# N14335: 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: 23573
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 28, 1986
- Certificate issued: September 2, 1997
- Last registry action: January 19, 2010
- Mode S code: A0B0B4
- 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: 29.7633° N, 95.3633° W: Placed by OpenAirDocs: center of Houston, TX, within about 14 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14335
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14335
- Page: https://openairdocs.org/deregistered/N14335-2013-03-21

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 (75, newest 50)

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

- [SDR CALA2009042000209](https://openairdocs.org/sdr/CALA2009042000209), Apr 20, 2009: SKIN. CRACKED. DURING C-SCAN INSPECTION FOUND 1EA 1.75 INCH LONG CRACK ON S-23LT 3 INCHES AFT OF STA 727D. INSTALLED REPAIR PER 53-00-01, REPAIR 31, FIG 201, PROCEDURE V. PLAC
- [SDR CALA2009032400162](https://openairdocs.org/sdr/CALA2009032400162), Mar 23, 2009: BATTERY PACK. DISCHARGED. L2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED AFT LEFT BATTERY PACK FOR THE L2 DOOR EMERGENCY LIGHTS.
- [SDR CALA2009031600142](https://openairdocs.org/sdr/CALA2009031600142), Mar 14, 2009: SKIN. CRACKED. RT AFT FUSELAGE AFT OF STA 787 S-18R SHOWS CRACK APPROX 2 INCHES LONG. REPAIRED AS PER SRM REF 53-00-01 REPAIR 5.
- [SDR CALA2009031600141](https://openairdocs.org/sdr/CALA2009031600141), Mar 14, 2009: SKIN. CRACKED. RT AFT FUSELAGE AT STA 767 S-23R C-SCAN SHOWS INDICATION OF CRACK. REPAIRED AS PER SRM 53-00-01 REPAIR 5.
- [SDR CALA0800115](https://openairdocs.org/sdr/CALA0800115), Feb 8, 2008: INTERCOSTAL. CRACKED. BS 294.5 STRINGER 7L INTERCOSTAL WEB CRACKED AT IB FORWARD CORNER. REMOVED AND REPLACED PER ECRA 5310-04700.
- [SDR CALA0800114](https://openairdocs.org/sdr/CALA0800114), Feb 7, 2008: LINK. CORRODED. RT MAIN GEAR STABILIZER LINK HAS CORROSION AT END. REMOVED AND REPLACED RT MAIN GEAR STABILIZER LINK PER MM 57-15-00.
- [SDR CALA0800106](https://openairdocs.org/sdr/CALA0800106), Jan 31, 2008: ATTACH ANGLE. CRACKED. ATTACH ANGLE CRACKED AT STA350 STRINGER 15L AFT SIDE OF L-1 DOOR. REMOVED AND REPLACED ANGLE PER SRM 51-40-02 AND EA 354-53-002 CAL REV 2.
- [SDR CALA0800107](https://openairdocs.org/sdr/CALA0800107), Jan 30, 2008: SEAT TRACK. CORRODED. FOUND RBL 18 HAS SIGNS OF SURFACE CORROSION. REMOVED FLOORBOARDS FOR FOM IAW SRM 51-40-02. REMOVED AND REPLACED CORRODED SEAT TRACK SECTION IAW SRM 53-00-52 FIG
- [SDR CALA0500283](https://openairdocs.org/sdr/CALA0500283), Aug 26, 2005: KEELBEAM. CORRODED. INSPECTION FOUND KEEL BEAM CORRODED AT STA 500D-540, S28R. THE CORRODED SECTION OF KEEL BEAM WAS CUT OUT AND A NEW SECTION OF KEEL BEAM WAS INSTALLED IAW ECRA 5
- [SDR CALA0500270](https://openairdocs.org/sdr/CALA0500270), Aug 20, 2005: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25R IN THE AFT BAGGAGE BIN CORRODED AT STA 867-887, RBL 27. A SECTION OF STRINGER AND DOUBLERS WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0500267](https://openairdocs.org/sdr/CALA0500267), Aug 18, 2005: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616, S18L TO S19L. A FILLER AND ANGLE REPAIR WAS INSTALLED IAW ECRA 5311-01158, P
