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 = 'CT75A2' 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 = 'CT75A2' 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 CA110509004Line · twisted(CAN) UPON PERFORMING LC-2 INSPECTION, MAINTENANCE FOUND FUEL LINE TWISTED ON LT ENGINE LOWER NACELLE.SDR CA110411005Oil System · leaking(CAN) DURING LEVEL CRUISE FLIGHT, IT WAS NOTED THAT THE NR 2 ENG PARAMETERS BEGAN TO FLUCTUATE & AN INCREASE IN ITT WAS OBSERVED. THE POWER LEVER WAS PULLED BACK TO REDUCE THE TEMP & THE TORQUED REDUCED FROM 80% TO 40%. THE POWER WAS ADJUSTED AGAIN TO STABILSDR CA100301003Hinge Pin · cracked(CAN) OTBD ELEVATOR HINGE PIN BRACKET FOUND CRACKED AT THE FLANGES THAT HOLD THE BOLT THAT HOLDS THE ELEVATOR HINGE PIN. THIS IS DUE TO OVERTIGHTENING THE BOLT WHICH BENDS THE TABS, WHICH EVENTUALLY CRACKS THE TABS.SDR 2010F00017Engine · overtempON JAN. 18, 2010 WHILE IN CRUISE FLIGHT, THE CREW NOTICED THE ENG OIL PRESSURE DROPPING, AND GOT THE MASTER WARNING LIGHT FOLLOWED BY AN OVERTEMP LIGHT AS WELL AS A CHIP DETECTOR LIGHT. THE CREW IMMEDIATELY SHUTDOWN AND SECURED THE ENGINE. THE FLIGHT WAS THEN SDR 2010F00020Gearbox · failedWHILE IN CRUISE AT FLT LVL 210, PIC NOTICED THAT RT PROPELLER GEARBOX OIL PRESSURE WAS LOW FOLLOWED IMMEDIATELY BY THE MASTER WARNING LIGHT. THE PILOT IMMEDIATELY SHUTDOWN AND SECURED ENGINE AND CONTINUED TO DESTINATION AND LANDED UNEVENTFULLY. UPON LANDING ISDR OZCA060809001Latch · defectiveON DEPARTURE FROM MIA THE PILOT NOTED THE LT ENGINE COWLING HAD POPPED OPEN AND WAS COLLAPSED AGAINST THE ENGINE. POWER TO THE AFFECTED ENGINE WAS REDUCED AND A UNEVENTFUL LANDING IN MIA WAS PERFORMED. MX INSPECTED THE AIRFRAME , ENGINE AND COWLING AND SUSPESDR CA090305004Limiter · faulty(CAN) MX CREW HAD AN ISSUE WITH THE RUDDER LIMITER UNIT. THEY FOUND THE UNIT TO HAVE 3 BURNED TRANSISTORS ON THE CIRCUIT BOARD. P/N OF THE RUDDER LIMITER UNIT IS (9121836-10-4). THE FAULTY UNIT HAD A STICKER STAMPED WITH THE DATE,1988 ON IT. THE ACTUAL TIME INSDR CA081212005Blade · cracked(CAN) THE PROP IN QUESTION WAS REMOVED FOR DISASSEMBLY TO BE SENT FOR DELAMINATION BEYOND LIMITS TO THE MANUFACTURER. WHEN THE PROP ASSEMBLY WAS DISASSEMBLED, A RADIAL CRACK WAS DISCOVERED IN NR 2 BLADE MEASURING IN EXCESS OF 6 INCHES IN THE HUB OF THE BLADE SDR CA081210015Pressure Switch · malfunctionedHYD PRESSURE SWITCH CONTROLLING THE HYD PUMP WOULD NOT ACTUATE THE PUMP UNTIL THE HYD PRESSURE DROPPED BELOW 1900 PSI. THE HYD PRESSURE WARNING LIGHT ILLUMINATED AT 2100 PSI. THIS IS THE SECOND SWITCH TO FAIL AS THE PREVIOUS ONE HAD 196 HOURS ON IT. THE BATCSDR CA080916001Swivel Fitting · sheared(CAN) AFTER TAKE-OFF, DURING GEAR