# N857FT: 1971 Boeing 747-132, registration cancelled 2007-08-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 30, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 747-132](https://openairdocs.org/model/boeing-747-132) (registry code 1384882)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) (OpenAirDocs)
- Serial number: 20246
- Year built: 1971
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, normal
- Airworthiness date: February 21, 1995
- Certificate issued: February 16, 1995
- Last registry action: July 17, 2007
- Mode S code: ABC1E8
- 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/N857FT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=857FT
- Page: https://openairdocs.org/deregistered/N857FT-2007-08-30

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 747-132: https://openairdocs.org/model/boeing-747-132.md

## Service difficulty reports (306, newest 50)

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

- [SDR P5CA9900568](https://openairdocs.org/sdr/P5CA9900568), May 16, 1999: PANEL. DELAMINATED. LEFT WING TOP FIXED T/E PANEL BETWEEN I/B AILERON AND SPOILER NR 5 TOP SURFACE FOUND DELAMINATED. REMOVED OLD REPAIR AND WATER. REPLACED DAMAGED CORE, FILLERS A
- [SDR P5CA9900569](https://openairdocs.org/sdr/P5CA9900569), May 14, 1999: PANEL. DELAMINATED. LEFT WING T/E UPPER FIXED PANEL AT WING STA 1190 LOWER SURFACE FOUND DELAMINATED. SANDED CLEANED AREA, REMOVED DAMAGED AREA, FABRICATED REPAIR, APPLIED PARTS UN
- [SDR P5CA9801619](https://openairdocs.org/sdr/P5CA9801619), Dec 4, 1998: SKIN. HOLE. LEFT WING OUTBOARD POSITION FORE FLAP LEADING EDGE HAS HOLE IN PREVIOUS REPAIR. REPAIRED DAMAGED AREA PER SRM 51-40-09.
- [SDR P5CA9801618](https://openairdocs.org/sdr/P5CA9801618), Dec 4, 1998: SPOILER. HOLE. RIGHT WING NR 12 SPOILER HAS SMALL HOLE IN TOP SIDE SURFACE. CLEANED, POTTED DAMAGED AREA AND REPAIRED PER SRM 51-40-06.
- [SDR P5CA9801617](https://openairdocs.org/sdr/P5CA9801617), Dec 4, 1998: LINER. CRACKED. APU EXHAUST INNER LINER HAD 12 INCH CRACK. REMOVED AND REPLACED EXHAUST LINER PER MM 49-81-03.
- [SDR P5CA9801616](https://openairdocs.org/sdr/P5CA9801616), Dec 3, 1998: COWL. HOLE. NR 3 ENGINE OUTBOARD CORE COWL HAS HOLE IN SKIN AND TEMPORARY FASTENER INSTALLED. FABRICATED DOUBLER AND INSTALLED PER SRM 54-30-03.
- [SDR P5CA9801615](https://openairdocs.org/sdr/P5CA9801615), Dec 2, 1998: FAIRING. DAMAGED. NR 4 ENGINE FWD FAIRING HAS A HOLE WORN THRU STRUCTURE. FABRICATED DOUBLER AND INSTALLED PER SRM 54-30-03.
- [SDR P5CA9801275](https://openairdocs.org/sdr/P5CA9801275), Aug 12, 1998: LONGERON. DAMAGE. STA 1900 LONGERON 19R TO 26R FRAME HAS SERVERAL GOUGES ON I/B LIP. REPAIRED FRAME IAW SRM 51-40-03.
- [SDR P5CA9801274](https://openairdocs.org/sdr/P5CA9801274), Aug 12, 1998: FRAME. CRACKED. RT I/B MIDFLAP INBOARD MOST FRAME CRACKED. STOPPED DRILLED CRACK AND FABRICATED DOUBLER AND TREATED, PRIMED AND INSTALLED IAW SRM 51-40-03.
- [SDR P5CA9801273](https://openairdocs.org/sdr/P5CA9801273), Aug 11, 1998: STRINGER. CRACKED. STA 2330 LONGERON 14R IS CRACKED. REMOVED CRACKED STRINGER AND SPLICE. FABRICATED, TREATED, PRIMED AND REINSTALLED STRINGER AND SPLICE IAW SRM 53-10-03 FIG 4 AN
- [SDR P5CA9801272](https://openairdocs.org/sdr/P5CA9801272), Aug 11, 1998: LONGERON. CRACKED. STA 2330 LONGERON 17R IS CRACKED. REMOVED CRACKED STRINGERS AND SPLICE. FABRICATED, TREATED, PRIMED AND REINSTALLED STRINGER AND SPLICE IAW SRM 53-30-02 FIG 4 A
- [SDR P5CA9801260](https://openairdocs.org/sdr/P5CA9801260), Aug 11, 1998: FRAME. DAMAGED. FRAME AT STA 2060 HAS SEVERAL GOUGES FROM GILL LINER SUBSTRUCTURE AT LONGERON 14R TO 21R. REPAIRED FRAME IAW SRM 51-10-03. INSTALLED DOUBLER IAW SRM 51-30-02.
