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 = 'CF343A1' 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 = 'CF343A1' 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 CA991103077Adc · failed(CAN) FLAP FAIL WHEN SELECTING FLAPS TO 45 DEGREES. FLAPS STOPPED AT 40 DEGREES AT 168 IAS.SDR CA991210028Skin · lightning strike(CAN) LIGHTNING STRIKE ON LEFT SIDE OF FUSLAGE. FOUND LEFT ICE DETECTOR TRAILING EDGE DAMAGE AND EVERY 9-10 INCHES RIVET HEAD BURNT ALL THE WAY BACK TO LEFT WING. BURNS WITHIN LIMITS EXCEPT UNDER WINSHIELD. RIVETS REPLACED.SDR CA991103076Sensor · failed(CAN) FLAP FAIL IN-FLIGHT AT 8 DEGREES. INDICATION ZERO. CHANGE BPSU.SDR CA991103075Flex Shaft · damaged(CAN) FLAP FAIL ON APPROACH AT 190 KNOTS. ZERO DEGREES FLAP LANDING. POWER DRIVE UNIT CHANGED DUE TO HIGH CURRENT DRAW. RIGHT NR 4 FLEXSHAFT DAMAGED. REPLACED. LEFT NR 5 CONDUIT ASSY REPLACED. AD 98-14R1 C/W.SDR SWIA971582Bpsu · failedCLIMBING THROUGH 22,000 FEET, FLAPS FAIL MESSAGE ON EICAS. CYCLED CIRCUIT BREAKERS PER MAINTENANCE CONTROL WITH NO CHANGE. RETURNED TO SLC AND LANDED O FLAPS, (FLAPS FAILED AT 0 DID NOT OPERATE FLAP SELECTOR). REMOVED AND REPLACED LEFT BRAKE POSITION SENSORSDR CA991103073Ecu · failed(CAN) DURING TAXI FLAPS FAIL MESSAGE CAME ON. UNABLE TO RESET. FECU REPLACED AND BPSU.SDR CA991028046Actuator · failed(CAN) FLAPS FAILED ON APPROACH. NR 3 ACTUATOR AND NR 5 LEFT ACTUATOR REPLACED.SDR CA991103074Te Flap · failed(CAN) FLAP FAIL ON APPROACH. RESET CARRIED OUT SERV.SDR CA030417004Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.SDR AU991028042Valve · failed(AU) LEFT COWL ANT-I ICE FAILED. COWL ANTI-ICE VALVE REPLACED.SDR CA991028043Sensing Unit · failed(CAN) FLAPS FAIL ON APPROACH AT ZERO DEGREES. NR 5 FLEX SHAFT AND RIGHT BRAKE SENSOR REPLACED.SDR COMA9960532Engine · vibrationRIGHT HAND ENGINE N1 VIB 2.7 ABOVE LIMITS. BALANCED ENGINE TO ACCEPTABLE LIMITS.SDR COMA9960534Engine · failedRIGHT HAND ENGINE FAILED AFTER TAKEOFF (IFSD). REPLACED THE RIGHT HAND ENGINE.SDR COMA9960537Engine · failedIDG NR 2 CAUTION MESSAGE, FOLLOWED BY GEN NR 2 CAUTION MESSAGE ON TAKEOFF. IDG NR 2 CAUTION MESSAGE WENT OUT DURING ABORT. NR 2 GEN WAS RESET. FOUND SKYDROL IN ACCESSORY GEARBOX OF RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE.SDR CA991008023Wire · failed(CAN) FLAP FAILED ON DESCENT. BROKEN WIRE ON BPSU IN WHEELWELL. REPAIRED.SDR COMA9960511Engine · failedDURING CRUISE FLIGHT AFTER DEPARTING FROM IAD, THE HOT WARNING ACTIVATED FOR THE RIGHT ENGINE, THE RIGHT ENGINE WAS SHUTDOWN INFLIGHT AND AIRCRAFT CONTINUED DESTINATION FLIGHT TO CVG WHERE AN EMERGENCY WAS DECLARED. FOUND THE RIGHT ENGINE CONTAMINATED WITH MSDR COMA9960497Spring · brokenWHILE PERFORMING A MAINTENANCE SERVICE CHECK 50 HOUR INSPECTION MECHANIC FOUND A BROKEN BLOCKER DOOR (P/N 228-50219-111) ON THE LEFT ENGINE THRUST REVERSER, VISIBLE