# N17345: 1987 Boeing 737-3TO, registration cancelled 2009-08-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 21, 2009 - 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: 23583 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 18, 1987 - Certificate issued: April 17, 2007 - Last registry action: April 17, 2007 - Mode S code: A12754 - 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/N17345 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17345 - Page: https://openairdocs.org/deregistered/N17345-2009-08-21 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 (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0600270](https://openairdocs.org/sdr/CALA0600270), Jul 26, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R CORRODED IN A/C BAY AT STA 520. THE CORRODED SECTION WAS CUT OUT AND A NEW SEGMENT WAS INSTALLED IAW SRM 53-60-12, REPAIR 3, FIGUR - [SDR CALA0600265](https://openairdocs.org/sdr/CALA0600265), Jul 22, 2006: SKIN. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 861-864 JUST BELOW S22L ON THE BONDED DOUBLER LINE. THE CRACKED AREA OF STRINGER WAS REMOVED AND A DOUBL - [SDR CALA0600253](https://openairdocs.org/sdr/CALA0600253), Jul 15, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R CORRODED BETWEEN STA 312 AND 323.7. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW STRINGER SECTION WAS INSTALLED IAW SRM - [SDR CALA0600252](https://openairdocs.org/sdr/CALA0600252), Jul 15, 2006: ANGLE. CORRODED. INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED FROM STA 954-994. THE Z-ANGLE WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0600251](https://openairdocs.org/sdr/CALA0600251), Jul 15, 2006: ANGLE. CORRODED. INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED FROM STA 291.5-344, RBL 52-54. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-01. - [SDR CALA0600247](https://openairdocs.org/sdr/CALA0600247), Jul 14, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND SURFACE CORROSION ON O/B SEAT TRACK AT STA 328, RBL 41. REPAIRED SEAT TRACK IAW SRM 53-00-52. - [SDR CALA0600246](https://openairdocs.org/sdr/CALA0600246), Jul 14, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND SURFACE CORROSION ON I/B SEAT TRACK AT STA 328-344, RBL 21. REPAIRED SEAT TRACK IAW SRM 53-00-52. - [SDR CALA0600274](https://openairdocs.org/sdr/CALA0600274), Jul 12, 2006: FLAP TRACK. CORRODED. INSPECTION FOUND NR 2 FLAP TRACK TRANSMISSION ATTACH HOLES AT AFT UPPER AND LOWER FORWARD LOCATION, RSS 330, CORRODED. A O/S REPAIR SLEEVE WAS INSTALLED IAW SOP - [SDR CALA0600273](https://openairdocs.org/sdr/CALA0600273), Jul 12, 2006: FLAP TRACK. CORRODED. INSPECTION FOUND NR 7 FLAP TRACK TRANSMISSION MOUNT HOLES AT BOTH AFT AND FORWARD LOWER POSITIONS, RSS 330, CORRODED. THE CORROSION WAS REMOVED AND REPAIR SLEEV - [SDR CALA0600244](https://openairdocs.org/sdr/CALA0600244), Jul 12, 2006: FLAP TRACK. CORRODED. INSPECTION FOUND THE NR 8 FLAP TRACK TRANSMISSION MOUNT HOLE CORRODED AT LOWER AFT POSITION. THE CORROSION WAS REMOVED. SLEEVES WERE FABRICATED AND THE BORES AN - [SDR CALA0400675](https://openairdocs.org/sdr/CALA0400675), Oct 12, 2004: SKIN. DENTED. DENT IN FUSELAGE BS 837 - STR 19L. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229. - [SDR CALA0400666](https://openairdocs.org/sdr/CALA0400666), Oct 8, 2004: FRAME. CRACKED. LEFT MAINFRAME CRACKED. REPAIRED PER ECRA 5311-01158 AND SRM 51-40-20. - [SDR CALA0300546](https://openairdocs.org/sdr/CALA0300546), Sep 20, 2003: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AFT OF EQUIPMENT COOLING EXHAUST DUCT AT STA 373. A REPAIR WAS INSTALLED IAW 5330-02894. - [SDR CALA0200391](https://openairdocs.org/sdr/CALA0200391), Jul 3, 2002: KEELBEAM. CORRODED. INSPECTION FOUND KEEL BEAM LOWER CHORD I/B FLANGE CORRODED AT S28R AND S28L BETWEEN STA 500D AND 520. REPAIRED IAW ECRA 5311-01128. - [SDR CALA0200376](https://openairdocs.org/sdr/CALA0200376), Jun 30, 2002: SKIN. CRACKED. INSPECTION FOUND 1/2 INCH CRACK IN NR 1 PYLON ACCESS PANEL CUTOUT FOR PANEL 5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230. - [SDR CALA0200368](https://openairdocs.org/sdr/CALA0200368), Jun 26, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CARGO FLOOR SUPPORT CORRODED AT STA 772, LBL 7.5 AND LBL 12. REPAIRED FLOOR SUPPORT IAW ECRA 5320-01603 AND SRM 53-60-53. - [SDR CALA0200367](https://openairdocs.org/sdr/CALA0200367), Jun 26, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CARGO FLOOR SUPPORTS CORRODED AT STA 772, RBL 2.5 AND LBL 2.5. REPAIRED FLOOR SUPPORTS IAW ECRA 5320-01603 AND SRM 53-60-53. - [SDR CALA0200366](https://openairdocs.org/sdr/CALA0200366), Jun 25, 2002: CHANNEL. CORRODED. INSPECTION FOUND CHANNEL CORRODED UNDER NUT PLATE BETWEEN STA 787 AND 801, RBL 9. THE CHANNEL WAS REPAIRED IAW SRM 53-00-53, FIGURE 201. - [SDR CALA0200364](https://openairdocs.org/sdr/CALA0200364), Jun 24, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CARGO FLOOR SUPPORT CORRODED AT STA 847, LBL 2.5 AND RBL 2.5. THE CORRODED AREAS WERE CUT OUT AND REPAIRS WERE INSTALLED IAW ECRA 5320-01603. - [SDR CALA0200363](https://openairdocs.org/sdr/CALA0200363), Jun 24, 2002: PAN. CRACKED. INSPECTION FOUND A 0.375 INCH CRACK IN L1 DOOR PAN SKIN AT NR 5 FROM BOTTOM STOP PIN ACCESS HOLE. A REPAIR WAS INSTALLED IAW SRM 51-70-13. - [SDR CALA0200350](https://openairdocs.org/sdr/CALA0200350), Jun 18, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED BELOW #1 GALLEY BETWEEN STA 277-294.5. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02. - [SDR CALA0001768](https://openairdocs.org/sdr/CALA0001768), Nov 14, 2000: FIRE DETECTOR. MALFUNCTIONED. THE FORWARD CARGO COMPARTMENT FIRE DETECTION AND WARNING ACTIVATED AFTER TAKEOFF FROM SEA. BOTH FIRE EXTINGUISHING BOTTLES WERE DISCHARGED AS A PRECAUTIONARY ME - [SDR CALA9701760](https://openairdocs.org/sdr/CALA9701760), Dec 11, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 927, RBL 14. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR SECTION WAS INSTALLED IAW SRM 53-00-51. - [SDR CALA9700770](https://openairdocs.org/sdr/CALA9700770), May 25, 1997: TIRE. FAILED. THE NR 1 TIRE THREW TREAD INTO FLAP WELL RESULTING IN A SHEARED INBOARD SPOILER RETURN LINE AND SUBSEQUENT LOSS OF A SYSTEM HYDRAULICS ON TAKEOFF. THE AIRCRAFT - [SDR CALA9600926](https://openairdocs.org/sdr/CALA9600926), Jun 30, 1996: HYD PUMP. LEAKING. THE B-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/2 ACCOMPANIED BY ILLUMINATION OF THE B-ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT WHILE EN ROUTE. THE B-ENGINE HYDRAU - [SDR CAL950986](https://openairdocs.org/sdr/CAL950986), Oct 30, 1995: M982 CARD. INOPERATIVE. FLT NR 0309 - PHX - THE RIGHT MLG RED LIGHT DID NOT ILLUMINATE DURING GEAR TRANSIT TO EXTENDED POSITION. THE GEAR WAS RAISED AND THE RED LIGHT REMAINED OFF. THE --- 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.