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 = 'CF680C2B6' 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 = 'CF680C2B6' 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 DL76L070057Connector · looseATB DUE TO NO DUCT PRESSURE FROM LEFT ENGINE AND LEFT PACK WOULD NOT COME ON LINE. OPERATED WITH RIGHT ENGINE AND PACK AND DUCT PRESSURE NORMAL. FOUND CONNECTOR ON PRV CONTROLLER LOOSE. TIGHTENED SAME. RAN ENGINE AND PRESSURE CAME UP. A/C RTS.SDR DL76L070055Circuit Breaker · failedDUE RT A/C BUSS FAILURE DURING TAXI. T/S PER SSM NTF. REMOVED AND REPLACED AUX POWER BREAKER C905 PER MM. NORMAL RT/LT APU BUSS ISOLATION OPS NORMAL.SDR AALA20061307Tube · leakingDURING FLIGHT, LEFT ENGINE N2 INDICATION AND STANDBY INDICATION SHOWING 0.0. ALL OTHER ENGINE INDICATIONS NORMAL. AFTER LANDING FOUND EVIDENCE OF FUEL LEAK FROM LEFT ENGINE. FOUND LEAK FROM FUEL PIPE LOW PRESSURE FILTER TO OIL COOLER, PIPE FRACTURED. REPLASDR DL76G060934Fan · inoperativeCREW REPORTS EICAS EQUIP COOLING SUPPLY FAN 1 FAILED WITH STRONG BURNED SMELL WINDING THROUGHOUT COCKPIT. MTC IN PROGRESS. FOUND NR 1 SUPPLY FAN FAILED. REPLACED EQUIPMENT COOLING FAN. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.SDR DL76G060890Valve · intermittentADVANCED THE POWER FOR T/O AND GOT T/O CONFIG WARNING HORN AND LIGHT ALONG WITH A FALSE RED PARKING BRAKE EICAS MSG. WE WERE ROLLING T/O AND WERE BELOW 60 KTS. THE PARKING BRAKE WAS NOT SET. RAN CONFIG TEST IAW AMM. PARK BRAKE SWITCH CKS, GOOD. REPLCD PARK BRASDR AALA20061061Sill · corrodedFORWARD CARGO DOOR SILL LOWER CHORD HAD CORROSION BLENDED FROM THE HORIZONTAL INSIDE FLANGE AT STATION 616. AREA OF DISCREPANCY IS 2.5 INCHES BY 2.5 INCHES WITH A DEPTH OF .033 INCH. REMOVED FASTENERS AND BLENDED CORROSION AWAY USING A MINIMUM 0.5 INCH BLEND SDR DL76G060861Controller · unserviceableRT BLEED OFF LIGHT ILLUMINATED WITH BLEED LATCH ON. PERFORMED BITE ON ABCU FAULTED PRC AND WIRE FAULT REPLACED PRC PERFORMED BITE FAULT CLEARED RAN ENG OPS NORMAL.SDR AALA20060778Connector · looseLAX - EMERGENCY LIGHTS AT SEATS 22HJ THROUGH 24HJ INOPERATIVE. SECURED LOOSE CONNECTOR FOR INOPERATIVE EMERGENCY LIGHTS AT SEATS 22HJ THROUGH 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20060770Bulb · inoperativeDFW - EMERGENCY LIGHT AT RT FORWARD OVERWING INOPERATIVE. RELAMPED RT FORWARD OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DL76G060577Engine · fireLEFT ENG FIRE ON DEPARTURE RETURNING TO GIG. REPLACED NR 1 ENG PER TRAN 1T160.SDR DL76G060556Engine · damagedNR 2 ENG FAILED OVERTEMP BORO HPC. 2 ENG OPENED UP AND BORO PLUGS REMOVED. C/W BORO INSP NR 2 S/N 695442 PER FIM. HPC FOUND DAMAGED BEYOND MTC LIMITS. ENG CHG REQUIRED QC 1513. REINSTALLED ALL BORO PLUGS THAT WERE REMOVED. NR 2 ENG CHANGE TO BE C/W BY TOSDR DL76G091055Switch · inaccurateHUNG START LT ENG CRASH ENG STARTER TO EXT TAIL PIPE FIRE. REPLACED LT ENG FUEL CUTOFF SWITCH WRANG OUT, REF WDM 76-11-11 AND 28-22-21 CKS OK REQS OPS CHECK. PERFORMED ENG RUN PER MM OPS NORMAL.SDR DL76G060288Shutoff Valve · faultedAFTER ENGINE START LEFT ENGINE BLEED WOULD NOT OPEN. BITE