- [SDR P5CA9801259](https://openairdocs.org/sdr/P5CA9801259), Aug 11, 1998: FRAME. DAMAGED. FRAME AT STA 1780 RIGHT SIDE HAS DEEP GOUGE CAUSED FROM GILL LINER SUBSTRUCTURE AT LONGERON 21R. BLENDED GOUGE AT FRAME IAW SRM 51-10-01. INSTALLED DOUBLER REPA
- [SDR P5CA9801258](https://openairdocs.org/sdr/P5CA9801258), Aug 11, 1998: FAIRING. DAMAGED. NR 3 FLAP CANOE TRAILING EDGE DAMAGED. REMOVED DAMAGED AREA AND APPLIED FIBERGLASS LAY UP OF 3 PLY SKINS IAW SRM 51-40-15.
- [SDR P5CA9801257](https://openairdocs.org/sdr/P5CA9801257), Aug 11, 1998: SKIN. PUNCTURED. HOLE IN LOWER SURFACE OF LEFT INBOARD AILERON. CLEANED AREA, REMOVED DAMAGED MATERIAL, AND REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-06.
- [SDR P5CA9801264](https://openairdocs.org/sdr/P5CA9801264), Aug 10, 1998: ANGLE. CRACKED. L ANGLE BELOW SPLICE FITTING AT RIGHT BODY GEAR WHEEL WELL STA 1480 CRACKED. REMOVED AND REPLACED L ANGLE IAW SRM 51-10-01 AND 51-30-02.
- [SDR P5CA9801263](https://openairdocs.org/sdr/P5CA9801263), Aug 10, 1998: FITTING. DAMAGED. RT I/B MIDFLAP AFT SUPPORT FITTING GOUGED. REMOVED AND REPLACED RT O/B MIDFLAP AFT SUPPORT FITTING IAW SB 747-27-2280.
- [SDR P5CA9801262](https://openairdocs.org/sdr/P5CA9801262), Aug 10, 1998: SKIN. CORROSION. LEVEL 1 CORROSION, FOUND UNDER BOTH ATC ANTENNAS. REMOVED CORROSION IAW SRM 51-10-06.
- [SDR P5CA9801261](https://openairdocs.org/sdr/P5CA9801261), Aug 10, 1998: SKIN. DAMAGED. RT I/B MIDFLAP HAS DEEP GOUGE AT LEADING EDGE I/B CARRIAGE CUT OUT. REWORKED GOUGES IAW SRM 57-50-01. TREATED AND PRIMED IAW SRM 51-10-02.
- [SDR P5CA9801271](https://openairdocs.org/sdr/P5CA9801271), Aug 9, 1998: PIN. CORRODED. RIGHT WING NR 7 SPINDLE AFT BOGIE O/B SUPPORT PIN CORRODED. REPLACED O/B SUPPORT PIN ON NR 7 SPINDLE AFT BOGIE IAW 747 OHM 27-51-75.
- [SDR P5CA9801270](https://openairdocs.org/sdr/P5CA9801270), Aug 9, 1998: SKIN. DELAMINATED. RIGHT FLYING DOOR LOWER SECTION HAS SPOTS OF DELAMINATION ON ITS INNER SURFACE AT DENT LOCATION. SANDED AND REMOVED DAMAGED AREA AND REPAIRED IAW SRM 51-40-09.
- [SDR P5CA9801269](https://openairdocs.org/sdr/P5CA9801269), Aug 9, 1998: COWLING. DAMAGED. NR 4 ENG INBOARD T/R TRAILING EDGE AT 8 O'CLOCK POSITION SKIN DAMAGED AND PEELING IN THREE AREAS. REPAIRED SKIN ROUTED SMALL CRACK AND REBONDED SKIN IAW 51-40-0
- [SDR P5CA9801268](https://openairdocs.org/sdr/P5CA9801268), Aug 9, 1998: SKIN. DAMAGED. NR 2 LEFT AFT FLAP TRAILING EDGE DAMAGED. REPAIRED DAMAGE AT AFT T/E FLAP IAW SRM 51-40-09.
- [SDR P5CA9801267](https://openairdocs.org/sdr/P5CA9801267), Aug 9, 1998: FAIRING. DAMAGED. NR 2 FLAP FAIRING CANOE HAS HOLE DAMAGE INSIDE. APPLIED FIBERGLASS OVERLAYS AND REPAIRED IAW SRM 51-40-15.
