# N14337: 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: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 23575
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 30, 1987
- Certificate issued: April 17, 2007
- Last registry action: April 17, 2007
- Mode S code: A0B0B6
- 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/N14337
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14337
- Page: https://openairdocs.org/deregistered/N14337-2009-07-21

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 (63, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA0600269](https://openairdocs.org/sdr/CALA0600269), May 19, 2006: STIFFENER. CRACKED. INSPECTION FOUND A CRACK IN THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT LBL AND RBL 6.15. THE VERTICAL STIFFENER WAS REPAIRED IAW ECRA 5714-01018.
- [SDR CALA0600076](https://openairdocs.org/sdr/CALA0600076), Mar 1, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27L CORRODED JUST FORWARD OF STA 1016. A REPAIR SECTION WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0600075](https://openairdocs.org/sdr/CALA0600075), Mar 1, 2006: WEB. CORRODED. INSPECTION FOUND AFT PRESSURE BULKHEAD WEB FORWARD FACE CORRODED AT LEFT AND RIGHT CHANNEL, STA 1016, BL 0. A WEB AND CHANNEL REPAIR WAS INSTALLED IAW BOEING DR
- [SDR CALA0600074](https://openairdocs.org/sdr/CALA0600074), Mar 1, 2006: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1009, S27L. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, REPAIR 31.
- [SDR CALA0600072](https://openairdocs.org/sdr/CALA0600072), Feb 27, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27L IN FORWARD BAGGAGE BIN CORRODED AT STA 440-460. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201, DETAIL VI.
- [SDR CALA0600070](https://openairdocs.org/sdr/CALA0600070), Feb 26, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27L CORRODED AT STA 480-500B. A NEW SECTION OF STRINGER WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0600065](https://openairdocs.org/sdr/CALA0600065), Feb 21, 2006: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME AT STA 616 JUST BELOW MAIN DECK FLOOR, LBL 0 TO LBL 60. REPAIRED FRAME IAW ECRA 5311-01158.
- [SDR CALA0600167](https://openairdocs.org/sdr/CALA0600167), Mar 3, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 277, LBL 19. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED 
- [SDR CALA0600166](https://openairdocs.org/sdr/CALA0600166), Mar 2, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, LBL 20. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICE
- [SDR CALA0500070](https://openairdocs.org/sdr/CALA0500070), Mar 2, 2005: THRESHOLD. CORRODED. INSPECTION FOUND R-1 DOOR THRESHOLD DRAIN FRAME CORRODED AT STA 294-342, BL 0 TO RBL 36. A CHORD WAS INSTALLED IAW SRM 51-40-02 AND DRAWING 55-45875.
- [SDR CALA0500067](https://openairdocs.org/sdr/CALA0500067), Feb 27, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21, RBL 36, AND RBL 49. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51.
- [SDR CALA0500062](https://openairdocs.org/sdr/CALA0500062), Feb 27, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED IN E&E COMPARTMENT ON RT SIDE ABOVE AIRFONE CONTROL BOX AT STA 312, RBL 21. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLAC
- [SDR CALA0500061](https://openairdocs.org/sdr/CALA0500061), Feb 27, 2005: FLOORBEAM. CRACKED. INSPECTION FOUND A 1.625 INCH CRACK IN FORWARD GALLEY FLOORBEAM WEB AT STA 312, RBL 18. THE WEB WAS REPAIRED IAW ECRA 5310-04462.
- [SDR CALA0400635](https://openairdocs.org/sdr/CALA0400635), Sep 12, 2004: SKIN. DENTED. INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 264 ABOVE S19L. THE SKIN WAS REPAIRED IAW ECRA 5330-03366. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR IAW PA
- [SDR CALA0400480](https://openairdocs.org/sdr/CALA0400480), May 8, 2004: FLOORBEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 540, RBL 48. THE FLOORBEAM WAS REPAIRED IAW ECRA 5331-01146.
- [SDR CALA0400476](https://openairdocs.org/sdr/CALA0400476), May 6, 2004: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON ANGLE JUST AFT OF I/B MIDSPAR ATTACH BOLT. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00.