CHECK ASCM - FAULTED L PRSOV. RESET BLEED AIR AND ASCM RAN ENGINE AT GATE PER PFHB. LEFT ENGINE BLEED AIR CHECKS NORMAL.SDR CA051221006Cooling Fan · seizedCREW REPORTED SLIGHT SMOKE AND PLASTIC BURNING ODOR IN COCKPIT. ACFT DIVERTED TO SNN. MX CARRIED OUT INSPECTION, FOUND EQUIP COOL EXHAUST FAN FAILED AND TRIPPED THE CB, AREA INSP. NO FURTHER DAMAGE FOUND, FAN PLACED ON MEL ACFT DISPATCHED.SDR DL76G050632Engine · damagedDAMAGED BRACKETS, VSV LEVER ARMS, AND HEAT SHIELDS ON NR 1 ENGINE. REPLACED ENGINE.SDR CA050909003Wire Harness · failed(CAN) FAULT: FLT DEP.YYZ WITH LT FUEL DENSIOMETER UNDER MEL. FLT CREW CONFIRMS LT IND DID BLANK OUT ON OCCASION DURING THE FLT AND HAD BEEN CALCULATING THE FUEL REMAINING THROUGHOUT THE FLT. AT FL370 AND 50NM FROM TOP OF DESCENT, THE LT ENG FLAMED OUT, ENG RSDR CA050510008Throttle Cable · misaligned(CAN) ON CLIMB OUT THRU FL 130 EICAS (L PRV) QRH COMPLETED - THRU FL 200 LT THROTTLE VERY HARD TO ADVANCE OR MOVE TO IDLE. A/T ARM OFF NO IMPROVEMENT. RETURN TO LHR. NO LT REVERSE ON LANDING. FOR T/S AND INFO ON PRV REFER TO L1425969. LT ENG PUSH PULL CABLE RSDR DL76G050240Compressor · stalledAFTER LEVEL OFF AND UPON ADVANCING THRUST LEVERS TO INCREASE SPEED RT ENGINE BEGAN TO HAVE COMPRESSOR STALLS. REPLACED ENGINE FOR INTERNAL DAMAGE.SDR DL76G041077Engine · unknownSHORTLY AFTER T/O WITH ALL PARAMETERS NORMAL ON BOTH ENGINES THE LEFT ENGINE FIRE WARNING ANNUNCIATED. THE CREW PULLED BACK THE THROTTLE AND THE FIRE WARNING EXTINGUISHED. THE CREW ELECTED TO SHUT DOWN THE ENGINE. NO FIRE BOTTLES WERE BLOWN. A/C DID A ATBSDR CA041126010Axle · broken(CAN) ACFT 684 ON LANDING, DISCOVERED RT ML GEAR AFT AXLE BROKEN, IT SEEMS THAT HAPPEN DURING TAKEOFF IN XXX, BECAUSE FLIGHT CREW REPORT ANTI- SKID LIGHT WAS ON DURING WHOLE FLIGHT. MORE INFO AND PICTURES WILL FOLLOW AS IT BECOME AVAILABLE.SDR AALA20040914Nut · looseDFW - ABOUT 150 MILES FROM DFW OIL QUANTITY WENT TO ZERO AND OIL PRESSURE WENT TO APPROXIMATELY 23 PSI IN THE AMBER BAND. SECURED RIGHT HAND ENGINE PER QHR AS A PRECAUTION. NO OIL TEMPERATURE OR ENGINE TEMPERATURE ON ENGINE TEMPERATURE RED INDICATIONS. LANDSDR AALA20040917Battery Pack · inoperativeDFW EMERGENCY LIGHT AT BOTTOM FORWARD LAVATORY FS3 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT BOTTOM FORWARD LAVATORY FS3. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)SDR AALA20040901Connector · looseEMERGENCY LIGHTS AT SEAT ROWS 28, 29, AND 30AB INOPERATIVE. RESECURED CONNECTOR AT SEAT 28AB FOR EMERGENCY LIGHTS AT SEAT ROWS 28 THROUGH 30AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)SDR AALA20040848Pseu · inoperativeHNL INFLIGHT T296/11 LEADING EDGE SLAT ASYMMETRY WITH FLAP INDICATION BETWEEN ONE AND UP. RETURNED TO HNL AND LANDED OVERWEIGHT WITHOUT INCIDENT. OVERWEIGHT INSPECTION ACCOMPLISHED IAW WORK CARD 05 96 11 WITH NO DISCREPANCIES FOUND. REPLACED FSEU AND PSEUSDR AALA20040747Bearing · failedSJC - INFLIGHT T0073/17 LEFT ENGINE N2 ALTERNATOR DRIVE BEARINGS FAILED ON CLIMBOUT. REPLACED NUMBER 1 ENGINE PER SPECIAL ITEM CARDS 71-93-01 AND 71-95-22. