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 = 'CF680A2' 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 = 'CF680A2' 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 HALA0800032Ignition Lead · inoperativeETOPS SIGNIFICANT SYSTEM, NR 1 IGNITION ON LEFT ENG INOP. REPLACED NR 1 ENG FWD LEAD PER AMM 74-21-01. CHECKED LEAD, COND SAME. REPLACED NR 1 ENG AFT LEAD, OPS CHECK GOOD PER AMM 74-21-01.SDR HALA0800025Unknown · leakingETOPS SIGNIFICANT SYSTEM, DURING WALK AROUND NOTICED NR 1 ENG LEAKING OIL. CLEANED ENG COWL FOR NR 1 ENG RAN ENG FOR 5 MINUTES. NO LEAKS NOTED. NO OIL ADDED. QUANTITY CHECK OF IDG AND ENG OIL LEVEL CHECK GOOD. OK FOR SERVICE.SDR DL76S071590Engine · failedADVANCED THROTTLES ON T/O AND GOT A LOUD POP FROM RT ENGINE REMOVED AND REPLACED NR 2 ENG IAW TRANS 1T145.SDR HALA0700486Indication Sys · fluctuatesETOPS SIGNIFICANT SYSTEM, RIGHT ENGINE EGT FLUCTUATED ERRATICALLY DURING DESCENT WITH POWER LEVER RETARDED BELOW CRUISER POWER BETWEEN 600 DEGREES AND 55 DEGREES. PERFORMED FIM 77-21-00 FIG 103. NO DAMAGE OR FAULTS FOUND. OPERATED ENGINES. NO FLUCTUATIONS SDR DL76S071307Warning Light · illuminatedDURING T/O ROLL, RT ENG FUEL FILTER ADVISORY STATUS MSG INDICATED. OCCURRED APPROX 100-110 KNTS T/S PER FIM. REMOVED FUEL FILTER ELEMENT INSP FOR DEBRIS, NONE FOUND. INSTALLED NEW FILTER ELEMENT PER MM. RAN ENG, OPS CHECK AND LEAK CHECK OK.SDR DL76S071046Mec · malfunctionedRTO DUE TO RT ENGINE WOULD NOT MAKE TAKEOFF POWER. REPLACED RT ENGINE MEC. AFTER RUNUP ENGINE MAKES TAKEOFF POWER.SDR DL76S071022Engine · making metalLT ENGINE OIL PRESSURE WENT TO 16-18 PSI (AMBER NUMBERS). OIL QTY AT ZERO. LEFT ENGINE STOP WORKING. REMOVED AND INSPECTED LT ENG OIL FILTER. FOUND FULL OF DEBRIS MAIN ENG OIL CHIP DETECTOR SAME. COULD NOT REINSTALL MAIN E OIL FILTER DUE TO DEBRIS ON HOUSSDR DLM90071027Control Valve · stickingRETURNED TO SLC BECAUSE WITH ONLY THE LEFT PACK ON FLOW LIGHT ILLUMINATED. WITH CLIMB POWER AT 7000'. FLOW LEVEL AT 10000 TO RETURN FOR LANDING, CABIN CLIMBED TO 7000'. VERY HOT IN CABIN. FOUND LT FLOW CONTROL VALVE STICKING INTERMITTENTLY. REPLACED LEFT SDR ABXA070206Connector · looseDURING CRUISE, RIGHT ENGINE VIBRATION EXCEEDED INDICATION, BECAME INTERMITTENT. MADE PRECAUTIONARY LANDING AT KIX. FOUND N1 VIBRATION SENSOR CONNECTOR LOOSE, TIGHTENED CONNECTOR. PERFORMED FIM PROCEDURE 77-31-00. REMOVED AND REPLACED RIGHT AVM. BITE CHECKSDR ABXA070183Starter · unknownOUT OF SJO EN ROUTE TO MIA, THE NR 1 ENGINE OIL QUANTITY STARTED TO DECREASE. THE CREW ELECTED TO DIVERT TO GCM. CREW PULLED THE THROTTLE BACK TO IDLE AND MAINTAINED GOOD OIL PRESSURE. DID NOT HAVE TO SHUT THE ENGINE DOWN BUT DID DECLARE AN EMERGENCY. REMOSDR HALA0700253Oil System · lowETOPS SIGNIFICANT SYSTEM, BTB OIL QUANTITY AT PUSH 18, AT START WENT TO 13-14 NEVER WENT TO REQUIRED 19 FOR DISPATCH. INSPECTED FOR LEAKS, NONE