# N859FT: 1971 Boeing 747-123, registration cancelled 2013-03-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 21, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Boeing 747-123](https://openairdocs.org/model/boeing-747-123) (registry code 1384873) - Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054) - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) (OpenAirDocs) - Serial number: 20326 - Year built: 1971 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 9, 1995 - Last registry action: December 15, 2005 - Mode S code: ABC956 - Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City) - Owner type: Individual - Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N859FT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=859FT - Page: https://openairdocs.org/deregistered/N859FT-2013-03-21 From the FAA registry file of November 5, 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 747-123: https://openairdocs.org/model/boeing-747-123.md ## Service difficulty reports (261, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR P5CA0100605](https://openairdocs.org/sdr/P5CA0100605), Oct 31, 2001: POWER SUPPLY. DISCHARGED. CREW RIGHT UPPER DECK DOOR FRAME MOUNTED EXIT LIGHTS DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. REMOVED AND REPLACED UPPER DECK RT CREW DOOR FRAME LIGHT POW - [SDR P5CA0100600](https://openairdocs.org/sdr/P5CA0100600), Sep 29, 2001: WEB. CRACKED. NOSE WHEEL WELL - INTERNAL VERTICAL BEAM WEB CRACKED AT INSULATION HOLE - 2 INCHES LONG - FOUND BY H.F.E.C. REPAIRED BY REMOVING CRACKED SECTION. INSTALLED SPLI - [SDR P5CAO100599](https://openairdocs.org/sdr/P5CAO100599), Sep 29, 2001: WEB. CRACKED. NOSE WHEEL WELL - BS300 INTERNAL VERTICAL BEAM WEB CRACKED BY INSULATION HOLE. FOUND BY H.F.E.C. REPAIRED BY HOLE OPENED UP & DOUBLER INSTALLED PER BOEING FAX - - [SDR P5CA0100598](https://openairdocs.org/sdr/P5CA0100598), Sep 29, 2001: WEB. CRACKED. NOSEWHEEL WELL - BS320 INTERNAL VERTICAL BEAM WEB WITH 2 INCH LONG CRACK FROM INSULATION HOLE FOUND BY E.F.E.C. REPAIRED WITH DOUBLER INSTALLED WITH "T" ANGLE P - [SDR P5CA0100597](https://openairdocs.org/sdr/P5CA0100597), Sep 29, 2001: WEB. CRACKED. NOSE WHEEL WELL - BS300 INTERNAL VERTICAL BEAM WEB CRACKED BY INSULATION HOLES. FOUND BY H.F.E.C. (3) CRACKS TOTAL. REPAIRED WITH DOUBLER INSTALLED PER BOEING F - [SDR P5CA0100587](https://openairdocs.org/sdr/P5CA0100587), Jul 17, 2001: WARNING LIGHT. ILLUMINATED. NR 1 OIL PRESSURE FLUCTUATING BETWEEN 40 AND 42 PSI, OIL QTY NORMAL, NO LIGHTS. ON POWER REDUCTION AT TOP OF DESCENT NR 1 OIL PRESSURE LIGHT AND FILTER BYPASS L - [SDR P5CA0100586](https://openairdocs.org/sdr/P5CA0100586), Jul 15, 2001: BYPASS VALVE. FILTER BYPASS LIGHT & OIL PRESSURE LIGHT ILLUMINATED (FLICKERING). EXTINGUISHED WHEN #1 THROTTLE RETARDED TO IDLE. RETURNED FOR LANDING. FILTER PYPASS REPLACED - [SDR P5CA0100567](https://openairdocs.org/sdr/P5CA0100567), May 30, 2001: WINDOW. RH #1 OUTER PLY SHATTERED. R&R R1 WINDOW PER 56-11-01, INSTALLED R1 WINDOW, LEAK CHECKS GOOD REPLACED HEAT & CONTROLLER P/N ON 617154-5, S/N ON 084C-857, P/N OF - [SDR