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 = 'CF650C2' 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 = 'CF650C2' 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 CA970904015Gen Control Unit · failed(CAN) GENERATOR OFF LIGHT CAME ON IN FLIGHT, AFTER 10 SECONDS ELAPSED THE LIGHT EXTINGUISHED. CYCLE REPEATED UNTIL THE GENERATOR SWITCH SELECTED TO OFF. THE GENERATOR CONTROL UNIT AND LOAD CONTROLLER WERE REPLACED.SDR CA970909005Midframe · cracked(CAN) ON DESCENT, NOTICEABLE BUZZ IN NR 1 ENGINE FUEL LEVER AND SOFTER BUT STILL NOTICEABLE BUZZ FROM NR 1 FIRE HANDLE. TURBINE VIBS INCREASED TO 4.5 UNITS. TURBINE CASE CRACKED 12-1 O'CLOCK POSITION 12 INCHES LONG. HEAT SHIELD ABOVE CRACK MISSING FROM PYLOSDR 97UAL900673Rib · crackedDURING C-CHECK EDDY CURRENT INSPECTION, CRACKS WERE FOUND IN THE LEFT HAND OUTBOARD FLAP CLOSING RIB ASSEMBLY. LEFT HAND OUTBOARD FLAP CLOSING RIB REPLACED.SDR CALA9701213Bolt · failedNR 2 ENG FIRE WARNING ACTIVATED AFTER T/O. FUEL WAS DUMPED AND THE ACFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENG WAS REMOVED AND REPLACED. A POWER ASSURANCE RUN WAS PERFORMED AND ALL PARAMETERS WERE NORMAL. *S/D* ENG DISASSEMBLY SDR 97UAL900610Fitting · crackedTHE NR 1 PYLON RIGHT-HAND TRUSS FITTING IS CRACKED. THE CRACKS PROPAGATE FROM THREE FASTENER HOLES. THE CRACKS ARE NOT CONTINUOUS AND DO NOT EXTEND INTO FILLET RADIUS. *S/D* INSTALLED INTERIM REPAIR PER EVA SFO-1503 AND ALERT BULLETIN A54-99/A54-103. THE SDR 97UAL900612Longeron · corrodedLONGERON 52 AND LONGERON 51R WERE FOUND WITH EXTENSIVE CORROSION DAMAGE AT BODY STATION 879. THE DAMAGE WAS DETECTED BY DISHED FASTENERS AND QUILTING OF THE SKIN. EACH LONGERON REQUIRED A 14.0 SECTION TO BE REMOVED AND REPAIRED. ACCESS TO THE AREA WAS OBTAISDR CA970731006Check Valve · wrong pos(CAN) NR2 ENGINE FLAMED OUT DUE TO NR1 TRANSFER PUMP TURNED OFF DURING FUEL IMBALANCE MANAGEMENT. NR1 TRANSFER PUMP CHECK VALVE OPERATING UNDER MEL 28-06 WHICH REQUIRES THE TRANSFER PUMP TO BE ON AT ALL TIMES MANIFOLD IS PRESSURIZED. ENGINE RESTARTED AT FL300,SDR AU971643Arm · broken(AUS) NOSE LANDING GEAR LH AFT DOOR ACTUATING ROD BROKEN.SDR AU971656Spring · broken(AUS) LH MAIN LANDING GEAR AFT DOWNLOCK ASSEMBLY AFT OUTER DOWNLOCK SPRING BROKEN AND SPRING LOWER ATTACHMENT FITTING BENT.SDR CALA9701101Carbon Seal · leakingTHE NR 3 ENGINE OIL QUANTITY AND PRESSURE DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF THE OIL LOW PRESSURE LIGHT WHILE EN ROUTE FROM FCO TO EWR. THE NR 3 ENGINE WAS SHUT DOWN, FUEL WAS DUMPED AND THE A/C WAS DIVERTED TO LGW WHERE IT LANDED WITHOUT INCIDENT.SDR 97FDEA00401Engine · flamed outNR 1 ENGINE FAIL AFTER T/O, HIGH EGT 999+, AFTER THROTTLE RETARD FUEL FLOW AND EGT REMAIN EXCESSIVE. WHILE DUMPING FUEL ENGINE FLAMED OUT. RETURNED TO ANC. *S/D* REMOVED AND REPLACED NR 1 ENG AS PER MM 71-00-00-4 RUN UP LC CK NR 1 ENG. ALL CKS OK TDS 9822SDR CA970715003Tire · blown(CAN) AIRCRAFT LANDED WITH ANTI-SKID OFF. BLEW TWO TIRES ON LANDING. 