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 engine_model_key = 'CF650C2' 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 engine_model_key = 'CF650C2' 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 96UAL900880Control Cable · brokenON FLIGHT CHECK DURING TAXI OUT, LEFT HAND SPOILER INDICATED ONLY PARTIAL EXTENSION. *S/D* FOUND SPOILER CABLE 11B, LT SPOILER 1, 4 AND 5 UP BROKEN. REPLACED CABLE.SDR 96UAL900884Warning Syst · inoperativeCENTER CARGO DOOR A-LOOP INDICATING SYSTEM INOPERATIVE. *S/D* CYCLED DOOR SEVERAL TIMES AND COULD NOT DUPLICATE.SDR 96UAL900886Coalescer Bags · dirtyVERY STRONG ODOR IN CABIN AFTER TAKEOFF WITH PNEUMATIC AND RECIRCULATION FANS ON. REPLACED COALESCER BAGS, ACCOMPLISHED ENGINE RUN AND THERE WAS NO SMELL.SDR SCNA96378Engine · failedDURING CLIMB, EXPERIENCED EXTREME VIBRATION AND NUMBER 3 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. RETARDED NUMBER 3 ENGINE THROTTLES AND LIGHT EXTINGUISHED. AFTER SEVERAL MINUTES, OIL PRESSURE DROPPED RAPIDLY, ENGINE FIRE LIGHT ILLUMINATED AND SMOKE ENTERSDR 96UAL900845Light · inoperativeEMERGENCY EXIT LIGHTING TEST FAILED. FORWARD SECTION AT FAULT. FOUND FORWARD SECTION LIGHT ASSEMBLY INOPERATIVE AND BROKEN CABLE NEAR LIGHT CONNECTION. REPLACED LIGHT ASSEMBLY AND REPAIRED CABLE.SDR CA961104003Engine · fire(CAN) TAKE-OFF ABORTED AT 60 KNOTS. TOWER ADVISED FLAMES COMING FROM TAIL PIPE OF NR 1 ENGINE. FIRE EXTINGUISHER BOTTLES ACTIONED. MAINTENANCE INVESTIGATION REVEALED METAL IN TAILPIPE. BORESCOPE CHECK CONFIRMED ENGINE FAILURE.SDR CA961025005Steering Collar · cracked(CAN) NOSE WHEEL LANDING GEAR STEERING COLLAR FOUND CRACKED AT RH STEERING CYLINDER UPPER ATTACHMENT LUG. COLLAR REPLACED.SDR CALA9601504Fuel So Vlv · out of rigTHE NR 2 ENG SPOOLED DOWN TO IDLE RPM SHORTLY AFTER TAKEOFF. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED. MAINTENANCE FOUND THE NR 2 ENG FUEL PUMP HAD FAILED. THE NR 2 ENG FUEL PUMP WAS REMOVED AND REPLACED. IN ADDITION, THE FUEL/OIL HEAT EXCHANGER AND ESDR 96UAL900829Tq Link Bushing · brokenSLIGHT NOSE WHEEL SHIMMY ON ROLLOUT DURING LANDING. *S/D* REPLACED LOWER NOSE GEAR TORQUE LINK DUE TO BROKEN BUSHING AT DISCONNECT.SDR 96UAL900814Bulkhead · failedDURING TIME CONTROLLED OVERHAUL, RAMP PORTION OF SLIDE SUFFERED INTERNAL BULKHEAD FAILURE. ALSO, LT RAMP RAIL, LOWER END SUFFERED INTERNAL BULKHEAD FAILURE. SCRAPPED RAMP PORTION OF SLIDE.SDR 96UAL900770Press Ind · inoperativeNR 2 L-DOOR SLIDE TEST INOPERATIVE. REMOTE PRESSURE INDICATOR FOUND TO BE INOPERATIVE. REPLACED INDICATOR.SDR WRLA96041Fuel Filter · cloggedDURING TAXIING OUT, FLIGHT CREW NOTED NR 2 ENGINE FUEL FILTER PRESSURE DROP LIGHT ON, AIRCRAFT RETURNED