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 = 'CT79B' 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 = 'CT79B' 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 CA021118012Smoke Detector · failed(CAN) CARGO BAY FIRE WARNING ON TAKEOFF. TAKEOFF ABORTED. FALSE WARNING.DETECTOR REMOVED S/N 663. INSTALLED 19/06/01. TIS 3339.4 HOURS. THE INSTALLATION OF THESE SMOKE DETECTORS WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY.CONSULTATION WITH SAAB REVSDR CA021118013Smoke Detector · failed(CAN) CARGO BAY SMOKE DETECTOR FAILED TO TEST AFTER RECTIFICATION OF ABOVE INCIDENT. MAINTENANCE. DETECTOR REMOVED S/N 662. INSTALLED 19/06/01. TIS 3339.4 HOURS. THE INSTALLATION OF THESE SMOKE DETECTORS WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY.SDR CA021118010Smoke Detector · failed(CAN) CARGO BAY SMOKE DETECTOR FALSE WARNING. MAINTENANCE.DETECTOR REMOVED S/.N 337. INSTALLED 19/06/01. TIS 2531.5 HOURS.THE INSTALLATION OF THESE SMOKE DETECTORS WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY.CONSULTATION WITH SAAB REVEALED 12 CONFISDR MALA020621Gearbox · damagedON FLIGHT NR 2972, HAD AN INFLIGHT SHUTDOWN EVENT. CREW SHUTDOWN RT ENGINE, DECLARED AN EMERGENCY, DID AN AIR TURNBACK AND LANDED IN MSP WITHOUT INCIDENT. MAINTENANCE REMOVED COWLS, FOUND HOLE IN REAR PGB CASE AT APPROXIMATELY THE 4:30 POSITION, AFT LOOKING SDR SIMA200229501Control Valve · malfunctionedDURING APPROACH, LANDING GEAR FAILED TO EXTEND WHEN SELECTED DOWN. RECYCLED GEAR HANDLE WITHOUT SUCCESS. ATTEMPTED MANUAL EXTENSION WITHOUT SUCCESS. ACTUATED EMERGENCY EXTENSION/GEAR FREEFALL, NOSE AND LT MAIN GEAR EXTENDED AND LOCKED, RIGHT MAIN GEAR EXTESDR MALA020608Anti-Ice Valve · failedDURING CLIMB-OUT ON FLIGHT NR 3251, RT AIR VALVE LIGHT ILLUMINATED SEVERAL TIMES. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RT ANTI-ICE VALVE PER GE MM 75-00-00, OPS CHECK GOOD.SDR NSV2002F00001Power Supply · inoperativeEMERGENCY LIGHTING, INOPERATIVE, FOUND PRIOR TO FIRST FLIGHT OF THE DAY. MAINTENANCE REMOVED AND REPLACED ALL POWER SUPPLIES. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RELEASED FOR SERVICE. SUSPECT LIGHTS WERE INADVERTENTLY LEFT ON AFTER POWER WAS REMOVED.SDR SIMA200228703Fire Detector · malfunctionedDURING TAKE OFF CREW REPORTED THE CARGO SMOKE WARNING CAME ON. CREW ELECTED TO ABORT TAKE OFF AND BLOW THE NUMBER ONE FIRE BOTTLE. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. MEL WAS ISSUED AND AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200228702Control Valve · malfunctionedCREW REPORTED UNCOMMANDED PITCH CHANGES IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL VALVE AND FLAP CONTROL VALVE AND FLAP CONTROL BOX IAW MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200228203Smoke Detector · dirtyCREW REPORTED THE LAVATORY SMOKE DETECTOR LIGHT CAME ON DURING DESCENT. CREW REPORTED NO SMOKE. MAINTENANCE CLEANED THE LAVATORY SMOKE DETECTOR OF DUST. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.SDR MALA020600Ecu · malfunctionedDURING FLIGHT NR 3158, LEFT ENGINE TORQUE SURGE INFLIGHT FOR 2-3 SECONDS. AN UNCOMMANDED POWER INCREASE ON LEFT ENGINE WITH ENGINE ICE OFF DESCENT CHECK COMPLETE POWER SET AT 80-85 PERCENT. INCREASED TO 120 PERCENT FOR 2-3 SECONDS, THEN RETURNED TO SET PWR TESDR SIMA200228202Indicator · malfunctionedCREW REPORTED TO OPERATIONS THAT THEY SMELLED A STRONG ELECTRICAL SMOKE SMELL WITH THE AVIONICS FAN ON. MAINTENANCE REMOVED AND REPLACED THE STANDBY ADI IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200228201Engine · malfunctionedDURING CLIMB CREW REPORTED LEFT ENGINE OIL PRESSURE FLUCTUATION WITH MASTER WARNING. CREW FOLLOWED NORMAL SHUTDOWN PROCEDURES AND DECLARED AN EMERGENCY. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW AE WSDR UHL2002F00004Connector · wornTAIL PIPE, HOT LIGHT ILLUMINATED AT 6300 FEET. SHUT DOWN NR 2 ENGINE, DISCHARGED NR1 AND NR2 FIRE BOTTLE, RETURNED TO AIRPORT, LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRING AT EXHAUST COWLING CONNECTORS. NO EVIDENCE OF FIRE NOTED.SDR UHLA66511Connector · looseAFTER DEPARTURE, RT ITT GAUGE FLUCTUATED 25 DEGREES, POWER REDUCED, FLUCTUATION WAS AT 5-10 DEGREE SWING. RETURNED TO FIELD. FOUND LOOSE CONNECTION AT ECU RESECURED, RAN ENGINE AT VARIOUS SETTINGS, OPS NORMAL.SDR CX7A194J16O-Ring · cutENGINE OIL PRESSURE (RT) CWP LIGHT ILLUMINATED INNTERMITTENTLY IN FLIGHT. RT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 25 PSI-60 PSI. REPLACED O-RING ON OIL BYPASS SENSOR IAW GE MM.SDR AUS20020883Engine · failed(AUS) LT ENGINE FAILURE. LIMITED INFORMATION PROVIDED.SDR CX7A194J15Engine · seizedAFTER ROTATION LT ENGINE OIL PRESSURE CWP- OIL PRESSURE GAUGE READ 0 PSI WHILE RUNNING ENGINE OIL PRESSURE CHECKLIST (TWO MINUTES MAX) ENGINE FAILED. RAN MEMORY ITEM AND CHECKLIST RETURNED FOR LANDING. REMOVED AND REPLACED LT ENGINE IAW GE AND SAAB AMM.SDR CX7A194J13Engine · stoppedDuring T/O roll, Tq was 94% on both engines, ITT below 890 degrees. After rotation at 80-100 feet, a bang and shudder was felt and ITT on the right engine ran away to max. Tq reduced to zero, prop autocoarsened. Engine had failed. Emergency declared.Mx R/RSDR MALA020438Engine · power lossDURING FLIGHT 3392, EXPERIENCED ROLLBACK AT 21,000 FT. -11 DEGREES CELSIUS, 59 PERCENT TORQUE. IN ICING CONDITIONS NO SHIFT IN ITT OR TORQUE WAS NOTICED. IGNITION LIGHT DID NOT ILLUMINATE. CREW COULD NOT DETERMINE WHICH ENGINE HAS THE ROLLBACK BUT BELIEVE ISDR CX7A194J12HmuDuring climbout of MDW noticed that L/H engine torque was fluctuating 3%. Fluctuations then went to 5% swings. Ran checklist and put in T/M lockout. With T/M lockout engine still fluxed +/- 3% with prop sync on and off.R/R L/H engine HMU IAW SAAB AMMSDR MALA020403Control Unit · failedDURING FLIGHT 3395, LT PROP RPM INDICATION WENT TO ZERO. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED DECU, ALSO REPLACED YELLOW HARNESS. ALL CHECKS GOOD AT THIS TIME.SDR MALA020354Engine · malfunctionedDURING CLIMBOUT ON FLIGHT 2935, RT TORQUE AND RT ITT GAUGE FLICKERING, ABOUT 4-5 PERCENT. ALL OTHER ENGINE AND PROP INDICATIONS WERE NORMAL. AIR RETURN TO MEM. MAINTENANCE CHECKED FOR SHORTS BETWEEN PINS 16,17 & 18 OF DECU, CLEANED CONNECTOR PLUG. NO DEFECTSSDR MALA020353Engine · malfunctionedDURING APPROACH OF FLIGHT 3326, RH ENGINE POWER SURGE. UNCOMMANDED TORQUE POWER SURGES OF 15 PERCENT ON RT ENGINE DURING CRUISE FLIGHT AT 60 PERCENT TORQUE. THIS WAS AN ACTUAL POWER SURGE WITH AN ASSOCIATED YAW. AC LANDED WITHOUT INCIDENT. MAINTENANCE REMOVSDR MALA020351Wire Harness · faultyDURING FLIGHT 3320, HAD A UNCOMMANDED AUTO COARSEN EVENT. EVENT OCCURRED DURING APPROACH TO CRW, AT 1,000 FT AGL. RT ENGINE AUTO COARSEN, ENGINE CONTINUED TO RUN, LANDED NORMALLY. MAINTENANCE BORESCOPED RT ENGINE, NO DEFECTS NOTED. REMOVED AND REPLACED RT SDR AUS20020479Engine · failed(AUS) RT ENGINE LOST OIL ON STARTUP. OIL CONTAMINATION OF TURBINE BLADES. LIMITED INFORMATION PROVIDED.SDR AUS20020470Smoke Detector · faulty(AUS) AVIONICS SMOKE DETECTION SYSTEM OPERATED. NO SIGN OF SMOKE COULD BE FOUND. SYSTEM COULD NOT BE FAULTED AND IT IS SUSPECTED THAT DUST IN THE AVIONICS BAY MAY HAVE ACTIVATED THE DETECTORS.SDR SIMA200214401Engine · malfunctionedCLE - FLT 4836 - DISC - AT CRUISE ALTITUDE OF FL 190', LEFT ENGINE OIL PRESSURE FLUCTUATED 15 TO 20 PSI. OIL PRESSURE DROPPED APPROX 40 PSI FOR AN UNKNOWN DURATION. CREW SHUT DOWN ENGINE AND DECLARED EMERGENCY AND DIVERTED INTO PIT. REMOVED AND REPLACED LEFSDR SIMA200213816Engine · failedCREW REPORTED AT 500-600 FT JUST AFTER CTOT ROTATION, 60-70 PERCENT ON CTOT, AND 80-85 TORQUE, THE NUMBER 2 ENGINE FAILED. C/A MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IAW WORK CARD 4903. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RESDR MALA020288Bulb · faultyDURING FLIGHT 2945, LT PGB OIL TEMP FLUCTUATES. AIR RETURN TO DTW. MAINTENANCE REPLACED TEMP BULBS. MAINTENANCE INSPECTED ELECTRICAL CONNECTORS AT LT PROP OIL TEMP GAUGE AND AT TEMP BULB. NO DISCREPANCIES NOTED. MAINTENANCE REMOVED AND REPLACED LT PGB TEMSDR MALA020276Bleed Valve · malfunctionedDURING FLIGHT 2789, LT AIR VALVE LIGHT ILLUMINATED IN ICING CONDITIONS. LT AIR VALVE LIGHT CAME ON AT 16,000 FT MSL FOLLOWED QRH AND RESET SWITCH. LIGHT STAYED ON OPERATED LEFT ENGINE BELOW 86 PERCENT NG UNTIL CLEAR OF ICING CONDITIONS AS PER QRH. AIR RETURSDR AUS20020442Engine · leaking(AUS) LT ENGINE LEAKING OIL FROM AREA OF THE B' SUMP.SDR MALA020263Gearbox · failedON APPROACH OF FLIGHT 2753 RT ENGINE FLAMED OUT. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. WEATHER CLEAR. THE ENGINE DID NOT FLAME OUT BUT WAS OPERATING NORMALLY. A/C DID HAVE AN UNCOMMANDED AUTO COARSEN EVENT. THE DATA INDICATES IT WAS NOT CAUSED BY TSDR AUS20020373Wheel · fractured(AUS) DURING A TURN-A-ROUND INSPECTION, THE PILOT DISCOVERED A 7.8IN(20CM) BEAD SECTION MISSING FROM THE NR 3 MAIN WHEEL AND THE TIRE WAS DEFLATED.SDR AUS20020354Circuit Breaker · faulty(AUS) CARGO/LAVATORY CIRCUIT BREAKER SUSPECT FAULTY.SDR MALA020241Seal · defectiveDURING FLIGHT 2775 LT ENGINE OIL PRESSURE FLUCTUATION ALONG WITH CWP LIGHT CAME ON INFLIGHT. LT PROP OR PSI AND TEMP WERE OK. NO