- [SDR CALA0400464](https://openairdocs.org/sdr/CALA0400464), May 4, 2004: ANGLE. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE FOR RIGHT RAM AIR INLET AT BS 540, S22R. THE CRACKED SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-7
- [SDR CALA0400461](https://openairdocs.org/sdr/CALA0400461), May 4, 2004: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LEFT WING L/E NR 3 SLAT ACTUATOR CUTOUT. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-40-01, FIG
- [SDR CALA0400447](https://openairdocs.org/sdr/CALA0400447), May 1, 2004: SEAT TRACK. BROKEN. THE RIGHT I/B SEAT TRACK UPPER LOBE BROKE DURING REMOVAL AT STA 827. A SEAT TRACK REPAIR SECTION WAS INSTALLED IAW SRM 53-00-52.
- [SDR CALA0400444](https://openairdocs.org/sdr/CALA0400444), May 1, 2004: SEAT TRACK. BROKEN. THE RIGHT O/B SEAT TRACK UPPER LOBE BROKE DURING SEAT REMOVAL AT STA 887, RBL 34. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA0400413](https://openairdocs.org/sdr/CALA0400413), Apr 24, 2004: CHARGER. INOPERATIVE. THREE EMERGENCY LIGHTS OVER EMERGENCY ESCAPE HATCH ARE INOP. REPLACED BATTERY CHARGERS AND BATTERIES PER MM 33-51-51.
- [SDR CALA0200127](https://openairdocs.org/sdr/CALA0200127), Mar 8, 2002: SKIN. CRACKED. INSPECTION FOUND TWO INCH CRACKS AT THE EDGES OF THREE LIGHTENING HOLES IN C-2 DOOR INNER SKIN OVER CENTER BALANCE SPRINGS. A 1" CRACK WAS FOUND AT THE EDGE OF 
- [SDR CALA0200126](https://openairdocs.org/sdr/CALA0200126), Mar 8, 2002: SKIN. CRACKED. INSPECTION FOUND A 1" CRACK IN CAPTAIN'S WINDSHIELD O/B POST OUTER SKIN AT UPPER CORNER. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-01104.
- [SDR CALA0200125](https://openairdocs.org/sdr/CALA0200125), Mar 7, 2002: SKIN. CRACKED. INSPECTION FOUND A 1.25" CRACK IN C-2 DOOR INNER SKIN AT AFT LOWER CORNER. THE SKIN WAS REPAIRED IAW ECRA 5230-01650.
- [SDR CALA0200124](https://openairdocs.org/sdr/CALA0200124), Mar 7, 2002: WEB. CRACKED. INSPECTION FOUND A 1/2" CRACK IN WEB AT LIGHTENING HOLE AFT OF STA 1040 AND I/B OF TAIL COMPARTMENT ACCESS. A REPAIR WAS INSTALLED IAW ECRA 5320-01768.
- [SDR CALA0200122](https://openairdocs.org/sdr/CALA0200122), Mar 6, 2002: SPAR CAP. CRACKED. INSPECTION FOUND A 1/2" CRACK AT HOLE IN SPAR CAP AT R/H WING MLG BEAM ATTACH FITTING. REPAIRED IAW ECRA 5740-02000. THE ITEM WAS PLACED ON DIP TO PERFORM AN HF
- [SDR CALA0200118](https://openairdocs.org/sdr/CALA0200118), Mar 4, 2002: SKIN. CRACKED. INSPECTION FOUND A 3" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR JUST I/B OF #4 ELEVATOR HINGE. A PERMANENT REPAIR DOUBLER WAS INSTALLED IAW ECR
- [SDR CALA0200117](https://openairdocs.org/sdr/CALA0200117), Mar 2, 2002: WEB. WORN. INSPECTION FOUND C-1 AFT DOOR JAMB LOWER WEB WORN AROUND EDGES. A NEW WEB WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0200116](https://openairdocs.org/sdr/CALA0200116), Mar 2, 2002: KEELBEAM. CHAFED. INSPECTION FOUND LT AFT UPPER SURFACE OF KEEL BEAM FLANGE HAD WORN HOLES ON UPPER SURFACE FROM PANEL ATTACH NUTS AT STA 719-727. REPAIRED IAW ECRA 5310-03740.
- [SDR CALA0200115](https://openairdocs.org/sdr/CALA0200115), Mar 2, 2002: SKIN. CRACKED. INSPECTION FOUND A 4" CRACK IN #4 L/E SLAT PANEL AT O/B ACTUATOR. REPAIRED IAW SRM 57-43-01.
- [SDR CALA0200108](https://openairdocs.org/sdr/CALA0200108), Feb 27, 2002: STRAP. CORRODED. INSPECTION FOUND FLOOR H-STRAP CORRODED AT STA 1022-1026, LBL 3. A NEW H-STRAP WAS INSTALLED IAW SRM 51-10-2 AND 51-30-3.
- [SDR CALA0200107](https://openairdocs.org/sdr/CALA0200107), Feb 27, 2002: SKIN. WORN. INSPECTION FOUND UPPER FUSELAGE SKIN WORN AT STA 867, RBL 6. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 214.
- [SDR CALA0200099](https://openairdocs.org/sdr/CALA0200099), Feb 25, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ABOVE AND BELOW NUT CLIP HOLES AT STA 986, RBL 46 TO LBL 46. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851.
- [SDR CALA0200096](https://openairdocs.org/sdr/CALA0200096), Feb 25, 2002: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR SUPPORT AT STA 578, BBL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-2.
