# N14334: 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: 23572 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 30, 1986 - Certificate issued: September 2, 1997 - Last registry action: August 18, 2009 - Mode S code: A0B0B3 - 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/N14334 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14334 - Page: https://openairdocs.org/deregistered/N14334-2013-03-21 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 (76, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CAL0700595](https://openairdocs.org/sdr/CAL0700595), Oct 18, 2007: BRACKET. CRACKED. S-10L, UPPER HINGE, LOWER INTERCOSTAL, O/B ATTACHMENT CLIP CRACKED .75 INCH IN AT AFT BEND. REPAIRED PER ECRA 5311-01369. - [SDR CALA0700593](https://openairdocs.org/sdr/CALA0700593), Oct 17, 2007: BRACKET. CRACKED. INTERCOSTAL ATTACH BRACKET CRACKED AT STA 294.5 STR 11L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01368. - [SDR CALA0700591](https://openairdocs.org/sdr/CALA0700591), Oct 17, 2007: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT STA 294.5. S-16L. REMOVED AND REPLACED PER ECRA 5311-01368. - [SDR CALA0700590](https://openairdocs.org/sdr/CALA0700590), Oct 17, 2007: STRINGER. CORRODED. FBB STRINGER S-28R HAS SEVERE CORROSION AFT STA 500 FRAME CUTOUT DAMAGE. REPAIR PER SRM 53-00-03 FIG 201. - [SDR CAL0700594](https://openairdocs.org/sdr/CAL0700594), Oct 17, 2007: KEELBEAM. CORRODED. FBB KEEL BEAM S-28R HAS CORROSION ON I/B FLANGE AROUND FASTENER HOLES AFT OF 500D. REPAIRED RT KEEL BEAM AFT OF STA 500D PER ECRA 5311-01367 AND SRM 53-30-12 FI - [SDR CAL0700592](https://openairdocs.org/sdr/CAL0700592), Oct 17, 2007: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT STA 294.5 STR 12L. FABRICATED AND INSTALLED PER ECRA 5311-01368. - [SDR CALA0700588](https://openairdocs.org/sdr/CALA0700588), Oct 16, 2007: SKIN. CRACKED. C1 DOOR CRACKED AT EXT HANDLE CUTOUT. INSTALLED AND REPAIR DOUBLER IAW SRM 52-00-01 REPAIR 3. - [SDR CALA0700587](https://openairdocs.org/sdr/CALA0700587), Oct 15, 2007: SKIN. CRACKED. C2 DOOR CRACKED AT EXTERIOR DOOR HANDLE CUTOUT. TRIMMED OUT CRACKED AREA AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 52-00-01 FIG 201. - [SDR CALA0700582](https://openairdocs.org/sdr/CALA0700582), Oct 13, 2007: KEELBEAM. CORRODED. KEELBEAM CORRODED ON I/B AND O/B FLANGES AROUND FASTENERS STA 500D-520 & O/B FLANGE STA 520. REMOVED & REPLACED FWD SEC OF LEFT KEELBEAM FROM STA 500C TO STA 54 - [SDR 0700574](https://openairdocs.org/sdr/0700574), Oct 11, 2007: DOOR FRAME. CRACKED. FWD CARGO DOOR CUTOUT AFT FRAME CRACKED. REPLACED FRAME PER SRM 51-40-02. - [SDR CALA0600200](https://openairdocs.org/sdr/CALA0600200), May 6, 2006: DOUBLER. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN SECTION 41 UPPER SKIN DOUBLER AT STA 178-196.5, S2L TO S2R. THE SKIN DOUBLER WAS REPLACED IAW SRM 51-40-02 AND 53-10-01. - [SDR CALA0500224](https://openairdocs.org/sdr/CALA0500224), Jul 18, 2005: FRAME. CORRODED. INSPECTION FOUND STA 727 BULKHEAD FRAME FLANGE CORRODED BETWEEN LEFT AND RIGHT KEELBEAM AS SEEN FROM AFT CARGO COMPARTMENT, LBL 6.3. REPAIRED IAW ECRA 5311-0123 - [SDR CALA0500223](https://openairdocs.org/sdr/CALA0500223), Jul 17, 2005: SKIN. CRACKED. INSPECTION FOUND A 0.5 IN CRACK AT EDGE OF NR 1 PYLON SKIN PANEL OPENING NR 5724L UPPER FORWARD CORNER. SKIN REPAIRED IAW ECRA 5430-01204. - [SDR CALA0500222](https://openairdocs.org/sdr/CALA0500222), Jul 16, 2005: SKIN. CRACKED. INSPECTION FOUND 0.5 IN CRACK IN 2 PLACES ON NR 1 ENGINE PYLON SKIN ON EXTERNAL SURFACE ACCESS PANEL NR 5724 CUTOUT. PYLON SKIN REPAIRED IAW ECRA 5430-01204. - [SDR CALA0500221](https://openairdocs.org/sdr/CALA0500221), Jul 15, 2005: KEELBEAM. CRACKED. INSPECTION FOUND 1.0 IN CRACK IN LT KEEL BEAM AT STA 727 ON O/B SIDE, LBL 6.5. CRACKED SECTION OF KEEL BEAM LOWER CHORD CUT OUT AND NEW SECTION SPLICED IN IAW E - [SDR CALA0500215](https://openairdocs.org/sdr/CALA0500215), Jul 10, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 967, RBL 38 TO LBL 0. REPLACED FLOORBEAM UPPER CHORD IAW ECRA 5311-01231. - [SDR CALA0500209](https://openairdocs.org/sdr/CALA0500209), Jul 1, 2005: FLOOR SUPPORT. CRACKED. INSPECTION FOUND 4 INCH CRACK IN FLOOR SUPPORT AT STA 328, LBL 11. CRACKED AREA CUT OUT AND REPAIRED IAW SRM 51-70-12, FIGURE 1, SHEET 6. - [SDR CALA0400038](https://openairdocs.org/sdr/CALA0400038), Jan 17, 2004: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED AT STA 927 BETWEEN S27L AND S27R IN AFT CARGO AREA. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 53-00-07, FIGURE 210. - [SDR CALA0400037](https://openairdocs.org/sdr/CALA0400037), Jan 17, 2004: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 927 BETWEEN S27L AND S27R. INSTALLED REPAIR IAW SRM 53-00-01, FIGURE 202. - [SDR CALA0400034](https://openairdocs.org/sdr/CALA0400034), Jan 16, 2004: SKIN. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK NR 2 PYLON PANEL NR 5842R. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204. - [SDR CALA0400027](https://openairdocs.org/sdr/CALA0400027), Jan 15, 2004: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 4 SLAT SKIN LOWER SURFACE O/B OF ACTUATOR ATTACH. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLER WERE INSTAL - [SDR CALA0400025](https://openairdocs.org/sdr/CALA0400025), Jan 14, 2004: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL IN E&E COMPARTMENT CORRODED AT STA 227.8, BL 0 TO RBL 7. THE CORROSION WAS REMOVED AND THE INTERCOSTAL AND A STIFFENER WERE REMOVED - [SDR CALA0300536](https://openairdocs.org/sdr/CALA0300536), Sep 18, 2003: APU. FIRE. APU FIRE LT ILLUMINATED WHILE AT CRUISE FLT ENROUTE. FIRE BOTTLE WAS DISCHARGED, LT EXT. FLT CONTINUED W/O FURTHER PROBLEM. MAINT INSP APU AND FOUND EVIDENCE OF - [SDR CALA0100876](https://openairdocs.org/sdr/CALA0100876), Sep 14, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, RBL 4 TO LBL 24. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-04187 AND SRM 53-00-51, FIGURE 202. - [SDR CALA0100873](https://openairdocs.org/sdr/CALA0100873), Sep 13, 2001: FLOORBEAM. DAMAGED. INSPECTION FOUND A NOTCH CUT INTO FLOORBEAM WEB AT STA 328, LOCATED JUST FORWARD OF RT HORIZONTAL STABILIZER PULLEY CABLE. A REPAIR DOUBLER WAS INSTALLED IAW EC - [SDR CALA0100869](https://openairdocs.org/sdr/CALA0100869), Sep 13, 2001: RIB. GOUGED. INSPECTION FOUND R/H WING L/E RIB GOUGED AROUND SCREW HOLE AT #4 SLAT(SLAT STA 30). THE SLAT RIB WAS REPAIRED IAW ECRA 5750-03584. - [SDR CALA0100860](https://openairdocs.org/sdr/CALA0100860), Sep 11, 2001: PAN. CRACKED. INSPECTION FOUND A 0.20 INCH CRACK IN L-1 DOOR PAN AT AFT SIDE OF DOOR AT STOP SCREW BELOW CENTERING GUIDE. A DOUBLER WAS INSTALLED IAW ECRA 5210-01398. - [SDR CALA0100859](https://openairdocs.org/sdr/CALA0100859), Sep 10, 2001: PANEL. DELAMINATED. INSPECTION FOUND O/B TRAILING EDGE OF #5 SLAT PANEL DELAMINATED. THE #5 SLAT ASSY WAS REMOVED AND REPLACED IAW MM 27-81-21. - [SDR CALA0100858](https://openairdocs.org/sdr/CALA0100858), Sep 10, 2001: FITTING. CORRODED. INSPECTION FOUND RT MLG SIDE STRUT FITTING LUG CORRODED AT STA 685. THE LUG WAS REPAIRED IAW ECRA 5340-01354. - [SDR CALA0100849](https://openairdocs.org/sdr/CALA0100849), Sep 9, 2001: SLAT. DENTED. INSPECTION FOUND #3 SLAT LEADING EDGE DENTED APPROXIMATELY 30" FROM O/B END. REPAIRED SLAT IAW SRM 57-43-01. - [SDR CALA0100840](https://openairdocs.org/sdr/CALA0100840), Sep 7, 2001: SKIN. DENTED. INSPECTION FOUND C-1 DOOR SKIN DENTED 13 INCHES AFT OF FORWARD EDGE AND 12 INCHES FROM TOP. A DOUBLER WAS INSTALLED IAW SRM 52-00-01. - [SDR CALA0100838](https://openairdocs.org/sdr/CALA0100838), Sep 7, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FASTENER HOLE AFT OF STA 787, BL 0. A REPAIR WAS INSTALLED IAW SRM 53-00-53. - [SDR CALA0100836](https://openairdocs.org/sdr/CALA0100836), Sep 6, 2001: PLATE. CRACKED. INSPECTION FOUND A 3" CRACK ON UPPER WEB OF DOOR THRESHOLD PLATE AT STA 847. A NEW THRESHOLD PLATE WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0100834](https://openairdocs.org/sdr/CALA0100834), Sep 