# Service difficulty reports: N851FT, cancelled Oct 8, 2002

A list on [N851FT, cancelled Oct 8, 2002](https://openairdocs.org/deregistered/N851FT-2002-10-08.md).

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

Page 1 of 11 · 501 reports

- [SDR P5CA9900233](https://openairdocs.org/sdr/P5CA9900233.md): Beam · corroded · Mar 1, 1999 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION FOUND ON LEFT WHEEL WELL CEILING BEAM. REMOVED LIGHT CORROSION AND TREATED AND PRIMED PER SRM 53-10-01 AND 51-10-02.
- [SDR P5CA9900232](https://openairdocs.org/sdr/P5CA9900232.md): Skin · cracked · Mar 1, 1999 · N851FT · Boeing 747122 · Landing Gear Doors
  > LEFT AFT MAIN LANDING GEAR DOOR INNER SURFACE CRACK IN SKIN. FABRICATED DOUBLER AND INSTALLED, TREATED AND PRIMED PER SRM 51-40-02 AND 51-30-01.
- [SDR P5CA9900231](https://openairdocs.org/sdr/P5CA9900231.md): Doubler · corroded · Mar 1, 1999 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION FOUND ON UPPER DOUBLER HORIZONTAL BEAM ON AND UNDER ATTACH FITTING AT STA 1335 LBL 90. REMOVED CORROSION AND PRIMED AND PAINTED PER SRM 53-10-02.
- [SDR P5CA9900230](https://openairdocs.org/sdr/P5CA9900230.md): Panel · delaminated · Mar 1, 1999 · N851FT · Boeing 747122 · Horizontal Stabilizer, Plate/Skin
  > RIGHT LOWER TRAILING EDGE PANEL 334 IS BADLY DELAMINATED ON HORIZ STAB. REMOVED AND REPLACED PANEL PER SRM 51-30-02.
- [SDR P5CA9801613](https://openairdocs.org/sdr/P5CA9801613.md): Antenna · malfunction · Nov 26, 1998 · N851FT · Boeing 747122 · Weather Radar System
  > RADAR SYSTEM TILT APPEARS TO POINT FULL DOWN IN SYSTEMS 1 AND 2, TESTS OK. AIRCRAFT RETURNED TO JFK. REMOVED AND REPLACED WEATHER RADAR ANTENNA REF MM 34-43-03. OPERATIONS CHECK OK. REPLACED NR 1 R/T REF MM 34-43-02. OPS CHECK NORMAL.
- [SDR P5CA9801557](https://openairdocs.org/sdr/P5CA9801557.md): Seat Track · corroded · Oct 17, 1998 · N851FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK AT BS 520R TO 720R. REPLACED FOR CONVIENENCE PER SRM 52-10-21 PG 45.
- [SDR P5CA9801556](https://openairdocs.org/sdr/P5CA9801556.md): Seat Track · corrosion · Oct 17, 1998 · N851FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK BS 520L TO 740L. REPLACED SEAT TRACK FROM BS 520L TO 740L FOR CONVIENENCE PER SRM 53-10-21 PG 45.
- [SDR P5CA9801555](https://openairdocs.org/sdr/P5CA9801555.md): Panel · cracked · Oct 17, 1998 · N851FT · Boeing 747122 · Wing, Plate/Skin
  > LEFT WING PANEL FWD OF LEFT FLYING PANEL HAS CRACK. REPAIRED PER SRM 51-40-09 AND 51-24-11.
- [SDR P5CA9801554](https://openairdocs.org/sdr/P5CA9801554.md): Intercostal · damaged · Oct 17, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > AFT CARGO BULK PIT BS 1720L TO BS 1740L SPACING RIB DAMAGED. REPAIRED PER SRM 51-10-01.