P5CA0000336](https://openairdocs.org/sdr/P5CA0000336), Oct 5, 2000: B-NUT. LEAKING. ABNORMALITY FOUND ON NR 4 HYD QTY DROPPED 6 GAL AFTER LANDING GEAR RETRACTION CONTINUED FLIGHT WITH AOP OFF AND EDP IN DEPR. FOUND HYD LEAK FORM PRESS LINE B-NU - [SDR P5CA0000198](https://openairdocs.org/sdr/P5CA0000198), Apr 25, 2000: PLUG. DAMAGED. ON PRE-DEPARTURE, NR 1 EXHAUST PLUG SUSTAINED DAMAGE. REMOVED EXHAUST PLUG ASSY, INSPECTED AREA, NO CRACKS NOTED ON FLANGE OR ANY DEFECTS. EXHAUST PLUG ASSY INS - [SDR P5CA0000099](https://openairdocs.org/sdr/P5CA0000099), Feb 22, 2000: SKIN. DELAMINATED. RT WING INBD TRAILING EDGE FORE FLAP BETWEEN 5/6 CANOE ASSY DELAMINATED/MARKED. REPAIRED PER SRM 51-40-15. - [SDR P5CA0000098](https://openairdocs.org/sdr/P5CA0000098), Feb 22, 2000: SKIN. DELAMINATED. RT WING OUTBOARD FORE FLAP ASSY AFT OUTBOARD CORNER LS DELAMINATED. REPAIRED PER SRM 51-40-15. - [SDR P5CA0000097](https://openairdocs.org/sdr/P5CA0000097), Feb 22, 2000: SKIN. DELAMINATED. RT OUTBOARD T/E MID FLAP LWR OUTBOARD END DAMAGE/DELAMINATION MARKED. REPAIRED PER SRM 51-40-09. - [SDR P5CA0000096](https://openairdocs.org/sdr/P5CA0000096), Feb 22, 2000: PANEL. DELAMINATED. UPPER LEADING EDGE FWD SURFACE OF FIBERGLASS PANEL DELAMINATED. REPAIRED PER SRM 51-40-09. - [SDR P5CA0000095](https://openairdocs.org/sdr/P5CA0000095), Feb 22, 2000: SKIN. DELAMINATED. RT WING INBD TE MID FLAP 1 AFT FLAP UPPER SURFACE HAS AREAS OF DELAMINATION. REPAIRED PER SRM 51-40-15. - [SDR P5CA0000094](https://openairdocs.org/sdr/P5CA0000094), Feb 22, 2000: SKIN. DELAMINATED. WING UPPER SURFACE TRAILING EDGE PANEL BETWEEN 4/5 SPOILER VARIOUS AREAS LIGHT DELAMINATION. REPAIRED PER SRM 51-40-15. - [SDR P5CA0000093](https://openairdocs.org/sdr/P5CA0000093), Feb 22, 2000: SKIN. DAMAGED. OUTBOARD AILERON UPPER SURFACE ONE OFF LOCATION DAMAGED. REPAIRED PER SRM 51-40-15. - [SDR P5CA0000092](https://openairdocs.org/sdr/P5CA0000092), Feb 22, 2000: FAIRING. ERRODED. NR 4 ENGINE PYLON STRUT TO WING FAIRING EROSION. REPAIRED PER SRM 51-40-09. - [SDR P5CA9900788](https://openairdocs.org/sdr/P5CA9900788), Nov 28, 1999: ACTUATOR. FAILED. ON APPROACH NOSE GEAR DOOR WARNING BOTH PRIMARY AND ALTERNATE. REPLACED NOSE LANDING GEAR DOOR ACTUATOR PER MAINTENANCE MANUAL 32-34-14 PAGE 201. - [SDR P5CA9900795](https://openairdocs.org/sdr/P5CA9900795), Nov 22, 1999: MUFFLER. CRACKED. CRACKED APU EXHAUST MUFFLER AT 8 AND 12 O'CLOCK POSITIONS. REPAIRED PER BOEING MAINTENANCE MANUAL 49-21-03. - [SDR P5CA9900794](https://openairdocs.org/sdr/P5CA9900794), Nov 22, 1999: DOOR. DAMAGED. DAMAGED LEFT BODY LANDING GEAR WHEEL WELL DOOR FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-03. - [SDR P5CA9900793](https://openairdocs.org/sdr/P5CA9900793), Nov 22, 1999: ACTUATOR. INOPERATIVE. INOPERATIVE RIGHT WING LANDING GEAR ALTERNATE EXTENSION MOTOR. REPLACED PER BOEING MAINTENANCE MANUAL 32-35-01. - [SDR P5CA9900792](https://openairdocs.org/sdr/P5CA9900792), Nov 22, 1999: SKIN. CRACKED. CRACK IN FUSELAGE SKIN JUST ABOVE LEFT ELEVATOR BS 2650. REPAIRED PER BOEING SRM 53-30-03. - [SDR P5CA9900791](https://openairdocs.org/sdr/P5CA9900791), Nov 22, 1999: ACTUATOR. INTERMITTENT. INTERMITTENT OPERATION OF THE LEFT WING GEAR ALTERNATE EXTENTION ACTUATOR (DURING SCHEDULED OPERATIONAL CHECK). REPLACED ACTUATOR PER BOEING MAINTENANCE MANUAL - [SDR P5CA9900790](https://openairdocs.org/sdr/P5CA9900790), Nov 22, 1999: PANEL. DAMAGED. DAMAGED RIGHT WING TIP HF PANEL COVER. REPAIRED PER BOEING SRM 51-40-15. - [SDR P5CA9900789](https://openairdocs.org/sdr/P5CA9900789), Nov 22, 1999: SKIN. DELAMINATED. DELAMINATION RIGHT INBOARD TRAILING EDGE AFT FLAP INBOARD OF NR 6 CANOE AREA. REPAIRED PER BOEING SRM 51-40-15. - [SDR P5CA9900661](https://openairdocs.org/sdr/P5CA9900661), Jul 13, 1999: SKIN. DELAMINATION. LEFT OUTBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED DELAMINATION PER SRM 51-40-06. - [SDR P5CA9801376](https://openairdocs.org/sdr/P5CA9801376), Aug 27, 1998: KEEL BEAM. CORRODED. LEVEL 1 CORROSION FOUND ON RT WING GEAR WHEEL WELL INBOARD KEEL BEAM UPPER SURFACE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. - [SDR P5CA9801375](https://openairdocs.org/sdr/P5CA9801375), Aug 27, 1998: ANGLE. CORRODED. LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL OUTBOARD CHORD ANGLE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. - [SDR P5CA9801374](https://openairdocs.org/sdr/P5CA9801374), Aug 27, 1998: BRACKET. CORRODED. LEVEL 1 CORROSION FOUND ON RT BODY GEAR WW VALVE SUPPORT BRACKET. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. - [SDR P5CA9801373](https://openairdocs.org/sdr/P5CA9801373), Aug 27, 1998: BEAM. CORRODED. LEVEL 1 CORROSION ON RT BODY GEAR WW OUTBOARD BEAM BS 1352 TO 1353 BL R70-R80. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. - [SDR P5CA9801372](https://openairdocs.org/sdr/P5CA9801372), Aug 27, 1998: BRACKET. CORRODED. LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL WELL BRACKET AT BS 2352L WL 160. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. - [SDR P5CA9801371](https://openairdocs.org/sdr/P5CA9801371), Aug 27, 1998: SKIN. CORRODED. LEVEL 1 CORROSION FOUND ON LEFT WING UPPER SKIN AT REAR SPAR AREA. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. - [SDR P5CA9801370](https://openairdocs.org/sdr/P5CA9801370), Aug 27, 1998: BEAM. CRACKED. LEFT WING TRAILING EDGE BEAM UPPER CHORD INBOARD END CRACKED. REPAIRED PER SRM 51-40-14 FIG 2. - [SDR P5CA9801369](https://openairdocs.org/sdr/P5CA9801369), Aug 27, 1998: STRINGER. CORRODED. LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL WELL OUTBOARD STRINGER BS 1368 TO 1371 STR R33. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. - [SDR P5CA9800524](https://openairdocs.org/sdr/P5CA9800524), Mar 17, 1998: PANEL. DAMAGED. RT WING TOP L/E FIXED PANEL INBD OF PYLON PREVIOUS REPAIR PEELING OFF. REMOVED PREVIOUS REPAIR, REPAIRED PER SRM 51-40-15. - [SDR P5CA9800523](https://openairdocs.org/sdr/P5CA9800523), Mar 17, 1998: STANCHION. DAMAGED. FWD CARGO COMPARTMENT STA 480 PLUG SUPPORT CHANNEL DAMAGED. REMOVED AND REPLACED BOTH RT SIDE STANCHIONS AT STA 480 PER SRM 51-30-02 AND 51-10-01. - [SDR P5CA9800522](https://openairdocs.org/sdr/P5CA9800522), Mar 17, 1998: PANEL. CRACKED. NR 1 ENGINE INLET 3 INCH CRACK