RETRACTION, THE RT MLG DOWNLOCK ACTUATOR SWIVEL FITTING LOCATED ON THE DRAG BRAC, FAILED. THIS CAUSED A SUBSTANTIAL LOSS OF FLUID. AN EMERGENCY GEAR EXTENSION WAS CARRIED OUT AND THE ACFT RETURNED TO BASE WITH NO FURTHER PROBSDR CA080826004Strut · contaminated(CAN) AFTER TAKEOFF CHECKS COMPLETED AND CONDITION LEVER RETARDED, RESULTING IN CONFIG WARNING AND OAT LIGHT ILLUMINATING. THIRD OCCURANCE. UNSCHEDULED LANDING MADE. (FUEL BURNED OFF TO ACCOMODATE LANDING WEIGHT) THE LT MLG WAS NOT FULLY EXTENDED DUE TO AIR RESDR CA080826005Squat Switch · out of rig(CAN) AFTER TAKEOFF CHECKS WERE COMPLETED AND CONDITION LEVERS RETARDED, CONFIG WARNING AND OAT LIGHT CAME ON. UNSCHEDULED LANDING COMPLETED, RETURNED TO BASE. GEAR SWING COMPLETED, FAULT NOT DUPLICATED. LANDING GEAR HAD BEEN SERVICED PRIOR TO FLIGHT. RE-SERVISDR CA080826003Unknown · unknown(CAN) GPU VOLTAGE SPIKED WHILE PROVIDING POWER FOR ENGINE START. GROUND POWER WAS SHUT OFF AND ENGINES STARTED USING INTERNAL BATTERIES. BOTH ESSENTIAL DC ELECTRICAL CBS FOUND TRIPPED WHILE PERFORMING TAXI CHECK LIST. RETURNED TO GATE.SDR CA080715004Shaft · sheared(CAN) RT AC GENERATOR FAIL LIGHT ILLUMINATED IN FLIGHT, SYSTEM WAS DEFERRED AS PER THE MEL. WHEN ACFT WAS AT A MX BASE, THE AC GENERATOR WAS REMOVED AND FOUND TO HAVE A SHEARED SHAFT. GENERATOR WAS REPLACED. NO FURTHER ISSUES.SDR CA080711001Fan · overheated(CAN) ON JULY 8/2008, SHORTLY AFTER TAKEOFF THE CREW NOTICED AN ELECTRICAL ODOR WHICH WAS ALSO CONFIRMED BY THE F/A. THE CREW DECLARED AN EMERGENCY AND PROCEEDED TO LAND WITHOUT INCIDENT. MX WAS DISPATCHED TO THE ACFT WHERE IT WAS NOTICED THAT WHEN THE FLIGHT SDR CA080625003Pipe · cracked(CAN) ON TAKE OFF ROLL WITH THE CTOT ENGAGED, THE NR1 ENGINE TEMP INCREASED TO 900 DEGREES AT A TORQUE OF 60 PERCENT. THE CREW REDUCED ENGINE POWER AND AT THIS TIME THEY DID HAVE A STEADY DECREASE IN ENGINE TEMP. THE ACFT RETURNED TO THE RAMP AND MAINT WAS DISSDR OZC2008F00000Swivel · brokenPILOT NOTED THE HYD LIGHT ON DUE TO LOSS OF PRESSURE IN MAIN ACCUMULATOR AND HYD QUANTITY READING ZERO. PERFORMED AN EMERGENCY GEAR EXTENSION IAW QRH AND HAD AN UNEVENTFUL LANDING. MAINT INSPECTED THE AC AND FOUND THE HYD SWIVEL IN THE RT MAIN GEAR WELL PN LSDR CA080227001Bearing · failed(CAN) CABIN CREW NOTED AN ABNORMAL ODOR IN THE CABIN AND ADVISED THE COCKPIT CREW. IT WAS DECIDED TO LAND AT THE CLOSEST AIRPORT AS A PRECAUTION. PRIOR TO LANDING THERE WERE SEVERAL WISPS OF SMOKE OBSERVED IN THE FLOOR/SIDEWALL AREA. THE AC LANDED UNEVENTFUL. SDR CA070801006Light · overheated(CAN) CABIN OVERHEAD FLOURESCENT LIGHTING FIXTURE OVERHEATED. BURNED OUT BULB FOUND AND CONTACTS IN FIXTURE THAT CONDUCT ELECTRICITY TO BULB FOUND