- [SDR P5CA9801553](https://openairdocs.org/sdr/P5CA9801553.md): Intercostal · broken · Oct 17, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT AT STATION 570 RBL 30 TO 35 FOUND BROKEN INTERCOSTAL. REMOVED AND REPLACED PER SRM 51-10-01 AND SRM 51-30-02.
- [SDR P5CA9801552](https://openairdocs.org/sdr/P5CA9801552.md): Angle · cracked · Oct 17, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO PIT AT STATION 1960 TO 1980 BL 22L ATTACH ANGLE FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-10-01 AND 51-30-02.
- [SDR P5CA9801551](https://openairdocs.org/sdr/P5CA9801551.md): Angle · cracked · Oct 17, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT AT STA 2000/2100L ATTACH ANGLES FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-10-01 AND 51-30-02.
- [SDR P5CA9801550](https://openairdocs.org/sdr/P5CA9801550.md): Floor · delaminated · Oct 17, 1998 · N851FT · Boeing 747122 · Fuselage Floor Panel
  > REPLACED UPPER DECK FLOOR PANELS AT BS 720R DUE DELAMINATION. REMOVED AND REPLACED PER SRM 53-22-01, 51-10-01 AND 51-30-02.
- [SDR P5CA9801549](https://openairdocs.org/sdr/P5CA9801549.md): Angle · cracked · Oct 17, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO STA 1940 BL 22L ATTACH ANGLE FOUND CRACKED. REPAIRED PER SRM 51-01-01, 51-30-02 AND 51-40-04.
- [SDR P5CA9801540](https://openairdocs.org/sdr/P5CA9801540.md): Support · cracked · Oct 16, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT STA 1960 BLR 34 TO STA 2020 BLR 34 FLOOR PANEL SUPPORT CRACKED. REMOVED AND REPLACED PER SRM 51-30-01.
- [SDR P5CA9801539](https://openairdocs.org/sdr/P5CA9801539.md): Angle · cracked · Oct 16, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK PIT STA 1970/1980 BL 22R ATTACH ANGLE HAS CRACK. REMOVED AND REPLACED PER SRM 51-10-01 AND SRM 51-30-03.
- [SDR P5CA9801538](https://openairdocs.org/sdr/P5CA9801538.md): Angle · cracked · Oct 16, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK PIT STA 2000 STR 22 SUPPORT ANGLE CRACKED. REMOVED AND REPAIRED PER SRM 51-10-01, 51-30-02 AND 51-40-04.
- [SDR P5CA9801545](https://openairdocs.org/sdr/P5CA9801545.md): Channel · cracked · Oct 15, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT STA 1940 TO STA 2060R SEVERAL HAT CHANNELS CRACKED. REMOVED AND REPAIRED HAT CHANNEL PER SRM 51-10-01 AND 51-30-02.
- [SDR P5CA9801544](https://openairdocs.org/sdr/P5CA9801544.md): Stringer · punctured · Oct 15, 1998 · N851FT · Boeing 747122 · Fuselage Main, Longeron/Stringer
  > UPPER DECK AT STA 1820R STR 15R FLANGE PUNCTURED. REPAIRED PER SRM 53-10-04, 51-30-02.
- [SDR P5CA9801543](https://openairdocs.org/sdr/P5CA9801543.md): Channel · cracked · Oct 15, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO AREA STA 2060L SUPPORT CHANNEL HAS CRACK AT LT SIDE. REMOVED AND REPLACED PER SRM 51-40-03.
- [SDR P5CA9801542](https://openairdocs.org/sdr/P5CA9801542.md): Support · cracked · Oct 15, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO PIT AT STA 2000L FLOOR PANEL SUPPORT CRACKED AT TIEDOWN AREA. REMOVED AND REPLACED PER SRM 51-30-02.
- [SDR P5CA9801541](https://openairdocs.org/sdr/P5CA9801541.md): Frame · gouged · Oct 15, 1998 · N851FT · Boeing 747122 · Fuselage Main, Frame
  > UPPER DECK FRAME AT BS 2060 STR 16L FOUND GOUGE. REPAIRED PER SRM 53-10-04.
