# N14358: 1988 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: 23943
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 3, 1988
- Certificate issued: June 5, 2009
- Last registry action: June 5, 2009
- Mode S code: A0B0FD
- 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/N14358
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14358
- Page: https://openairdocs.org/deregistered/N14358-2013-03-21

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 (53, newest 50)

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

- [SDR CALA0700388](https://openairdocs.org/sdr/CALA0700388), Aug 1, 2007: FUSE. INOPERATIVE. THE EMERGENCY LIGHT OVER COCKPIT DOOR WAS FOUND INOPERATIVE. THE F2 FUSE ON BATTERY PACK M1133 WAS REMOVED AND REPLACED IAW AMM 33-51-51.
- [SDR CALA0700233](https://openairdocs.org/sdr/CALA0700233), May 4, 2007: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN ANGLE CLIP AT BS 348.20, S16L. REPAIRED IAW ECRA 5311-01320.
- [SDR CALA0700232](https://openairdocs.org/sdr/CALA0700232), May 4, 2007: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN ANGLE CLIP AT STA 351.20, S16L. REPAIRED IAW ECRA 5311-01320.
- [SDR CALA0700231](https://openairdocs.org/sdr/CALA0700231), May 4, 2007: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN ANGLE CLIP AT BS 348.20, S16L. REPAIRED IAW ERCA 5311-01320.
- [SDR CALA0700226](https://openairdocs.org/sdr/CALA0700226), May 2, 2007: KEELBEAM. CRACKED. INSPECTION FOUND A 2" CRACK IN LT KEEL BEAM AT STA 540, S29L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, PAGE 206, DETAIL NR 2.
- [SDR CALA0700224](https://openairdocs.org/sdr/CALA0700224), May 2, 2007: FRAME. CRACKED. INSPECTION FOUND A 1/4" CRACK IN THE FORWARD BAGGAGE BIN FORWARD FRAME AT THE FOURTH STOP PAD FROM TOP, STA 440, S13R TO S28R. THE FRAME WAS REMOVED AND REPLACE
- [SDR CALA0700223](https://openairdocs.org/sdr/CALA0700223), May 1, 2007: STOP FITTING. CRACKED. INSPECTION FOUND A 1" CRACK IN L-1 DOOR TOP AFT STOP FITTING. THE STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0700056](https://openairdocs.org/sdr/CALA0700056), Feb 7, 2007: SKIN. CRACKED. INSPECTION FOUND A 1.875 INCH CRACK IN FORWARD GALLEY DOOR CUTOUT LOWER CORNER FUSELAGE FRAME SKIN, STA 330, L17R. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5331
- [SDR CALA0500463](https://openairdocs.org/sdr/CALA0500463), Dec 22, 2005: STIFFENER. CRACKED. A 2 INCH CRACK WAS FOUND TO THE WING CENTER SECTION REAR SPAR AT STA 540, RBL 6.15 VERTICAL STIFFENER DURING A WALKAROUND INSPECTION. AN INTERIM REPAIR WAS INST
- [SDR CALA0500216](https://openairdocs.org/sdr/CALA0500216), Jul 11, 2005: SKIN. CRACKED. WALK AROUND FOUND 3.5 IN CRACK IN STA 767 LOWER LAP SKIN, S25L. REPAIRED IAW SRM 53-00-01, FIGURE 229. DIP WAS ISSUED TO REINSPECT REPAIR EVERY 60,000 CYCLES.
- [SDR CALA0500111](https://openairdocs.org/sdr/CALA0500111), Apr 17, 2005: TRU. SMOKE. DURING CRUISE, ELECTRICAL SMOKE IN COCKPIT AND CABIN. REPLACED NR 2 TRANSFORMER RECTIFIER PER AMM 24.
- [SDR CALA0500003](https://openairdocs.org/sdr/CALA0500003), Jan 8, 2005: SKIN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN L-1 DOOR SKIN AT UPPER AFT INSPECTION HOLE. THE SKIN WAS REPAIRED IAW ECRA 5210-01812.
- [SDR CALA0400752](https://openairdocs.org/sdr/CALA0400752), Dec 29, 2004: STRINGER. CORRODED. INSPECTION FOUND RT APU TORQUE BOX CORRODED ON TOP STRINGER 14R AT AIR INLET CUTOUT, STA 1121-1156. THE UPPER APU TORQUE BOX STRINGER WAS REMOVED AND REPLACED I
- [SDR CALA0400751](https://openairdocs.org/sdr/CALA0400751), Dec 19, 2004: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR THRESHOLD ZEE ANGLE CORRODED AT STA 907-1006, LBL 58. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400747](https://openairdocs.org/sdr/CALA0400747), Dec 18, 2004: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT FASTENER OF STRINGER 4L SPLICE, STA 907. REPLACED STRINGER SPLICE IAW SRM 51-10-02.
- [SDR CALA0400745](https://openairdocs.org/sdr/CALA0400745), Dec 17, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK BELOW G-1 GALLEY CORRODED AT STA 290. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02 AND BOEING DRAW