- [SDR CALA0500090](https://openairdocs.org/sdr/CALA0500090), Mar 30, 2005: SKIN. CRACKED. A 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN DURING WALKAROUND. THE CRACK WAS LOCATED APPROXIMATELY 2.5 FEET FORWARD OF AFT CARGO DOOR AND 2.5 FEET BELOW WATER
- [SDR CALA0400465](https://openairdocs.org/sdr/CALA0400465), May 5, 2004: CHARGER. INOPERATIVE. THE EMERGENCY LIGHTS IN FIRST CLASS CABIN AND AT FORWARD SERVICE ENTRY DOOR WERE FOUND INOPERATIVE. THE BATTERY CHARGER AT STA 338 WAS REPLACED IAW MM 33-51-51.
- [SDR CALA0400105](https://openairdocs.org/sdr/CALA0400105), Feb 11, 2004: SKIN. CRACKED. INSPECTION FOUND A 0.75 INCH CRACK IN NR 2 PYLON STRUT SKIN AT ACCESS DOOR 5824R CUTOUT, TOP FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER AND
- [SDR CALA0400100](https://openairdocs.org/sdr/CALA0400100), Feb 11, 2004: SKIN. DELAMINATED. INSPECTION FOUND THE NR 1 T/E FOREFLAP DELAMINATED BELOW NR 2 SPOILER PANEL, LT WING. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-37.
- [SDR CALA0400099](https://openairdocs.org/sdr/CALA0400099), Feb 10, 2004: SKIN. PUNCTURED. INSPECTION FOUND RT WING NR 6 FLIGHT SPOILER PANEL PUNCTURED IN CENTER SECTION. REPAIRED SPOILER PANEL IAW SRM 57-70-1.
- [SDR CALA0400091](https://openairdocs.org/sdr/CALA0400091), Feb 8, 2004: STRAP. CORRODED. INSPECTION FOUND STRAP UNDER BEAM AT C-2 DOOR CUTOUT I/B SILL STRUCTURE CORRODED AT STA 800. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400090](https://openairdocs.org/sdr/CALA0400090), Feb 8, 2004: STRAP. CORRODED. INSPECTION FOUND STRAP I/B OF C-2 DOOR THRESHOLD CORRODED FROM STA 787 TO 847 IN AFT BAG BIN. REPLACED STRAP IAW SRM 51-40-02.
- [SDR CALA0400082](https://openairdocs.org/sdr/CALA0400082), Feb 6, 2004: ATTACH ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN ATTACH ANGLE I/B OF NR 2 PYLON JUST AFT OF MIDSPAR ATTACH BOLT. REPAIRED ANGLE IAW SRM 51-70-12.
- [SDR CALA0300520](https://openairdocs.org/sdr/CALA0300520), Sep 9, 2003: FAN. SEIZED. THE NR 2 ENGINE GAVE OFF A LOUD BANG FOLLOWED BY VIBRATION AND THE ENGINE SPOOLED DOWN TO IDLE. THE ENGINE NEVER DID SHUTDOWN. CREW WAS UNABLE TO GET POWER ABOV
- [SDR CALA0300005](https://openairdocs.org/sdr/CALA0300005), Jan 6, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND AN 8 INCH CRACK IN LT MAIN WHEEL WELL PRESSURE DECK WEB AT STA 664-675. THE AREA WAS REPAIRED IAW SRM 53-60-51.
- [SDR CALA0300003](https://openairdocs.org/sdr/CALA0300003), Jan 6, 2003: SKIN. CRACKED. INSPECTION FOUND A 1/4" CRACK IN BELLY SKIN AFT OF EXHAUST DUCT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02894.
- [SDR CALA0200587](https://openairdocs.org/sdr/CALA0200587), Dec 15, 2002: OVEN. MALFUNCTIONED. FLIGHT ATTENDANTS REPORTED SMOKE COMING FROM BEHIND OVENS IN AFT GALLEY WHILE AT CRUISE EN ROUTE TO CLE. ASSOCIATED CIRCUIT BREAKERS WERE PULLED AND THE SMOKE C
- [SDR CALA0200492](https://openairdocs.org/sdr/CALA0200492), Oct 11, 2002: MEGAPHONE. WEAK. INSPECTION FOUND AFT PORTABLE MEGAPHONE WEAK. THE MEGAPHONE WAS REMOVED AND REPLACED.
- [SDR CALA0100961](https://openairdocs.org/sdr/CALA0100961), Oct 17, 2001: SKIN. GOUGED. FORWARD BAG BIN DOOR INNER SKIN PREVIOUS REPAIR DAMAGED / GOUGED. INSTALLED REPAIR DOUBLER PER EC/RA 5230-01633.