- [SDR P5CA9801537](https://openairdocs.org/sdr/P5CA9801537.md): Floor · delaminated · Oct 10, 1998 · N851FT · Boeing 747122 · Fuselage Floor Panel
  > FLOOR PANEL STATION 500 TO 580 RBL 20 FOUND DELAMINATED. REMOVED AND REPAIRED PER SRM 51-10-01 AND 51-30-02.
- [SDR P5CA9801548](https://openairdocs.org/sdr/P5CA9801548.md): Frame · damaged · Oct 7, 1998 · N851FT · Boeing 747122 · Fuselage Main, Frame
  > MAIN CABIN FRAME STATION 1740R STR 12R FOUND DAMAGED. REPAIRED DAMAGE PER SRM 53-10-04.
- [SDR P5CA9801547](https://openairdocs.org/sdr/P5CA9801547.md): Angle · cracked · Oct 7, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT AT STATION 1960 BL 50R ANGLE FOUND CRACKED. REPAIRED PER SRM 51-10-01, 53-10-03 AND 51-30-02.
- [SDR P5CA9801546](https://openairdocs.org/sdr/P5CA9801546.md): Support · cracked · Oct 7, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > BULK CARGO PIT STA 2080R FLOOR PANEL SUPPORT FOUND CRACKED. REPAIRED PER SRM 51-40-03.
- [SDR P5CA9801378](https://openairdocs.org/sdr/P5CA9801378.md): Engine · failed · Aug 29, 1998 · N851FT · Boeing 747122 · Engine (Turbine/Turboprop)
  > DURING CLIMBOUT PASSING FL120, ACFT EXPERIENCED LOUD NOISE AND SHUDDER AND FLASH OF LIGHT FOLLOWED BY INCREASE IN NR 1 ENG EGT TO 960 DEGREES. ENGINE SHUT DOWN. DUMPED FUEL AND RETURNED TO SNN. REPLACED NR 1 ENGINE PER BMM 71-00-02 AND PAC M7100-002/M7111-0
- [SDR P5CA9801207](https://openairdocs.org/sdr/P5CA9801207.md): Engine · flamed out · Jul 26, 1998 · N851FT · Boeing 747122 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FLAMED OUT FL350. ENG RESTART AT FL 290. RESTART NORMAL. PERFORMED FUEL CONTAMINATION CHECK PER MM 73-00-00 PG 201. VERIFIED FUEL REMAIN NR 2 TANK VIA STICK 17 AT 20.0, 10,962 LBS. SUMPED TANKS FOR EVIDENCE OF WATER, VERIFIED CONDITON MOTOR OP
- [SDR P5CA9801208](https://openairdocs.org/sdr/P5CA9801208.md): Wire · chafed · Jul 22, 1998 · N851FT · Boeing 747122 · Fire Detection
  > REJECTED TAKEOFF FROM RTA DUE TO AFT CARGO FIRE INDICATION AND FIRE BELL DURING T/O ROLL. PARKED AND INSPECTED FOR FIRE. NO SMOKE OR FIRE NOTED. TRANSFERED TO DMI NR 20623 AND 20624. REMOVED AND REPLACED SMOKE DETECTOR PANEL P-4 FOR T/S PER MM 26-16-00 DMI
- [SDR P5CA9800795](https://openairdocs.org/sdr/P5CA9800795.md): Case · cracked · May 20, 1998 · N851FT · Boeing 747122 · Engine Collector/Tailpipe/Nozzle
  > NR 1 ENGINE TURBINE EXHAUST CASE CRACKED, FLANGE AT 10 O'CLOCK POSITION. REPLACED CASE PER P AND W OVERHAUL MANUAL 72-00-00.