- [SDR CALA0300674](https://openairdocs.org/sdr/CALA0300674), Nov 21, 2003: STRINGER. CORRODED. INSPECTION FOUND STRINGERS 26R AND 27R IN FORWARD CARGO AREA CORRODED AT STA 535-539. A STRINGER SECTION REPAIR WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0300659](https://openairdocs.org/sdr/CALA0300659), Nov 21, 2003: SKIN. LIGHTNING STRIKE. INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON RUDDER T/E APPROXIMATELY 30 INCHES BELOW STATIC WICK. REPAIRED IAW ECRA 5540-01171.
- [SDR CALA0300646](https://openairdocs.org/sdr/CALA0300646), Nov 14, 2003: FRAME. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME FITTING JUST BELOW CABIN FLOOR AT BOTTOM TWO FASTENERS, STA 616, W/ 200, LT SIDE. REPAIRED IAW ECRA 5311-01158.
- [SDR CALA0300645](https://openairdocs.org/sdr/CALA0300645), Nov 14, 2003: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FRAME INNER CHORD AT STA 616, WL 200, RT SIDE. THE INNER CHORD WAS REPAIRED IAW ECRA 5311-01158.
- [SDR CALA0300043](https://openairdocs.org/sdr/CALA0300043), Feb 6, 2003: SKIN. CRACKED. INSPECTION FOUND A 1.5" CRACK IN FUSELAGE SKIN BETWEEN STA 727D +9.9 AND STA 727E JUST ABOVE S23L. THE SKIN WAS REPAIRED IAW ECRA 5330-03205.
- [SDR CALA0100663](https://openairdocs.org/sdr/CALA0100663), Jul 20, 2001: STOP FITTING. GOUGED. INSPECTION FOUND C-2 DOOR FORWARD LOWER STOP FITTING GOUGED. THE STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-2.
- [SDR CALA0100662](https://openairdocs.org/sdr/CALA0100662), Jul 20, 2001: SKIN. CRACKED. INSPECTION FOUND A 0.375" CRACK IN SKIN AT C-2 DOOR LIGHTENING HOLE ABOVE INTERIOR HANDLE. A DOUBLER WAS INSTALLED IAW ECRA 5230-01613.
- [SDR CALA0100661](https://openairdocs.org/sdr/CALA0100661), Jul 20, 2001: FRAME. DENTED. INSPECTION FOUND FRAME DENTED AT STA 787, S25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11, FIGURE 1.
- [SDR CALA0100659](https://openairdocs.org/sdr/CALA0100659), Jul 17, 2001: SPAR. CRACKED. INSPECTION FOUND A CRACK INDICATION IN NR 2 HOLE OF LT WING REAR SPAR UPPER CHORD AT GEAR BEAM CASTING ATTACH POINT. THE HOLE WAS REAMED AND THE CRACK WAS FOUND
- [SDR CALA0100656](https://openairdocs.org/sdr/CALA0100656), Jul 14, 2001: SKIN. DENTED. INSPECTION FOUND C-2 DOOR EXTERNAL SKIN DENTED AT LOWER AFT CORNER. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.
- [SDR CALA0100654](https://openairdocs.org/sdr/CALA0100654), Jul 13, 2001: SKIN. CRACKED. INSPECTION FOUND A 1.6" CRACK IN L/H HORIZONTAL STABILIZER LOWER SKIN ALONG REAR SPAR AREA AT STA 138.7. THE SKIN WAS REPAIRED IAW ECRA 5510-01586.
- [SDR CALA0100650](https://openairdocs.org/sdr/CALA0100650), Jul 11, 2001: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 219, S23L, TEN INCHES ABOVE L/H SIDE OF FORWARD ACCESSORY DOOR AT EDGE OF BONDED DOUBLER. THE DENTED SKIN WAS REMOVE
- [SDR CALA0100647](https://openairdocs.org/sdr/CALA0100647), Jul 10, 2001: SKIN. DENTED. INSPECTION FOUND TWO DENTS IN FORWARD CARGO DOOR EXTERNAL SKIN AT CENTER OF DOOR AND 14" FROM AFT EDGE OF DOOR. A DOUBLER WAS INSTALLED IAW SRM 52-00-01.
- [SDR CALA0100646](https://openairdocs.org/sdr/CALA0100646), Jul 10, 2001: SKIN. CRACKED. INSPECTION FOUND A 1" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN FORWARD OF AFT SPAR AT I/B ELEVATOR BALANCE PANEL. THE SKIN WAS REPAIRED IAW ECRA 5510-01585
- [SDR CALA0100645](https://openairdocs.org/sdr/CALA0100645), Jul 10, 2001: ANGLE. CORRODED. INSPECTION FOUND COCKPIT FLOOR Z-ANGLE CORRODED AT BS 270, LBL 10 TO RBL 10. A REPAIR WAS INSTALLED IAW ECRA 5320-01683.
- [SDR CALA0100644](https://openairdocs.org/sdr/CALA0100644), Jul 9, 2001: SKIN. DENTED. INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 917, S19L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01.
- [SDR CALA0100640](https://openairdocs.org/sdr/CALA0100640), Jul 8, 2001: SKIN. DENTED. INSPECTION FOUND THREE DENTS ON C-1 DOOR EXTERNAL SKIN. THE DENTS WERE LOCATED 12 INCHES FROM FORWARD EDGE OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00
- [SDR CALA0100639](https://openairdocs.org/sdr/CALA0100639), Jul 8, 2001: ACCESS PANEL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL 5727. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.
- [SDR CALA0100637](https://openairdocs.org/sdr/CALA0100637), Jul 6, 2001: SKIN. DAMAGED. INSPECTION FOUND FUSELAGE SKIN "DAMAGED" AT STA 807, S28L TO S26R. THE DAMAGE WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-00-01.
