# Service difficulty reports: N852FT, cancelled Jun 17, 2002

A list on [N852FT, cancelled Jun 17, 2002](https://openairdocs.org/deregistered/N852FT-2002-06-17.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 7 · 331 reports

- [SDR P5CA0200663](https://openairdocs.org/sdr/P5CA0200663.md): Valve · binding · Mar 12, 2002 · N852FT · Boeing 747122 · Fuel Storage
  > DURING REFUELING, NR 1 RESERVE VALVE FAILED TO OPEN AND UNABLE TO PUT FUEL INTO NR 1 RESERVE TANK. FOUND EXCESSIVE SHAFT BINDING THAT WOULD ONLY ALLOW PARTIAL OPENING OF THE VALVE. FUELED TANK, MANUALLY CLOSED VALVE. AFTER REFUELING, NR 2 MAIN TANK READ 38.
- [SDR P5CA0200652](https://openairdocs.org/sdr/P5CA0200652.md): Switch · faulty · Feb 23, 2002 · N852FT · Boeing 747122 · Landing Gear Brake System
  > REF DMI 28874 / MEL 27-9: AUTOSPOILER BRAKE DID NOT DEPLOY ON LANDING. TROUBLESHOT & FOUND THROTTLE SWITCH S860 AT FAULT. REPLACED SAME & OPS CHKD OK PER MM 27-62-00. THIS CLEARS DMI 28874 / MEL 27-9. PLACARDS REMOVED.
- [SDR P5CA0200638](https://openairdocs.org/sdr/P5CA0200638.md): Compressor · failed · Feb 1, 2002 · N852FT · Boeing 747122 · Turbine Engine Compressor Section
  > WHILE CLIMBING, NR 3 FAILED WITH LOUD BANG AND VIBRATION. EPR DECREASED RAPIDLY AND EGT INCREASED TO APPROX 910. PERFORMED ENG FIRE/SEVERE DAMAGE CHECKLIST. SECURED ENGINE WITH ENGINE SHUTDOWN CHECKLIST. EMERGENCY DECLARED; DIVERTED TO SIN - CHANGI AIRPORT
- [SDR P5CA0100617](https://openairdocs.org/sdr/P5CA0100617.md): Web · cracked · Nov 23, 2001 · N852FT · Boeing 747122 · Fuselage Main, Structure
  > NOSE WHEEL WELL VERTICAL BEAM INSPECTION IAW MA A5310-33:01 REVEALED A CRACK 1-3/8" LONG AT WEB TO CHORD FASTENER LOCATION AT VERTICAL BEAM STN 320 R/H SIDE, WEB 2. REPAIRED IAW SRM 51-40-02, PAGE 5, DETAIL 111.
- [SDR P5CA0100616](https://openairdocs.org/sdr/P5CA0100616.md): Web · cracked · Nov 23, 2001 · N852FT · Boeing 747122 · Fuselage Main, Structure
  > NOSE WHEEL WELL VERTICAL BEAM INSPECTION IAW MA A5310-33:01 REVEALED A CRACK AT STANDOFF HOLE 2-3/8" LONG AT VERTICAL BEAM STN 320 R/H SIDE, WEB 2. CRACK REPAIRED IAW SRM 51-40-02, PAGE5, DETAIL 111.
- [SDR 0100570](https://openairdocs.org/sdr/0100570.md): Panel · delaminated · Jul 2, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > LT WING PANEL AT L/E 4TH PANEL FROM FUSELAGE DELAMINATED. REMOVED AND REPLACED LT WING PANEL L/E 4TH FORM FUSELAGE AS PER SRM 51-30-02.
- [SDR P5CA0100529](https://openairdocs.org/sdr/P5CA0100529.md): Panel · delaminated · Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > RT WING PANEL BEHIND NR 2 INBOARD SPOILER FIBERGLASS COMING LOOSE. FIBERGLASS PANEL REPAIRED PER SRM 51-40-08.
