# N17407: 1976 Boeing 727-243, registration cancelled 2002-01-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 18, 2002 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Boeing 727-243](https://openairdocs.org/model/boeing-727-243) (registry code 138408D) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 21270 - Year built: 1976 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 3, 1984 - Certificate issued: October 16, 2001 - Last registry action: October 16, 2001 - Mode S code: A12A81 - Owner when cancelled: [International Trading Company Of Yukon Inc](https://openairdocs.org/faa-owner/INTERNATIONAL%20TRADING%20COMPANY%20OF%20YUKON%20INC) - Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City) - Owner type: Corporation - Owner's area on the map: 35.5180° N, 97.5730° W: Placed by OpenAirDocs at the center of ZIP code 73112, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N17407 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17407 - Page: https://openairdocs.org/deregistered/N17407-2002-01-18 From the FAA registry file of October 29, 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 727-243: https://openairdocs.org/model/boeing-727-243.md ## Service difficulty reports (68, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9900377](https://openairdocs.org/sdr/CALA9900377), Apr 9, 1999: POWER SUPPLY. INOPERATIVE. THE INTERIOR EMERGENCY EXIT LIGHTS FOR LEFT OVERWING DOOR WOULD NOT ILLUMINATE. THE POWER SUPPLY WAS REMOVED AND REPLACED. - [SDR CALA9900143](https://openairdocs.org/sdr/CALA9900143), Feb 15, 1999: BATTERY. DISCHARGED. INSPECTION FOUND THE LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9900142](https://openairdocs.org/sdr/CALA9900142), Feb 12, 1999: DUCT. FAILED. NR 3 ENG FIRE WARNING ACTIVATED AFTER T/O FROM BWI. THE A/C WAS RETURNED TO BWI WHERE IT LANDED W/O INCIDENT. MX FOUND THE PNEUMATIC DUCT LEADING TO NR 3 NOSE C - [SDR CALA9900115](https://openairdocs.org/sdr/CALA9900115), Feb 7, 1999: DUCT. BROKEN. A FIRE WARNING INDICATION ON THE NR 3 ENGINE WAS RECEIVED AFTER TAKEOFF FROM BWI. CHECKLIST PROCEDURES WERE FOLLOWED, FUEL WAS DUMPED AND THE AIRCRAFT WAS RETUR - [SDR CALA9802196](https://openairdocs.org/sdr/CALA9802196), Dec 24, 1998: ANTI ICE DUCT. BROKEN. THE NR 3 ENGINE FIRE WARNING LIGHT CAME ON DURING CLIMB-OUT OF IAH. THE ENGINE POWER WAS REDUCED AND THE LIGHT EXTINGUISHED. WHEN POWER WAS ADVANCED THE WARNING - [SDR CALA9802172](https://openairdocs.org/sdr/CALA9802172), Dec 11, 1998: CHORD. CORRODED. INSPECTION FOUND AFT RT LAV FLOOR REINFORCEMENT CHORD CORRODED AT BS 1176, RBL 26. THE CORRODED AREA WAS BLENDED OUT. A FILLER AND DOUBLER WERE INSTALLED IAW EC - [SDR CALA9802171](https://openairdocs.org/sdr/CALA9802171), Dec 10, 1998: TRACK. CORRODED. THE RT WING NR 5 FLAP TRACK WAS FOUND CORRODED. THE NR 5 FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-57-31. - [SDR CALA9802170](https://openairdocs.org/sdr/CALA9802170), Dec 10, 1998: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR UPPER AFT OVERCENTER STOP LOCK FITTING. THE STOP LOCK, FITTING, AND PLATE WERE REMOVED. A NEW FITTING, STOP LOCK, A - [SDR CALA9802168](https://openairdocs.org/sdr/CALA9802168), Dec 9, 1998: CYLINDER. CORRODED. INSPECTION FOUND THE RT MLG OUTER CYLINDER THREADS FOR GLAND NUT CORRODED. THE RT MLG WAS REMOVED AND REPLACED. - [SDR CALA9802167](https://openairdocs.org/sdr/CALA9802167), Dec 9, 1998: STIFFENER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR CONTROL TAB ROD STIFFENER PLATE IN COVE AREA. THE CRACKED