- [SDR CALA0100602](https://openairdocs.org/sdr/CALA0100602), Jun 25, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, BL 0 TO LBL 59. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA0100590](https://openairdocs.org/sdr/CALA0100590), Jun 23, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 49. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA9901039](https://openairdocs.org/sdr/CALA9901039), Jul 22, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED ON UPPER CHORD LOWER SURFACE FORWARD AND AFT OF STA 986.5, RBL 25-35. REPAIRED IAW ECRA 5310-03851.
- [SDR CALA9900065](https://openairdocs.org/sdr/CALA9900065), Jan 17, 1999: WIRE. PINCHED. ROW 7 TO 12 EMERGENCY LIGHTS INOP. FOUND WIRE PINCHED IN SEAT TRACK AT ROW 12. REPAIRED WIRE, OPS CHECK GOOD.
- [SDR CALA9701003](https://openairdocs.org/sdr/CALA9701003), Jun 9, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED UNDER LEFT AFT LAV AT STA 1016. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-00-51, PAGES 207 TO 211.
- [SDR CALA9701002](https://openairdocs.org/sdr/CALA9701002), Jun 9, 1997: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE AT L-2 DOOR LOWER JAMB CORRODED FROM STA 947.5 TO 986.5. THE ANGLE WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9701001](https://openairdocs.org/sdr/CALA9701001), Jun 9, 1997: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE AT LOWER R-2 DOOR JAMB CORRODED FROM STA 947.5 TO 1006. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-3
- [SDR CALA9701000](https://openairdocs.org/sdr/CALA9701000), Jun 9, 1997: WEB. CORRODED. INSPECTION FOUND WEB CORRODED UNDER RIGHT LAV FROM STA 1016 TO 1040. THE WEB WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9700999](https://openairdocs.org/sdr/CALA9700999), Jun 9, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03450.
- [SDR CALA9700998](https://openairdocs.org/sdr/CALA9700998), Jun 9, 1997: STRINGER. CRACKED. INSPECCTION FOUND A .5 INCH CRACK IN STRINGER 16L AT STA 500C. THE CRACKED AREA OF STRINGER WAS REMOVED, REPAIR DOUBLER, FILLER, AND CHANNEL WERE FABRICATED AND
- [SDR CALA9700997](https://openairdocs.org/sdr/CALA9700997), Jun 9, 1997: FRAME. CORRODED. INSPECTION FOUND BELTFRAME WEB AND CHORD CORRODED AT STA 1121R. THE WEB AND CHORD WERE REPLACED IAW SRM 51-10-02.
- [SDR CALA9700996](https://openairdocs.org/sdr/CALA9700996), Jun 9, 1997: ANGLE. CORRODED. INSPECTION FOUND ANGLE CORRODED AT STA 1121R, WL 240. THE ANGLE WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA9700991](https://openairdocs.org/sdr/CALA9700991), Jun 9, 1997: WEB. CORRODED. INSPECTION FOUND WEB UNDER LEFT AFT LAV CORRODED AT STA 1016 TO 1040. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9700995](https://openairdocs.org/sdr/CALA9700995), Jun 8, 1997: ANGLE. CORRODED. INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 276R TO 300R. THE FLOOR ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA9700994](https://openairdocs.org/sdr/CALA9700994), Jun 8, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 228L TO 312L, LBL 26.75. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-2.

All 53: https://openairdocs.org/deregistered/N14358-2013-03-21/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 20050430019209I](https://openairdocs.org/incident/20050430019209I), Apr 30, 2005: Boeing 7373TO (N14358), Norfolk, VA. (-23) Flight 1205 departed on 04/30/05, from cle and while enroute to tpa, the 1st class cabin flight attendant reported that an oven started to emit a smoke.…
- [Incident 19970218009109I](https://openairdocs.org/incident/19970218009109I), Feb 18, 1997: Boeing 7373T0 (N14358), Cleveland, OH. Narrative: aircraft experienced pressurization problem 100 miles east of Cleveland, descended to 10,000 feet and landed at Cleveland without incident…

## Other aircraft with N14358

- [Cancelled 1955-10-19](https://openairdocs.org/deregistered/N14358-1955-10-19): Fairchild 24 C8C, S/N 2621. Owner: [Joseph W Cross](https://openairdocs.org/faa-owner/JOSEPH%20W%20CROSS), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)

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