SERVICED ENG 1 PINT MM 12-22-01. ENG OK FOR SERVICE.SDR ABXA070174Engine · defectiveRIGHT ENGINE SHUTDOWN IN FLIGHT DUE TO HIGH EGT AND HIGH ENGINE VIBRATION (METAL FOUND IN THE TAILPIPE). REMOVED AND REPLACED RIGHT ENGINE ON WO 600272604, REF JOB CARD 7010 FOR WORK ACCOMPLISHED IAW B767 MM.SDR DL76S070345Engine · power lossWHILE IN CLIMB AND AT LEVEL 34K AND THROTTLING BACK TO CRZ POWER THE LEFT ENGINE HAD A LOUD POP WITH LOSS OF THRUST WITH ENGINE AT IDLE THERE WAS NO THROTTLE RESPONSE THEN THE ENGINE WAS SHUT DOWN BY THE PILOT. A/C RETURNED TO ATL AND LANDED SAFELY. NUMBER OSDR HALA0700177Duct · crackedNR 1 ENG TURBINE CASE COOLING DUCT CRACKED 2 PLACES APPROX 10 O'CLOCK POSITION 1" LONG AND .75" LONG. CRACKED LPT TURBINE CASE COOLING MANIFOLD IN TWO LOCATIONS AT THE WELD JOINT IS ACCEPTABLE AS IS. NEED TO REINSPECT CRACKED MANIFOLD EVERY 30 CYCLES. MEASUSDR DL76S070173Engine · making metalLT ENG INOP, ON DESCENT LOUD BOOM AND SERVERE VIBS-ENG CONT TO RUN UNTIL SHUTDOWN-THRUST LOST. FOUND METAL IN TAILPIPE. REMOVED AND REPLACED NR 1 ENGINE ON ROUNTINE CARD TRANSMITTAL.SDR DL76S070088Engine · failedDURING DESCENT INTO MCO, RT ENG FAILED. UNKNOWN REASON FOR FAILURE NO VIBRATION OR NOISES NO BY CREW. A/C WAS LEVEL AT 11000 FEET RUNNING FINE. CLEARED TO 9000 FEET RT ENGINE FAILED TO RESPOND AT 9000 FT. CARD MESSAGE. T/S PER FIM BOROSCOPED HPC ALL NML. SDR DL76S060889Bulkhead · crackedTHE NLG BULKHEAD AFT WEB AND CHORD AT STA. 287, RBL 25 HAS DRILL DAMAGE TO THE WEB AND CHORD AND THE CHORD WAS STOP DRILLED INSTEAD OF CUT OUT AS REQUIRED PER THE SRM. THE EXISTING REPAIR ANGLE WAS REMOVED AND THE CRACKED CHORD WAS CUT OUT. THE DRILL DAMAGEDSDR DL76S060838Web · damagedWEB AT STA 654+121, LBL 40 WAS FOUND DAMAGED, CARGO COMPARTMENT JUST BELOW INNER CHORD. REPAIR WILL INVOLVE CUTTING THE WEB, SPLICING IAW INSTRUCTIONS. REPAIRED IAW ERA 455777-14.SDR DL76S060839Spar · crackedCRACK WAS FOUND IN LOWER OB FASTENER HOLE IN REAR SPAR. THE CRACK WAS REMOVED BY OVERSIZING HOLE AND INSTALLATION OF A FLANGED BUSHING IAW MFG INSTRUCTIONS. REPAIR ERA 455471-14.SDR DL76S060834Skin · corrodedDURING ROUTINE MTC CORROSION AND MINOR CRACKS WERE FOUND IN FUSELAGE SKIN AT 789.5 AND S-38L. SKIN WAS TRIMMED, DOUBLER AND TRIPLER INSTALLED IAW 455466-14 IAW MFG INSTRUCTIONS.SDR DL76S060738Engine · overtempLEFT ENGINE HIGH EGT DURING TAKEOFF ROLL. MAX 941C. ABORTED T/O AT LAS. PERFORMED ENGINE OVERTEMP INSPECTION PER FIM 71-05-00 FIG 112. ENG INLET AND EXH INSP, NO DAMAGE FOUND.SDR AALA20060820Stringer · corrodedFOUND CORROSION ON STRINGERS 35 LT AT STA 419 (FORWARD CARGO BIN). REPLACED STRINGERS 35 AT STA 419. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)SDR DL76S060479Gasket · out of positionCLIMBING THROUGH 10000 FT LEFT ENGINE FAILED TO A NEAR FLIGHT IDLE CONDITION. OPENED ENGINE FOUND FUEL LEAK AT MANIFOLD TO FUEL/OIL COOLER REALIGNED GASKET PLATE TIGHTENED. RAN ENGINE IN NORMAL/ALTERNATE MODE. PERFORMED QUICK SNAP CHECK. ENGINE ACCELERATE/SDR DL76S060337Engine · leakingLEFT ENGINE HOC B SUMP LEAKING, ITEM WILL REQUIRE A ENGINE CHANGE. FOUND OIL LEAKING FROM NR 6 BEARING B-SUMP BREATHER EXHAUST REPLACED NR 1 ENG PER TRANS 1T144.SDR DL767060016Skin · crackedCRACK DAMAGE WAS FOUND ON THE NR 8 LEADING EDGE SLAT, END RIB AT OSS 531.611. REPAIRED ERA 452170-14.SDR DL76S050794Packing · leakingRIGHT ENGINE LOST OIL QTY IN FLIGHT. REPLACED STARTER SHAFT PACKING.SDR DL76S050662Engine · making metalIN CRUISE, THE RT ENG HAD VIBRATION TO 5.0. DURING T/S IN FLT, THE ENG ANALYST AT HOME GOT A SMART SIGNAL THAT SHOWED A SHIFT IN F/F GET AND LOW N-2 ROTOR SPEED OCCURRED. CALLED THE MTC COORDINATOR WHILE ON THE RADIO PATCH AND ADVISED WHAT OBSERVED. ADVISEDSDR DL76S050470Pump · leakingFUEL IMBALANCE OF 3500LBS, DIVERTED TO OMA, FOUND BOLT AT LT ENGINE FUEL PUMP MISSING AND LEAKING. REPLACED GASKET AND 4 BOLTS.SDR DL76S050139Controller · malfunctionedNR 1 ENG WOULD NOT ACHIEVE T/O POWER WITH ANTI-ICE ON OR OFF. RETURNED TO GATE. REPLACED MAIN ENGINE CONTROLLER.SDR DL76S041096Engine · making metalLEFT ENG OIL FILTER MESSAGE. DID NOT EXT WITH THROTTLE REDUCTION. OIL PRESS AND TEMP NORMAL. PERFORMED ENG SHUTDOWN PER QRH. DIVERTED TO JAX. DEBRIS FOUND ON CHIP DETECTORS. REPLACED ENGINE.SDR DL76S041098Engine · making metalLT ENGINE OIL FILTER MSG IN FLIGHT RETARDED LT ENGINE TO IDLE WITH MSG STILL THERE SHUTDOWN LT ENG IN FLIGHT. CHECKED SCAVENGE FILTERS AND ALL CHIP DETS FOUND HEAVY FUZZON MASTER CHIP DET LARGE AMOUNT OF SHINY FLAKES ON AFT B-SUMP DET FOUND TWO OR THREE SHINYSDR DL76S041080Door · missingON ARRIVAL FOUND MISSING BLOW OUT PANEL ON NR 2 ENGINE INBOARD PYLON. PANEL SIZE APPROX 9 INCHS DIAMETER. INSTALLED NEW ACCESS DOOR NR 2 PYLON INBOARD.SDR DL76S040997Housing · fracturedCENTER HYD SYSTEM FAILURE ON TAKEOFF. QUANTITY ZERO RETURNED. FOUND NBR 6 SPOILER ACTUATOR HOUSING CRACKED. REPLACED NR 6 SPOILER PCA IAW MM 27-61-02.SDR DL767040957Odor · detectedRAN ENGINES AND PACKS. INSPECTED AIRCRAFT, UNABLE TO DUPLICATE.SDR AALA20040963Battery Pack · inoperativeEMERGENCY EXIT SIGN LIGHT AT RT FORWARD GALLEY AT FLOOR IS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT RT HAD FORWARD GALLEY AT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED.SDR DL767040792Pressure Switch · inoperativeRIGHT ENG FUEL FILTER EICAS MSG ON TAKEOFF, ATB. REPLACED NR 2 ENG FUEL FILTER/FUEL PRESS SW. NO DEBRIS FOUND. OK FOR SERVICE PER FIM 73-11-00 PG 106.SDR DL767040780Fan · inoperativeFORWARD EQ SUPPLY FAN 2 EICAS MSG WITH EQUIP COOLING SUPPLY FAN 2 CB POPPED STRONG ELECTRICAL FUMES IN COCKPIT, REPLACED FAN.SDR DL76S040501Turbine Blades · damagedRT ENGINE EGT 950 ON TAKEOFF FOR LESS THAN ONE MINUTE. FOUND LPT BLADES DAMAGED AND BROKEN PER FIM. REPLACED NR 