- [SDR P5CA9801266](https://openairdocs.org/sdr/P5CA9801266), Aug 9, 1998: SKIN. DAMAGED. LEFT INBOARD MIDFLAP HAS HOLE IN UPPER SURFACE JUST AFT OF INBOARD CARRIAGE. REMOVED DAMAGED SKIN AND REPAIRED WITH FIBERGLASS DOUBLERS IAW SRM 51-40-09.
- [SDR P5CA9801265](https://openairdocs.org/sdr/P5CA9801265), Aug 9, 1998: ANTENNA. CORROSION. NR 1 AND NR 2 ATC ANTENNAS HAVE SURFACE CORROSION. REPLACED BOTH NR 1 AND NR 2 ATC ANTENNAS. OPS CHECKED GOOD IAW 3450-01-01.
- [SDR P5CA9801250](https://openairdocs.org/sdr/P5CA9801250), Aug 6, 1998: DOOR. CORRODED. LEVEL 1 CORROSION LEFT FLYING DOOR LOWER SECTION ALONG LOWER EDGE OF ITS INNER SURFACE AROUND BOLD HEADS. REMOVED AND REPLACED FASTENERS AND CLEANED AREAS IAW S
- [SDR P5CA9801249](https://openairdocs.org/sdr/P5CA9801249), Aug 6, 1998: SKIN. CRACKED. NR 3 ENG O/B FAN COWL CRACK ON UPPER FWD AND AFT HINGE CUTOUT. BLENDED OUT CRACKED AREA AROUND FORWARD HINGE. CRACK WITHIN SRM LIMITS PER SRM 51-40-06 FIG 2. RE
- [SDR P5CA9801248](https://openairdocs.org/sdr/P5CA9801248), Aug 6, 1998: FLOORBEAM. CORRODED. LEVEL 1 CORROSION FOUND ON BOTTOM OF FLOORBEAM BS 600. REMOVED SURFACE CORROSION IAW SRM 51-10-01.
- [SDR P5CA9801247](https://openairdocs.org/sdr/P5CA9801247), Aug 6, 1998: SUPPORT. CORRODED. LEVEL 1 CORROSION FOUND UNDER F/E SEAT FLOOR PANEL SUPPORT BEAM. REMOVED SURFACE CORROSION ON SUPPORT BEAM AND TREATED IAW SRM 51-10-06.
- [SDR P5CA9801246](https://openairdocs.org/sdr/P5CA9801246), Aug 6, 1998: SUPPORT. CORRODED. LEVEL 1 CORROSION AT SUPPORT CHANNEL FOR DRAIN PAN AT BS 340. CORROSION REMOVED FROM SUPPORT CHANNEL AT STA 340 IAW SRM 51-10-01.
- [SDR P5CA9801222](https://openairdocs.org/sdr/P5CA9801222), Aug 4, 1998: SKIN. CORROSION. RT BODY MLG BOTH INBOARD AND OUTBOARD STRUT DOOR ASSEMBLIES HAVE MANY SPOTS WITH LOST FINISH AND SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION IAW SRM 51-1
- [SDR P5CA9801215](https://openairdocs.org/sdr/P5CA9801215), Jul 27, 1998: SKIN. CORROSION. LEFT BODY MLG INBD AND OTBD STRUT DOOR ASSEMBILES HAVE MANY SPOTS WITH LOST FINISH AND SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION IAW SRM 51-10-01. TREA
- [SDR P5CA9800776](https://openairdocs.org/sdr/P5CA9800776), May 21, 1998: COWL. DENTED. NUMBER 2 ENGINE NOSE COWL SKIN DENTED AT 0630 POSITION. REPAIRED NOSE COWL PANEL AT 0630 POSITION PER SRM 51-40-07.
- [SDR P5CA9800774](https://openairdocs.org/sdr/P5CA9800774), May 15, 1998: TRANSMITTER. INOPERATIVE. NR 2 ENGINE WOULD NOT MAKE TAKEOFF THRUST. TEMP 912 DEGREES 1:08 EPR. ABORTED TAKEOFF. REMOVED AND REPLACED EPR TRANSMITTER REF MM 77-11-00. REMOVED AND REPLACE
- [SDR 98ZZZX2249](https://openairdocs.org/sdr/98ZZZX2249), May 11, 1998: BRAKE. DAMAGED. WHILE PARKED ON GATE, NR 9, NR 11, AND NR 15, MAIN WHEELS COLLAPSED DUE TO BRAKE OVERHEAT. ON WHEEL CHANGE, NR 11 AND NR 15 BRAKE UNITS WERE FOUND DAMAGED AND W
- [SDR P5CA9800767](https://openairdocs.org/sdr/P5CA9800767), Apr 30, 1998: FITTING. GOUGED. LEFT I/B AILERON I/B PRIMARY HINGE WING FITTING LT SIDE IS GOUGED BY RETAINER BOLT HOLE AREA. BLENDED GOUGE LESS THAN 10 PERCENT MATERIAL LOSS PER SRM 57-50-01.
