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 01092006BUnknown · unknownAUTOCOARSEN EVENT WHEN PL WERE ADVANCED BEYOND 64 DEGREES PLA- LT ENG. NO ING LIGHT ON SHUTDOWN. PERFORMED AUTOCOARSEN AND CTOT, OPS CHECK GOOD NO DEFECTS NOTED.SDR SIMA200600302Skin · damagedHAIL DAMAGE ON THE LT HORIZONTAL STABILIZER TOPSKIN. REMOVED THE EXISTING LT HORIZONTAL STAB TOP SKIN PANEL. POSITIONED NEW LT HORIZONTAL STABILIZER SKIN. MARKED AND DRILLED FASTENER HOLES. REPOSITIONED AND INSTALLED SKIN. REPAIR DONE IAW SRM. (K)SDR SIMA200600303Skin · damagedHAIL DAMAGE ON THE RT HORIZONTAL STABILIZER TOP SKIN PANEL. REMOVED THE EXISTING SKIN PANEL AND MARKED AND DRILLED FASTENER HOLES. REPOSITIONED AND INSTALLED SKIN. REPAIR DONE IAW SRM. (K)SDR SIMA200600304Frame · dentedTHE RT SIDEWALL CARGO FRAME AT STA 677 WAS FOUND TO BE DENTED. RECONTOURED THE DENT. PREPARED A REPAIR ANGLE. REPAIR DONE IAW SRM. (K)SDR SIMA200600905Frame · damagedTHE FUSELAGE FRAME AT STA 258 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A FILLER AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K)SDR AU510001803Actuator · sluggishRT MAIN LANDING GEAR RETRACTION ACTUATOR SLUGGISH IN OPERATION. INVESTIGATION CONTINUING.SDR AU510001952Engine · failedPASSENGER REPORTED `FLAMES OF RED METAL COMING FROM LEFT ENGINE 3-4 METRES BACK` AND AN EMERGENCY LANDING WAS CARRIED OUT. ENGINEERING INSPECTION THE IGV`S, FIRST STAGE COMPRESSOR, AFT FACE OF POWER TURBINE ASSEMBLY FOUND NIL DAMAGE. A GROUND POWER ASSURANCESDR AU510002012Warning System · faultyRT ENGINE BLEED AIR LEAK LIGHT ILLUMINATED. INVESTIGATION CONTINUING.SDR AU510002201Valve · seized(AUS) LANDING GEAR EMERGENCY UPLOCK VALVE SEIZED. (OTHER CAUSE: INDETERMINABLE ) (CASA NR 510002201)SDR PNSA051106Engine · misriggedWHILE SETTING CTOT TO 80 PERCENT POWER AUTOCOARSEN ARMED LIGHT WENT FROM HIGH TO LOW WITH A POWER FLUCTUATION. FLIGHT CREW REDUCED POWER AND ABORTED TAKEOFF. MAINTENANCE FOUND MANUAL ENGINE RIGGING TO BE INTERFERING WITH AUTOCOARSEN ELECTRICAL SETTINGS. ENGISDR 11302005ABattery · inoperativeDURING A LINE CHECK 1 INSPECTION 3 FLOOR PROXIMITY LIGHTS AND 2 OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY 22LN WAS REPLACED AND BOTH THE FLOOR PROXIMITY AND OVERHEAD EMERGENCY LIGHTS WORKED NORMALLY IAW 33-50-01S.SDR CA051124007Engine · overheated(CAN) AS THE POWER LEVERS WERE ADVANCED TO 80 PERCENT THE FLIGHT CREW HEARD POPPING NOISES AND THE TAKEOFF WAS REJECTED. THE NR 2 ENGINE OVERHEAT LIGHT WAS ILLUMINATED AND THE ENGINE WAS SHUTDOWN. THIS ENGINE HAS BEEN REMOVED AND RETURNED TO MANUFACTURER FOR ESDR MALA050823Warning Light · activatedENGINE CHIP DETECTOR INDICATION. NO FURTHER INFORMATION AT THIS TIME.SDR MALA050816Warning Light · illuminatedON DEPT FROM DTW, THE CAPTAIN NOTICED A RT ENGINE CHIP DETECTOR LIGHT ON. FOLLOWED QRH, LIGHT WENT OUT, THEN CAME BACK 4 TIMES. RETURNED TO DTW. NO FURTHER INFORMATION AT THIS TIME.SDR 11022005BIgnition Lead · damagedFOUND RT ENGINE FAILED ON TAKEOFF. HEARD POPPING AND THEN PROP AUTO COARSENED. PERFORMED BORESCOPE NO DEFECTS NOTED, FOUND BROKEN IGNITION LEAD. REMOVED AND REPLACED RT ENGINE OUTBOARD IGNITER LEAD, PN 4052T54P02 SN ON UNJM3914, SN OFF UNJC3349. OPS CHECKS SDR SIMA200529003Dpu · inoperativeCREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. REPLACED NR 2 DPU IAW AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600453) (K)SDR SIMA200528311Power Supply · dischargedEMERGENCY LIGHT OVERHEAD SIGN AT ROW 8, INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY 201N. