# N14347: 1987 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: 23585
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 29, 1987
- Certificate issued: December 18, 2008
- Last registry action: January 23, 2013
- Mode S code: A0B0D9
- 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/N14347
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14347
- Page: https://openairdocs.org/deregistered/N14347-2013-03-21

From the FAA registry file of November 4, 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 (80, newest 50)

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

- [SDR CALA0700576](https://openairdocs.org/sdr/CALA0700576), Oct 14, 2007: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT SIGN IN ADT GALLEY CENTER ASSOCIATED WITH CUSTOMER CALL LIGHT ILLUMINATES INTERMITTENTLY INFLIGHT. FOUND PROBLEM PIN NR 2 ON PWR SUPP CONNECTOR. 
- [SDR CALA0700563](https://openairdocs.org/sdr/CALA0700563), Oct 4, 2007: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR OUTER SKIN AT DOOR HANDLE CUTOUT. THE CRACKED AREA OF SKIN WAS CUTOUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLE
- [SDR CALA0700603](https://openairdocs.org/sdr/CALA0700603), Oct 3, 2007: SKIN. CRACKED. INSPECTION FOUND CRACKS IN THE INNER SKIN OF THE AFT CARGO DOOR AT LIGHTENING HOLES ABOVE THE DOOR HANDLE CUTOUT. THE SKIN WAS REPAIRED IAW ECRA 5232-01092.
- [SDR CALA0700561](https://openairdocs.org/sdr/CALA0700561), Oct 2, 2007: WEB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AND STRINGER 12L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700560](https://openairdocs.org/sdr/CALA0700560), Oct 2, 2007: STRINGER CLIP. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 11L FORWARD SUPPORT CLIP. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311
- [SDR CALA0700559](https://openairdocs.org/sdr/CALA0700559), Oct 2, 2007: WEB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 15L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700558](https://openairdocs.org/sdr/CALA0700558), Oct 2, 2007: WEB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 16L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700557](https://openairdocs.org/sdr/CALA0700557), Oct 2, 2007: WEB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 303.9 AT STRINGER 16L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700556](https://openairdocs.org/sdr/CALA0700556), Oct 2, 2007: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 TO 303.9 AT STRINGER 10L O/B SUPPORT ANGLE FOR WEB. WEB INTERCOSTALS WERE INSTALLED I
- [SDR CALA0700555](https://openairdocs.org/sdr/CALA0700555), Oct 2, 2007: STRINGER CLIP. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 10L ANGLE CLIP. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01361.
- [SDR CALA0700552](https://openairdocs.org/sdr/CALA0700552), Oct 2, 2007: SUPPORT. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR AFT SIDE SUPPORT CLIP AT STA 360, S10L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01363.
- [SDR CALA0700551](https://openairdocs.org/sdr/CALA0700551), Oct 2, 2007: SUPPORT. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE FORWARD SUPPORT CLIP AT STA 360, S15L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01363.
- [SDR CALA0700550](https://openairdocs.org/sdr/CALA0700550), Oct 2, 2007: SUPPORT. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE STA 360 SUPPORT CLIP AT STRINGER 8L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01363.
- [SDR CALA0700549](https://openairdocs.org/sdr/CALA0700549), Oct 2, 2007: STRINGER. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE STRINGER 15L AT STA 360. REPAIRED IAW ECRA 5311-01363.
- [SDR CALA0700548](https://openairdocs.org/sdr/CALA0700548), Oct 1, 2007: SKIN. CRACKED. INSPECTION FOUND A 0.5 INCH CRACK IN FUSELAGE SKIN AT STA 727D +3 BELOW STRINGER 23R. A DOUBLER WAS INSTALLED IAW ECRA 5330-03730 AND SRM 53-00-01, FIGURE 201, 