SIGNS OF OIL LEAKS NOTED FROM CABIN WINDOW. ENGINE SHUTDOWN IN FLIGHT. QRH COMPLETE. MAINTENANCE PERFORMED ALL PROPER MAINT PRSDR MALA020235Engine · malfunctionedDURING FLIGHT 3247 FROM MQT, LT ENGINE SHUTDOWN AFTER TAKEOFF. AIR RETURN TO MQT. MAINTENANCE WENT UP TO REMOVE AND SEND DFDR FOR DOWNLOAD. REMOVED AND REPLACED LT ENGINE. OPS AND LEAK CHECK GOOD.SDR MALA020228Weu · malfunctionedON DESCENT INTO MSP, RT ENGINE FIRE ILLUMINATED WITH FIRE BELL FOR 1-2 SECONDS. NO MASTER CAUTION OR T-HANDLE LIGHT. MAINTENANCE PERFORMED OPS CHECK OF FIRE DETECTION SYSTEM IAW AMM 25-1-00-2 PARA 2A, OPS CHECK GOOD. PERFORMED VIS INSPECTION OF RT NACELLE FSDR MALA020193Engine · erraticDURING FLIGHT 2900, LT ENGINE AND TEMP SPIKES. LT ENGINE SHOWED ERRATIC INDICATIONS IN CRUISE. FLIGHT BROUGHT PL TO FLIGHT IDLE AND INDICATIONS AND AND NOISES STOPPED. A/C DIVERTED INTO FWA. MAINTENANCE BORESCOPED LT ENGINE AND THOROUGHLY INSPECTED ENGINE.SDR NSVA0208Linkage · disconnectedORF - DURING TAKEOFF ROLL, LEFT PROP DROPPED TO 400 RPM AND TORQUE DROPPED 200. TAKEOFF WAS ABORTED AFTER ROLL BACK OF ENGINE POWER WAS EVIDENT. FOUND VG ACTUATOR/START BLEED VALVE LINKAGE DISCONNECTED. GE REP WAS CONTACTED AND A BORESCOPE OF THE ENGINE WASSDR MALA020181Control Unit · malfunctionedREPORTED SMOKE FROM RT AIRCRAFT VENTS IN CABIN ON ENGINE START. MAINTENANCE BORESCOPED POWER UNIT, FOUND NO EVIDENCE OF OVERTEMP OR OTHER DEFECTS. REMOVED DECU IAW GE MM 71-00-00. OPS & LEAK CHECK GOOD.SDR MALA020197Control Unit · malfunctionedWHEN STARTING RT ENGINE, AFTER STARTER CUT OUT, NG AND ITT KEPT ACCELERATING. WHEN NG REACHES 85 PERCENT WHITE SMOKE APPREARS FROM VENTILATION SYSTEM. SMOKE IS FAIRLY DENSE WITH NO ODOR. MAINTENANCE BORESCOPED POWER UNIT, FOUND NO EVIDENCE OF OVERTEMP OR OTSDR MALA020179Chip Detector · dirtyAFTER STARTING LT ENGINE CHIP DETECTOR LIGHT CAME ON. REMOVED AND CLEANED CHIP DETECTOR. NO CHIPS FOUND, RAN ENGINE NO DISCREPANCIES FOUND.SDR CX7A194JWarning Light · false indicationRT TAIL PIPE HOT LIGHT ON T/O. NO TAIL WIND, ABORTED, REDUCED POWER, LIGHT WENT OUT. RAIN AND MOISTURE PREVAILED IN THE AREA.SDR AUS20020068Control Cable · broken(AUS) LT ENGINE POWER CONTROL CABLE BROKEN.SDR SIMA200201001Engine · malfunctionedDFW - FLT 3826 - ON DESCENT, LEFT ENGINE TQ WENT TO MAX, GOT OVERTEMP LIGHT. CREW SHUT LEFT ENGINE DOWN. (M)SDR AUS20020310Channel · cracked(AUS) RH ENGINE NACELLE CHANNEL CRACKED UNDER DOUBLER AT STN NS 240.SDR AUS20011363Bolt · sheared(AUS) NOSE LANDING GEAR STRUT LT TRUNNION PIN RETENTION BOLT SHEARED IN AREA JUST BELOW THE THREADED PORTION.SDR CA011221002Engine · malfunctioned(CAN) ON TAKE OFF ACCELERATING THROUGH 60 KTS TME A/C YAWED TO PORT AND THE PORT ENGINE TORQUE WAS SEEN TO DROP. THE ENGINE WAS SHUT DOWN AND THE TAKE OFF ABORTED. AT PRESENT THE INCIDENT IS SUBJECT TO A FULL ENGINEERING INVESTIGATION. FURTHER DETAILS WILLSDR AUS20011090Control Valve · failed(AUS) LANDING GEAR CONTROL VALVE FAULTY. ELECTRICAL POWER TO THE VALVE WAS OK.
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