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600359) (K)SDR 10102005AStator · faultyBOTTOM GOVERNOR WILL NOT ENGAGE AND TORQUE REMAINS AT 0 PERCENT WITH POWER LEVER MOVEMENT. PRPM SEEMS TO OPERATE NORMALLY. REMOVED AND REPLACED NR 1 ENG ALT STATOR P/N 6043T28P05, S/N GJA45098, ROTOR P/N 4068T18P02. S/N OFF GJAJ4130, IAW AMM 77-11-10-2. ALSDR 09232005ATire · flatDURING TAKEOFF, EXPERIENCED STRONG YAW TO RT AT +80 KIAS. ABORTED TAKEOFF AND EXITED RUNWAY. SHUTDOWN AND NOTICED NR3 AND NR4 TIRES BLOWN DUE TO MISSING TREAD. FOUND NR1 AND NR2 TIRES FLAT. REMOVED AND REPLACED NR1 TIRE IAW CHAPTER 32-41-05-4 OF THE AMM P/NSDR 09212005FHmu · malfunctionedLEFT ENGINE WILL NOT SHUT DOWN, HAD TO PULL T-HANDLE TO SHUT DOWN. RIGGED CONDITION LEVER INPUT TO HMU GEAR BOX AND THE PCU.SDR 09162005AO-Ring · leakingLEFT ENG SMOKING FROM NACELLE. REMOVED AND REPLACED STARTER SHAFT O-RING. NO LEAKS NOTED.SDR SIMA200526406Seat Track · corrodedSEAT TRACK BL0 WAS FOUND TO BE CORRODED BETWEEN STA 339 AND 363. BLENDED THE SEAT TRACKS TO REMOVE THE CORROSION. CUT A SECTION FROM U-BEAM FOR REPAIR. CLEANED TREATED AND INSTALLED U-BEAM IN SEAT TRACK. REPAIR DONE IAW SRM. (K)SDR 09122005GEngine · overtempLT ENGINE EXCEEDED ITT ON TAKEOFF (931 FOR 30 SECS. PERFORMED CAPPED AND UNCAPPED RUNS. ENGINE PERFORMANCE WITHIN LIMITS PER GE MANUAL.SDR 08302005BControl Unit · malfunctionedRT ENGINE TORQUE FLUX. REMOVED AND REPLACED DECU. OPS CHECK GOOD.SDR MALA050666Engine · odorCLIMBING THROUGH 15000 FEET EN ROUTE TO DTW SMELLED A WEIRD ODOR IN FLIGHT DECK. LOOKED DOWN AT THE ENGINE INSTRUMENTS AND NOTED THE RIGHT ENGINE OIL PRESSURE GAUGE FLUCTUATING INTO THE YELLOW ARC, THEN INTO GREEN CONTINUOUSLY ABOUT 30 SEC. AFTER THAT, HEARDSDR MALA050667Engine · failedADVANCING THE POWER ON THE LEFT ENGINE AFTER THE RT FAILED. ACCIDENTALLY PUSHED THE POWER LEVER UP TO MUCH AND THE RED OVER TEMP LIGHT CAME ON AND ITT WAS 1000C. CORRECTED AFTER 5 TO 10 SECONDS. REPLACED LT ENGINE ASSY IAW JC 7100-301. WO 381423 FOR DETAILSSDR 08122005EEngine · surgesABORTED TAKEOFF DURING POWER UP LT ENGINE SURGED. MAINTENANCE INSPECTION FOUND NO FAULT.SDR 08092005AEngine · flamed outLEFT ENGINE HAD MOMENTARY FLAMEOUT IN FLIGHT AT FL210-11 DEGREES W/TRACE ICE, IGNITION KICKED IN RIGHT AWAY. PERFORMED ENGINE RUN AFTER LT ENGINE BORESCOPE TO VERY PROPER ENGINE PERFORMANCE. ALSO, PERFORMED ENGINE OVERSPEED TEST IAW COLGAN WORKCARD 73-20-01SSDR 08082005JEngine · flamed outDISCREPANCY: LH ENGINE HAD MOMENTARY FLAMEOUT INFLIGHT AT 21000FT. AND -11 DEGREES PERFORMED BORESCOPE INSPECTION, NO DEFECTS NOTEDSDR SIMA200522009Compressor · stalledDURING TAKEOFF, RIGHT ENGINE BEGAN TO GO INTO COMPRESSOR STALLS. ENGINE OVERTEMPED BETWEEN 1013 AND 1025. REMOVED AND REPLACED RIGHT ENGINE IAW W/C 4903. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR CA050808006Cover · misinstalledDURING CLIMB, RT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE WAS SEEN TO DROP TO NEAR ZERO. ENG WAS SHUTDOWN AND THE ACFT RETURNED FOR AN UNEVENTFUL LANDING. MX INVESTIGATION REVEALED THAT ACCESSORY GEARBOX DRIVE SHAFT AXIS `A` COVER WAS MISSING ALLSDR 07192005Pressure Switch · leakingRT ENGINE APPEARS TO BE LEAKING FUEL FROM PRESSURE SWITCH.SDR 07172005BCompressor · stalledNR 2 ENGINE SHUTDOWN ON TAKEOFF AFTER SUSPECTED COMPRESSOR STALL.SDR SIMA200520301Line · rupturedDISC, UPON GEAR SELECTION UP THE HYDRAULIC QUANTITY STARTED DROPPING TO -0-, MANUAL PUMP OVERRIDE FAILURE. REPLACED RUPTURED NOSE LANDING GEAR RETRACT/EXTENSION ACTUATOR HYDRAULIC LINE. LEAK AND OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR AU510001971Detector · faultyLT ENGINE TAILPIPE OVERHEAT DETECTOR FAULTY. SUSPECT CAUSED BY WATER INGRESS DUE TO HEAVY RAIN.SDR SIMA200518608Skin · chafedTHE LT IB NACELLE WAS FOUND CHAFED AT THE FILLET FAIRING SEAL CONTACT POINT. BLENDED THE DAMAGED AREA. FABRICATED AND INSTALLED A REPAIR DOUBLER. WORK DONE IAW SRM. (K)SDR 06262005Engine · overtempON TAKEOFF, RT ENGINE HAD AN ITT OF 907 WITH TAKEOFF POWER ON BOTH ENGINES AT 88 PERCENT WHILE CLIMBING TO POWER.SDR 06252005Engine · failedRIGHT ENGINE FAILED INFLIGHT.SDR SIMA200518604Frame · damagedTHE CARGO SIDEWALL FRAME AT STA 686.888 WAS FOUND BENT AND DENTED. RECONTOURED THE FRAME. PREPARED AND INSTALLED REPAIR SECTION OF NEW FRAME. REPAIR DONE IAW SRM. (K)SDR SIMA200518605Floorbeam · corrodedTHE GALLEY FLOOR FRAME AT STA 272 WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200518606Floorbeam · corrodedFLOORBEAM AT STA 225.0 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR 06232005BTransducer · malfunctionedRT ENGINE OIL PRESSURE LIGHT ILLUMINATED AFTER TOUCHDOWN, PROP PSI READS 0. REMOVED AND REPLACED TRANSDUCER, OPS CHECK GOOD.SDR 06222005Gearbox · malfunctionedLT PROPELLER FEATHERED DURING TAKEOFF ROLL.SDR SIMA200518601Web · corrodedTHE REINFORCEMENT WEB AT STA 294 WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW REPAIR. (K)SDR SIMA200518602Frame · corrodedTHE RT SIDEWALL CARGO FRAME AT STA 677 WAS FOUND DENTED. RECONTOURED THE DENT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200518603Frame · damagedTHE CARGO SIDEWALL FRAME AT STA 640 WAS FOUND DENTED. RECONTOURED THE DENT. FABRICATED AND INSTALLED REPAIR SECTION OF NEW FRAME. REPAIR DONE IAW SRM. (K)SDR 06222005CConnector · looseLEFT OIL PRESSURE READS 0 PSI IN FLIGHT. FOUND LOOSE CONNECTOR ON OIL PRESSURE TRANSMITTER. CLEANED AND SECURED.SDR SIMA200518607Floorbeam · damagedTHE CARGO FLOOR FRAME AT STA 710.0 WAS FOUND BENT IN 2 AREAS. RECONTOURED BOTH DENTS. FABRICATED AND INSTALLED 2 DOUBLERS AND 2 ANGLES. REPAIR DONE IAW SRM. (K)SDR 06202005Engine · malfunctionedAT 5 TO 6 MINUTES IN FLIGHT OIL PRESSURE FLUCUATED. STARTED SMALL AND INCREASED, OIL PRESSURE DROPPED. SHUTDOWN ENGINE WHEN CLOSE TO 0, OIL TEMP STILL IN GREEN.SDR PNSA050602Engine · malfunctionedLT ENGINE HAD AUTO IGNITION EVENT DURING CRUISE IN CLOUDS ANTI-ICE SYSTEM WAS ON. NO VISIBLE ICE NOTED BY CREW HOWEVER THERE WAS ICE FORECAST. CREW REPORTED ONE IGNITION RELIT AND CONFIRMED IGNITION LIGHTS ON. ALL OTHER PARAMETERS NORMAL. CREW ELECTED TO R
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