- [SDR P5CA0100528](https://openairdocs.org/sdr/P5CA0100528.md): Panel · delaminated · Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > RT WING PANEL BEHIND NR 1 INBOARD SPOILER WBL 264 FIBERGLASS COWLING LOOSE. FIBERGLASS PANEL REPAIRED AS PER SRM 51-40-08.
- [SDR P5CA0100527](https://openairdocs.org/sdr/P5CA0100527.md): Fairing · damaged · Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > DAMAGE FOUND ON NR 6 CANOE FIXED FAIRING WBL 353. FAIRING REPAIRED PER SRM 51-40-08.
- [SDR P5CA0100526](https://openairdocs.org/sdr/P5CA0100526.md): Fairing · damaged · Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > DAMAGE FOUND ON FIX FAIRING IN FRONT OF NR 6 CANOE. FAIRING REPAIRED PER SRM 51-40-08.
- [SDR P5CA0100525](https://openairdocs.org/sdr/P5CA0100525.md): Skin · delaminated · Mar 27, 2001 · N852FT · Boeing 747122 · Trailing Edge Flaps
  > DELAMINATION FOUND ON RT WING INBOARD LOWER FLAP WBL 163. REPAIRED PER SRM 51-40-08.
- [SDR P5CA0100524](https://openairdocs.org/sdr/P5CA0100524.md): Panel · delaminated · Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > LT WING PANEL WBL 461 OF INBOARD AILERON HAS LOOSE FIBERGLASS. REPAIR CARRIED OUT IAW SRM 51-40-08.
- [SDR P5CA0100532](https://openairdocs.org/sdr/P5CA0100532.md): Panel · delaminated · Mar 23, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > LT WING PANEL THAT IS BEHIND FLYING PANEL HAS FIBERGLASS COMING LOOSE STA 197. REPAIRED CARREID OUT IAW SRM 51-40-08.
- [SDR P5CA0100531](https://openairdocs.org/sdr/P5CA0100531.md): Panel · delaminated · Mar 23, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > LT PANEL DIRECTLY BEHIND FLYING PANEL LT WING WBL 197 HAS LOOSE FIBERGLASS. REPARIED CARRIED OUT IAW SRM 51-40-08.
- [SDR P5CA0100530](https://openairdocs.org/sdr/P5CA0100530.md): Panel · delaminated · Mar 23, 2001 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > LT WING PANEL ON L/EDGE OF FUSELAGE WBL 150 HAS LOOSE FIBERGLASS. REPAIRED CARRIED OUT PER SRM 51-40-08.
- [SDR P5CA0100467](https://openairdocs.org/sdr/P5CA0100467.md): Skin · delaminated · Feb 13, 2001 · N852FT · Boeing 747122 · Trailing Edge Flaps
  > DELAMINATION FOUND ON LEFT O/B MID FLAP. REPAIRED PER PAO-LGB01-00045F.
- [SDR P5CA0200631](https://openairdocs.org/sdr/P5CA0200631.md): Light · defective · Jan 16, 2001 · N852FT · Boeing 747122 · Emergency Lighting
  > EMERGENCY LIGHT IN CEILING AFT OF P6 PANEL ILLUMINATES ONLY MOMENTARILY. REPLACED EMERGENCY LIGHT AFT OF P6. OPS CHECK OK.
- [SDR P5CA0000207](https://openairdocs.org/sdr/P5CA0000207.md): Bolt · sheared · Jun 14, 2000 · N852FT · Boeing 747122 · Nacelle/Pylon, Attach Fittings
  > ON PYLONS NR 1, 3 AND 4, SHEARED.375 BOLTS ON HORIZONTAL FIRE WALL ADJACENT TO THE AFT MOUNT LUGS. BOLTS ARE VERTICAL THROUGH AFT MOUNT FITTING AND LOWER PYLON SKIRT CHORDS. REMOVED AND REPLACED ALL 8 BOLTS PER PYLON. REPLACED WITH OVERSIZED TO.4375 PER B
- [SDR P5CA0000195](https://openairdocs.org/sdr/P5CA0000195.md): Torque Tube · damaged · May 17, 2000 · N852FT · Boeing 747122 · Passenger/Crew Doors
  > LEFT ENTRY DOOR LIGHT DR1 CAME ON DURING DESCENT AND REMAINED ON. DR1 LIGHT CAME ON AT APPROX 2.4 PSI DIF PRESS. REMOVED AND REPLACED LOWER TORQUE TUBE ASSY, PER MM 52-11-00, ADJUSTED DOOR WARNING LIGHT PER MM 52-17-00. OPS CHECK OK ON GROUND.
