# N17329: 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: 23459
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 14, 1986
- Certificate issued: August 27, 2008
- Last registry action: August 27, 2008
- Mode S code: A12712
- 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/N17329
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17329
- Page: https://openairdocs.org/deregistered/N17329-2013-03-21

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 (67, newest 50)

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

- [SDR CALA0800487](https://openairdocs.org/sdr/CALA0800487), May 25, 2008: SKIN. CRACKED. APPROXIMATELY .75 INCH SKIN CRACK NOTED RT FUSELAGE 2.5 INCH BELOW AND 15 INCH AFT OF EMERGENCY EXIT LIGHT, JUST AFT OF WHEEL WELL STATION 727E STRINGER 23R. RE
- [SDR CALA0800312](https://openairdocs.org/sdr/CALA0800312), Apr 7, 2008: DOOR FRAME. CRACKED. FWD CARGO COMPARTMENT DOOR CUTOUT, AFT FRAME SHOWS CRACK INDICATION WITH HFEC AT LOWER STOP UPPER AREA. REMOVED AND REPLACED FWD CARGO AFT DOOR CUTOUT FRAME PER
- [SDR CALA0700235](https://openairdocs.org/sdr/CALA0700235), May 5, 2007: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR CUTOUT, STA 328, S18R. REPAIRED IAW SRM 53-10-01. A DIP WAS ISSUED TO 
- [SDR CALA0700234](https://openairdocs.org/sdr/CALA0700234), May 4, 2007: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN FORWARD OF R-2 DOOR BETWEEN UPPER AND LOWER HINGES AT STA 950. THE INNER SKIN WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700230](https://openairdocs.org/sdr/CALA0700230), May 4, 2007: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN BENEATH NR 1 DME ANTENNA CORRODED AT STA 460, S29L. THE CORRODED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW ECRA
- [SDR CALA0700228](https://openairdocs.org/sdr/CALA0700228), May 3, 2007: SKIN. CRACKED. INSPECTION FOUND A 0.65" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER. THE SKIN WAS REPAIRED IAW SRM 53-60-01.
- [SDR CALA0700227](https://openairdocs.org/sdr/CALA0700227), May 3, 2007: FRAME. CORRODED. INSPECTION FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED AT STA 500 BETWEEN STRINGER 26L AND 27L. A SHEAR TIE AND FILLER WERE INSTALLED IAW SRM 53-00-07.
- [SDR CALA0700225](https://openairdocs.org/sdr/CALA0700225), May 2, 2007: SKIN. CRACKED. INSPECTION FOUND A 1/2" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR LOWER HINGE CUTOUT FWD LOWER CORNER, STA 947.5, S13R TO S14R. THE CRACKED AREA OF SKIN WAS CUT OU
- [SDR CALA0500451](https://openairdocs.org/sdr/CALA0500451), Dec 16, 2005: WIRE HARNESS. BURNED. LT WING BODY OVERHEAT LIGHT, FLAP IND SHOWED RT FLAP RETRACTED, LT FLAP 0700 POSITION. PRESSURIZATION AUTO FAIL LIGHT ILLUM. EMERGENCY DESCENT. M1205 ELEMENT RE
- [SDR CALA0400744](https://openairdocs.org/sdr/CALA0400744), Dec 17, 2004: SKIN. CRACKED. INSPECTION FOUND TWO 0.3 INCH CRACKS AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01056.
- [SDR CALA0400743](https://openairdocs.org/sdr/CALA0400743), Dec 17, 2004: SKIN. CRACKED. INSPECTION FOUND A 0.3 INCH CRACK AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01057.
- [SDR CALA0400742](https://openairdocs.org/sdr/CALA0400742), Dec 10, 2004: FRAME. CORRODED. INSPECTION FOUND FORWARD SIDE OF FRAME CORRODED IN FORWARD CARGO PIT AT STA 500D BETWEEN S27L AND S28L. INSTALLED REPAIR IAW SRM 53-00-07, FIGURE 205.
- [SDR CALA0400737](https://openairdocs.org/sdr/CALA0400737), Dec 4, 2004: STIFFENER. CORRODED. INSPECTION FOUND APB BOTTOM CENTER STIFFENER CORRODED ON LEFT HALF, BS 1016-1020. THE CORRODED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW ECRA 5311-01
- [SDR CALA0400746](https://openairdocs.org/sdr/CALA0400746), Dec 3, 2004: ANGLE. CORRODED. INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED AT STA 991.5, RBL 46 TO LBL 46. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400736](https://openairdocs.org/sdr/CALA0400736), Dec 3, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN RIGHT I/B SEAT TRACK CORRODED AT STA 328-355, BL 0 TO RBL 23. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 202.