FROM THE GROUND. FURTHER INVESTIGATION FOUND PROBABLE CAUSE TO BE TWO BROKEN RETURN SPRINGS (PSDR COMA9960493Engine · failedOILY SMELL FROM LEFT HAND ENGINE BLEED AIR. REPLACED ENGINE.SDR COMA9960484Engine · failedLEFT ENGINE ITT 880 DEGREES, VIB 4.0 IFSD. REPLACED LEFT HAND ENGINE.SDR COMA9960485Engine · failedTHICK OILY SMOKE IN COCKPIT FROM THE AIRCRAFT SYSTEM. REPLACED THE LEFT ENGINE.SDR CA991104009Transmitter · failed(CAN) AILERON POSITION TRANSMITTER ARM INCORRECTLY INSTALLED WHICH CAUSED THE ARM TO RUB ON AILERON CABLE.SDR COMA9960479Exhaust Frame · crackedRIGHT HAND LOW OIL PRESSURE. REPLACED CRACKED EXHAUST FRAME.SDR COMA9960466Seal · failedCREW REPORTED OIL SMELL FROM LEFT PACK WITH 10TH STAGE BLEED OPEN. CHANGED NR 3 CARBON SEAL ON LEFT ENGINE, PERFORMED COMPRESSOR WASHES. NO SMELL NOTED.SDR COMA9960459Engine · leakingAFTER ENGINE WAS CHANGED, AN OIL SMELL WAS NOTED IN COCKPIT WITH LEFT 10TH STAGE BLEED OPEN DURING GROUND RUNS. REMOVED ENGINE (LEFT) (S/N 807070) AND INSTALLED (S/N 807255).SDR CA990927081Actuator · failed(CAN) FLAP FAIL MESSAGE ON FINAL AFTER FLAPS APPEARED TO REACH 45 DEGREES. FLAP FLEX SHAFTS INSPECTED, LUBRUCATED. NR 3 RT ACTUATOR REPLACED AND SYSTEM RIGGED.SDR CA990927076Ecu · failed(CAN) ON APPROACH, FLAPS SELECTED FROM 8-20, LT FLAP STOPPED AT 13 AND RT AT 14. REPLACED FLAP SYSTEM ELECTRONIC UNIT AND RT BRAKE.SDR CA990916005Engine · failed(CAN) HIGH VIBRATIONS.SDR COMA9960413Engine · failedOIL SMELL IN COCKPIT DURING FLIGHT. REPLACED LEFT ENGINE.SDR SWIA971539Seal · leakingUPON DEPARTURE, NOSE GEAR INDICATION DOWN AND LOCKED AFTER SELECTING GEAR UP. COMPLIED WITH CHECK LIST AND LOWERED GEAR. RETURNED TO FAT, MEL 32-30-1. REMOVED AND REPLACED NOSE GEAR STRUT TEE SEAL AND SERVICED NOSE STRUT. LEAK CHECKS OK IAW 32-21-00. SWUSDR CA990812032Window · cracked(CAN) TWO LARGE CRACKS NOTICED AFTER TAKEOFF IN LOWER CORNER OF LEFT WINDOW.SDR CA990812030Apu · leaking(CAN) AFTER APU START, STRONG SMELL IN COCKPIT AND SMOKE SMELL IN CABIN. LAVATORY SMOKE DETECTOR WENT OFF ONCE. AIRCRAFT AT GATE. APU OIL LEAKING INTO BLEED AIR SYSTEM. APU CHANGED AND COALESCER BAGS CLEANED.SDR CA990812031Bpsu · failed(CAN) FLAPS FAILED AT 20 DEGREES AFTER TAKE-OFF. BPSU CHANGED ON LEFT SYSTEM.SDR CA990812029Ecu · failed(CAN) FLAP FAILED AT ZERO DEGREES. FLAP ELECTRONIC CONTROL UNIT POTENTIOMETER NR 1 AND NR 8 ADJUSTED.SDR CA990812027Ecu · failed(CAN) FLAPS CAUTION LIGHT ON WITH FLAPS AT 30 DEGREES, BUT SELECTED TO 45. FLAP ELECTRONIC UNIT AND FLAP CONTROL LEVER REPLACED.SDR JBXA9900091Priorty Valve · inoperativeGEAR DISAGREE, 2 NOSE OPEN DOOR MESSAGES ON GEAR RETRACTION. REMOVED AND REPLACED HYDRAULIC PRIORTY VALVE IAW CL-65 MM 32-33-15. PERFORMED FUNCTIONAL CHECK ON PRIORTY VALVE IAW CL-65 MM 32-30-00. OPERATIONAL CHECK GOOD.SDR COMA9960393Pin · shearedCREW REPORTED MAIN CABIN DOOR IS VERY HARD