N852FT, cancelled Jun 17, 2002

Service difficulty reports · 331

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR P5CA0200663Valve · bindingDURING 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.Mar 12, 2002 · N852FT · Boeing 747122 · Fuel StorageSDR P5CA0200652Switch · faultyREF 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.Feb 23, 2002 · N852FT · Boeing 747122 · Landing Gear Brake SystemSDR P5CA0200638Compressor · failedWHILE 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 AIRPORTFeb 1, 2002 · N852FT · Boeing 747122 · Turbine Engine Compressor SectionSDR P5CA0100617Web · crackedNOSE 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.Nov 23, 2001 · N852FT · Boeing 747122 · Fuselage Main, StructureSDR P5CA0100616Web · crackedNOSE 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.Nov 23, 2001 · N852FT · Boeing 747122 · Fuselage Main, StructureSDR 0100570Panel · delaminatedLT 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.Jul 2, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100529Panel · delaminatedRT WING PANEL BEHIND NR 2 INBOARD SPOILER FIBERGLASS COMING LOOSE. FIBERGLASS PANEL REPAIRED PER SRM 51-40-08.Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100528Panel · delaminatedRT WING PANEL BEHIND NR 1 INBOARD SPOILER WBL 264 FIBERGLASS COWLING LOOSE. FIBERGLASS PANEL REPAIRED AS PER SRM 51-40-08.Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100527Fairing · damagedDAMAGE FOUND ON NR 6 CANOE FIXED FAIRING WBL 353. FAIRING REPAIRED PER SRM 51-40-08.Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100526Fairing · damagedDAMAGE FOUND ON FIX FAIRING IN FRONT OF NR 6 CANOE. FAIRING REPAIRED PER SRM 51-40-08.Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100525Skin · delaminatedDELAMINATION FOUND ON RT WING INBOARD LOWER FLAP WBL 163. REPAIRED PER SRM 51-40-08.Mar 27, 2001 · N852FT · Boeing 747122 · Trailing Edge FlapsSDR P5CA0100524Panel · delaminatedLT WING PANEL WBL 461 OF INBOARD AILERON HAS LOOSE FIBERGLASS. REPAIR CARRIED OUT IAW SRM 51-40-08.Mar 27, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100532Panel · delaminatedLT WING PANEL THAT IS BEHIND FLYING PANEL HAS FIBERGLASS COMING LOOSE STA 197. REPAIRED CARREID OUT IAW SRM 51-40-08.Mar 23, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100531Panel · delaminatedLT PANEL DIRECTLY BEHIND FLYING PANEL LT WING WBL 197 HAS LOOSE FIBERGLASS. REPARIED CARRIED OUT IAW SRM 51-40-08.Mar 23, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100530Panel · delaminatedLT WING PANEL ON L/EDGE OF FUSELAGE WBL 150 HAS LOOSE FIBERGLASS. REPAIRED CARRIED OUT PER SRM 51-40-08.Mar 23, 2001 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA0100467Skin · delaminatedDELAMINATION FOUND ON LEFT O/B MID FLAP. REPAIRED PER PAO-LGB01-00045F.Feb 13, 2001 · N852FT · Boeing 747122 · Trailing Edge FlapsSDR P5CA0200631Light · defectiveEMERGENCY LIGHT IN CEILING AFT OF P6 PANEL ILLUMINATES ONLY MOMENTARILY. REPLACED EMERGENCY LIGHT AFT OF P6. OPS CHECK OK.Jan 16, 2001 · N852FT · Boeing 747122 · Emergency LightingSDR P5CA0000207Bolt · shearedON 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 BJun 14, 2000 · N852FT · Boeing 747122 · Nacelle/Pylon, Attach FittingsSDR P5CA0000195Torque Tube · damagedLEFT 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.May 17, 2000 · N852FT · Boeing 747122 · Passenger/Crew DoorsSDR 99ZZZX3706Push Rod · failedDURING 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. Aug 22, 1999 · N852FT · Boeing 747122 · Trailing Edge Flap Control SystemSDR P5CA9900152Engine · failedNR 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 295Feb 8, 1999 · N852FT · Boeing 747122 · Engine (Turbine/Turboprop)SDR P5CA9900002Skin · puncturedCENTER AFT LOWER FUSELAGE APPROX STA 2500 FOUND HOLE. REPAIRED IAW SRM 53-30-03.Jan 10, 1999 · N852FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9900001Skin · puncturedRT APU DOOR PUNCTURED BY WORK STAND DURING LIGHT WIND STORM. REPAIRED IAW SRM 