- [SDR CALA0400735](https://openairdocs.org/sdr/CALA0400735), Dec 3, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN RIGHT O/B SEAT TRACK CORRODED AT STA 328-360, RBL 48 TO LBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0400733](https://openairdocs.org/sdr/CALA0400733), Dec 3, 2004: GALLEY TRACK. CORRODED. INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 275-294, RBL 43. A NEW FLOOR TRACK SECTION WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300313](https://openairdocs.org/sdr/CALA0300313), Jun 14, 2003: STRAP. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN STRAP CORRODED BETWEEN STA 777 AND 847, RBL 20. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300312](https://openairdocs.org/sdr/CALA0300312), Jun 13, 2003: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, LBL 8 AND LBL 12. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5320-016
- [SDR CALA0300311](https://openairdocs.org/sdr/CALA0300311), Jun 12, 2003: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK ON LIP OF HOLE CUT ON O/B SIDE OF ACCESS PANEL 5727L OF NR 1 PYLON. REPAIRED ACCESS PANEL IAW ECRA 5430-01230.
- [SDR CALA0300310](https://openairdocs.org/sdr/CALA0300310), Jun 12, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN MAIN WHEEL WELL PRESSURE DECK AT STA 673, LBL 31. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51, FIGURE 203.
- [SDR CALA0300309](https://openairdocs.org/sdr/CALA0300309), Jun 12, 2003: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, LBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01603.
- [SDR CALA0300308](https://openairdocs.org/sdr/CALA0300308), Jun 11, 2003: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, RBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01603.
- [SDR CALA0300303](https://openairdocs.org/sdr/CALA0300303), Jun 10, 2003: STRAP. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT STRAP CORRODED AT STA 727E, LBL 21. THE FLOOR SUPPORT STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0100424](https://openairdocs.org/sdr/CALA0100424), Apr 26, 2001: ARM. OUT OF ADJ. L1 DOOR WILL NOT CLOSE. ADJUSTED L1 DOOR GUIDE ARM. OPS CHECK OK.
- [SDR CALA0100231](https://openairdocs.org/sdr/CALA0100231), Mar 14, 2001: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN. A REPAIR WAS INSTALLED IAW ECRA 5230-01604.
- [SDR CALA0100223](https://openairdocs.org/sdr/CALA0100223), Mar 13, 2001: SKIN. GOUGED. INSPECTION FOUND FUSELAGE SKIN GOUGED AT L-1 DOOR TORQUE TUBE UPPER HINGE AREA, BS 312 , S13L. THE GOUGED AREA OF SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED.
- [SDR CALA0100222](https://openairdocs.org/sdr/CALA0100222), Mar 12, 2001: SKIN. GOUGED. INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 395, STRINGER 20-21R. A DOUBLER WAS INSTALLED.
- [SDR CALA0100215](https://openairdocs.org/sdr/CALA0100215), Mar 8, 2001: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807 BETWEEN STRINGER 27L AND 27R. A REPAIR WAS INSTALLED IAW SRM 53-00-07.
- [SDR CALA0100212](https://openairdocs.org/sdr/CALA0100212), Mar 7, 2001: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR JAMB LOWER FORWARD INSIDE CORNER WEB AT STA 440, S25. REPAIRED WEB IAW SRM 51-70-13, FIGURE 1.
- [SDR CALA0100193](https://openairdocs.org/sdr/CALA0100193), Mar 2, 2001: RIB. GOUGED. INSPECTION FOUND L/E RIB OF VERTICAL STABILIZER GOUGED AT STA 10-40. THE DORSAL FIN RIB WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100186](https://openairdocs.org/sdr/CALA0100186), Mar 1, 2001: FITTING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT WING MLG SUPPORT BEAM O/B ATTACH FITTING AT AFT SPAR. A NEW FITTING WAS INSTALLED IAW WORK CARD 03-5743-1-0003.
- [SDR CALA0100165](https://openairdocs.org/sdr/CALA0100165), Feb 25, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 967-986, LBL 18.32. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9900145](https://openairdocs.org/sdr/CALA9900145), Feb 12, 1999: INTERCOSTAL. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL AT STA 332, STRINGER 10R. THE INTERCOSTAL WAS REMOVED AND A REPAIR INTERCOSTAL AND REPAIR PARTS WERE INSTALLED 
- [SDR CALA9900133](https://openairdocs.org/sdr/CALA9900133), Feb 11, 1999: INTERCOSTAL. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN INTERCOSTAL IN AFT BAGGAGE BIN AT STA 947.5, BELOW CABIN FLOOR CENTERLINE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9900132](https://openairdocs.org/sdr/CALA9900132), Feb 11, 1999: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN OF UPPER WINDOW POST AT CAPTAIN'S NR 2 SLIDING WINDOW. A REPAIR WAS INSTALLED IAW ECRA 5330-02769.