TO GATE. MAINTENANCE PERSONNEL REPLACED FUEL FILTER, GROUND RUN THE AIRCRAFT, NO FAULT NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR 96UAL900735Fire Loop · no testNR 3 ENGINE A FIRE DETECTION LOOP NO TEST.SDR 96UAL900736B-Fire Loop · no testNR 3 ENGINE B-LOOP NO TEST.SDR 96UAL900680Strip · defectiveDEFECTIVE EEL STRIP AT LAVATORY 2 RIGHT. *S/D* REPAIRED EEL STRIP, OPERATION NORMAL.SDR CA960826013Atach Bolt · sheared(CAN) MAIN LANDING GEAR RETRACT ACTUATOR SUPPORT FITTING ATTACHMENT BOLTS SHEARED AND ACTUATOR FELL OVER AND DOWN WHEN GEAR WAS EXTENDED. FREE FALL EXTENSION INITIATED, NO PROBLEMS. MAINTENANCE CHECK REVEALED ACTUATOR SUPPORT FITTING BOLTS SHEARED. BOLTS, NUTSSDR 96UAL900626Skin · corrodedTHE FUSELAGE SKIN AT BODY STATION 1133 HAD EXCESSIVE MATERIAL LOSS DUE TO CORROSION IN THE AREA OF STRINGER 46L. APPROXIMATELY 50 PERCENT OF THE ORIGINAL SKIN THICKNESS WAS REMOVED OVER A 2.5 DIAMETER AREA. THE DAMAGE WAS DETECTABLE FROM THE OUTSIDE OF THE ASDR 96UAL900629Fuel Quantity · droppedRETURNED TO SFO DUE TO A SIGNIFICANT DROP IN FUEL QUANTITY.SDR 96UAL900610Cable Pin · brokenEEL LIGHTS INOPERATIVE IN B-ZONE LEFT SIDE STRIP. FOUND CABLE PIN BROKEN. REPLACED CABLE.SDR CA960826101Door · departed(CAN) ON DEPARTURE, LOWER TAIL CONE ACCESS DOOR AT STA 2184 SEPARATED FROM TAIL CONE OF AIRCRAFT. AS THE DOOR OPENED INTO THE SLIP STRESAM WIND, THE HINGE POINTS WERE TORN FROM THE STRUCTURE. THE SEPARATED DOOR STRUCK THE UNDERSIDE OF THE TAIL CONE RESULTING SDR 9617031229Fuel Filter · cloggedDURING TAKEOFF ROLLOUT, THE NR 1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE FUEL FILTER AND FOUND SLIGHTLY CLOGGED. REPLACED THE NR 1 FUEL FILTER AND PERFORMED ENGINESDR AU961147Seal · damaged(AUS) GREEN HYDRAULIC SYSTEM UNION SEAL LEAKING - SEAL WAS LOCATED AT RH KRUGER FLAP RETURN LINE UNION - LOSS OF HYDRAULIC FLUIDSDR CA960808107Shear Pin · sheared(CAN) DURING DESCENT, AIRSPEED DECREASED TO 280 KNOTS, AUTO PILOT OUT OF TRIM LIGHT ILLUMINATED. AIRCRAFT LEVELED OUT AT 11,000 FEET AND AIRSPEED REDUCED TO 250 KNOTS, LIGHT REMAINED ON. AUTO PILOT #1 DISENGAGED AND AIRCRAFT NOTICEABLY NOSE HEAVY. ALL TRIMS TRSDR AU961024Torque Tube · sheared(AUS) LH FLAP TORQUE TUBE SHEARED IN AREA OF ATTACHMENT TO LH SHOCK ABSORBERSDR 96UAL900542Jumper Chord · failedEEL LIGHTING INOPERATIVE ON RT SIDE FROM FORWARD GALLEY THROUGH B-SECTION OF COACH. REPLACED JUMPER CHORD FOR RIGHT HAND SECTION B.SDR 96UAL900528Wire · looseEEL LEFT SIDE FIRST CLASS AT FWD END PULLED LOOSE AND PIN BROKEN. *S/D* REPLACED EEL POWER FEEDER STRIP AT DOOR ONE LEFT.SDR CALA9600959Duct · separatedTHE 1 ENGINE FIRE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS. THE