N859FT, cancelled Mar 21, 2013
Service difficulty reports · 261
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 = 'N859FT' AND deregistration_id = 'N859FT-2013-03-21' 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.
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 = 'N859FT' AND deregistration_id = 'N859FT-2013-03-21' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR P5CA0100605Power Supply · dischargedCREW RIGHT UPPER DECK DOOR FRAME MOUNTED EXIT LIGHTS DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. REMOVED AND REPLACED UPPER DECK RT CREW DOOR FRAME LIGHT POWER SUPPLY IAW MM 33-51-04.SDR P5CA0100600Web · crackedNOSE WHEEL WELL - INTERNAL VERTICAL BEAM WEB CRACKED AT INSULATION HOLE - 2 INCHES LONG - FOUND BY H.F.E.C. REPAIRED BY REMOVING CRACKED SECTION. INSTALLED SPLICE & DOUBLER PER BOEING FAX - PAO-LGB-01-00155H & SRM A5310-33-01.SDR P5CAO100599Web · crackedNOSE WHEEL WELL - BS300 INTERNAL VERTICAL BEAM WEB CRACKED BY INSULATION HOLE. FOUND BY H.F.E.C. REPAIRED BY HOLE OPENED UP & DOUBLER INSTALLED PER BOEING FAX - PAO-LGB-01-00155H & SRM A5310-33-01.SDR P5CA0100598Web · crackedNOSEWHEEL WELL - BS320 INTERNAL VERTICAL BEAM WEB WITH 2 INCH LONG CRACK FROM INSULATION HOLE FOUND BY E.F.E.C. REPAIRED WITH DOUBLER INSTALLED WITH "T" ANGLE PER BOEING FAX - PAO-LGB-01-00155H & SRM A5310-33-01.SDR P5CA0100597Web · crackedNOSE WHEEL WELL - BS300 INTERNAL VERTICAL BEAM WEB CRACKED BY INSULATION HOLES. FOUND BY H.F.E.C. (3) CRACKS TOTAL. REPAIRED WITH DOUBLER INSTALLED PER BOEING FAX - PAO-LGB-01-00155H & SRM A5310-33-01.SDR P5CA0100587Warning Light · illuminatedNR 1 OIL PRESSURE FLUCTUATING BETWEEN 40 AND 42 PSI, OIL QTY NORMAL, NO LIGHTS. ON POWER REDUCTION AT TOP OF DESCENT NR 1 OIL PRESSURE LIGHT AND FILTER BYPASS LIGHT CAME ON. ENG SHUTDOWN AS PRECAUTIONARY. OIL TEMP AND QTY STILL NORMAL.SDR P5CA0100586Bypass ValveFILTER BYPASS LIGHT & OIL PRESSURE LIGHT ILLUMINATED (FLICKERING). EXTINGUISHED WHEN #1 THROTTLE RETARDED TO IDLE. RETURNED FOR LANDING. FILTER PYPASS REPLACED IN ORD INITIALLY BY MX. REPLACED PRESSURE VALVE.SDR P5CA0100567WindowRH #1 OUTER PLY SHATTERED. R&R R1 WINDOW PER 56-11-01, INSTALLED R1 WINDOW, LEAK CHECKS GOOD REPLACED HEAT & CONTROLLER P/N ON 617154-5, S/N ON 084C-857, P/N OFF 617154-5, S/N OFF 123C-846.SDR P5CA0000336B-Nut · leakingABNORMALITY FOUND ON NR 4 HYD QTY DROPPED 6 GAL AFTER LANDING GEAR RETRACTION CONTINUED FLIGHT WITH AOP OFF AND EDP IN DEPR. FOUND HYD LEAK FORM PRESS LINE B-NUT ABOVE PYLON LWR BLHD THEN RETIGHTED B-NUT SO LEAK CKED OK WITH MOTORING.SDR P5CA0000198Plug · damagedON PRE-DEPARTURE, NR 1 EXHAUST PLUG SUSTAINED DAMAGE. REMOVED EXHAUST PLUG ASSY, INSPECTED AREA, NO CRACKS NOTED ON FLANGE OR ANY DEFECTS. EXHAUST PLUG ASSY INSTALLED IAW MM 78-11-01-01.SDR P5CA0000099Skin · delaminatedRT WING INBD TRAILING EDGE FORE FLAP BETWEEN 5/6 CANOE ASSY DELAMINATED/MARKED. REPAIRED PER SRM 51-40-15.SDR P5CA0000098Skin · delaminatedRT WING OUTBOARD FORE FLAP ASSY AFT OUTBOARD CORNER LS DELAMINATED. REPAIRED PER SRM 51-40-15.SDR P5CA0000097Skin · delaminatedRT OUTBOARD