- [SDR CALA0200095](https://openairdocs.org/sdr/CALA0200095), Feb 24, 2002: COLLAR. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 FLAP FAIRING HORSE COLLAR. A NEW COLLAR WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0200094](https://openairdocs.org/sdr/CALA0200094), Feb 24, 2002: SKIN. CRACKED. INSPECTION FOUND A 1/2" CRACK IN R/H WING #6 FLAP FAIRING LOWER SKIN WITH RIVETS PULLING THROUGH. A STIFFENER WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0200093](https://openairdocs.org/sdr/CALA0200093), Feb 24, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1006-1016, LBL 7 AND RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-02-01.
- [SDR CALA0200092](https://openairdocs.org/sdr/CALA0200092), Feb 23, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND A RT AND LT LAV FLOOR SUPPORT CORRODED AT STA 994, RBL 14 TO RBL 44, AND LBL 14 TO LBL 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM
- [SDR CALA0200091](https://openairdocs.org/sdr/CALA0200091), Feb 23, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT STA 986-1006. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200090](https://openairdocs.org/sdr/CALA0200090), Feb 22, 2002: WEB. CRACKED. INSPECTION FOUND A 1/2" CRACK IN WEB AT STA 270, S14R. A WEB INTERCOSTAL WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0200088](https://openairdocs.org/sdr/CALA0200088), Feb 22, 2002: STRINGER. CRACKED. INSPECTION FOUND A 1" CRACK IN STRINGER 16L AFT OF STA 500C. REPAIRED STRINGER IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0200087](https://openairdocs.org/sdr/CALA0200087), Feb 22, 2002: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 663.75, LBL 65. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200086](https://openairdocs.org/sdr/CALA0200086), Feb 22, 2002: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE CORRODED AT L-2 DOOR JAMB, STA 927. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-05.
- [SDR CALA0200084](https://openairdocs.org/sdr/CALA0200084), Feb 20, 2002: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN AC BAY FLOOR SUPPORT AT STA 559, RBL 24, IN FORWARD BAGGAGE BIN. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200081](https://openairdocs.org/sdr/CALA0200081), Feb 18, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 1016, RBL 37 TO LBL 37. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851.
- [SDR CALA0200080](https://openairdocs.org/sdr/CALA0200080), Feb 17, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 967, LBL 50 TO RBL 50 AND AT RBL 18 TO LBL 18. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 
- [SDR CALA0200079](https://openairdocs.org/sdr/CALA0200079), Feb 17, 2002: ANGLE. CRACKED. INSPECTION FOUND A 3" CRACK IN ANGLE AT STA 927-947, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-03.
- [SDR CALA0200078](https://openairdocs.org/sdr/CALA0200078), Feb 16, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 951, LBL 14 TO LBL 16 AND AT LBL 18 TO LBL 24. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200077](https://openairdocs.org/sdr/CALA0200077), Feb 16, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200076](https://openairdocs.org/sdr/CALA0200076), Feb 16, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 947-967, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.

All 63: https://openairdocs.org/deregistered/N14337-2009-07-21/reports.md

## FAA accident and incident reports (2)

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 19941115043509I](https://openairdocs.org/incident/19941115043509I), Nov 15, 1994: Boeing 7372A1 (N14337), Ft Lauderdale, FL, Minor damage. Struck three landing lights on runway 09L while landing.
- [Incident 19930101008249I](https://openairdocs.org/incident/19930101008249I), Jan 1, 1993: Boeing 7373T0 (N14337), Oklahoma City, OK. Aircraft slid off icy taxiway while attempting a turn.

## Other aircraft with N14337

- [Cancelled 1979-01-24](https://openairdocs.org/deregistered/N14337-1979-01-24): Piper PA-23-250, S/N 27-7304920, built 1973. Exported to Australia. Owner: [Zed-Air Inc](https://openairdocs.org/faa-owner/ZED-AIR%20INC), [Hollister, CA](https://openairdocs.org/faa-place/CA/Hollister)

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