LOOSE AND OVERHEATED, CAUSING PLASTIC PART OF ASSY TO OVERHEAT. PARTS REPLACED AND A/C RELEASED TO SERVICE WITHOSDR NSVA20070173Warning Light · false indicationABORTED TAKEOFF 70KTS, LT ENGINE OIL MASTER WARNING LIGHT ILLUMINATED. RAN LT ENG AT 80 PERCENT TORQUE FOR 30 MIN, AFTER CHECK OIL LEVEL AND VERIFIED IT WAS FULL. RECHECK OIL AFTER RUN AND OIL LEVEL DID NOT DROP FROM FULL LINE, PRIOR TO FIRST ENG RUNS SERVICSDR NSVA20070157Control Quadrant · defectiveFI STOP OPEN LIGHT ILLUMINATED IN FLIGHT. REPLACED CONTROL QUADRANT IAW SAAB AMM 76-10-05, NO DISCREPANCIES NOTED, PN ON: 53162-4, SN ON: 074, PN OFF: 53082-16 SN OFF: 187.SDR NSVA20070078Wire · brokenLEFT TORQUE READS "0" WHEN POWER IS APPLIED. ALSO FLUCTUATES AT TIMES, NOTE: AFTER APPROX 15 MINUTES RUNNING. INSPECTED LT TORQUE SENSOR AND LT ALTERNATOR UNITS FOR SECURITY AND PROPER INSTALLATION, NO OBVIOUS FAULT FOUND, REJECTED TAKEOFF. INSPECTED AND PESDR PSNA070303Pressure Switch · malfunctionedPILOT ABORTED TAKEOFF DUE TO ENGINE OIL PRESSURE LOW MASTER WARNING LIGHT RETURNED TO GATE. REMOVED AND REPLACED ENGINE OIL PRESSURE DIFFERENTIAL SWITCH.SDR NSVA20070047Stop · malfunctionedFLIGHT IDLE STOP HAD TO BE OVERRIDDEN DURING LANDING ROLL OUT. RESET FLIGHT STOP WITH F1 REST TOOL. OPS CHECK GOOD.SDR NSVA200600222Oil System · unknownLEFT ENGINE OIL PRESS LIGHT ILLUMINATED DURING TAKEOFF AT 115 KNOTS. C/W SEI 576 72-00-00 LOW OIL LEVEL CLEARING PROCEDURES CWC 79-11-07S INSP AND CLEANING POWER UNIT SCAVENGE SCREENS, CWC 79-11-06/1S LT POWER UNIT CHIP DETECTOR, OIL CONSUMPTION RUN WITHIN LISDR CA061117007Pdu · failed(CAN) WHEN GROUND POWER WAS ATTACHED TO THE AIRCRAFT THE LT ENGINE BEGAN AN UNCOMMANDED START SEQUENCE. THE FAULT WAS TRACED TO THE LT STARTER RELAY CONTACTS LOCATED IN THE LT POWER DISTRIBUTION UNIT (PDU). THE PDU WAS REPLACED AND THE AIRCRAFT OPERATED NORMSDR CA061016003Clamp · cracked(CAN) ENGINE CONTROL CLAMP FOUND CRACKED ON ENGINE INSPECTION. REFERENCE AIRCRAFT IPC 71-00-02 FIG 15, ITEM NR 6 THE PART WAS NOT IDENTIFIED BY A SPECIFIC PN MARKED ON THE CLAMP. SUSPECT POSSIBLE UNAPPROVED PART PREVIOUSLY INSTALLED. (TC NR 20061016003)SDR CA061130003Element · chafed(CAN) AIRCRAFT RETURNED TO BASE SHORTLY AFTER DEPARTURE DUE TO A NR 2 BLEED AIR LEAK LIGHT ILLUMINATION DURING CLIMB OUT. THE BLEED AIR WAS SELECTED OFF BUT THE LIGHT REMAINED ILLUMINATED. IAW THE REQUIRED PROCEDURES THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT LASDR 05092006BScavenge Pump · malfunctionedRT ENGINE OIL TEMP IN RED, OIL PRESSURE 50 PSI. ALL OTHER INDICATIONS NORMAL. ON LANDING RT ENG WAS SHUTDOWN. DATA OBTAINED FROM FDR INDICATES ENGINE SHUTDOWN BY FUEL FLOW. PILOT RETARDING CONDITION