- [SDR P5CA9800765](https://openairdocs.org/sdr/P5CA9800765), Apr 30, 1998: ENGINE. MALFUNCTIONED. VIBRATION ON TAKEOFF. RETARDED AND ADVANCED NR 2 ENG THROTTLE. VIBRATION FOLLOWED THROTTLE MOVEMENT. A/C PACKS WERE OFF. REMOVED AND REPLACED NR 2 ENGINE PER MM
- [SDR P5CA9800747](https://openairdocs.org/sdr/P5CA9800747), Mar 31, 1998: KEEL BEAM. DAMAGED. SHEET METAL DAMAGE TO LOWER KEEL BEAM AREA AND LOWER WEB AT STA 1380 RT BODY WHEEL WELL. REPAIRED DAMAGED SECTION BY CUTTING OUT DAMAGE AND FABRICATION FILLERS,
- [SDR P5CA9800746](https://openairdocs.org/sdr/P5CA9800746), Mar 31, 1998: ACCUMULATOR. FAILED. BRAKE ACCUMULATOR LOWER CAP BROKEN OFF COMPLETELY. REMOVED AND REPAIRED BRAKE ACCUMULATOR PER MM 32-41-09. PRECHARGED ACCUMULATOR PER MM 12-15-09. SYSTEM TESTS 
- [SDR P5CA9800745](https://openairdocs.org/sdr/P5CA9800745), Mar 31, 1998: KEEL BEAM. DAMAGED. SHEET METAL DAMAGE TO UPPER KEEL BEAM WEB AT STATION 1380 IN THE RIGHT BODY WHEEL WELL. REPAIRED DAMAGED SECTION BY CUTTING DOUBLERS AND TRIPLERS PER PAC MA 531
- [SDR P5CA9800738](https://openairdocs.org/sdr/P5CA9800738), Mar 25, 1998: ACCUMULATOR. RUPTURED. DURING APPROACH, AFTER GEAR DOWN LOST NR 4 HYD SYSTEM, 0 BRAKE PRESSURE ON GUAGE. HYD BRAKE ACCUMULATOR RUPTURED, DAMAGE TRIM AIR DUCT, APU FUEL DRAIN LINE, HYD
- [SDR P5CA9800572](https://openairdocs.org/sdr/P5CA9800572), Mar 23, 1998: SUPPORT. CRACKED. APU VERTICAL SUPPORT TUBE AT BS 2705 WL 364 HAS CRACK. REPLACED PER SRM 51-10-01.
- [SDR P5CA9800571](https://openairdocs.org/sdr/P5CA9800571), Mar 23, 1998: FLAP. CORROSION. LEVEL 1 CORROSION AT LEADING EDGE FRONT SPAR WS 972 NR 7 FLAP. REPAIRED CORROSION PER SRM 51-10-01.
- [SDR P5CA9800570](https://openairdocs.org/sdr/P5CA9800570), Mar 23, 1998: STIFFENER. CORROSION. LEVEL 1 CORROSION ON RT WING GEAR STA 1350 STIFFENER. REPAIRED CORROSION PER SRM 51-10-01.
- [SDR P5CA9800569](https://openairdocs.org/sdr/P5CA9800569), Mar 23, 1998: FRAME. CRACKED. BS 540 S26L FRAME CRACKED. REPAIRED FRAME PER RS53-22-33687 BOEING.
- [SDR P5CA9800567](https://openairdocs.org/sdr/P5CA9800567), Mar 23, 1998: SEAT TRACK. CORROSION. LEVEL 1 CORROSION ON SEAT TRACK STA 920 RBL 97R. REPAIRED CORROSION PER SRM 53-10-05.
- [SDR P5CA9800734](https://openairdocs.org/sdr/P5CA9800734), Mar 21, 1998: SUPPORT. CRACKED. LEVEL 1 CORROSION MAIN DECK FLOOR SUPPORT BL 22 TO 24. REPAIRED CORROSION PER SRM 51-40-04.
- [SDR P5CA9800733](https://openairdocs.org/sdr/P5CA9800733), Mar 21, 1998: TIE DOWN. CORRODED. LEVEL 1 CORROSION AT TIE DOWN FITTING SUPPORT FUSELAGE BS 2300 BL 22. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.
- [SDR P5CA9800732](https://openairdocs.org/sdr/P5CA9800732), Mar 21, 1998: TIE DOWN. CORRODED. LEVEL 1 CORROSION AT TIE DOWN FUSELAGE BS 2180 BL 30. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

All 306: https://openairdocs.org/deregistered/N857FT-2007-08-30/reports.md

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