AT 3 O'CLOCK POSITION ON ACCOUSTIC PANEL. REPAIRED CRACK BY CUTTING IT OUT AND APPLYING POTTING COMPOUND PER SRM 54-31-03. - [SDR P5CA9800521](https://openairdocs.org/sdr/P5CA9800521), Mar 17, 1998: SKIN. DELAMINATED. RT WING MLG LOWER FLYING DOOR IS DELAMINATED. REMOVED DAMAGE, APPLIED FIBERGLASS AND BONDING PER SRM 51-40-06. - [SDR P5CA9800520](https://openairdocs.org/sdr/P5CA9800520), Mar 17, 1998: BUMPER PAD. CRACKED. LT WING GEAR BOGIE BEAM TILT BUMPER CRACKED AND DAMAGED. REMOVED AND REPLACED BUMPER PAD PER SRM 51-10-01. - [SDR P5CA9800519](https://openairdocs.org/sdr/P5CA9800519), Mar 17, 1998: SKIN. TORN. FWD CARGO DOOR TORN IN UPPER RT CORNER AT PREVIOUS REPAIR. INSTALLED DOUBLER ON FWD RT CORNER OF DOOR PER SRM 51-30-02. - [SDR P5CA9800518](https://openairdocs.org/sdr/P5CA9800518), Mar 17, 1998: FASTENER. MISSING. RT HORIZ STAB NAV LIGHT FIXED WITH SEALANT FASTENERS MISSING. INSTALLED FASTENERS PER SRM 51-30-02. - [SDR P5CA9800517](https://openairdocs.org/sdr/P5CA9800517), Mar 17, 1998: SILL. CORROSION. LEVEL 1 CORROSION FOUND ON FWD LOWER CARGO SERRATED PLATE ON DOOR SILL NR 5, 6 AND7 BOTTOM AFT HOLE NR 8 HAS CORROSION. REMOVED CORROSION FROM PLATE PER SRM 51- - [SDR P5CA9800504](https://openairdocs.org/sdr/P5CA9800504), Mar 16, 1998: OVERHEAT LIGHT. ILLUMINATED. ON CLIMBOUT, RT WING OVERHEAT LIGHT CAME ON. APPLIED CHECKLIST AND RETURNED TO JFK. INSPECTED LEADING EDGE DUCT AREA FOR LEAKS AND FAULTY WIRE CONNECTIONS. FOUN - [SDR P5CA9800027](https://openairdocs.org/sdr/P5CA9800027), Jan 19, 1998: SEQUENCE VALVE. CRACKED. ON MAINTENANCE WALK AROUND, FOUND NOSE LANDING GEAR OPEN DOOR SEQUENCE VALVE ASSEMBLY LEAKING. VALVE FOUND TO BE CRACKED. REMOVED AND REPLACED NOSE GEAR, OPERAT - [SDR P5CA9701842](https://openairdocs.org/sdr/P5CA9701842), Nov 26, 1997: SKIN. TORN. TEAR AND DELAMINATION AT INBOARD AFT CORNER LEFT OUTBOARD ELEVATOR. REPAIRED PER BOEING SRM 51-40-15. - [SDR P5CA9701844](https://openairdocs.org/sdr/P5CA9701844), Nov 23, 1997: CLAMP. BROKEN. UPPER ATTACH CLAMP ON PORTABLE OXYGEN BOTTLE IN COCKPIT BROKEN. REPLACED BRACKET ASSEMBLY PER BOEING MAINTENANCE MANUAL 35-31-00. - [SDR P5CA9701843](https://openairdocs.org/sdr/P5CA9701843), Nov 22, 1997: PANEL. DELAMINATED. FIBERGLASS SURFACE RIPPING AWAY FROM RIGHT WING UPPER SURFACE LEADING EDGE PANEL. REPAIRED PER BOEING SRM 51-40-12. - [SDR P5CA9701826](https://openairdocs.org/sdr/P5CA9701826), Nov 11, 1997: LINE. BROKEN. ON GEAR EXTENSION AND FLAP EXTENSION LOST ALL HYDRAULIC SYSTEM 1 PRESSURE. FOUND AIR DRIVEN HYDRAULIC PUMP PRESSURE FLEX LINE BROKEN. REPLACED LINE PER BOEING M - [SDR P5CA9701615](https://openairdocs.org/sdr/P5CA9701615), Oct 6, 1997: PARK BRAKE VALVE. STICKING. ANTI-SKID LIGHT ON AT START OF TAKEOFF ROLL, LIGHT REMAINED ON STEADY. PARKING BRAKE VALVE OPERATION CHECKED AT MODULE, RIGHT BODY GEAR BAY OPERATIONAL CHECK SA All 261: https://openairdocs.org/deregistered/N859FT-2013-03-21/reports.md ## Other aircraft with N859FT - [Registered now](https://openairdocs.org/aircraft/N859FT): Cessna 560XL, S/N 560-5528, built 2004 --- 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.