# N830FT: 1969 Boeing 747-121, registration cancelled 2015-05-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 21, 2015 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 747-121](https://openairdocs.org/model/boeing-747-121) (registry code 1384871) - 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: 19642 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 26, 1993 - Certificate issued: May 21, 1993 - Last registry action: July 17, 2007 - Mode S code: AB58E9 - Owner when cancelled: [Palc II Inc](https://openairdocs.org/faa-owner/PALC%20II%20INC) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N830FT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=830FT - Page: https://openairdocs.org/deregistered/N830FT-2015-05-21 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 747-121: https://openairdocs.org/model/boeing-747-121.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 P5CA9600141](https://openairdocs.org/sdr/P5CA9600141), Feb 15, 1996: SKIN. DELAMINATED. FOUND SMALL AREA OF LEFT OUTBOARD ELEVATOR T/E DELAMINATED. REPAIRED BOTH TOP AND BOTTOM ELEVATOR T/E IAW SRM 51-40-12. - [SDR P5CA9600140](https://openairdocs.org/sdr/P5CA9600140), Feb 15, 1996: SKIN. DELAMINATED. FOUND LEFT INBOARD ELEVATOR, INBOARD T/E CORNER DELAMINATED. REPAIRED IAW SRM 51-40-12. - [SDR P5CA9600139](https://openairdocs.org/sdr/P5CA9600139), Feb 15, 1996: EXHAUST SLEEVE. BENT. FOUND NR 1 ENGINE EXHAUST SLEEVE INNER T/E SKIN BENT AT 8 O'CLOCK POSITION. STRAIGHTENED AS NEEDED IAW SRM 54-10-02. - [SDR P5CA9600138](https://openairdocs.org/sdr/P5CA9600138), Feb 15, 1996: EXHAUST SLEEVE. WORN. FOUND NR 2 ENGINE EXHAUST SLEEVE OUTER SKIN LEADING EDGE WORN AT 7 O'CLOCK POSITION. REMOVED OLD DOUBLER, MANUFACTURED AND INSTALLED NEW DOUBLER IAW SRM 51-10-0 - [SDR P5CA9600137](https://openairdocs.org/sdr/P5CA9600137), Feb 15, 1996: SPAR. CORRODED. FOUND LEVEL ONE SURFACE CORROSION ON LEFT WING FRONT SPAR UPPER CHORD CAP LOWER SURFACE, AT FS 1395 AFT OF NR 3 LED. REMOVED CORROSION IAW SRM 51-10-01. - [SDR P5CA9600136](https://openairdocs.org/sdr/P5CA9600136), Feb 15, 1996: SKIN. DELAMINATED. FOUND RIGHT WING O/B FOREFLAP LOWER SURFACE DELAMINATED, 6 INCHES BY 6 INCHES. REMOVED DAMAGE, FABRICATED FIBERGLASS REPAIR IAW SRM 51-40-15. - [SDR P5CA9600090](https://openairdocs.org/sdr/P5CA9600090), Jan 27, 1996: INDICATOR. INOPERATIVE. RETURNED TO RAMP DUE TO IMPROPER RT OUTBOARD AILERON INDICATION. FUNCTIONAL CHECK OF ALL CONTROL SURFACES NORMAL, ALL COCKPIT INDICATIONS NORMAL IAW MM 27-00-00 - [SDR P5CA9500872](https://openairdocs.org/sdr/P5CA9500872), Dec 13, 1995: TIRES. FAILED. DURING TAKEOFF ROLL, AIRCRAFT SWUNG VIOLENTLY TO THE LEFT, CAUSING LEFT WING AND BODY GEAR TRUCKS TO DEPART LEFT SIDE OF RUNWAY. ABORTED TAKEOFF. INCIDENT CAUSE - [SDR P5CA9500867](https://openairdocs.org/sdr/P5CA9500867), Dec 11, 1995: TRANSMITTER MNT. OUT OF RIG. DURING CLIMBOUT, OUTBOARD FLAPS WOULD NOT RETRACT HYDRAULICALLY PAST APPROX 7 DEGREES. FOUND LEFT OUTBOARD TRANSMITTER MOUNT ASSY OUT OF RIG. RE-RIGGED AND REPL - [SDR P5CA9500868](https://openairdocs.org/sdr/P5CA9500868), Dec 10, 1995: MOTOR CLUTCH. SLIPS. DURING AIR TURN BACK FOR SPLIT FLAP, INBOARD FLAPS DID NOT WORK IN ALTERNATE WORK, OK IN NORMAL. FOUND THAT THE INBOARD FLAP ELECTRIC MOTOR CLUTCH SLIPPING REPL - [SDR P5CA9500836](https://openairdocs.org/sdr/P5CA9500836), Nov 6, 1995: TRANSMITTER. FAILED. DURING TAXI OUT, FLAPS SELECTED 10 DEGREES, THE OUTBOARD STOP AT 5 DEGREES, RECYCLED NO HELP. FOUND RIGHT OUTBOARD FLAP TRANSMITTER AT