- [SDR CALA0100957](https://openairdocs.org/sdr/CALA0100957), Oct 16, 2001: SKIN. CRACKED. LIGHTING HOLES DAMAGED ABOVE COUNTER BALANCE CABLES AT A/B/B (1" CRACK). INSTALLED REPAIR AS PER EC/RA 5230-01632.
- [SDR CALA0100955](https://openairdocs.org/sdr/CALA0100955), Oct 16, 2001: WEB. DENTED. FORWARD CARGO DOOR INNER SKIN LOWER CENTER DENT AT LIGHTENING HOLE. INSTALLED DOUBLER REPAIR PER EC/RA 5230-1631.
- [SDR CALA0100949](https://openairdocs.org/sdr/CALA0100949), Oct 15, 2001: SKIN. CRACKED. THIRD LIGHTENING HOLE FROM AFT END OF DOOR AND THIRD LIGHTENING HOLE FROM TOP OF DOOR HAS A CRACK. INSTALLED REPAIR PER EC/RA 5230-01630.
- [SDR CALA0100945](https://openairdocs.org/sdr/CALA0100945), Oct 14, 2001: DOUBLER. GOUGED. #2 ENGINE PYLON UPPER LEFT SIDE OF PYLON ACCESS PANEL 5827 SUPPORT FOR PANEL HAS DEEP GOUGES. BLENDED AREA. INSTALLED DOUBLER PER EC/RA 5430-01230.
- [SDR CALA0100939](https://openairdocs.org/sdr/CALA0100939), Oct 10, 2001: SILL. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FORWARD LOWER SILL CORRODED AT STA 767-787, S26R. THE SILL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100938](https://openairdocs.org/sdr/CALA0100938), Oct 10, 2001: CARGO TRACK. CORRODED. INSPECTION FOUND RT TIE DOWN CHANNEL CORRODED AROUND FASTENERS AT STA 500A-500D IN FORWARD BAGGAGE BIN. THE TIE DOWN CHANNEL WAS REMOVED AND REPLACED IAW SRM 51
- [SDR CALA0100937](https://openairdocs.org/sdr/CALA0100937), Oct 10, 2001: SEAT TRACK. CRACKED. INSPECTION FOUND A 2 INCH CRACK COMING FROM HI-LOC HOLE IN BOTH THE RT AND LT O/B FLOOR TRACKS AT STA 727B. BOTH FLOOR TRACKS WERE REPAIRED IAW ECRA 5310-04202.
- [SDR CALA0100935](https://openairdocs.org/sdr/CALA0100935), Oct 6, 2001: DOUBLER. DAMAGED. INSPECTION FOUND SKIN DOUBLER TORN IN TWO LOCATIONS AT EXHAUST DUCT ATTACH POINT IN E&E COMPARTMENT BELLY OF AIRCRAFT. THE DOUBLER WAS REMOVED AND REPLACED IAW 
- [SDR CALA0100928](https://openairdocs.org/sdr/CALA0100928), Oct 3, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AT STA 947.5, LBL 6 TO RBL 6. THE FLOORBEAM UPPER CAP WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100925](https://openairdocs.org/sdr/CALA0100925), Oct 3, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT STA 294, RBL 53. THE FLOORBEAM UPPER SURFACE WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA0100921](https://openairdocs.org/sdr/CALA0100921), Oct 2, 2001: FITTING. CORRODED. INSPECTION FOUND GALLEY MOUNT FITTINGS ON FLOORBEAM CORRODED AT STA 270-294, RBL 43 AND AT STA 294, RBL 12. THE TWO GALLEY MOUNT FITTINGS WERE REMOVED AND REPLA
- [SDR CALA0100919](https://openairdocs.org/sdr/CALA0100919), Oct 2, 2001: ANGLE. CORRODED. INSPECTION FOUND FWD LAV WALL MOUNT L-ANGLES ON HAT SECTION CORRODED AT STA 302, LBL 36-56 AND AT STA 306, LBL12-43. NEW ANGLES WERE INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100920](https://openairdocs.org/sdr/CALA0100920), Oct 1, 2001: CHANNEL. CORRODED. INSPECTION FOUND FWD LAV WALL HAT SECTION CORRODED AT STA 306, LBL 36-56. THE HAT SECTION WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0100918](https://openairdocs.org/sdr/CALA0100918), Oct 1, 2001: CHANNEL. CORRODED. INSPECTION FOUND U-CHANNEL UNDER L-1 DOOR THRESHOLD CORRODED AT STA 312-344. THE CHANNEL WAS REPLACED IAW SRM 51-40-00.