- [SDR CALA0700545](https://openairdocs.org/sdr/CALA0700545), Oct 1, 2007: PAN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR FORWARD UPPER PAN AT PULLEY BRACKET ATTACH POINT. THE FRAME PAN WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0700544](https://openairdocs.org/sdr/CALA0700544), Oct 1, 2007: DOOR FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR AT FORWARD LOWER PAN PULLEY BRACKET. THE LOWER FRAME PAN WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0700547](https://openairdocs.org/sdr/CALA0700547), Sep 30, 2007: SHEAR TIE. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 947 BETWEEN STRINGERS 23L AND 24L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700553](https://openairdocs.org/sdr/CALA0700553), Sep 29, 2007: SKIN. DELAMINATED. INSPECTION FOUND LT SIDE OF RUDDER T/E SKIN DELAMINATED AT STA 175.0. THE DELAMINATION MEASURED 0.4"L X 0.2"W. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5540-01
- [SDR CALA0700546](https://openairdocs.org/sdr/CALA0700546), Sep 27, 2007: SKIN. CRACKED. INSPECTION FOUND A 0.8 INCH CRACK IN R-1 DOOR CUTOUT AFT LOWER CORNER OUTER SKIN, STA 328-344, S16R TO S17R. A REPAIR WAS INSTALLED IAW SRM 53-10-01, REPAIR 2, 
- [SDR CALA0700542](https://openairdocs.org/sdr/CALA0700542), Sep 27, 2007: PAN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN L-1 DOOR PAN ON AFT SIDE AT 5TH DOOR STOP FROM BOTTOM. THE DOOR PAN WAS REPAIRED IAW ECRA 5210-01954.
- [SDR CALA0700540](https://openairdocs.org/sdr/CALA0700540), Sep 27, 2007: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INTERIOR SKIN AT 4TH DOOR STOP FROM BOTTOM OF L-1 DOOR, STA 312, S13L. THE DOOR SKIN WAS REPAIRED IAW ECRA 5210-01954.
- [SDR CALA0700538](https://openairdocs.org/sdr/CALA0700538), Sep 25, 2007: KEELBEAM. CORRODED. INSPECTION FOUND O/B SPLICE CORRODED ON RIGHT KEEL BEAM FORWARD OF STA 727, RBL 7, IN AFT BAG BIN. THE SPLICE WAS REMOVED AND A NEW SPLICE ANGLE WAS INSTALLED I
- [SDR CALA0700537](https://openairdocs.org/sdr/CALA0700537), Sep 25, 2007: SKIN. CRACKED. INSPECTION FOUND A .75 INCH CRACK WITH CREASE IN SKIN AT STA 900 BETWEEN S23R AND S24R. THE DAMAGED AREA OF SKIN WAS REMOVED AND DOUBLER AND FILLER WERE INSTALL
- [SDR CALA0700532](https://openairdocs.org/sdr/CALA0700532), Sep 23, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED AT FORWARD ENTRY STA 344, BL 0. REPAIRED FLOORBEAM IAW SRM 53-10-51.
- [SDR CALA0700528](https://openairdocs.org/sdr/CALA0700528), Sep 22, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 22L CORRODED AT STA 1013. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA0700524](https://openairdocs.org/sdr/CALA0700524), Sep 18, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED NEAR FOWRD ENTRY DOOR AT STA 312, BL 0 TO LBL 10. THE UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600290](https://openairdocs.org/sdr/CALA0600290), Aug 2, 2006: STRINGER. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 21L CORRODED ON UPPER FLANGE AT STA 897. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0600281](https://openairdocs.org/sdr/CALA0600281), Jul 30, 2006: SKIN PANEL. CRACKED. INSPECTION FOUND A 2" CRACK IN BOTTOM SKIN PANEL BETWEEN KEEL BEAMS AT STA 685, S29L TO S29R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-
- [SDR CALA0600278](https://openairdocs.org/sdr/CALA0600278), Jul 30, 2006: WEB. CORRODED. INSPECTION FOUND WEB AT L-1 DOOR CORRODED FROM STA 312-350, LBL 62. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 53-10-15 AND 51-10-15.
- [SDR CALA0600275](https://openairdocs.org/sdr/CALA0600275), Jul 29, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND RT I/B CABIN SEAT TRACK CORRODED AT STA 847, RBL 24. A REPAIR WAS INSTALLED IAW SRM 53-60-52.
- [SDR CALA0400147](https://openairdocs.org/sdr/CALA0400147), Feb 21, 2004: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 400 BETWEEN S17L AND S18L. REPAIRED IAW ECRA 5331-01139.
- [SDR CALA0400145](https://openairdocs.org/sdr/CALA0400145), Feb 20, 2004: SKIN. GOUGED. INSPECTION FOUND NR 3 MID FLAP OUTBOARD L/E SKIN GOUGED JUST FORWARD OF EXHAUST GATE. FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5752-01144.
- [SDR CALA0400144](https://openairdocs.org/sdr/CALA0400144), Feb 20, 2004: STIFFENER. CORRODED. INSPECTION FOUND AFT PRESSURE BULKHEAD LOWER WEB AND STIFFENER CORRODED JUST AFT OF FS 1016, S23L. REPAIRED IAW ECRA 5311-01186.
- [SDR CALA0400142](https://openairdocs.org/sdr/CALA0400142), Feb 20, 2004: SKIN. CRACKED. INSPECTION FOUND 0.2 INCH CRACKS AT THREE FASTENERS IN NR 3 SLAT LOWER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.
