# N17410: 1978 Boeing 727-243, registration cancelled 2004-07-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 22, 2004 - 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: 21663 - Year built: 1978 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 17, 1984 - Certificate issued: July 20, 2004 - Last registry action: July 20, 2004 - Mode S code: A12A9D - Owner when cancelled: [International Trading Co Of Yukon Inc](https://openairdocs.org/faa-owner/INTERNATIONAL%20TRADING%20CO%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/N17410 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17410 - Page: https://openairdocs.org/deregistered/N17410-2004-07-22 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 (60, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EISA20010151](https://openairdocs.org/sdr/EISA20010151), Dec 27, 2001: SKIN. TORN. ACCOMPLISHED SHEET METAL REPAIR AREA FORWARD OF RT OUT FLOW VALVE, STA 1166, STR. 24R.CORRECTIVE ACTION:CUT OUT DAMAGED AREA. FABRICATED DOUBLER .071 2024-T3 8" - [SDR EISA20010119](https://openairdocs.org/sdr/EISA20010119), Aug 29, 2001: STRUCTURE. CRACKED. RT HORIZONTAL STAB O/B T/E CORNER IS CRACKED, TOP SIDE. FOUND DURING B-CHECK. ROUTED OUT CRACK IAW B727 SRM 55-10-1. NDT VERIFIED CRACK BEING REMOVED. FABRICATE - [SDR EISA20000196](https://openairdocs.org/sdr/EISA20000196), Oct 28, 2000: PLATE. MISALIGNED. PACK FAN REMAINED ON AFTER FLAPS UP. RUDDER LOAD LIMITER LIGHT REMAINED ON FOR 4 MINUTES AFTER FLAPS UP. REMOVED AND REPLACED RIVETS ON STRIKER ON INBOARD FLAP - [SDR EISA2000001](https://openairdocs.org/sdr/EISA2000001), Dec 29, 1999: RECEIVER. SHORTED. NR 1 NAV RECEIVER INOPERATIVE. INSTALLED SERVICEABLE NAV RECEIVER. (M) - [SDR CALA9800863](https://openairdocs.org/sdr/CALA9800863), May 14, 1998: FUEL PUMP. FAILED. NUMBER 2 ENGINE FAILED AT ROTATION. FOUND FUEL PUMP SHAFT SHEARED. REPLACED NUMBER 2 ENGINE FUEL PUMP AND FUEL CONTROL PER MM 71-00-67. - [SDR CALA9800856](https://openairdocs.org/sdr/CALA9800856), May 14, 1998: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED BATTERY PACK. - [SDR CALA9800469](https://openairdocs.org/sdr/CALA9800469), Mar 17, 1998: STIFFENER. CRACKED. INSPECTION FOUND A .1562 INCH CRACK THROUGH FASTENER HOLE AT BOTTOM OF STIFFENER AT INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0, ACCESS CUTOUT 6303. A RE - [SDR CALA9800468](https://openairdocs.org/sdr/CALA9800468), Mar 16, 1998: FLOOR TRACK. CORRODED. INSPECTION FOUND FLOOR TRACK CORRODED AT STA 380 TO 420, RBL 25. THE TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-05-01 AND 51-10-0 - [SDR CALA9800467](https://openairdocs.org/sdr/CALA9800467), Mar 16, 1998: SKIN. WORN. INSPECTION FOUND A GROOVE WORN ON BOTTOM OF LT WING NR 7 SPOILER. THE NR 7 SPOILER WAS REMOVED AND REPLACED. - [SDR CALA9800466](https://openairdocs.org/sdr/CALA9800466), Mar 16, 1998: WINDOW. DELAMINATED. INSPECTION FOUND A BURNED SPOT AND A DELAMINATION BUBBLE IN R-1 WINDOW UPPER EDGE. THE R-1 WINDOW WAS REMOVED AND REPLACED IAW MM 56-11-11. - [SDR CALA9800465](https://openairdocs.org/sdr/CALA9800465), Mar 16, 1998: BEAM. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN J-BEAM ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE J-BEAM WAS REPAIRED IAW ECRA 5750-02193 AND EA 26865-5075. - [SDR CALA9800464](https://openairdocs.org/sdr/CALA9800464), Mar 16, 1998: FOREFLAP. DAMAGED. INSPECTION FOUND LT INBOARD FOREFLAP CRUSHED (4 AREA) AT INBOARD END. THE FOREFLAP WAS REMOVED AND REPLACED. - [SDR CALA9800463](https://openairdocs.org/sdr/CALA9800463), Mar 16, 1998: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN R-1 DOOR CUTOUT AT FS 417. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5307-01141. - [SDR CALA9800442](https://openairdocs.org/sdr/CALA9800442), Mar 13, 1998: SKIN. DENTED. INSPECTION FOUND LT OUTBOARD AILERON OUTBOARD UPPER TRAILING EDGE HAD A PREVIOUSLY FILLED SMALL DENT WITH FILLER BREAKING OUT. THE DENTED AREA WAS CUT OUT AND A - [SDR CALA9800441](https://openairdocs.org/sdr/CALA9800441), Mar 13, 1998: SKIN. CRACKED. INSPECTION FOUND A .375 INCH CRACK IN LT WING FIXED LEADING EDGE CUTOUT ABOVE NR 3 SLAT OUTBOARD TRACK AREA. A SKIN FLUSH REPAIR WAS INSTALLED IAW SRM 57-30-4. - [SDR CALA9800440](https://openairdocs.org/sdr/CALA9800440), Mar 13, 1998: SKIN. DENTED. INSPECTION FOUND A DENT 19.5 INCHES FROM OUTBOARD END IN LT WING NR 2 LEADING EDGE SLAT UPPER SKIN. A REPAIR WAS INSTALLED IAW SRM 57-50-3. - [SDR CALA9800439](https://openairdocs.org/sdr/CALA9800439), Mar 13, 1998: SPLICE. CRACKED. INSPECTION FOUND A 3 INCH CRACK AT SPLICE PLATE ON LOWER SURFACE OF LT WING UPPER LEADING EDGE SKIN DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR, FSS 224. THE - [SDR CALA9800438](https://openairdocs.org/sdr/CALA9800438), Mar 13, 1998: BRACKET. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN BRACKET AT AFT FACE OF LT GEAR BEAM WHERE HYDRAULIC LINES PASS THROUGH ACCESS DOOR 8405. THE BRACKET WAS REMOVED AND A NEW BR - [SDR CALA9800437](https://openairdocs.org/sdr/CALA9800437), Mar 13, 1998: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK THROUGH AFT FASTENER HOLE AT REPAIR ANGLE INSIDE LT WING LEADING EDGE RIB, WS 330, AFT OF NR 4 SLAT, INBOARD END. A NEW ANGLE W - [SDR CALA9800436](https://openairdocs.org/sdr/CALA9800436), Mar 13, 1998: BRACKET. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 1 SLAT LOWER LEADING EDGE SKIN TO INBOARD TRACK ATTACH BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INST - [SDR CALA9800435](https://openairdocs.org/sdr/CALA9800435), Mar 13, 1998: SKIN. DISBONDED. INSPECTION FOUND RT TRAILING EDGE INBOARD FOREFLAP DISBONDED IN TWO AREAS. THE FOREFLAP WAS REMOVED AND REPLACED. - [SDR CALA9800434](https://openairdocs.org/sdr/CALA9800434), Mar 13, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1.6 INCH CRACK AT BOTTOM OF LEFT CURVED SIDEWALL SUPPORT ANGLE MOUNTED TO FORWARD SIDE OF CIRCUMFERENTIAL STA 950D. A NEW SUPPORT ANGLE WAS F - [SDR CALA9800433](https://openairdocs.org/sdr/CALA9800433), Mar 13, 1998: SKIN. CORRODED. INSPECTION FOUND CORROSION IN SKIN ATTACH LEG AT FORWARD SIDE OF CIRCUMFERENTIAL, BS 1148, STRINGER 28L AND 29L. THE CORROSION WAS CUT OUT IAW SRM 51-10-6. A DO - [SDR CALA9800432](https://openairdocs.org/sdr/CALA9800432), Mar 13, 1998: ANGLE. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL UPPER SUPPORT ANGLE BETWEEN FLOORBEAM SUPPORT, STA 720 AND 720A. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTA - [SDR CALA9800431](https://openairdocs.org/sdr/CALA9800431), Mar 13, 1998: SKIN. CRACKED. INSPECTION FOUND A .0937 INCH CRACK AT LT WING UPPER SKIN CUTOUT FOR NR 2 SPOILER. THE FASTENERS WERE REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM - [SDR CALA9800430](https://openairdocs.org/sdr/CALA9800430), Mar 13, 1998: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FALSE SPAR LOWER ANGLE BELOW AND INBOARD OF NR 7 SPOILER ACTUATOR INBOARD COVE AREA. REPAIRED FALSE SPAR LOWER ANGLE IAW EA - [SDR CALA9800429](https://openairdocs.org/sdr/CALA9800429), Mar 13, 1998: HINGE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR BALANCE PANEL NR 9214 FORWARD HINGE. THE HINGE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. - [SDR CALA9800428](https://openairdocs.org/sdr/CALA9800428), Mar 13, 1998: STRINGER. CRACKED. INSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 9 RT NR 3 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR WAS FA - [SDR CALA9800427](https://openairdocs.org/sdr/CALA9800427), Mar 13, 1998: STRINGERS. CRACKED. INSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 6 RT NR 3 STRINGER AND NR 5 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30- - [SDR CALA9800426](https://openairdocs.org/sdr/CALA9800426), Mar 13, 1998: GUSSET. CRACKED. INSPECTION FOUND A 2 CRACK IN GUSSET ON FORWARD SIDE OF RT FUSELAGE FRAME AT STA 825, RBL 70. THE GUSSET WAS REMOVED AND A NEW ONE WAS INSTALLED IAW EA SA012-53 - [SDR CALA9800425](https://openairdocs.org/sdr/CALA9800425), Mar 13, 1998: WEB. CRACKED. INSPECTION FOUND A 7 CRACK JUST BELOW DRAIN CHUTE IN LT AFT LAV FLOOR WEB AT BS 1176, LBL 50. THE CRACKED SECTION OF WEB WAS REMOVED. A NEW SECTION WAS FABRICAT - [SDR CALA9800424](https://openairdocs.org/sdr/CALA9800424), Mar 13, 1998: SKIN. BULGED. INSPECTION FOUND RT FUSELAGE SKIN BULGED JUST AFT AND BELOW FORWARD LAV SERVICE PANEL. THE BULGED AREA WAS REMOVED. A DOUBLER REPAIR WAS FABRICATED AND INSTALLE - [SDR CALA9800423](https://openairdocs.org/sdr/CALA9800423), Mar 13, 1998: FLOOR TRACK. CORRODED. INSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1050 TO 1130, BL 25R. THE CORRODED SECTION OF FLOOR TRACK WAS REPLACED IAW SRM 53-10-5 AND 51-10-1. - [SDR CALA9800422](https://openairdocs.org/sdr/CALA9800422), Mar 13, 1998: FLOOR TRACK. CORRODED. INSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1100, BL 45R. THE CORRODED SECTION OF FLOOR TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5. - [SDR CALA9800718](https://openairdocs.org/sdr/CALA9800718), Mar 12, 1998: BATTERY PACK. DISCHARGED. THE EMERGENCY EXIT SIGN IVER COCKPIT DOOR FELL OUT AND WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK AND LENSE ASSEMBLY WAS REMOVED AND REPLACED AND O - [SDR CALA9800421](https://openairdocs.org/sdr/CALA9800421), Mar 12, 1998: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1.25 CRACK IN SUPPORT INTERCOSTAL AT AFT BAGGAGE COMPARTMENT BETWEEN BS 1030 AND 1050 ABOVE STRINGER 25L. THE INTERCOSTAL WAS REMOVED AND A N - [SDR CALA9800143](https://openairdocs.org/sdr/CALA9800143), Jan 31, 1998: LIGHT. INOPERATIVE. INSPECTION FOUND EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED. - [SDR CALA9700787](https://openairdocs.org/sdr/CALA9700787), May 26, 1997: BRAKE HOUSING. CRACKED. ACFT RETURNED TO THE GATE AFTER DRAGGING THE NR 3 BRAKE DURING TAXI. THE NR 3 TIRE CAUGHT ON FIRE, FOAM WAS USED TO EXTINGUISH THE FIRE. THE NR 3 AND 4 MAIN TIR - [SDR CALA9700516](https://openairdocs.org/sdr/CALA9700516), Mar 27, 1997: SKIN. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT INTERIOR SKIN CORRODED AT ANTENNA, STA 1030 TO 1050, STRINGER 29R TO 30. THE AREA WAS REPAIRED IAW SRM 51-40-3. - [SDR CALA9700581](https://openairdocs.org/sdr/CALA9700581), Mar 26, 1997: ANGLE. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN VENTRAL STAIRWELL TORQUE BOX ANGLE AT STAIR ACTUATOR FITTING, STA 1272, RBL 22. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C - [SDR CALA9700519](https://openairdocs.org/sdr/CALA9700519), Mar 26, 1997: SKIN. DISBONDED. INSPECTION FOUND LT INBOARD MIDFLAP UPPER SURFACE OF TRAILING EDGE WEDGE DISBONDED 24 INCHES FROM INBOARD END. THE DISBONDED AREA WAS CUT OUT, CORE AND DOUBLERS - [SDR CALA9700515](https://openairdocs.org/sdr/CALA9700515), Mar 26, 1997: SKIN. CORRODED. INSPECTION FOUND LT FUSELAGE SKIN CORRODED AT STA 1130. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1. - [SDR CALA9700512](https://openairdocs.org/sdr/CALA9700512), Mar 26, 1997: SPAR WEB. CRACKED. INSPECTION FOUND A .75 CRACK IN WEB AT FRONT SPAR JUST OUTBOARD OF LT FORWARD TERMINAL PIN FITTING. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INS - [SDR CALA9700511](https://openairdocs.org/sdr/CALA9700511), Mar 26, 1997: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT AFT OUTBOARD END OF CUTOUT FOR NR 6 SLAT OUTBOARD HOOK OF RT WING FIXED LEADING EDGE. THE CRACK WAS STOP DRILLED, A REPAIR W - [SDR CALA9700580](https://openairdocs.org/sdr/CALA9700580), Mar 25, 1997: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD TRACK CUTOUT, STA 216. THE CRACK WAS CUT OUT, A FILLER AND DOUBLER REP - [SDR CALA9700518](https://openairdocs.org/sdr/CALA9700518), Mar 25, 1997: SKIN. DELAMINATED. INSPECTION FOUND OUTBOARD END OF LT OUTBOARD AILERON TAB DELAMINATED. THE TAB WAS REMOVED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. THE TAB WAS RE - [SDR CALA9700514](https://openairdocs.org/sdr/CALA9700514), Mar 25, 1997: SKIN. DISBONDED. INSPECTION FOUND LEFT OUTBOARD FOREFLAP DISBONDING AT INBOARD END. THE END CAP WAS REMOVED, THE DISBONDED AREA WAS CUT OUT, A HOT BOND REPAIR WAS ACCOMPLISHED I - [SDR CALA9700513](https://openairdocs.org/sdr/CALA9700513), Mar 25, 1997: RIB. CRACKED. INSPECTION FOUND A 1 INCH CRACK BETWEEN TWO AFT UPPER BOLTS OF LT WING LEADING EDGE RIB AT SLAT STA 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. - [SDR CAL960427](https://openairdocs.org/sdr/CAL960427), Feb 27, 1996: FRAME. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN AFT BAG PIT FLOOR LEVEL FRAME AT BS 1166, RBL 24. THE CRACKED AREA WAS CUT OUT. REPAIR DOUBLERS WERE FABRICATED AND INSTALL - [SDR CAL960431](https://openairdocs.org/sdr/CAL960431), Feb 25, 1996: FLOORBEAM. OVERSIZED HOLE. INSPECTION FOUND OVERSIZED HOLE ON MAIN CABIN INTERIOR FLOORBEAM AT BS 350, RBL 40. THE EFFECTED SECTION WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATE All 60: https://openairdocs.org/deregistered/N17410-2004-07-22/reports.md ## Other aircraft with N17410 - [Registered now](https://openairdocs.org/aircraft/N17410): Boeing 737-9, S/N 68810, built 2025 - [Cancelled 2008-10-23](https://openairdocs.org/deregistered/N17410-2008-10-23): Cessna 172R, S/N 17281499, built 2008. Exported to India. Owner: [Weaver Aero International Inc](https://openairdocs.org/faa-owner/WEAVER%20AERO%20INTERNATIONAL%20INC), [Moundridge, KS](https://openairdocs.org/faa-place/KS/Moundridge) - [Cancelled 1951-03-02](https://openairdocs.org/deregistered/N17410-1951-03-02): Aeronca LC, S/N 2052, built 1936. Owner: [Maglione Ralph](https://openairdocs.org/faa-owner/MAGLIONE%20RALPH), [Akron, OH](https://openairdocs.org/faa-place/OH/Akron) --- 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.