- [SDR CALA0100917](https://openairdocs.org/sdr/CALA0100917), Oct 1, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 360-380. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52.
- [SDR CALA0100916](https://openairdocs.org/sdr/CALA0100916), Oct 1, 2001: FITTING. CORRODED. INSPECTION FOUND L-1 DOOR GIRT BAR LATCH ATTACH FITTING CORRODED AT STA 344. THE ATTACH FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100915](https://openairdocs.org/sdr/CALA0100915), Oct 1, 2001: ANGLE. CORRODED. INSPECTION FOUND ANGLE BELOW SCUFF PLATE AREA OF R-1 DOOR JAMB CORRODED AT STA 298-328. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100914](https://openairdocs.org/sdr/CALA0100914), Oct 1, 2001: STIFFENER. CRACKED. INSPECTION FOUND AN 8" CRACK IN STIFFENER LOCATED JUST FORWARD OF HORSE COLLAR IN #6 FLAP TRACK FAIRING. THE STIFFENER WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0100913](https://openairdocs.org/sdr/CALA0100913), Oct 1, 2001: ANGLE. CORRODED. INSPECTION FOUND L-1 DOORWAY ANGLE CORRODED AT STA 312-344, LBL 60. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100912](https://openairdocs.org/sdr/CALA0100912), Oct 1, 2001: STIFFENER. CRACKED. INSPECTION FOUND A 5" CRACK IN ANGLE STIFFENER INSIDE #3 FLAP TRACK FAIRING. THE ANGLE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0100911](https://openairdocs.org/sdr/CALA0100911), Oct 1, 2001: SPLICE. CRACKED. INSPECTION FOUND A 5" CRACK IN #3 FLAP TRACK FAIRING SPLICE. THE #3 FAIRING SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100908](https://openairdocs.org/sdr/CALA0100908), Sep 30, 2001: SKIN. CRACKED. INSPECTION FOUND A 1.125" CRACK AT UPPER R/H CORNER I/B SIDE OF CO-PILOT'S R/H WINDOW POST SKIN AND GUSSET. THE CRACKED AREA WAS ROUTED OUT AND FILLER AND DOUBL
- [SDR CALA0100906](https://openairdocs.org/sdr/CALA0100906), Sep 28, 2001: ANGLE. CRACKED. INSPECTION FOUND A 2" CRACK IN INTERCOSTAL UPPER ANGLE AT STA 380-400, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100905](https://openairdocs.org/sdr/CALA0100905), Sep 28, 2001: STRINGER. CRACKED. INSPECTION FOUND A 6" CRACK IN STRINGER 10R AT STA 338. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100904](https://openairdocs.org/sdr/CALA0100904), Sep 28, 2001: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 967-986.5, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

All 75: https://openairdocs.org/deregistered/N14335-2013-03-21/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 20000518016719I](https://openairdocs.org/incident/20000518016719I), May 18, 2000: Boeing 7373TO (N14335), Kansas City, MO. (-23)On 5-18-00 Continental flight 672 would not pressurize shortly after takeoff. The captain made an emergancy overweight landing at Kansas City…
- [Incident 19891005055519I](https://openairdocs.org/incident/19891005055519I), Oct 5, 1989: Boeing 7373T0 (N14335), Pittsburgh, PA. NR1 engine shut down. Landed without incident. Found loose b nut on oil scavange filter line.

## Other aircraft with N14335

- [Cancelled 1972-11-22](https://openairdocs.org/deregistered/N14335-1972-11-22): Piper PA-23-250, S/N 27-7304918, built 1972. Exported to Nigeria. Owner: [Moody Walter](https://openairdocs.org/faa-owner/MOODY%20WALTER), [Lock Haven, PA](https://openairdocs.org/faa-place/PA/Lock%20Haven)

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