2 ENGINE PER JIC CARD DECK 1T145. C/W NR 2 ENGINE PREFLIGHT AND LEAK CHECKS, NO DISCREPANCIES NOTED.SDR AALA20040464Compressor · stalledORD - DURING CRUISE AT FL370 EXPERIENCED THREE COMPRESSOR STALLS. ALL ENGINE INDICATIONS REMAINED NORMAL, NO VARIATIONS. FLIGHT ATTENDANTS REPORTED SPARKS COMING OUT OF RIGHT HAND ENGINE. SPARKS CONTINUED INTERMITTANTLY DURING DECENT WHENEVER POWER WAS CHANSDR DL767040506Wire · corrodedDURING HMV IN GSO FOUND NR 1 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRING AND PLUGS.SDR DL76S040114Cap · missingDURING FLIGHT, NR ENGINE PYLON DEPARTED AIRCRAFT. UNDER INVESTIGATION.SDR DL76S031013Gasket · failedON LANDING ROLL TOWER REPORTED SMOKE AND FUEL COMING FROM LT ENG AFTER TOUCHDOWN ALL LEFT ENGINE INDICATION VERY LOW. TURNED FUEL SWITCH OFF. MTC FOUND FUEL LINE FROM PUMP TO MEC GASKET BAD. REPLACED GASKET. RAN ENGINE. CHECKS GOOD.SDR DL76S030726Bleed Valve · inoperativeREJECTED TAKEOFF SHORTLY AFTER TAKEOFF POWER APPLIED. (LESS THAN 30 KTS) FOR MASTER CAUTION LIGHT AND AURAL WARNING. EICAS MSG RT ENGINE BLEED VALVE AND BLEED ANNUNCIATOR LIGHT IN OVERHEAD PANEL ILLUMINATED. REPLACED VALVESDR DL76S030586Link · crackedA/C LOG E302036 ITEM 007 DETAILS REPLACEMENT OF AFT MOUNT O/B TANGENTAL LINK DUE TO CRACK THROUGH ONE SIDE OF LINK EVEN WITH CENTERLINE OF BEARING. CRACK WAS FOUND BY MTC ON WALK AROUND AND REPLACED. NO OPERATIONAL PROBLEMS WERE NOTED BEFORE OR AFTER REPLACMSDR DL76S030378Engine · leakingENROUTE TO EWR LT ENGINE OIL QUANTITY AND PRESSURE BEGAN TO DROP. QUANTITY REACHED 0.SHUT DOWN ENGINE WHEN LOW OIL PRESSURE LIGHT CAME ON AT APPROXIMATELY 10-11 PSI. FOUND OIL LEAK FROM OIL INLET PRESSURE TUBE. REMOVED AND REPLACED SCAVENGE TUBE ON NBR 6 BEASDR DL76S030048Duct · crackedPILOT REPORTED NR 1 ENGINE HAD OVERHEAT LOOP 1 EICAS MSG AMD ALSO HAD OVERHEAT LOGHT ON PEDESTAL FLICKERING, CLOSED BLEED VALVE, LIGHT STILL FLICKERS, WENT OUT AFTER RETARDING THROTTLE. ON ENGINE INSPECTION FOUND TURBINE CASE COOLING DUCT CRACKED, REPLACED SDR DL767021462Coupling · leakingLEFT DUCT LEAK ON CLIMBOUT. RESEALED COUPLING ON BODY CROSSOVER DUCT IN LEFT AC BAY. RAN TO TAKEOFF POWER PER PFHB. OK FOR SERVICE.SDR DL76S021424Thrust Reverser · malfunctionedRT THRUST REVERSER YELLOW LIGHT CAME ON ON TAKEOFF WITH NO THRUST REVERSER SELECTED. ABORTED T/O AT 90KTS. FWD MCO/PLAC PER MEL 78-36-01. RT THRUST REVERSER LOCKED OUTSDR DL767021395Engine · failedLEFT ENG SURGE IN FLIGHT AND ON LANDING. ENG SHUT ITSELF DOWN ON LANDING AT 5 THOUSAND FT. ENG CHANGE IS IN WORKSDR DL76S021038Apu · leakingAT TOP OF CLIMB AND CRUISE AT 410 HOT PACK ODOR IN COCKPIT NO LIGHTS OR WARNINGS. NO REPORTED ODOR FROM THE CABIN. F/A'S LATER REPORTED HAZE AND LAV SMOKE DETECTOR ALARMS. TURNED RT PACK OFF, SMOKE SEEMED TO ABATE. REMOVED RT PACK BYPASS VALVE AND DUCT HAS
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