- [SDR P5CA9800794](https://openairdocs.org/sdr/P5CA9800794.md): Mount · worn · May 20, 1998 · N851FT · Boeing 747122 · Engine Mount Section
  > NR 1 ENGINE FORWARD UPPER ENGINE MOUNT INBOARD HANGER FITTING INNERMOST LUG WAS PREVIOUSLY REWORKED AND BUSHIN MIGRATED OUT. SPOT FACED THE LUG, SHOT PEENED THE REWORKED SURFACE, REWORKED THE BUSHING AND INSTALLED WITH NEW WASHER PER BOEING TELEX PAO-HKG-98-0
- [SDR P5CA9800793](https://openairdocs.org/sdr/P5CA9800793.md): Skin · damaged · May 20, 1998 · N851FT · Boeing 747122 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON LEFT OUTER SKIN AT NAC STN 220 AND RT SKIN AT STN 233 FOUND DAMAGED. REPAIRED PER BOEING SRM 54-30-03.
- [SDR P5CA9800792](https://openairdocs.org/sdr/P5CA9800792.md): Frame · cracked · May 20, 1998 · N851FT · Boeing 747122 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 PYLON RIGHT FRAME AT NAC STN 168 CRACKED AND LEFT FRAME AT NAC STN 193 FOUND CHAFED. REPLACED FRAMES PER BOEING SRM 51-10-01.
- [SDR P5CA9800791](https://openairdocs.org/sdr/P5CA9800791.md): Skin · corroded · May 20, 1998 · N851FT · Boeing 747122 · Wing, Plate/Skin
  > LEVEL 2 CORROSION LEFT WING LEADING EDGE SKIN PANEL AT FSSO 1486. REPAIRED PER BOEING SRM 57-30-03 FIG 4.
- [SDR P5CA9800790](https://openairdocs.org/sdr/P5CA9800790.md): Skin · corroded · May 20, 1998 · N851FT · Boeing 747122 · Wing, Plate/Skin
  > LEVEL 1 CORROSION LEFT WING LOWER SKIN AT NR 1 MAIN FUEL TANK INBOARD BOOST PUMP. REMOVED CORROSION AND SHOT PEENED INSTALLED A SEALANT RAMP PER BOEING TELEX PAO-HKG-98-0093TE AND HAECO REPAIR SCHEME R-57-26-33741.
- [SDR P5CA9800789](https://openairdocs.org/sdr/P5CA9800789.md): Frame · cracked · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Main, Frame
  > CRACKED FRAME WEB AT LEFT WING LANDING GEAR WHEEL WELL BS 1375 S-32L. REPAIRED PER BOEING TELEX PAO-HKG-98-0091TE/0108RE AND HAECO REPAIR SCHEME R-53-42-33743.
- [SDR P5CA9800788](https://openairdocs.org/sdr/P5CA9800788.md): Stringer · cracked · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER S-24L AT BS 380 TO 400. REPLACED STRINGER PER BOEING SRM 51-10-01.
- [SDR P5CA9800787](https://openairdocs.org/sdr/P5CA9800787.md): Web · cracked · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > MAIN DECK BS 360 TO 380 RT WEB FOUND CRACKED AT S-32R. WEB REPAIRED PER BOEING SRM 51-40-01.
- [SDR P5CA9800786](https://openairdocs.org/sdr/P5CA9800786.md): Stiffener · deformed · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > DEFORMED UPPER DECK FLOORBEAM ATTACH VERTICAL STIFFENERS AT BS 460 RBL 55 AND RBL 74. REPLACED STIFFENERS PER BOEING SRM 51-10-01.
- [SDR P5CA9800785](https://openairdocs.org/sdr/P5CA9800785.md): Frame · cracked · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Main, Frame
  > CRACKED FRAME WEB BS 360 S-23L. REPAIRED PER BOEING TELEX PAO=HKG-98-0109RE/0099TE AND HAECO REPAIR SCHEME R-53-12-33724.