- [SDR 99ZZZX3706](https://openairdocs.org/sdr/99ZZZX3706.md): Push Rod · failed · Aug 22, 1999 · N852FT · Boeing 747122 · Trailing Edge Flap Control System
  > DURING WALK-AROUND INSPECTION, NR 3 FAIRING CANOE WAS FOUND PIERCED WITH FLAP PUSH ROD. ON INVESTIGATION AFTER DROPPING THE FLAPS (T/E), FOUND THE FLAP PUSH ROD HAD SHEARED ON THE FORWARD END. THE BROKEN PUSH ROD PIERCED THE FAIRING DURING FLAP RETRACTION.
- [SDR P5CA9900152](https://openairdocs.org/sdr/P5CA9900152.md): Engine · failed · Feb 8, 1999 · N852FT · Boeing 747122 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE SHUT DOWN DUE TO STEADY STATE STALL AFTER DESCENDING FROM 370 TO 350. ATTEMPTED TO RESTART AT 350 AND 280, UNSUCCESSFUL. LAST START WAS AT 0050Z, WINDMILL TIME 1 HOUR AND 33 MIN. N1-30 PERCENT, N2-21 PERCENT, OIL PRESSURE 15 PSI, FL 280, IAS 295
- [SDR P5CA9900002](https://openairdocs.org/sdr/P5CA9900002.md): Skin · punctured · Jan 10, 1999 · N852FT · Boeing 747122 · Fuselage Main, Plate/Skin
  > CENTER AFT LOWER FUSELAGE APPROX STA 2500 FOUND HOLE. REPAIRED IAW SRM 53-30-03.
- [SDR P5CA9900001](https://openairdocs.org/sdr/P5CA9900001.md): Skin · punctured · Jan 6, 1999 · N852FT · Boeing 747122 · Auxiliary Power Unit (APU) Doors
  > RT APU DOOR PUNCTURED BY WORK STAND DURING LIGHT WIND STORM. REPAIRED IAW SRM 52-40-02.
- [SDR P5CA9900004](https://openairdocs.org/sdr/P5CA9900004.md): Panel · cracked · Jan 2, 1999 · N852FT · Boeing 747122 · Wing, Plate/Skin
  > RIGHT WING FLYING PANEL CRACKED ON LOWER SIDE IN BOX AREA. REMOVED AND REPLACED FLYING PANEL PER MM 57-22-01.
- [SDR P5CA9900003](https://openairdocs.org/sdr/P5CA9900003.md): Skin · delaminated · Dec 30, 1998 · N852FT · Boeing 747122 · Engine Cowling System
  > NR 2 ENGINE I/B FAN COWL UPPER AFT CORNER BENT AND DELAMINATED. REPAIRED IAW SRM 51-40-06.
- [SDR P5CA9801460](https://openairdocs.org/sdr/P5CA9801460.md): Engine · failed · Sep 18, 1998 · N852FT · Boeing 747122 · Engine (Turbine/Turboprop)
  > AT FL 330 NR 4 ENGINE STALLED WITH AN AUDIBLE SOUND AND WENT TO A OVER TEMP OF 950Ý FOR 3-4 SECONDS. ENGINE WAS THEN SHUT DOWN, PER CHECK LIST. RELIGHT WAS ATTEMPED AT FL 240 BUT THE EGT WAS MUCH HIGHER AS ENGINE STARTED TO ACCELERATE. THE ENGINE WAS SHUT D
- [SDR P5CA9801528](https://openairdocs.org/sdr/P5CA9801528.md): Logic Box · malfunction · Sep 4, 1998 · N852FT · Boeing 747122 · Landing Gear Position and Warning
  > FOLLOWING T/O, RED GEAR LIGHT ON P2 WITH HORN. AIR TURN BACK. REPLACED LANDING GEAR LOGIC MODULE IAW MM 31-26-03, OPS CHECK OK.