ENGINE FAIL/FIRE CHECKLIST WAS ACCOMPLISHED. THE FIRE LIGHT WENT OUT APPROXIMATELY 10 SECONDS AFTER RETARDING THE NR 1 THROTTLE. THE NR 1 ENGINE B-LOOP LIGHT WAS STISDR 96UAL900482Connector · looseEEL FLOOR LIGHTING INOPERATIVE AT ROWS 9 TO 16. *S/D* SECURED EEL LIGHT CONNECTION AFT OF 2R LAVATORY.SDR 96UAL900449Slide · failedDURING SHOP OVERHAUL OF SLIDE/RAFT FROM DOOR 3L, REMOVED FOR OVERHAUL TIME EXPIRATION, RAMP PORTION OF SLIDE EXPERIENCED INTERNAL BULKHEAD SEPARATION DURING INFLATION. SUPPLEMENTAL DATA UPDATE: SUBMITTER STATES CAUSE UNDETERMINED. SCRAPPED RAMP.SDR AU960877Slide · faulty(AUS) DOOR 3R SLIDE FAILED TO DROP OUT OF CONTAINERSDR CALA9600646Y-Duct · rupturedTHE NR 3 ENGINE FIRE WARNING ACTIVATED MOMENTARILY WHILE EN ROUTE. THE FIRE WARNING SYSTEM OF ALL ENGINES WAS TESTED AND ALL SYSTEMS CHECKED GOOD. THE FLIGHT WAS CONTINUED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 8TH STAGE SDR 96UAL900313Slide Raft · damagedDOOR 3 LEFT OFFWING SLIDE/RAFT REMOVED FOR TIME LIMIT. SHOP FOUND RAMP PORTION OF SLIDE DAMAGED DUE TO SEPARATION OF THE INTERNAL BULKHEADS. SCRAPPED RAMP PORTION OF SLIDE/RAFT.SDR WRLA96021Compressor · stalledDURING TAKEOFF AT ROTATION, FLIGHT CREW EXPERIENCED COMPRESSOR STALL ON NR 2 ENGINE. FLIGHT ENGINEER NOTED A 6 PERCENT DROP IN N-1 SPEED. DURING INITIAL CLIMB-OUT, CREW NOTED SECOND COMPRESSOR STALL. AIRCRAFT RETURNED TO POINT OF DEPARTURE, LANDING WITHOUT SDR 96UAL900287Reverser Cowl · delaminatedLARGE AREA OF HEAT AND DELAMINATION DAMAGE ON THE NR 2 ENGINE RIGHT REVERSER COWL. THERE IS ALSO INSULATION DAMAGE. THERE WAS NO FIRE WARNING INDICATION ON THE FLIGHT DECK. UNDER INVESTIGATION. SUPPLEMENTAL DATA UPDATE: DAMAGE CAUSED BY NR 2 PNEUMATIC DUCSDR 9609101229Engine · failedDURING TAXI TO RAMP, THE NR 3 ENGINE WAS SHUTDOWN DUE TO FUEL LEAKING OUT OF FRONT OF COMPRESSOR. REPLACED NR 3 ENGINE AFTER REPLACING THE FUEL/OIL EXCHANGER AND INDUCTOR VALVE. CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE.SDR 96UAL900257Skin · corrodedWHEN REMOVING NR 2 ADF ANTENNA FOUND CORROSION ON FUSELAGE MOUNTING SURFACE STATION 1069 AT LONGERON L52. REMOVED AFFECTED SKIN SECTION AND PERFORMED EXTERNAL DOUBLER/TRIPLER REPAIR.SDR CA960515101Smoke Detector · alarm activated(CAN)TAKEOFF REJECTED AFTER SMOKE DETECTOR SOUNDED IN LAV. E. SMOKE DETECTOR RESET. THERE WERE NO FURTHER INDICATIONS. BRAKE TEMP PEAKED AT 400 DEGREES "C". INVESTIGATION REVEALED ALARM ACTIVATED DUE TO PASSENGER SMOKING IN ADJACENT LAV. SMOKE DETECTORS OF LAVSDR CA960514101Control Cable · broken(CAN)WHILE CYCLING AILERON CONTROLS FOR INVESTIGATION OF A HYDRAULIC LEAK, THE CAPTAINS CONTROL WHEEL WOULD NOT RETURN TO THE CENTRE