# N17344: 1987 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: 23582 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 13, 1987 - Certificate issued: April 17, 2007 - Last registry action: September 13, 2010 - Mode S code: A12753 - 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/N17344 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17344 - Page: https://openairdocs.org/deregistered/N17344-2013-03-21 From the FAA registry file of November 3, 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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0600288](https://openairdocs.org/sdr/CALA0600288), Aug 1, 2006: SKIN. CRACKED. INSPECTION FOUND A 2" CRACK IN AFT CARGO DOOR INNER SKIN AT LOWER FORWARD LIGHTENING HOLE CUTOUT. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01078. - [SDR CALA0600287](https://openairdocs.org/sdr/CALA0600287), Aug 1, 2006: SKIN. CRACKED. INSPECTION FOUND A 1.4" CRACK IN C-2 DOOR SKIN AT LIGHTENING HOLE APPROXIMATELY 21 INCHES DOWN FROM UPPER DOOR FRAME AND 18 INCHES FORWARD OF AFT DOOR FRAME. TH - [SDR CALA0600277](https://openairdocs.org/sdr/CALA0600277), Jul 29, 2006: STRINGER. CRACKED. INSPECTION FOUND A 1" CRACK IN STRINGER 14L AT L-1 DOOR, STA 360-380. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02 AND ECRA 5311-01262. - [SDR CALA0600276](https://openairdocs.org/sdr/CALA0600276), Jul 29, 2006: STRINGER. CRACKED. INSPECTION FOUND A 1" CRACK IN S15L AT L-1 DOOR AFT SIDE, STA 360-380. THE STRINGER U CHANNEL WAS REMOVED AND REPLACED IAW ECRA 5311-01262. - [SDR CALA0600272](https://openairdocs.org/sdr/CALA0600272), Jul 26, 2006: BELTFRAME. CORRODED. INSPECTION FOUND BELTFRAME CORRODED AT STA 500C, S26L-27L, LBL 17 - LBL 22. A SHEAR TIE REPAIR ANGLE AND FILLER WERE INSTALLED IAW SRM 53-00-07, REPAIR 1, FIGUR - [SDR CALA0600271](https://openairdocs.org/sdr/CALA0600271), Jul 26, 2006: SHEAR TIE. CORRODED. INSPECTION FOUND CORROSION AROUND CLIP AT STA 500D BETWEEN S26L AND S27L, LBL 17-22. A SHEAR TIE REPAIR AND FILLER WERE INSTALLED IAW SRM 53-00-07, REPAIR 2, FI - [SDR CALA0600264](https://openairdocs.org/sdr/CALA0600264), Jul 22, 2006: SHEAR TIE. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FRAME SHEAR TIE CORRODED AT STA 867 BETWEEN S27R AND S27L, LBL 4 TO RBL 4. THE CORROSION WAS REMOVED AND A SHEAR TIE REPAIR WAS - [SDR CALA0600263](https://openairdocs.org/sdr/CALA0600263), Jul 22, 2006: SKIN. CORRODED. INSPECTION FOUND STRINGER AND ADJACENT SKIN IN AFT BILGE AREA CORRODED AT STA 986-1006, S27L. A DOUBLER WAS INSTALLED ON THE SKIN IAW SRM 53-00-01, FIGURE 201 A - [SDR CALA0600261](https://openairdocs.org/sdr/CALA0600261), Jul 21, 2006: STRINGER CLIP. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN S19L STRINGER TIE IN AFT BILGE AT STA 947.5. THE STRINGER TIE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0600258](https://openairdocs.org/sdr/CALA0600258), Jul 21, 2006: FRAME. CRACKED. AFT BILGE FRAME CRACKED AT STA 947.5, STR 19L. REPLACED FRAME PER SRM 51-40-02. - [SDR CALA0600257](https://openairdocs.org/sdr/CALA0600257), Jul 20, 2006: STRINGER. CORRODED. STRINGER S-25L CORRODED ON O/B FLANGE. REPAIRED STRINGER PER SRM 53-00-03. - [SDR CALA0600256](https://openairdocs.org/sdr/CALA0600256), Jul 20, 2006: FLOORBEAM. CRACKED. TWO INCH CRACK ON FLOORBEAM AT STA 328 & RBL 12. REPLACED FLOORBEAM CHORD PER SRM 53-10-51, FIG 201. - [SDR CALA0400734](https://openairdocs.org/sdr/CALA0400734), Dec 3, 2004: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27L CORRODED AT STA 385. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. - [SDR CALA0200431](https://openairdocs.org/sdr/CALA0200431), Jul 26, 2002: KEELBEAM. FRETTED. INSPECTION FOUND RT KEEL BEAM TOP OF LOWER CHORD HAD WASHER MILLED INTO IT AT STA 720-727, RBL 6. INSTALLED REPAIR IAW ECRA 5310-03740. - [SDR CALA0200426](https://openairdocs.org/sdr/CALA0200426), Jul 22, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CARGO FLOOR SUPPORT CORRODED AT STA 792-815, L27R. A NEW CARGO FLOOR SUPPORT WAS INSTALLED IAW SRM 53-00-53. - [SDR CALA0200425](https://openairdocs.org/sdr/CALA0200425), Jul 20, 2002: PANEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT EDGE OF ACCESS HOLE IN NR 1 ENGINE PYLON PANEL 5724L. INSTALLED REPAIR DOUBLER IAW ECRA 5430-01204. - [SDR CALA0200420](https://openairdocs.org/sdr/CALA0200420), Jul 19, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND DIAGONAL FLOOR SUPPORT CORRODED AT BS 1016, LBL 8 AND RBL 8. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-2. - [SDR CALA0200419](https://openairdocs.org/sdr/CALA0200419), Jul 19, 2002: STIFFENER. CORRODED. INSPECTION FOUND APB FORWARD FACE LOWEST POINT CENTER STIFFENER CORRODED AT R/H AND L/H SIDE STA 1016, BL 0. STIFFENER REPAIRS WERE INSTALLED IAW SRM 51-70-11. - [SDR CALA0200406](https://openairdocs.org/sdr/CALA0200406), Jul 18, 2002: BEAM. CORRODED. INSPECTION FOUND THE LT AND RT MLG SUPPORT BEAM O/B ATTACH POINTS CORRODED BETWEEN BUSHINGS. REPAIRED THE LT AND RT MLG BEAM IAW ECRA 5741-01025 AND 5741-01026. - [SDR CALA0200404](https://openairdocs.org/sdr/CALA0200404), Jul 16, 2002: FRAME. CORRODED. INSPECTION FOUND A 3/4" CRACK ON BOTTOM END OF R/H MAIN FRAME AT STA 616 BELOW FLOOR. REPAIRED IAW ECRA 5311-01129. - [SDR CALA0200403](https://openairdocs.org/sdr/CALA0200403), Jul 16, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LT AFT LAV DIAGONAL FLOOR SUPPORT CORRODED AT SCREW HOLES, BS 986-1006, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200397](https://openairdocs.org/sdr/CALA0200397), Jul 14, 2002: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED AT STA 1006-1016. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0200396](https://openairdocs.org/sdr/CALA0200396), Jul 14, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, RBL 36 TO RBL 49. A REPAIR WAS INSTALLED IAW SRM 53-10-51. - [SDR CALA0200393](https://openairdocs.org/sdr/CALA0200393), Jul 9, 2002: STRINGER. CRACKED. INSPECTION FOUND A 1/2" CRACK IN STRINGER 16R AFT OF STA 500D. THE CRACKED SECTION OF STRINGER WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 53-00-03. - [SDR CALA0001301](https://openairdocs.org/sdr/CALA0001301), Aug 22, 2000: SKIN. CRACKED. INSPECTION FOUND THREE 1 INCH CRACKS AT LIGHTENING HOLES IN FORWARD CARGO DOOR SKIN. REPAIRS WERE INSTALLED IAW ECRA 5230-01567. - [SDR CALA9900001](https://openairdocs.org/sdr/CALA9900001), Jan 2, 1999: TIRE. FAILED. A BUMP WAS FELT ON THE RT MLG WITH GEAR HANDLE IN THE UP AND OFF POSITION AFTER TAKEOFF. ALSO, THE RT MLG RED UNSAFE LIGHT WAS ILLUMINATED. THE AIRCRAFT WAS RET - [SDR CALA9801376](https://openairdocs.org/sdr/CALA9801376), Jul 30, 1998: SKIN. GOUGED. INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 440, STRINGER 23R. THE GOUGE WAS BLENDED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01, 51-10-02, AND 53-00-0 - [SDR CALA9801346](https://openairdocs.org/sdr/CALA9801346), Jul 26, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 947.5 SPAN OF BEAM, WL 208.1. A NEW SECTION OF UPPER T WAS SPLICED IN IAW ECRA 5321-01018 AND S - [SDR CALA9801334](https://openairdocs.org/sdr/CALA9801334), Jul 24, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND CORROSION AROUND FASTENER HOLES ON FLOORBEAM AT STA 967, RBL 27.5 TO LBL 41.5. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 203. - [SDR CALA9801324](https://openairdocs.org/sdr/CALA9801324), Jul 22, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 907-947. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 204. - [SDR CALA9601145](https://openairdocs.org/sdr/CALA9601145), Aug 8, 1996: DET. MODULE. INOPERATIVE. WHILE CLIMBING THROUGH 34,000 FEET, WITH THE APU SHUT OFF, THE APU FIRE LIGHT AND BELL ACTIVATED. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTINGUISHED - [SDR CAL950800](https://openairdocs.org/sdr/CAL950800), Sep 9, 1995: FIRE LOOP. INOPERATIVE. FLT NR 0655 - IAH - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT OF IAH. THE NR 2 ENGINE WAS SHUT DOWN AND THE RIGHT FIRE BOTTLE WAS DISCHARGED. - [SDR CAL950610](https://openairdocs.org/sdr/CAL950610), Jul 20, 1995: APU. MALFUNCTIONED. IAH - FLT 0426 - WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, THE APU GENERATOR CONTROL CIRCUIT BREAKER POPPED ON CLIMB-OUT OF IAH. TH ## Other aircraft with N17344 - [Registered now](https://openairdocs.org/aircraft/N17344): Boeing 737-8, S/N 67622, built 2024 - [Cancelled 1948-08-06](https://openairdocs.org/deregistered/N17344-1948-08-06): Ryan Aeronautical ST-A, S/N 144, built 1937. Owner: [Medlin Jack W](https://openairdocs.org/faa-owner/MEDLIN%20JACK%20W), [Caldwell, ID](https://openairdocs.org/faa-place/ID/Caldwell) --- 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.