TO OPEN AND THAT DOOR HANDLE SEEMS TO GET STUCK WHEN PULLING UPWARD ON HANDLE. WHILE TROUBLESHOOTING THE DOOR HANDLE (P/N 600-31887-11 ITEM NR 5 PAGE 1 FIG 1 RJ IPC CH 52-11-02) FOUND THE PIN (HSP 115BO94-900 ITEM NRSDR COMA9960360Wire Harness · looseAFTER TAKEOFF, RIGHT ENGINE ROLLED BACK AND THEN SURGED 10 PERCENT. SECURED LOOSE WIRING HARNESS AT FUEL CONTROL UNIT.SDR SWIA971514Seal · failedAFTER DEPARTURE AIRCRAFT MAIN DOOR HAD LOUD SQUEAL AND AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO SLC. REMOVED AND REPLACED CABIN DOOR SEAL IAW SB 601R-52-067. PRESSURIZED AIRCRAFT AND ALL CHECKS GOOD.SDR SWIA971515Pin · not removedGEAR DISAGREE ON DEPARTURE FROM SLC. BURNED FUEL DOWN TO LANDING WEIGHT AND RETURNED TO SLC. FOUND GEAR PIN IN NOSE GEAR. REMOVED PIN.SDR SWIA971516Sensing Element · looseON CLIMB-OUT RIGHT 14TH DUCT MSG ILLUMINATED. FOLLOWED QUICK REFERENCE HANDBOOK AND LIGHT EXTINGUISHED WHEN RIGHT 14TH BLEED VALVE WAS CLOSED. RETURNED TO SLC. TORQUED RIGHT 14TH STAGE DUCT SENSING ELEMENT IAW MM 36-21-00. OPS CHECKS GOOD AT THIS TIME.SDR CA990707070Hose · cracked(CAN) IN-FLIGHT, NR 2 SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. HOSE FOUND CRACKED.SDR CA990715034Mfc · failed(CAN) ENGINE WOULD NOT DECELERATE TO IDLE, WITH THE THRUST LEVER AT THE IDLE STOP THE ENGINE PARAMETERS REMAINED AT N1 66, ITT 570, N2 82, FF 400. MFC REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR CA990715039Trim Panel · failed(CAN) RUDDER TRIM RUNAWAY ON OPERATION OF RUDDER TRIM. DRILL COMPLETED/OPERATES NORMAL. TRIM PANEL REPLACED.SDR CA990719018Frame · cracked(CAN) FUSELAGE STATION 718.0, STRINGERS 10-12 FOUND CRACKED ON BOTH SIDES OF FUSELAGE.SDR CA990719019Frame · cracked(CAN) FUSELAGE STATION 718.0, STRINGERS 10-12 FOUND CRACKED ON BOTH SIDES OF FUSELAGE.SDR CA990719017Torque Tube · out of rig(CAN) DOOR WARNING LIGHT ON IN-FLIGHT. TORQUE TUBE UPPER LATCH CAMS FOUND OUT OF RIG.SDR SWIA971502Service Panel · not closedON TAKEOFF, ADC NR 2 FAILED. SHORTLY THEREAFTER A LOUD VIBRATION COULD BE HEARD AND FELT IN THE COCKPIT. RETURNED TO SLC. FOUND OXYGEN SERVICE PANEL UNLATCHED CAUSING A DISTURBANCE IN AIRFLOW TO THE NR 2 PITOT TUBE. PERFORMED INSPECTION OF O2 SERVICE PANELSDR SWIA971510Service Door · not closedAFTER TAKEOFF, A VERY LOUD SQUEAL WAS HEARD ALONG WITH IAS STALL FAIL, MACH TRIM AND EFIS COMP. RETURNED TO SLC. SECURED OXYGEN SERVICE DOOR IN FRONT OF RIGHT PITOT TUBE. ALL SYSTEMS FUNCTION NORMAL.SDR COMA9960250O Ring · cutRIGHT HAND ENGINE LOW OIL PRESSURE WARNING. REPLACED THE ENGINE DRIVER HYDRAULIC PUMP DRIVE PAD O-RING.SDR SWIA971497Indication · malfunctionedNOSE GEAR DISAGREE WARNING LIGHT AFTER GEAR RETRACTION. NOSE GEAR LIGHT STAYED GREEN. PERFORMED GEAR SWING IAW MM 32-30-00, NO PROBLEMS FOUND. COULD NOT DUPLICATE DISCREPANCY.
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