POSITION. FURTHER INVESTIGATION REVEALED THE AILERON DOWN CABLE RUN #7 BROKE INSIDE THE CONTROL COLUMN. AL SO THE AILERON "UPSDR 96UAL900210Spar Web · crackedNR 3 PYLON UPPER SPAR WEB HAD A CRACK INDICATION IN A FASTENER HOLE COMMON TO THE SPAR CHORD. REPAIRED PER DC-10 SRM 54-20-00 FIGURE 27.SDR 96UAL900197Battery Pack · dischargedEMERGENCY LIGHT BATTERY TEST FAILED. AFT POWER SUPPLY LIGHT ILLUMINATED BELOW SECOND OFFICER'S DESK. REPLACED BATTERY PACK AND POWER SUPPLY.SDR 96UAL900193Apu · malfunctionedPUNGENT ODOR OF SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. ODOR ISOLATED TO NR 2 PNEUMATICS WHEN USING APU BLEED. REPLACED APU.SDR 96UAL900144Spar Web · crackedDURING ENGINE CHANGE THE NR 3 PYLON CENTER SPAR WEB WAS FOUND TO BE CRACKED. THE CRACK IS AT STATION 416 AND PROPAGATES 2 INCHES FROM LIGHTENING HOLE TO EDGE OF WEB. A PERMANENT REPAIR WAS MADE PER DC-10-30 STRUCTURAL REPAIR MANUAL.SDR 96UAL900104Battery Pack · dischargedAFT EMERGENCY LIGHT FAILED BATTERY TEST. REPLACED AFT EMERGENCY LIGHT BATTERY (P/N EMSE299A).SDR CA960208101Apu · smoking(CAN)PRIOR TO DEPARTURE, APU AUTO SHUT DOWN, EMITTING CLOUDS OF SMOKE. APU WAS MEL'D AND AIRCRAFT DEPARTED. ON CLIMB, CABIN AIR CONDITIONING SYSTEM DISCHARGED OIL VAPOURS. AIRCRAFT RETURNED TO BLOCKS AND C OMPLETED AN OVERWEIGHT LANDING. OVERWEIGHT LANDING CHESDR 95UAL900328Ac Power Syst · malfunctionedDURING INITIAL CLIMB AC BUS NR 3 AND ASSOCIATED LIGHTS RT EMERGENCY, AC AND RT EMERGENCY DC BUS LIGHTS CAME ON. COULD NOT RESTORE THE RT EMERGENCY BUS. FLIGHT RETURNED TO ORD. REPLACED THE GENERATOR CONTROL UNIT AND THE BUS POWER CONTROL AND RECONNECTED THESDR 95UAL900293Pneu Manifold · fail indicationNR 2 MANIFOLD INDICATION FAILURE. THE TRIP WAS CANCELED.SDR 95UAL900241Skin · crackedSHEET METAL CRACKED AROUND RIVET, LEFT SIDE OF FUSELAGE, FORWARD OF OUTFLOW VALVE ALONG CIRCULAR FRAME LINE. THE SKIN CRACKING WAS ACTUALLY SKIN CORROSION DAMAGE COMMON TO FRAME LOCATIONS AND WAS REPAIRED PER SRM 53-20-00 FIGURE 6 SHEET 13 CLASS III REPAIR. SDR 95UAL900175Fitting · crackedNR 3 ENGINE PYLON FWD MOUNT TRUSS FITTING ASSY, PRIOR TO FURTHER FLIGHT, REPLACE AT LEAST ONE TRUSS FITTING ACCT RT FITTING PREVIOUSLY CRACKED AND REPAIRED. LT FITTING CRACKED AT HORIZ FLANGE INBD BOLT HOLE.SDR 95UAL900163Fillet · missingON ARRIVAL AT NRT, FOUND LEFT SLAT NR 1 DAMAGED AND FILLET MISSING. REPLACED FILLET. INSPECTED AREA AND REPAIRED MINOR DAMAGE TO SLAT. RELEASED COAT 3-8065 TO PERFORM A ONE TIME FLEET INSPECTION OF SLAT FILLET ATTACHMENTS.SDR 95UAL900149Eel Battery Pack · dischargedOVERWING EMERGENCY LIGHTS FAILED TEST. REPLACED BATTERY PACK.
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