- [SDR P5CA9801390](https://openairdocs.org/sdr/P5CA9801390.md): Logic Module · malfunction · Sep 4, 1998 · N852FT · Boeing 747122 · Landing Gear Position and Warning
  > FOLLOWING TAKEOFF HAD GEAR UP WARNING LIGHT AND AUDIBLE WARNING HORN. ALL LANDING GEAR WARNING LTS AT F/E STATION REMAINED ILL. RETURNED TO HKG. REPLACED LANDING GEAR LOGIC MODULE IAW MM 31-26-03. OPS CHECK OK.
- [SDR P5CA9801389](https://openairdocs.org/sdr/P5CA9801389.md): Frame · cracked · Sep 4, 1998 · N852FT · Boeing 747122 · Fuselage Main, Frame
  > FRAME AT BS 960L STR 5 LEFT FOUND CRACKED. REPAIRED PER SRM 53-10-04 FIG 54.
- [SDR P5CA9801386](https://openairdocs.org/sdr/P5CA9801386.md): Longeron · cracked · Sep 4, 1998 · N852FT · Boeing 747122 · Fuselage Main, Longeron/Stringer
  > OVERWING LONGERON BULKHEAD FORGING AT BS 1480 STR 32-33R FOUND CRACK 6 INCHES LONG PLUS NUMEROUS MINOR BOLT HOLE CRACKS IN FITTINGS OF ASSOCIATED AREA. REPAIRED PER HAECO REPAIR SCHEME R53-43-33825 AND NUMEROUS 8110-3 FORMS AND BOEING SB 53A2390.
- [SDR P5CA9801379](https://openairdocs.org/sdr/P5CA9801379.md): Deck · corroded · Sep 4, 1998 · N852FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION FOUND ON PRESSURE DECK SKIN BS 1354 BL 113 LEFT. REPAIRED PER REPAIR SCHEME R53-48-33819 AND 8110-03.
- [SDR P5CA9801388](https://openairdocs.org/sdr/P5CA9801388.md): Web · corrosion · Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION FOUND ON WING GEAR WHEEL WELL BS 1242 TO 1246 WL 155 RIGHT WEB. REPAIRED PER SRM 53-10-01 FIG 1.
- [SDR P5CA9801387](https://openairdocs.org/sdr/P5CA9801387.md): Bulkhead Splice · cracked · Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, Bulkhead
  > NUMEROUS BOLT HOLE CRACKS IN COMMON FITTINGS OF THE BODY STATION 1480 BULKHEAD LONGERON SPLICE. REPAIRED PER HAECO REPAIR SCHEME R53-61-33817 AND NUMEROUS 8110 REPORTS AND SB 53A2390.
- [SDR P5CA9801385](https://openairdocs.org/sdr/P5CA9801385.md): Frame · cracked · Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, Frame
  > FRAME CHORD AT BS 970 STR 8 AND 9 RIGHT FOUND CRACKS. REPAIRED FRAME PER SRM 53-10-04 FIG 54.
- [SDR P5CA9801383](https://openairdocs.org/sdr/P5CA9801383.md): Frame · cracked · Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, Frame
  > FRAME STRUCTURES AT BS 380 LEFT STR 23-25R FOUND EXTENSIVE CRACKING LEFT AND RIGHT SIDES. REPLACED FRAME ASSY PER PAO-HKG 98-0140 AND HAECO RS 5312-23812 AND 8110-03.
- [SDR P5CA9801382](https://openairdocs.org/sdr/P5CA9801382.md): Frame · cracked · Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, Frame
  > FRAME AT BS 960 STR 5-6 RIGHT FOUND CRACKED. REPAIRED PER SRM 53-10-04 FIG 54.