- [SDR CALA9900129](https://openairdocs.org/sdr/CALA9900129), Feb 11, 1999: PANEL. CRACKED. INSPECTION FOUND A 1 CRACK IN LT WING NR 3 SLAT PANEL AT FASTENER I/B OF SLAT ACTUATOR. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C30133.
- [SDR CALA9701681](https://openairdocs.org/sdr/CALA9701681), Nov 28, 1997: FUEL PUMP. INOPERATIVE. THE NR 2 ENGINE FLAMED OUT WHILE ON DESCENT. THE LOW IDLE LIGHT AND NR 2 GEN BUS OFF LIGHT ILLUMINATED AND THEN THE NR 2 LOW OIL PRESSURE LIGHT CAME ON. THE APU
- [SDR CALA9700335](https://openairdocs.org/sdr/CALA9700335), Feb 22, 1997: CHORD. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FAIL SAFE CHORD AT STA 520, RBL 24.50. A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA9700334](https://openairdocs.org/sdr/CALA9700334), Feb 21, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 328 BETWEEN RBL 12 AND RT SIDE AND BETWEEN RBL 12 AND LT SIDE. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-
- [SDR CALA9700333](https://openairdocs.org/sdr/CALA9700333), Feb 21, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 294 BETWEEN LBL 12 AND RBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA9700332](https://openairdocs.org/sdr/CALA9700332), Feb 21, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 344 BETWEEN LBL 12 AND LT SIDEWALL. THE CORRODED AREA WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9700331](https://openairdocs.org/sdr/CALA9700331), Feb 21, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 312 BETWEEN LBL 12 AND RT SIDEWALL. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9700326](https://openairdocs.org/sdr/CALA9700326), Feb 21, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT LBL 12 BETWEEN B.S. 312-328 AND BETWEEN B.S. 328-344. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03439.
- [SDR CALA9700325](https://openairdocs.org/sdr/CALA9700325), Feb 21, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED BETWEEN B.S. 294.5 AND 312 AT RBL 12 AND RBL 14. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-10-02.
- [SDR CALA9700324](https://openairdocs.org/sdr/CALA9700324), Feb 21, 1997: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE CORRODED BETWEEN B.S. 294.5 AND 328. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA9700323](https://openairdocs.org/sdr/CALA9700323), Feb 21, 1997: ANGLE. CORRODED. INSPECTION FOUND AFT L-ANGLE UNDER R-2 DOOR CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.
- [SDR CALA9700330](https://openairdocs.org/sdr/CALA9700330), Feb 20, 1997: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SUPPORT ANGLE AT STA 540, STRINGER 22. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-70-11.
- [SDR CALA9700329](https://openairdocs.org/sdr/CALA9700329), Feb 20, 1997: FAIRING SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING TO BODY FAIRING SUPPORT AT STA 540, STRINGER 22. A .25 INCH CRACK WAS FOUND IN LT WING TO BODY FAIRING SUPPORT AT STA
- [SDR CALA9700328](https://openairdocs.org/sdr/CALA9700328), Feb 20, 1997: SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, AIRCRAFT CENTERLINE, LT SIDE. THE ANGLE WAS REPAIRED IAW SRM 51-70-11.

All 67: https://openairdocs.org/deregistered/N17329-2013-03-21/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 19920622027599I](https://openairdocs.org/incident/19920622027599I), Jun 22, 1992: Boeing 7373T0 (N17329), Allentown, PA. NR2 engine overheat light on. Engine shutdown. Diverted to Allentown. Found a faulty detector system.

## Other aircraft with N17329

- [Registered now](https://openairdocs.org/aircraft/N17329): Boeing 737-8, S/N 67581, built 2023
- [Cancelled 1939-04-01](https://openairdocs.org/deregistered/N17329-1939-04-01): Handley ED HANDLEY SPORT, S/N 1. Owner: [Ed Handley](https://openairdocs.org/faa-owner/ED%20HANDLEY), [Long Beach, CA](https://openairdocs.org/faa-place/CA/Long%20Beach)
- [Cancelled 1937-05-27](https://openairdocs.org/deregistered/N17329-1937-05-27): Vultee V-11GB, S/N 33. Owner: [Carp Export & Import Corp](https://openairdocs.org/faa-owner/CARP%20EXPORT%20%26%20IMPORT%20CORP), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

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