- [SDR P5CA9800784](https://openairdocs.org/sdr/P5CA9800784.md): Frame · cracked · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Main, Frame
  > CRACKED FRAME WEB AND DOUBLER AT BS 380 S-24L. REPAIRED PER BOEING TELEX PAO-HKG-98-106TE/0116RE AND HAECO REPAIR SCHEME R-53-12-33742.
- [SDR P5CA9800783](https://openairdocs.org/sdr/P5CA9800783.md): Skin · dented · May 20, 1998 · N851FT · Boeing 747122 · Service Doors
  > DENT ON UPPER DECK CREW SERVICE DOOR AFT EDGE MID PORTION. REPAIRED PER BOEING SRM 52-00-03 FIG 3.
- [SDR P5CA9800782](https://openairdocs.org/sdr/P5CA9800782.md): Stringer · corroded · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Main, Longeron/Stringer
  > LEVEL 2 CORROSION RIVET SHEARED AND SKIN BULGED AT BS 1000 AT S-42L. CORROSION REMOVED AND STRINGER REPAIRED PER BOEING SRM 53-10-03 FIG 1.
- [SDR P5CA9800781](https://openairdocs.org/sdr/P5CA9800781.md): Skin · dented · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Main, Plate/Skin
  > DENT AFT FUSELAGE SKIN AT PREVIOUS REPAIR FORWARD AND AFT OF BS 2598 JACK POINT. REPAIRED PER BOEING SRM 53-30-03 FIG 1A.
- [SDR P5CA9800780](https://openairdocs.org/sdr/P5CA9800780.md): Skin · dented · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Main, Plate/Skin
  > DENT IN THE LOWER FUSELAGE AT BS 1780 TO 1800 S35R TO S36R. REPAIRED PER BOEING SRM 53-30-03 FIG 1.
- [SDR P5CA9800779](https://openairdocs.org/sdr/P5CA9800779.md): Skin · corroded · May 20, 1998 · N851FT · Boeing 747122 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION AT UNDERSIDE OF ANTENNA 10 AFT OF CENTER ELECTRONICS BAY DOOR CUTOUT BS 820 TO 840 S47L TO S47R. REMOVED CORROSION REPLACED DOUBLER PER BOEING SRM 53-30-03.
- [SDR P5CA9800971](https://openairdocs.org/sdr/P5CA9800971.md): Duct · cracked · May 5, 1998 · N851FT · Boeing 747122 · Engine Cowling System
  > NUMBER 2 ENGINE RT SIDE COWL BREATHER EXHAUST DUCT CRACKED AT FLANGE RADIUS. WELD REPAIRED PER BAC 5975 REV L.
- [SDR P5CA9800875](https://openairdocs.org/sdr/P5CA9800875.md): Web · cracked · May 4, 1998 · N851FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > M/D B/S 320-340 LT SIDE FLOOR SUPPORT WEB FOUND CRACKED AT S26L AREA. FLOOR SUPPORT WEB REPLACED AS PER SRM 51-10-01.
- [SDR P5CA9800879](https://openairdocs.org/sdr/P5CA9800879.md): Flap Track · corroded · May 1, 1998 · N851FT · Boeing 747122 · Trailing Edge Flaps
  > AFTER REMOVAL OF BEARING FROM L/W I/B MIDFLAP O/B SLIDING TRACK FWD ATTACH CORROSION FOUND IN BORE. TRACK REPAIRED IAW OHM 57-52-35.
- [SDR P5CA9800888](https://openairdocs.org/sdr/P5CA9800888.md): Web · cracked · Apr 29, 1998 · N851FT · Boeing 747122 · Trailing Edge Flaps
  > LEFT WING I/B FOREFLAP I/B WEB FOUND CRACKED. REPAIRED AS PER SRM 51-10-01.

Next page: https://openairdocs.org/deregistered/N851FT-2002-10-08/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N851FT' AND deregistration_id = 'N851FT-2002-10-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N851FT-2002-10-08/reports

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