LEVER TO FUEL CUT-OFF POSITION. MX DETERMINED RT ENG HIGH OISDR AU510001806Power Cable · separatedLT ENGINE POWER CABLE SEPARATED IN AREA LOCATED BETWEEN WHEEL WELL AND CABLE TERMINAL PULLEY SECTOR.SDR SF20051023Engine · surgesFLIGHT 7591 IAD-PIT ABORTED TAKEOFF AT 100 KNOTS DUE TO LT ENGINE SURGING. DEFERRED CTOT, CONT OPS PER MEL 76-10-1, CONTROL 3150, CAT C, DDD 11/02/05. RTO INSPECTION DUE FOR ABORTED T/O AT 100 KNOTS. C/W RTO INSPECTION IAW M/M 05-50-00-6 PROCEDURE NR 3, NO SDR SF200508161Engine · malfunctionedFLT NR 7558 FROM IAD-ABE, AIRCRAFT WAS EN ROUTE TO ABE IN CRUISE AT 75 PERCENT WHEN ENGINE WENT TO 101 PERCENT. AIRCREW PULLED POWER BACK TO 35 PERCENT PUT INTO TORQUE MOTOR LOCKOUT AND EVERYTHING STABILIZE. CONTINUED SAFELY TO ABE.SDR SF200508121Battery · odorVERY STRONG ELEC ODOR COMMING FROM COCKPIT BATTS/EXT POWER AND AVIONICS ON, MFD C/B G18 POPPED AFTER 30 SECS OF NOTICING ODOR. CONTRACTED MAINTENANCE, PULLED AND CAPPED C/B. MAINT CONFIRMED SMELL COMING FROM MFD.SDR SF20050730Engine · overtempFLT NR 7531 FROM CRW TO IAD, ON TAKEOFF ROLL, NR 1 ENGINE OVERTEMP. TEMP REACHED 933 FOR APPROX 2 SECONDS. AIRCREW REJECTED TAKEOFF AND RETURNED TO GATE.SDR SF20050726Engine · malfunctionedFLT 7539 IAD-DAY STARTED NR 1 ENGINE NORMALLY, AFTER TURNING ON NR 1 GENERATOR, LT ITT INCREASED TO 1068, MOTORED NR 1 ENGINE DOWN & SHUTOFF NR 1 GENERATOR.SDR SF20050717Engine · shutdownFLT 7574 FROM BGM TO IAD, 7-17-2005. ON CLIMBOUT, AIRCRAFT HAD AN UNCOMMANDED REDUCTION IN NR 1 PROP'S RPM. AIRCREW FOLLOWED QRH AND PUT INTO TORQUE MOTOR LOCKOUT. THE REDUCTION CONTINUED. AIRCREW CONTINUED TO FOLLOW QRH AND SHUT THE ENGINE DOWN AND RETURNED TSDR SF2005071505Engine · oil consumptionRIGHT ENGINE OIL PRESSURE LIGHT COMING ON FREQUENTLY IN FLIGHT, 30 PSI & SLIGHT FLUCTUATIONS STARTED COMING ON MORE FREQUENTLY. DECLARED EMERGENCY & MADE A PRECAUTIONARY LANDING IN PIT, WARNING WENT OFF 63 TIMES. FOUND NR 2 ENGINE OIL LEVEL LOW, SERVICED OILSDR SF20050708Warn Panel · fire warningAT 2000 FT RT ENGINE CENTRAL WARNING PANEL RED FIRE LIGHT CAME ON AND FIRE BELL SOUNDED. DISCHARGED 1 BOTTLE AND SHUT DOWN ENGINE IAW QRH. ESTIMATED LANDING WEIGHT 27,000 LBS. AIRCRAFT RETURNED AND IS AWAITING MAINTENANCE.SDR 20050627SFWarn Panel · fire warningON CLIMB-OUT, AIRCREW RECEIVED FIRE INDICATION ON NR 2 ENGINE. AIRCREW RETURNED.SDR CA050613007Swivel Fitting · failed(CAN) DURING DEPARTURE, LT MAIN WHEEL AND NOSE GEAR RETRACTED NORMALLY BUT RT MAIN GEAR WOULD NOT RETRACT. CREW OBSERVED HYDR FLUID LEVEL AND OPERATING PRESSURE INDICATED LOW. EMERGENCY GEAR EXTENSION AND AFTER ORBITING TO REDUCE FUEL LOAD, RETURN FOR A LANDSDR AU510001958Engine · shutdown(AUS) RT ENGINE