- [SDR CALA0400141](https://openairdocs.org/sdr/CALA0400141), Feb 20, 2004: SUPPORT FITTING. CRACKED. INSPECTION FOUND NR 2 ENGINE PYLON O/B MID SPAR FITTING PANEL AFT RETAINER (SUPPORT FITTING) CRACKED AT UPPER AREA, PYLON STA 279.5. THE SUPPORT FITTING WAS REM
- [SDR CALA0400135](https://openairdocs.org/sdr/CALA0400135), Feb 19, 2004: ATTACH FITTING. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN NR 2 PYLON PANEL 5842 FORWARD ATTACH RAIL. THE ATTACH RAIL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400132](https://openairdocs.org/sdr/CALA0400132), Feb 17, 2004: SKIN. DENTED. INSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 875 BELOW S19R AFT OF C-2 DOOR. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 210.
- [SDR CALA0400131](https://openairdocs.org/sdr/CALA0400131), Feb 17, 2004: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 1.2 INCH CRACK IN NR 2 FLAP TRACK FAIRING ATTACH ANGLE. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0400126](https://openairdocs.org/sdr/CALA0400126), Feb 16, 2004: ATTACH ANGLE. CORRODED. INSPECTION FOUND ATTACH ANGLE FOR FLOOR PANEL AROUND GEAR DOWNLOCK VIEWER CORRODED AT AFT ATTACH ANGLE, BS 270, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5321-01172
- [SDR CALA0400124](https://openairdocs.org/sdr/CALA0400124), Feb 16, 2004: WEB. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN C-2 DOOR OPENING LOWER FORWARD SILL WEB AT STA 787. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400123](https://openairdocs.org/sdr/CALA0400123), Feb 15, 2004: CARGO TRACK. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN TIE DOWN RAIL CORRODED AT FASTENER HOLES FROM STA 787-847. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 53-0
- [SDR CALA0400115](https://openairdocs.org/sdr/CALA0400115), Feb 14, 2004: ANGLE. CORRODED. INSPECTION FOUND ANGLE ATTACHED TO FORWARD WALL OF NOSE WHEEL WELL CORRODED AT STA 227, RBL 14. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400114](https://openairdocs.org/sdr/CALA0400114), Feb 13, 2004: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 324 JUST BENEATH S20R. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.
- [SDR CALA0400112](https://openairdocs.org/sdr/CALA0400112), Feb 13, 2004: HINGE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN R-2 DOOR HINGE HOUSING AT LOWER SURFACE, STA 954, RBL 55, WL 230. THE HOUSING WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400111](https://openairdocs.org/sdr/CALA0400111), Feb 13, 2004: FLOORBEAM. CORRODED. INSPECTION FOUND AFT CARGO FLOORBEAMS UNDER CROSS STRAP CORRODED AT STA 767 + 6, RBL 8, RBL 3, AND LBL 3. REPAIRS WERE INSTALLED IAW ECRA 5320-01603.
- [SDR CALA0400107](https://openairdocs.org/sdr/CALA0400107), Feb 12, 2004: INTERCOSTAL. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN AFT BAGGAGE BIN INTERCOSTAL UNDER TRANSITION PANEL AT STA 928, RBL 26. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10
- [SDR CALA0400106](https://openairdocs.org/sdr/CALA0400106), Feb 12, 2004: WEB. CORRODED. INSPECTION FOUND AFT WEB RT SIDE ADJACENT TO RUBBER MEMBRANE AT APB, STA 1016, RBL 0 TO RBL 48, CORRODED. A NEW WEB WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0400098](https://openairdocs.org/sdr/CALA0400098), Feb 9, 2004: WEB. CORRODED. INSPECTION FOUND SHEAR WEB IN RT AFT LAV AREA CORRODED AT FS 1019, RBL 28. THE SHEAR WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400097](https://openairdocs.org/sdr/CALA0400097), Feb 9, 2004: WEB. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN SHEAR WEB PANEL FORWARD OF STA 578, S17L. THE WEB WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-70-13. THE WEB WAS REINST

All 80: https://openairdocs.org/deregistered/N14347-2013-03-21/reports.md

## 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 19930823039019I](https://openairdocs.org/incident/19930823039019I), Aug 23, 1993: Boeing 7373T0 (N14347), Reno, NV, Minor damage. NR2 engine failed in flight. Diverted to mono lake. Forward lavatory flush cap was left unsecured. Blue ice in engine

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