T/E MID FLAP LWR OUTBOARD END DAMAGE/DELAMINATION MARKED. REPAIRED PER SRM 51-40-09.SDR P5CA0000096Panel · delaminatedUPPER LEADING EDGE FWD SURFACE OF FIBERGLASS PANEL DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA0000095Skin · delaminatedRT WING INBD TE MID FLAP 1 AFT FLAP UPPER SURFACE HAS AREAS OF DELAMINATION. REPAIRED PER SRM 51-40-15.SDR P5CA0000094Skin · delaminatedWING UPPER SURFACE TRAILING EDGE PANEL BETWEEN 4/5 SPOILER VARIOUS AREAS LIGHT DELAMINATION. REPAIRED PER SRM 51-40-15.SDR P5CA0000093Skin · damagedOUTBOARD AILERON UPPER SURFACE ONE OFF LOCATION DAMAGED. REPAIRED PER SRM 51-40-15.SDR P5CA0000092Fairing · errodedNR 4 ENGINE PYLON STRUT TO WING FAIRING EROSION. REPAIRED PER SRM 51-40-09.SDR P5CA9900788Actuator · failedON APPROACH NOSE GEAR DOOR WARNING BOTH PRIMARY AND ALTERNATE. REPLACED NOSE LANDING GEAR DOOR ACTUATOR PER MAINTENANCE MANUAL 32-34-14 PAGE 201.SDR P5CA9900795Muffler · crackedCRACKED APU EXHAUST MUFFLER AT 8 AND 12 O'CLOCK POSITIONS. REPAIRED PER BOEING MAINTENANCE MANUAL 49-21-03.SDR P5CA9900794Door · damagedDAMAGED LEFT BODY LANDING GEAR WHEEL WELL DOOR FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-03.SDR P5CA9900793Actuator · inoperativeINOPERATIVE RIGHT WING LANDING GEAR ALTERNATE EXTENSION MOTOR. REPLACED PER BOEING MAINTENANCE MANUAL 32-35-01.SDR P5CA9900792Skin · crackedCRACK IN FUSELAGE SKIN JUST ABOVE LEFT ELEVATOR BS 2650. REPAIRED PER BOEING SRM 53-30-03.SDR P5CA9900791Actuator · intermittentINTERMITTENT OPERATION OF THE LEFT WING GEAR ALTERNATE EXTENTION ACTUATOR (DURING SCHEDULED OPERATIONAL CHECK). REPLACED ACTUATOR PER BOEING MAINTENANCE MANUAL 32-35-01.SDR P5CA9900790Panel · damagedDAMAGED RIGHT WING TIP HF PANEL COVER. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9900789Skin · delaminatedDELAMINATION RIGHT INBOARD TRAILING EDGE AFT FLAP INBOARD OF NR 6 CANOE AREA. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9900661Skin · delaminationLEFT OUTBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED DELAMINATION PER SRM 51-40-06.SDR P5CA9801376Keel Beam · corrodedLEVEL 1 CORROSION FOUND ON RT WING GEAR WHEEL WELL INBOARD KEEL BEAM UPPER SURFACE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.SDR P5CA9801375Angle · corrodedLEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL OUTBOARD CHORD ANGLE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.SDR P5CA9801374Bracket · corrodedLEVEL 1 CORROSION FOUND ON RT BODY GEAR WW VALVE SUPPORT BRACKET. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.SDR P5CA9801373Beam · corrodedLEVEL 1 CORROSION ON RT BODY GEAR WW OUTBOARD BEAM BS 1352 TO 1353 BL R70-R80. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9801372Bracket · corrodedLEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL WELL BRACKET AT BS 2352L WL 160. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.SDR P5CA9801371Skin · corrodedLEVEL 1 CORROSION FOUND ON LEFT WING UPPER SKIN AT REAR SPAR AREA. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.SDR P5CA9801370Beam · crackedLEFT WING TRAILING EDGE BEAM UPPER CHORD INBOARD END CRACKED. REPAIRED PER SRM 51-40-14 FIG 2.SDR P5CA9801369Stringer · corrodedLEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL WELL OUTBOARD STRINGER BS 1368 TO 1371 STR R33. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9800524Panel · damagedRT WING TOP L/E FIXED PANEL INBD OF PYLON PREVIOUS REPAIR PEELING OFF. REMOVED PREVIOUS REPAIR, REPAIRED PER SRM 51-40-15.SDR P5CA9800523Stanchion · damagedFWD CARGO COMPARTMENT STA 480 PLUG SUPPORT CHANNEL DAMAGED. REMOVED AND REPLACED BOTH RT SIDE STANCHIONS AT STA 480 PER SRM 51-30-02 AND 51-10-01.SDR P5CA9800522Panel · crackedNR 1 ENGINE INLET 3 INCH CRACK AT 3 O'CLOCK POSITION ON ACCOUSTIC PANEL. REPAIRED CRACK BY CUTTING IT OUT AND APPLYING POTTING COMPOUND PER SRM 54-31-03.SDR P5CA9800521Skin · delaminatedRT WING MLG LOWER FLYING DOOR IS DELAMINATED. REMOVED DAMAGE, APPLIED FIBERGLASS AND BONDING PER SRM 51-40-06.SDR P5CA9800520Bumper Pad · crackedLT WING GEAR BOGIE BEAM TILT BUMPER CRACKED AND DAMAGED. REMOVED AND REPLACED BUMPER PAD PER SRM 51-10-01.SDR P5CA9800519Skin · tornFWD CARGO DOOR TORN IN UPPER RT CORNER AT PREVIOUS REPAIR. INSTALLED DOUBLER ON FWD RT CORNER OF DOOR PER SRM 51-30-02.SDR P5CA9800518Fastener · missingRT HORIZ STAB NAV LIGHT FIXED WITH SEALANT FASTENERS MISSING. INSTALLED FASTENERS PER SRM 51-30-02.SDR P5CA9800517Sill · corrosionLEVEL 1 CORROSION FOUND ON FWD LOWER CARGO SERRATED PLATE ON DOOR SILL NR 5, 6 AND7 BOTTOM AFT HOLE NR 8 HAS CORROSION. REMOVED CORROSION FROM PLATE PER SRM 51-10-01.SDR P5CA9800504Overheat Light · illuminatedON CLIMBOUT, RT WING OVERHEAT LIGHT CAME ON. APPLIED CHECKLIST AND RETURNED TO JFK. INSPECTED LEADING EDGE DUCT AREA FOR LEAKS AND FAULTY WIRE CONNECTIONS. FOUND LEADING EDGE DUCT BLANKET TORN AND SHORTING WIRES. REPAIRED WIRE AND REPLACED BLANKET, OPERATISDR P5CA9800027Sequence Valve · crackedON MAINTENANCE WALK AROUND, FOUND NOSE LANDING GEAR OPEN DOOR SEQUENCE VALVE ASSEMBLY LEAKING. VALVE FOUND TO BE CRACKED. REMOVED AND REPLACED NOSE GEAR, OPERATED DOOR SEQUENCE VALVE IAW BOEING M/M 32-34-07, LEAK AND OPERATIONAL CHECK OK.SDR P5CA9701842Skin · tornTEAR AND DELAMINATION AT INBOARD AFT CORNER LEFT OUTBOARD ELEVATOR. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9701844Clamp · brokenUPPER ATTACH CLAMP ON PORTABLE OXYGEN BOTTLE IN COCKPIT BROKEN. REPLACED BRACKET ASSEMBLY PER BOEING MAINTENANCE MANUAL 35-31-00.SDR P5CA9701843Panel · delaminatedFIBERGLASS SURFACE RIPPING AWAY FROM RIGHT WING UPPER SURFACE LEADING EDGE PANEL. REPAIRED PER BOEING SRM 51-40-12.SDR P5CA9701826Line · brokenON GEAR EXTENSION AND FLAP EXTENSION LOST ALL HYDRAULIC SYSTEM 1 PRESSURE. FOUND AIR DRIVEN HYDRAULIC PUMP PRESSURE FLEX LINE BROKEN. REPLACED LINE PER BOEING M/M 29-11-17.SDR P5CA9701615Park Brake Valve · stickingANTI-SKID LIGHT ON AT START OF TAKEOFF ROLL, LIGHT REMAINED ON STEADY. PARKING BRAKE VALVE OPERATION CHECKED AT MODULE, RIGHT BODY GEAR BAY OPERATIONAL CHECK SATISFACTORY. ELECTRICAL PLUG REMOVED AND CLEANED, 10 CYCLES OF PARKING BRAKE CARRIED OUT, ALL SATIS
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