FAULT REPLACED TRANSMITTE - [SDR P5CA9500822](https://openairdocs.org/sdr/P5CA9500822), Oct 20, 1995: AILERON. LOCKED OUT. RETURNED TO BLOCKS DUE TO RIGHT HAND OUTBOARD AILERON LOCKED OUT WITH FLAPS AT 20 UNITS. INSPECTED RIGHT HAND OUTBOARD AILERON LOCKOUT ACTUATOR INSTRUMENTS AND - [SDR P5CA9500802](https://openairdocs.org/sdr/P5CA9500802), Oct 2, 1995: RESERVOIR. RUPTURED. UPON ARRIVAL VCP, UNABLE TO OPEN SIDE CARGO DOOR. WHILE ATTEMPTING TO TROUBLESHOOT DOOR HYDRAULIC PROBLEM, DOOR HYDRAULIC RESERVOIR RUPTURED. FOUND BENT LINE CA - [SDR P5CA9500741](https://openairdocs.org/sdr/P5CA9500741), Sep 8, 1995: TURBINE. FAILED. JFK - ON CLIMBOUT, NR 4 ENGINE EXPERIENCED A COMPRESSOR STALL AT CONSTANT SPEED, ALTITUDE 17,000 MAX EGT 856, ENGINE SHUTDOWN. SECOND STAGE TURBINE FAILURE, FOU - [SDR P5CA9500716](https://openairdocs.org/sdr/P5CA9500716), Aug 22, 1995: ENGINE VANE CONT. MALFUNCTIONED. AT TAKEOFF, UNABLE TO REACH TARGET BEFORE HITTING STOPS. REPLACED ENGINE VANE CONTROL. - [SDR P5CA9500715](https://openairdocs.org/sdr/P5CA9500715), Aug 22, 1995: FUEL CONTROL. MALFUNCTIONED. DURING CLIMBOUT EXPERIENCED SLUGGISH ENGINE RESPONSE NR 4 ENGINE AT FL 210. CLIMBING THROUGH FL 290 HEARD AUDIBLE STALL AND OBSERVED SUBSEQUENT TOTAL LOSS OF EN - [SDR P5CA9500701](https://openairdocs.org/sdr/P5CA9500701), Aug 9, 1995: TE SKIN. SEPARATED. RIGHT OUTBOARD AILERON TRAILING EDGE SEPERATED OUTBOARD OF NR 2 STATIC WICK. REPAIRED PER BOEING SRM 51-40-09. - [SDR P5CA9500700](https://openairdocs.org/sdr/P5CA9500700), Aug 9, 1995: LE SKIN. GOUGED. RIGHT OUTBOARD FLAP, FOREFLAP OUTBOARD END LEADING EDGE IS GOUGED IN 3 PLACES. REPAIRED PER BOEING SRM 51-40-09. - [SDR P5CA9500699](https://openairdocs.org/sdr/P5CA9500699), Aug 9, 1995: TE SKIN. SEPARATING. RIGHT OUTBOARD AILERON TRAILING EDGE SEPARATING INBOARD APROXIMATELY 6 TO 10 INCHES. REPAIRED PER BOEING SRM 51-40-09. - [SDR P5CA9500698](https://openairdocs.org/sdr/P5CA9500698), Aug 9, 1995: FAIRING. CRACKED. NR 3 PYLON LOWER AFT FAIRING CRACKED ON RIGHT SIDE AND HAS LOOSE AND MISSING FASTENERS ON BOTH SIDES. REPAIRED PER BOEING SRM 51-40-02. - [SDR P5CA9500697](https://openairdocs.org/sdr/P5CA9500697), Aug 9, 1995: RADOME. DELAMINATED. RADOME HAS AREAS OF ERROSION AND APPROXIMATELY 2 BY 2 AREA OF DELAMINATION. REPAIRED PER BOEING SRM 51-40-09. - [SDR P5CA9500695](https://openairdocs.org/sdr/P5CA9500695), Aug 9, 1995: STRINGER. ELONGATED HOLE. S34L ELONGATED HOLE AT BS 1852. STRINGER REPLACED. - [SDR P5CA9500694](https://openairdocs.org/sdr/P5CA9500694), Aug 9, 1995: STRINGER. CORRODED. S34L FROM BS 1740 TO SPLICE ARE AT BS 1890 HAS LIGHT CORROSION ON LOWER UPPER SECTION OF HAT CHANNEL, NO PROTECTIVE COATING ON STRINGER. STRINGER REPLACED FOR O - [SDR P5CA9500693](https://openairdocs.org/sdr/P5CA9500693), Aug 9, 1995: STRINGER. MISDRILLED. FOUND AT BS 1820 TO BS 1850, S34L UPPER SIDE OF HAT CHANNEL HAS 32 HOLES .5 INCH APART AND 11 HOLES UPPER SIDE OF HAT CHANNEL IN SPLICE AREA AT BS 1890. REPLACE - [SDR P5CA9500692](https://openairdocs.org/sdr/P5CA9500692), Aug 9, 1995: SKIN. CRACKED. LEFT INBOARD ELEVATOR TRAILING EDGE CRACKED, UPPER AND LOWER SURFACE APPROXIMATLY 36 TO 40 INCHES FROM INBOARD END. REPAIRED PER BOEING SRM 51-40-14. - [SDR 95ZZZM3](https://openairdocs.org/sdr/95ZZZM3), Apr 7, 1995: SKIN. MISDRILLED. DURING STRUCTURAL INSPECTION REQUIRED BY AD 95-01-04, MISDRILLED AND PLUGGED FUSELAGE SKIN WAS FOUND BETWEEN BS 1740 AND 1960 AT STRINGER 4. REPAIR ACCOMPLISHED --- 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.