- [SDR P5CA9801381](https://openairdocs.org/sdr/P5CA9801381.md): Skin · cracked · Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, Plate/Skin
  > FOUND 65 LONGITUDINAL FASTENER HOLES IN SKIN CRACKED. REAMED OUT HOLES, HFEC, FREEZE PLUGS AND REPAIRED SKIN PER SRM 53-22-72.
- [SDR P5CA9801380](https://openairdocs.org/sdr/P5CA9801380.md): Longeron · corroded · Sep 2, 1998 · N852FT · Boeing 747122 · Fuselage Main, Longeron/Stringer
  > LEVEL 1 CORROSION FOUND ON LONGERON AT BS 1840 TO 1860 STR 45 LEFT. CORROSION REMOVED PER SRM 53-10-01.
- [SDR P5CA9801417](https://openairdocs.org/sdr/P5CA9801417.md): Seat Track · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL ONE CORROSION FOUND AT UPPER DECK RT SEAT TRACK, BS 600-710, WL 300, BL R46. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.
- [SDR P5CA9801415](https://openairdocs.org/sdr/P5CA9801415.md): Seat Track · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK CROWN AREA, BS 600-710, WL 300, LBL 46. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-05.
- [SDR P5CA9801414](https://openairdocs.org/sdr/P5CA9801414.md): Seat Track · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK CROWN SURFACE, BS 600-710, WL 300. CORROSION REMOVED AND SEAT TRACK REPLACED AS PER SRM 51-10-01, 53-10-01, 53-10-05 AND MM 51-24-11.
- [SDR P5CA9801413](https://openairdocs.org/sdr/P5CA9801413.md): Seat Track · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL ONE CORROSION FOUND AT UPPER DECK RT SEAT TRACK, BS 600-700, WL 300, BL R27. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-05.
- [SDR P5CA9801412](https://openairdocs.org/sdr/P5CA9801412.md): Seat Track · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL ONE CORROSIN FOUND AT UPPER DECK RT SEAT TRACK, BS 600-710, WL 300, RBL 64. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-01.
- [SDR P5CA9801411](https://openairdocs.org/sdr/P5CA9801411.md): Seat Track · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL ONE CORROSION FOUND AT CROWN AREA OF UPPER DECK LT SEAT TRACK, BS 600-700, WL 300. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-01.
- [SDR P5CA9801410](https://openairdocs.org/sdr/P5CA9801410.md): Seat Track · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK, BS 600-700, WL 300. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02, 53-10-01, AND MM 51-24-11.
- [SDR P5CA9801409](https://openairdocs.org/sdr/P5CA9801409.md): Seat Track · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL ONE CORROSION AND CRACK FOUND AT UPPER DECK RBL 23 SEAT TRACK OUTBOARD FLANGE, BS 545-560. CORROSION REMOVED, AREA REPAIRED AND REPROTECTED AS PER SRM 51-10-01, 51-10-02, AND 53-10-01.
- [SDR P5CA9801408](https://openairdocs.org/sdr/P5CA9801408.md): Intercostal · cracked · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > UPPER DECK BS 380-390 S5R-6R INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-10-01.
- [SDR P5CA9801407](https://openairdocs.org/sdr/P5CA9801407.md): Intercostal · cracked · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage Miscellaneous Structure
  > UPPER DECK BS 380-390 STR 7R INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-10-01.
- [SDR P5CA9801405](https://openairdocs.org/sdr/P5CA9801405.md): Skin · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage Main, Plate/Skin
  > LEVEL ONE CORROSION FOUND AT MAIN DECK CROWN BS 2200-2280 STR 4R LAP JOINT AREA. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02 AND 53-30-01.
- [SDR P5CA9801404](https://openairdocs.org/sdr/P5CA9801404.md): Skin · corroded · Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage Main, Plate/Skin
  > LEVEL ONE CORROSION FOUND AT MAIN DECK BS 1725 STR 12L LAP JOINT AREA. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02, 53-30-01 AND MM 51-24-11.

Next page: https://openairdocs.org/deregistered/N852FT-2002-06-17/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 = 'N852FT' AND deregistration_id = 'N852FT-2002-06-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N852FT-2002-06-17/reports

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