5, 2001: SEAT TRACK. CRACKED. INSPECTION FOUND A 1/2" CRACK IN L/H I/B SEAT TRACK AT AFT HI-LOCK, STA 727B. STRAP AND FILLER WERE INSTALLED IAW ECRA 5310-04183. - [SDR CALA0100833](https://openairdocs.org/sdr/CALA0100833), Sep 5, 2001: SEAT TRACK. CRACKED. INSPECTION FOUND A 1/4" CRACK IN UPPER FLANGE OF L/H O/B SEAT TRACK AT HI-LOCK ATTACH POINT, STA 727B. A STRAP WAS INSTALLED IAW ECRA 5310-04183. - [SDR CALA0100832](https://openairdocs.org/sdr/CALA0100832), Sep 4, 2001: STRINGER. CRACKED. INSPECTION FOUND A 4" CRACK IN STRINGER 10R AT STA 332. THE STRINGER WAS REMOVED AND REPLACED IAW EA 5363-01014. - [SDR CALA0100831](https://openairdocs.org/sdr/CALA0100831), Sep 4, 2001: INTERCOSTAL. CRACKED. INSPECTION FOUND A 4" CRACK IN INTERCOSTAL AT STA 332, STRINGER 10R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C33288 AND EA 5363-01014. - [SDR CALA0100830](https://openairdocs.org/sdr/CALA0100830), Sep 4, 2001: ANGLE. CORRODED. INSPECTION FOUND R/H LAV WALL & L/H LAV WALL ANGLES CORRODED AT STA 1014 RBL 4 AND LBL 4. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0100829](https://openairdocs.org/sdr/CALA0100829), Sep 2, 2001: ANGLE. CORRODED. INSPECTION FOUND ATTACH ANGLE FOR R/H AFT I/B WHEEL WELL FAIRING CORRODED ON FORWARD CURVED ATTACH POINTS. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51- - [SDR CALA0100822](https://openairdocs.org/sdr/CALA0100822), Aug 29, 2001: BRACE. CORRODED. INSPECTION FOUND L/H AND R/H DIAGONAL BRACES CORRODED AT STA 1006-1016. NEW DIAGONAL BRACES WERE INSTALLED IAW SRM 51-10-02. - [SDR CALA0100821](https://openairdocs.org/sdr/CALA0100821), Aug 29, 2001: STRAP. CORRODED. INSPECTION FOUND "H" STRAP IN AFT LAV AREA CORRODED. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0100820](https://openairdocs.org/sdr/CALA0100820), Aug 29, 2001: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100819](https://openairdocs.org/sdr/CALA0100819), Aug 29, 2001: ANGLE. CORRODED. INSPECTION R-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100818](https://openairdocs.org/sdr/CALA0100818), Aug 29, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND THREE FLOOR SUPPORTS CORRODED AT STA 950 FROM RBL 24 TO RBL 53. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW ECRA 5310-03585. - [SDR CALA0100817](https://openairdocs.org/sdr/CALA0100817), Aug 29, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 947 - 967, RBL 30 AND STA 967-987, RBL 16. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW ECRA 5310-03585. - [SDR CALA0100811](https://openairdocs.org/sdr/CALA0100811), Aug 27, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 907-947.5. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100810](https://openairdocs.org/sdr/CALA0100810), Aug 27, 2001: MOUNT. CORRODED. INSPECTION FOUND R/H AFT O/B GALLEY MOUNT CORRODED. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100803](https://openairdocs.org/sdr/CALA0100803), Aug 26, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT STA 312, LBL 24 TO RBL 23. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0100805](https://openairdocs.org/sdr/CALA0100805), Aug 25, 2001: ANGLE. CORRODED. INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 294-312, RBL 12. A NEW FLOOR SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0100804](https://openairdocs.org/sdr/CALA0100804), Aug 25, 2001: MOUNT. CORRODED. INSPECTION FOUND GALLEY FLOOR MOUNT CORRODED AT STA 292, RBL 12. A NEW GALLEY FLOOR MOUNT WAS INSTALLED IAW SRM 51-10-02. All 76: https://openairdocs.org/deregistered/N14334-2013-03-21/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 19980212012209I](https://openairdocs.org/incident/19980212012209I), Feb 12, 1998: Boeing 7373T0 (N14334), Cleveland, OH, Minor damage. Narrative: cala flt #438 lost a #1 main tire recap on t.o. out of fmy. A/c landed cle with no further incident. Cala maint. Discovered the recap missing and… --- 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.