECTION FOUND ATTACH ANGLE ON BOTTOM OF VERTICAL STABILIZER ON R/H SIDE WORN THIN AT STA 1104-1121. THE ATTACH ANGLE WAS REPLACED IAW ECRA 5300-01013, REV B. All 71: https://openairdocs.org/deregistered/N14308-2013-03-21/reports.md ## Other aircraft with N14308 - [Cancelled 1974-07-19](https://openairdocs.org/deregistered/N14308-1974-07-19): Piper PA-18-150, S/N 18-7409072. Exported to Brazil. Owner: [Aero Export International Inc](https://openairdocs.org/faa-owner/AERO%20EXPORT%20INTERNATIONAL%20INC), [Ft Lauderdale, FL](https://openairdocs.org/faa-place/FL/Ft%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.