AREA WAS REMOVED, AN ANGLE WAS INSTALLED IAW SRM 51-20 - [SDR CALA9802166](https://openairdocs.org/sdr/CALA9802166), Dec 9, 1998: FITTING. CORRODED. INSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-19297. - [SDR CALA9802165](https://openairdocs.org/sdr/CALA9802165), Dec 9, 1998: MOUNT PAD. CORRODED. INSPECTION FOUND NR 5 FLAP TRACK AFT MOUNTING FLANGE ON FALSE SPAR WORN AND CORRODED. THE MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 1. - [SDR CALA9802164](https://openairdocs.org/sdr/CALA9802164), Dec 9, 1998: SKIN. BENT. INSPECTION FOUND LT INBOARD FOREFLAP INBOARD MOST UPPER SKIN LOOSE AND BENT. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3. - [SDR CALA9802158](https://openairdocs.org/sdr/CALA9802158), Dec 9, 1998: POWER SUPPLY. INOPERATIVE. INSPECTION FOUND LT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REPLACED IAW MM 33-50-0. - [SDR CALA9802157](https://openairdocs.org/sdr/CALA9802157), Dec 9, 1998: POWER SUPPLY. INOP. INSPECTION FOUND RT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-50-0. - [SDR CALA9802156](https://openairdocs.org/sdr/CALA9802156), Dec 9, 1998: STIFFENER. CORRODED. INSPECTION FOUND THE LT WING NR 2 LE FLAP O/B HINGE CORRODED AROUND HINGE ARM BOLTS AND O/B VERTICAL STIFFENER HAD CORROSION AROUND BONDING WIRE BOLT HOLE. THE - [SDR CALA9802155](https://openairdocs.org/sdr/CALA9802155), Dec 9, 1998: SKIN. DEBONDED. INSPECTION FOUND LT O/B AILERON TRAILING EDGE O/B CORNER DEBONDED. THE AILERON WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2, PAGE 18 AND 51-8-4. - [SDR CALA9802154](https://openairdocs.org/sdr/CALA9802154), Dec 9, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 34. A REPAIR WAS INSTALLED IAW ECRA 5310-03790. - [SDR CALA9802153](https://openairdocs.org/sdr/CALA9802153), Dec 9, 1998: ANGLE. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN L ANGLE AT FORWARD I/B CORNER OF RT MLG WHEEL WELL, BEHIND APU, STA 870. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED - [SDR CALA9802152](https://openairdocs.org/sdr/CALA9802152), Dec 9, 1998: BRACKET. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN RT ELEVATOR NR 4 ATTACH HINGE BRACKET AT ELEVATOR STA 99.79. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLE - [SDR CALA9802151](https://openairdocs.org/sdr/CALA9802151), Dec 8, 1998: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT WING SECOND UPPER STRINGER FROM AFT SPAR AT WS 686.50. AN ANGLE REPAIR WAS WAS INSTALLED IAW EA 5762-01050. - [SDR CALA9802150](https://openairdocs.org/sdr/CALA9802150), Dec 8, 1998: STRINGER. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK LT STRINGER 9 INSIDE VERTICAL STABILIZER AT RIB NR 8. THE CRACKED AREA WAS CUT OUT IAW SRM 55-30-4, PAGE 1. REPAIR ANGLES WERE - [SDR CALA9802149](https://openairdocs.org/sdr/CALA9802149), Dec 8, 1998: SKIN. CORRODED. INSPECTION FOUND LT O/B AILERON TAB LOWER SURFACE CORRODED AT O/B END AND A SMALL DEBONDED AREA. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41, PAGE - [SDR CALA9802148](https://openairdocs.org/sdr/CALA9802148), Dec 8, 1998: CHORD. CORRODED. INSPECTION FOUND CHORD CORRODED IN COCKPIT FLOOR PANEL AT F/E SEAT AFT STOP. THE CHORD WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 4. - [SDR CALA9802147](https://openairdocs.org/sdr/CALA9802147), Dec 8, 1998: RIB. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK AROUND BOLT HEADS AT UPPER AFT END OF LT WING FIXED LE RIB, WS 330. THE RIB WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 5 - [SDR CALA9802146](https://openairdocs.org/sdr/CALA9802146), Dec 8, 1998: SKIN. DENTED. INSPECTION FOUND RT O/B AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41. - [SDR CALA9802124](https://openairdocs.org/sdr/CALA9802124), Nov 30, 1998: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT ANGLE CORRODED AT STA 420, RBL 62. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW 53-30-2 AND 51-30-2. - [SDR CALA9802123](https://openairdocs.org/sdr/CALA9802123), Nov 30, 1998: WEB. CORRODED. INSPECTION FOUND WEB CORRODED WHERE R-1 FORWARD DRAIN LINE FITTING ATTACHES, FS 378. THE CORRODED AREA OF WEB WAS REMOVED IAW SRM 51-40-2. A DOUBLER AND FILLER - [SDR CALA9802122](https://openairdocs.org/sdr/CALA9802122), Nov 30, 1998: BRACKET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30 - [SDR CALA9802121](https://openairdocs.org/sdr/CALA9802121), Nov 30, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 1110, RBL 44. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8, PAGE 44. - [SDR CALA9802111](https://openairdocs.org/sdr/CALA9802111), Nov 25, 1998: BRACKET. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN I/B AND O/B BRACKETS AT LT WING NR 2 LE FLAP ACTUATOR MOUNT. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SR - [SDR CALA9802104](https://openairdocs.org/sdr/CALA9802104), Nov 24, 1998: CHORD. CRACKED. INSPECTION FOUND A 2.25 INCH CRACK IN LT WING NR 3 SLAT AT LOWER CHORD BELOW OUTBOARD STOP PAD. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-1 - [SDR CALA9802102](https://openairdocs.org/sdr/CALA9802102), Nov 24, 1998: SKIN. CORRODED. INSPECTION FOUND RT FUSELAGE SKIN CORRODED AT STA 1050, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-1, - [SDR CALA9802097](https://openairdocs.org/sdr/CALA9802097), Nov 23, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND AFT CARGO FLOORBEAM CORRODED AT STA 1070, RBL 12 TO 48. A REPAIR WAS INSTALLED IAW SRM 53-10-8. - [SDR CALA9802094](https://openairdocs.org/sdr/CALA9802094), Nov 23, 1998: ANGLE. CRACKED. INSPECTION FOUND CRACKS IN LOWER ANGLE AT O/B SIDE OF RIB AROUND SEVEN BOLT HEADS INSIDE LT WING LE AFT OF NR 3 LE FLAP I/B END, FS 121. THE ANGLE WAS REMOVED I - [SDR CALA9802093](https://openairdocs.org/sdr/CALA9802093), Nov 23, 1998: STIFFENER. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN LT WING RIB STIFFENER AT LOWER END, WBL 92.0. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3. - [SDR CALA9800361](https://openairdocs.org/sdr/CALA9800361), Mar 2, 1998: LIGHT. INOPERATIVE. INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT ROW 28 AND 29 INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED. ALSO, MAINTENANCE FOUND PIN AT SIGN CANNON PLUG - [SDR CALA9800092](https://openairdocs.org/sdr/CALA9800092), Jan 20, 1998: FRAME. CRACKED. INSPECTION FOUND A 3.5 CRACK IN UPPER AFT CORNER OF R-1 DOOR FRAME. A REPAIR WAS FABRICATED AND INSTALLED IAW DRAWING 69-69978, SRM 57-10-02, AND ECRA 5240-0122 - [SDR CALA9800091](https://openairdocs.org/sdr/CALA9800091), Jan 19, 1998: LUGS. CORRODED. INSPECTION FOUND HORIZONTAL STABILIZER LEFT AND RIGHT BEARING SUPPORT VERTICAL LUGS CORRODED. THE LT VERTICAL LUGS WERE REWORKED IAW ECRA 5550-01033. THE RT VER - [SDR CALA9800090](https://openairdocs.org/sdr/CALA9800090), Jan 19, 1998: SKIN. CORRODED. INSPECTION FOUND RT WING INBOARD MID-FLAP UPPER SKIN PILLOWED WITH DISHED FASTENERS IN AREA ABOVE REAR SPAR UPPER CHORD APPROXIMATELY 21 INCHES FROM INBOARD END - [SDR CALA9800083](https://openairdocs.org/sdr/CALA9800083), Jan 19, 1998: TORUS. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN INBOARD WELD SEAM OF APU TORUS ASSEMBLY. THE APU WAS REMOVED AND REPLACED IAW MM 49-10-01. LEAK AND OPERATIONAL CHECKS WERE G - [SDR CALA9800082](https://openairdocs.org/sdr/CALA9800082), Jan 17, 1998: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1060, STRINGER 27L. THE CORROSION WAS REMOVED AND THE SKIN WAS REPAIRED IAW SRM 53-30-3. - [SDR CALA9800081](https://openairdocs.org/sdr/CALA9800081), Jan 17, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUTS, STA 380, RBL 24 TO RBL 62. TWO L-ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-30-8 FIGURE 8. - [SDR CALA9800080](https://openairdocs.org/sdr/CALA9800080), Jan 17, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUT ON UPPER FORWARD FLANGE LOWER SURFACE AT STA 328, LBL 48. THE FLOORBEAM WAS REMOVED, REPAIRED, AND REINSTALLED IA - [SDR CALA9701252](https://openairdocs.org/sdr/CALA9701252), Aug 29, 1997: SLIDE. LOW PRESSURE. THE CREW FOUND L-1 DOOR EMERGENCY SLIDE PRESSURE LOW. THE L-1 DOOR SLIDE WAS REMOVED AND REPLACED PER MM 25-60-15. - [SDR CALA9601700](https://openairdocs.org/sdr/CALA9601700), Nov 13, 1996: ANGLE. CRACKED. INSPECTION FOUND RT WING NR 11 SPOILER ACTUATOR SUPPORT FITTING INBOARD ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. - [SDR CALA9601687](https://openairdocs.org/sdr/CALA9601687), Nov 6, 1996: SKIN. CORRODED. INSPECTION FOUND SKIN CORRODED UNDER WEB IN AFT CARGO COMPARTMENT AT STA 970, STRINGER 28L. THE CORRODED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRI - [SDR CALA9601689](https://openairdocs.org/sdr/CALA9601689), Nov 5, 1996: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28L CORRODED AT STA 965 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A REPLACEMENT STRINGER AND SPLICE WERE - [SDR CALA9601697](https://openairdocs.org/sdr/CALA9601697), Nov 3, 1996: RIB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT ACTUATOR OUTBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-1 - [SDR CALA9601696](https://openairdocs.org/sdr/CALA9601696), Nov 3, 1996: RIB. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN NR 3 SLAT ACTUATOR INBOARD ATTACH RIB. A REPAIR PART WAS FABRICATED, HEAT TREATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2 All 68: https://openairdocs.org/deregistered/N17407-2002-01-18/reports.md ## FAA accident and incident reports (2) 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 19991005029179I](https://openairdocs.org/incident/19991005029179I), Oct 5, 1999: Boeing 727230 (N17407), San Antonio, TX, Substantial damage. (-23) On October 5, 1999, a Continental airlines B727, aircraft, flight number 623, declared and emergency landing at San Antonio International Airport with a… - [Incident 19951118041849I](https://openairdocs.org/incident/19951118041849I), Nov 18, 1995: Boeing 727230 (N17407), Ft Lauderdale, FL, Substantial damage. Narrative: shortly after t.o. from ft. Lauderdale international airport (fll) Continental airlines flight 382 aircraft N17407 experienced #3 engine fire… ## Other aircraft with N17407 - [Registered now](https://openairdocs.org/aircraft/N17407): Boeing 737-9, S/N 68816, built 2025 - [Cancelled 1951-10-22](https://openairdocs.org/deregistered/N17407-1951-10-22): Aeronca C-3, S/N 719. Owner: [New Mexico State Board For Vocational Education](https://openairdocs.org/faa-owner/NEW%20MEXICO%20STATE%20BOARD%20FOR%20VOCATIONAL%20EDUCATION), [Santa Fe, NM](https://openairdocs.org/faa-place/NM/Santa%20Fe) --- 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.