52-40-02.Jan 6, 1999 · N852FT · Boeing 747122 · Auxiliary Power Unit (APU) DoorsSDR P5CA9900004Panel · crackedRIGHT WING FLYING PANEL CRACKED ON LOWER SIDE IN BOX AREA. REMOVED AND REPLACED FLYING PANEL PER MM 57-22-01.Jan 2, 1999 · N852FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9900003Skin · delaminatedNR 2 ENGINE I/B FAN COWL UPPER AFT CORNER BENT AND DELAMINATED. REPAIRED IAW SRM 51-40-06.Dec 30, 1998 · N852FT · Boeing 747122 · Engine Cowling SystemSDR P5CA9801460Engine · failedAT 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 DSep 18, 1998 · N852FT · Boeing 747122 · Engine (Turbine/Turboprop)SDR P5CA9801528Logic Box · malfunctionFOLLOWING 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.Sep 4, 1998 · N852FT · Boeing 747122 · Landing Gear Position and WarningSDR P5CA9801390Logic Module · malfunctionFOLLOWING 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.Sep 4, 1998 · N852FT · Boeing 747122 · Landing Gear Position and WarningSDR P5CA9801389Frame · crackedFRAME AT BS 960L STR 5 LEFT FOUND CRACKED. REPAIRED PER SRM 53-10-04 FIG 54.Sep 4, 1998 · N852FT · Boeing 747122 · Fuselage Main, FrameSDR P5CA9801386Longeron · crackedOVERWING 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.Sep 4, 1998 · N852FT · Boeing 747122 · Fuselage Main, Longeron/StringerSDR P5CA9801379Deck · corrodedLEVEL 1 CORROSION FOUND ON PRESSURE DECK SKIN BS 1354 BL 113 LEFT. REPAIRED PER REPAIR SCHEME R53-48-33819 AND 8110-03.Sep 4, 1998 · N852FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9801388Web · corrosionLEVEL 1 CORROSION FOUND ON WING GEAR WHEEL WELL BS 1242 TO 1246 WL 155 RIGHT WEB. REPAIRED PER SRM 53-10-01 FIG 1.Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9801387Bulkhead Splice · crackedNUMEROUS 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.Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, BulkheadSDR P5CA9801385Frame · crackedFRAME CHORD AT BS 970 STR 8 AND 9 RIGHT FOUND CRACKS. REPAIRED FRAME PER SRM 53-10-04 FIG 54.Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, FrameSDR P5CA9801383Frame · crackedFRAME 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.Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, FrameSDR P5CA9801382Frame · crackedFRAME AT BS 960 STR 5-6 RIGHT FOUND CRACKED. REPAIRED PER SRM 53-10-04 FIG 54.Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, FrameSDR P5CA9801381Skin · crackedFOUND 65 LONGITUDINAL FASTENER HOLES IN SKIN CRACKED. REAMED OUT HOLES, HFEC, FREEZE PLUGS AND REPAIRED SKIN PER SRM 53-22-72.Sep 3, 1998 · N852FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9801380Longeron · corrodedLEVEL 1 CORROSION FOUND ON LONGERON AT BS 1840 TO 1860 STR 45 LEFT. CORROSION REMOVED PER SRM 53-10-01.Sep 2, 1998 · N852FT · Boeing 747122 · Fuselage Main, Longeron/StringerSDR P5CA9801417Seat Track · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9801415Seat Track · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9801414Seat Track · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9801413Seat Track · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9801412Seat Track · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9801411Seat Track · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9801410Seat Track · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9801409Seat Track · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9801408Intercostal · crackedUPPER DECK BS 380-390 S5R-6R INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-10-01.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9801407Intercostal · crackedUPPER DECK BS 380-390 STR 7R INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-10-01.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9801405Skin · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9801404Skin · corrodedLEVEL 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.Aug 5, 1998 · N852FT · Boeing 747122 · Fuselage Main, Plate/Skin
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