PARAMETERS DECREASED AND ENGINE SHUTDOWN. EXTENSIVE INVESTIGATION COULD FIND NO CAUSE FOR THE SHUTDOWN. THE AIRCRAFT WAS RETURNED TO SERVICE AND HAS OPERATED WITHOUT FURTHER INCIDENT. (OTHER CAUSE: UNKNOWN ) (CASA NR 510001958)SDR 249312Warning Light · illuminatedON 03-18-2005, APPROX 1700 (UTC), FLT 7886 SCE-IAD, AIRCRAFT N158SD DEPARTED SCE. AT ROTATION SPEED CREW HAD OBSERVED A NOSE GEAR SHOWED UNSAFE.SDR 071711Eec · malfunctionedLEFT ITT WAS 60 DEGREES HIGHER THAN RIGHT ON TAKEOFF. DURING CLIMBOUT LEFT ITT CONTINUED CLIMBING TO 100 DEGREES DIFFERENCE. UNABLE TO MAKE CHARTED TQ ON LT ENGINE BY 30 PERCENT. ALL OTHER INDICATIONS NORMAL. AIRCRAFT RETURNED TO IAD AND MAINTENANCE REPLACSDR 243733Ecu · failedLEFT ENGINE ERRATIC TQ FLUXUATES, ENGINE OVERTEMPS MULTIPLE TIMES. ENGINE SHUT DOWN MANUALLY. REMOVED AND REPLACED ECU, IAW GE CT7 M/M 74-00-00, GROUND RAN 45 MINS IAW GE CT7 M/M 71-00-00-5. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.SDR 225922Control Panel · inoperativeRT MLG, GREEN GEAR LIGHT INOP. WILL NOT TEST, CHANGED BULBS STILL NO FIX, LANDED PER QRH. INSPECTED AND FOUND LANDING GEAR HANDLE CONTROL PANEL TO BE INOP. REMOVED AND REPLACED LANDING GEAR HANDLE CONTROL PANEL IAW SAAB AMM 32-31-05-2, OPS CHECK AND GEAR SWSDR 155122Swivel · crackedFLT 7925, DURING TAXI TO RUNWAY, HYDRAULIC LIGHT ILLUMINATED, HYDRAULIC PUMP RAN CONT, HYDRAULIC QTY ON THE MAIN AND OB WENT TO 0, BIG 1800 PSI, EMERGENCY 2500 PSI. INSPECTED AND FOUND RT OB BRAKE SWIVEL TO BE CRACKED. REMOVED AND REPLACED RT BRAKE SWIVEL, LSDR CA041021001Powerplant · failed(CAN) ENG FLAMED OUT AT 13,000 FT DURING DESCENT WHEN THEY TRIED TO REAPPLY HIGHER POWER & RESTARTED SUCCESSFULLY AFTER FOLLOWING PROCEDURES. ACRFT LANDED. MX DISPATCHED, EVALUATION CARRIED OUT IAW GE MM. INTERNAL ENG INSPECTED NO FAULT FOUND, EXTERNAL INSPECTSDR 226121Warning Light · illuminatedON 09-30-04 APPROX 2105 (UTC), FLT 7891 IAD-ORF, DURING APPROACH, CREW OBSERVED RT ENGINE OIL LIGHT ON THE CWP AND NOTICED A OIL PRESSURE AROUND 30 PSI. FLIGHT LANDED WITHOUT INCIDENT.SDR CA041021006Hmu · failed(CAN) FOLLOWING A SCHEDULED ENGINE CHANGE AND DURING COMPLETION OF THE GROUND RUN OPERATIONAL CHECKS, THE BOTTOM GOVERNING FUNCTION OF THE ENGINE COULD NOT BE ENABLED. THE HMU WAS REPLACED AND RETURNED TO THE MANUFACTURER FOR INSPECTION AND REPAIR. THE SHOP RESDR CA041021007Hmu · failed(CAN) DURING COMPLETION OF ENGINE GROUND RUNS AFTER AN ENGINE CHANGE, THE ENGINE BOTTOM GOVERNING FUNCTION COULD NOT BE CONSISTENTLY ENABLED AS REQUIRED BY THE CHECK. IT WOULD INTERMITTENTLY FAULT TO A LOWER THAN SELECTED RPM. THE HMU WAS REPLACED AND SENT TO
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