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20040653Gasket · leakingGRU - INFLIGHT T0907 ON DESCENT THROUGH 22000 FEET RT ENGINE FLAMED OUT. ACCOMPLISHED AN INFLIGHT START WITHIN 2 MINUTES. DESCENDING THROUGH 6000 FT, RT ENGINE HAD UNCOMMANDED SHUTDOWN. ACCOMPLISHED SINGLE ENGINE LANDING. LANDED WITHOUT INCIDENT. FOUND FUSDR CA040513003Computer · failed(CAN) AFTER T/O EICAS MSGS (RUDDER RATIO,AILERON LOCKOUT) ALTIMETER, AIRSPEED, IVSI OUTSIDE LIMITS BETWEEN CAPT AND F/O, AUTO PILOTS WOULD NOT ENGAGE. NOTE: MOC REQUESTED F/O ALT ADC BE SELECTED, FAULT CLEARED. FLT CREW ELECTED TO RTN TO YVR. RT ADC FAULT BUSDR DL76G030610Pressure Switch · faultyDURING TAKEOFF AND CLIMB GOT A R ENG FUEL FILTER MESSAGE. MESSAGE GOES OUT BELOW 88 PERCENT N1. RETURNED TO JFK AFTER DUMPING FUEL. LANDED BELOW MAX LDG WEIGHT. FOUND DIFF PRESS SWITCH AT FAULT REPLACED SAME R/U AND LEAK CK OK. MAIN FUEL FILTER CLEAN. ETOSDR DL76G030555Control Panel · faultyRT ENGINE TOOK ONE MINUTE TO SHUTDOWN WHEN FUEL CONTROL SWITCH MOVED TO SHUTOFF. REPLACED FIRE CONTROL PANEL.SDR DL76G030265Eec · malfunctionedR ENG EEC EICAS MESSAGE ON T/O ROLL. FWD TO MCO AND PLACARD PER MEL 73-21-01A. PIMU MONITOR SHOWS NO FAULTS. T/S PER FIM. RAN ENG, NO FAULTS. OK FOR SERVICE. MCO/PLAC REMOVED.SDR AALA20021905Shutoff Valve · defectiveLT ENGINE HIGH PRESSURE SHUTOFF VALVE ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO LAX ACCOMPLISHED OVERWEIGHT LANDED WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION AND REPLACED NR 1 ENGINE HIGH PRESSURE CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL SDR DL76G021461Blade · damagedTWO AUDIBLE STALLS INTO ATL. DURING RT ENG BORESCOPE FOUND BLADE DAMAGE ON 12TH STAGE OF THE COMPRESSOR AND 1ST STAGE OF THE HPT. REPLACED ENGINE.SDR DL76G021348Towershaft · brokenAT CRUISE FL 350 RIGHT ENGINE EEC EICAS MSG AND AT SAME TIME ENG STARTED ROLLING BACK AND SHUTDOWN. FOUND GEARBOX TOWER SHAFT BROKEN. REPLACED ENGINE.SDR AALA20021439Wire · brokenBOS - FLT 146 - EN ROUTE BOS-CDG, RIGHT ENGINE BLEED LIGHT CAME ON ONE HOUR AFTER TAKEOFF. WIRE AT AFT TERMINAL ON AIR SUPPLY MODULE BROKEN. RETURNED BACK TO BOS. LANDED WITHOUT INCIDENT. REPLACED WIRE, INSTALLED NEW TERMINAL. BITE ON AIR SUPPLY MODULE SHSDR DL76G020836Frame · crackedON MTC CHECK FOUND 6.75 INCH CRACK AT TURBINE REAR FRAME. REPLACED ENGINE.SDR DL76G020484Sensor · malfunctionedRIGHT ENGINE SLOW TO SPOOL DOWN FROM CRUISE POWER TO IDLE SETTING. TOOK ABOUT 20-30 SECS FOR ENGINE TO SPOOL DOWN. EMERGENCY EQUIPMENT CALLED OUT, BUT NO EMERGENCY DECLARED. NR 2 ENG CIT SENSOR REMOVED. REPLACED NR 2 ENGINE CIT SENS PER M/M. LEAK CKS OK, SDR EVA200201Engine · damaged1. During initial climb, Captain notice the L Engine N1 vibration indicationin on the EICAS is up to 3.3 and N2 up to 5.0. All the rest parameters are normal.2. After 2 hours in cruise, "L ENG OIL FILTER" message appeared in the EICAS. Pilto followed the QRH pSDR DL76G020198Engine · vibrationON TAKEOFF ROLL, THE RIGHT ENGINE VIB INDICATED A 5.0 (LPT). TAKEOFF ABORTED AT 80 KNOTS INDICATED AIRSPEED. ALL OTHER ENGINE PARAMETERS ARE NORMAL. T/S PER FIM 71-05-00. CHIP DET CHECKED, CLEANED ACCEL CONNECTOR, LUBED FAN BLADES. PERFORMED VIBRATION SURSDR DL76G020066Engine · making metalMETAL FOUND ON CHIP DETECTOR,-A- -C- AND -D- SUMP CHIP DETECTORS. ATL MTC REPLACING ENGINE. UPON FURTHER EVALUATION FROM ENGINE, SHOP NOW SUSPECT METAL IS CLEAN-UP MATERIAL. MTC FURTHER EVALUATING WITH T/O POWER PENALTY RUN.SDR CA010924003Rib · cracked(CAN) LT AND RT WING RIB WEB, INBOARD OF SLAT ANTI-ICE TELESCOPING DUCT CRACKED/BROKEN AT TOP SURFACE. 4 - 6 INCH CRACK FOUND IN RADIUS OF L/H AND RT NOSE FORMER ON WING FIXED LEADING EDGE COMMON TO NR 5 AND 8 LEADING EDGE SLAT.SDR DL76G011202Manifold · crackedRT ENG FUEL MANIFOLD LEAK.REMOVED AND REPLACED FUEL PIPE. SDR DL76G010960Engine · failedSHIP 1505 FLT 107/13 FRA/JFK AT FL4K CAPT ATTEMPTED A LVL CHANGE AT FL4K RT ENG DID NOT RESPOND. THROTTLE BACK TO IDLE THE EGT CONTINUED TO CLIMB TO 895 THE ENG WAS SHUT DOWN./C MTC FOUND METAL IN TAIL PIPE. /C REPLACED THE ENG. SDR AALA20011136Engine · vibrationHNL - FLT 298 - RIGHT ENGINE VIBRATION IND 2.8 WITH MASTER CAUTION ON ROTATION. ACCOMPLISHED VIBRATION SURVEY PER MM 71-00-00-5-H NR 7 VIBRATION WITHIN LIMITS 1.8 ON RUN-UP. NO PRV LIGHT OR MASTER CAUTION LIGHT BITE CHECK ON AIRSUPPLY MODULE ENGINE VIBRATIONSDR CA010522009Fitting · cracked(CAN) DURING INSPECTION NR 2 PYLON INBOARD MIDSPAR FITTING WAS FOUND CRACKED AT UPPER AFT INBOARD FASTENER HOLE. NR 2 PYLON MIDSPAR FITTING REPLACED AS PER EVA 01-767-54-4058.SDR CA010301015Fseu · failed(CAN) ON TAKEOFF, WITH FLAPS SELECTED 5, FLAPS WOULD NOT MOVE. MOMENTARY TRAILING EDGE FLAP DISAGREE LIGHT. STATUS MESSAGE TE FLAP SHUTDOWN. WHEN AUTOPILOT DISENGAGED AIRCRAFT ROLLED TO THE RIGHT. AIRCRAFT RETURNED TO YYZ. MAINTENANCE ON ARRIVAL FOUND FLAPS/SLSDR DL76G010204Idg · failedRIGHT GEN DRIVE LIGHT FLICKERED TWICE, 30 MIN LATER LIGHT ON STEADY. IAW POM, DISCONNECTED RT GEN DRIVE. APU STARTED AT FL310. REMOVED AND REPLACED RT IDG. RUNUP AND OPS CHECK OK.SDR CA010404011Fitting · cracked(CAN) DURING INSPECTION OF NR 2 RT PYLON, THE MIDSPAN FITTING FOUND CRACKED BETWEEN FASTENERS. NR 2 ENGINE REMOVED AS PER WORK CRD 71125-2. NR 2 PYLON REMOVED AS PER WORK CARD 54102-2 FROM AIRCRAFT FOR REPAIR. NR 2 MIDSPAN FITTING RELACED AS PER ENGINEERING VASDR AUS20011453Compressor · cracked(AUS) HPC ROTOR SPOOL 3-9 GAVE CRACK INDICATIONS DURING ULTRASONIC INSPECTION IAW EI GEN-072-1792R05. FURTHER INSPECTION AT MANUFACTURER FOLLOWING ENGINE STRIP COULD NOT CONFIRM THE CRACKING.SDR AALA20002093Pump · defectiveMIA - FLT 912 - EN ROUTE MIA-LAX, DETECTED AIRCRAFT INTERMITTENTLY OSCILLATING SIDE TO SIDE. OSCILLATION INCREASED DURNIG CLIMB. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE HIGH PRESSURE FUEL PUMP. ACCOMPLISHED LEAK AND POWER ASSUSDR AALA20001785Clamp · looseLHR - FLT 45 - EN ROUTE CDG-JFK, DURING FILGHT LEFT SIDE BLEED DUCT LIGHT ILLUMINATED. PROCEEDED TO SHUTOFF LEFT SIDE ENGINE BLEED AND LEFT SIDE PACK. LEFT SIDE INDICATION TURNED OFF. DIVERTED LHR AND LANDED WITHOUT FURTHER INCIDENT. REPOSITIONED LEFT SIDE
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