8 OTHER TIRES WORN TO LIMITS. REPLACED 10 TIRES AND TWO BRAKE ASSEMBLIES.SDR G6OA010Engine · failedGVA - AT LIFT OFF, CREW REPORTED A LOUD BANG FOLLOWED BY VIBRATION, N1, AND N2 DECAYING, EGT RISE AND LOW FUEL FLOW INDICATIONS FOR NR 1 ENGINE. TOWER REPORTED LARGE FLAME FROM THE TAIL PIPE. NR 1 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNEDSDR 97UAL900485Battery Pack · dischargedAFT CABIN EMERGENCY LIGHTS FAIL TEST. REPLACED AFT BATTERY.SDR 97UAL900484Reverser · delaminatedON WALK AROUND INSPECTION, FOUND DELAMINATION OF RIGHT HAND SIDE UPPER SIDEWALL ON THE FLOW SIDE OF THE RIGHT REVERSER AT 12:00 O'CLOCK POSITION MEASURING 12 BY 8 INCHES. *S/D* THE DELAMINATION WAS DUE TO MOISTURE INTRUSION THROUGH SEAM. AIRFLOW CAUSED A LASDR WRLA97026Compressor · stalledDURING CLIMB-OUT, FLIGHT CREW EXPERIENCED 3 RAPID COMPRESSOR STALLS ON THE NR 3 ENGINE. FLIGHT CREW RETARDED NR 3 THROTTLE TO FLIGHT IDLE, AND ELECTED TO RETURN TO POINT OF DEPARTURE FOR MAINTENANCE ACTION. ACFT LANDED WITHOUT FURTHER INCIDENT. MX PERFORMESDR 97UAL900462Seal · damagedWHILE TAXIING, AFTER NORMAL LANDING BRAKES LOCKED UP. AFTER 15 MINUTES BRAKES RELEASED AND AIRCRAFT WAS TOWED TO GATE. *S/D* THE AIRCRAFT WAS TOWED WITH THE HYDRAULIC PRESSURE ON. REPLACED DUAL BRAKE CONTROL VALVE SEAL. BRAKE OPERATIONS CHECK NORMAL.SDR 97UAL900463Coupling Seal · wornFUEL RUNNING FROM NR 1 ENGINE PYLON AFT DRAIN TUBE. *S/D* REPLACED PYLON FUEL SUPPLY LINE GAMMA COUPLING SEALS.SDR 97UAL900432Tube · leakingHYDRAULIC FLUID SPRAYING FROM RIGID LINE FOR BRAKE CONTROL VALVE IN RIGHT WHEEL WELL. *S/D* DURING INSPECTION FOUND PIN HOLE LEAK AT THE BEND RADIUS. REPLACED SECTION OF TUBE ASSEMBLY.SDR WRLA97024Engine · oil lossDURING CRUISE, FLT CREW NOTED THAT NR 3 ENGINE OIL QTY WAS FALLING. FLIGHT CREW ELECTED TO DIVERT AIRCRAFT FOR MAINTENANCE INVESTIGATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL WERE UNABLE TO DETERMINE CAUSE OF LOSS. THERE WAS NO ESDR CALA9700822Fuel Filter · contaminatedNR 3 ENG FLAMED OUT WHILE DESCENDING THRU FL 220 EN ROUTE. ENG FAILURE WAS ACCOMPANIED BY ILLUMINATION OF BOTH NR 3 GEN OFF LIGHT AND THE NR 3 ENG LOW OIL PRESS LIGHT. ENG WAS RESTARTED, A/C LANDED W/O INCIDENT. INSPECT FOUND THE NR 3 ENG FUEL FILTER AND NRSDR CALA9700809Fire Loop · chafedTHE NR 2 ENGINE FIRE WARNING LIGHT FOR B-LOOP (A LOOP WAS ON PLACARD) ILLUMINATED TEN MINUTES AFTER TAKEOFF. THE NR 2 ENGINE WAS SHUT DOWN, BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FSDR CALA9700768Engine · flame-outTHE NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO FLAME-OUT. A RESTART ATTEMPT WAS UNSUCCESSFUL. THE ABNORMAL CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. THE FUEL PUMP AND MEC WERE REMOVED AND REPLACED. A POWER ASSURANCE RUN WAS PESDR CA970528006Lens · broken(CAN) LIGHTNING STRIKE CAUSED UPPER LENS OF ANTI-COLLISION BEACON TO DEPART AIRCRAFT AND ENTER #2 ENGINE. SEQ. NO.0165665 REPORTED RUMBLING AND AT 90 PERCENT N1 HEAVY VIBRATION FELT. FAN BLADES REPLACED, BORESCOPE INSPECTION CARRIED OUT, NIL INTERNAL DAMAGE FOSDR 97UAL900377Cdp Line · wornDURING TAKEOFF ROLL, NR 3 ENGINE WOULD NOT SPOOL UP BEYOND 70 PERCENT N1. ABORTED TAKEOFF AT 70 KNOTS. ENGINE NR 3 WOULD NOT RESPOND TO THROTTLE MOVEMENT ON TAXI WAY. *S/D* MULTIPLE PROBLEMS WERE FOUND AND CORRECTED. THE DISCREPANCIES THAT MOST LIKELY RESSDR WRLA97017Bleed Valve · failedDURING CRUISE, FLT CREW RECEIVED COCKPIT FIRE WARN ON NR 1 ENG. FLT CREW RETARDED THROTTLE IN FLT, THE FIRE WARN EXTINGUISHED. ADVANCE THROTTLE BACK TO CRUISE POWER, FIRE WARN WAS RECEIVED AGAIN. FLT CREW ELECTED TO SHUTDOWN ENG. BY HF RADIO, FLT CREW CONTSDR G6OA008Oil Line · looseSEL - AFTER TAKEOFF, CREW REPORTED LOSS OF OIL QUANTITY AND OIL PRESSURE FOR NR 1 ENGINE. THE NR 1 ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO SEL AND LANDED WITHOUT FURTHER INCIDENTS. NO EMERGENCY WAS DECLARED. GROUND MAINTENANCE DURING INSPECTION OF NR 1 SDR CALA9700636Compressor · damagedTHE NR 3 ENGINE EXPERIENCED COMPRESSOR STALLS WHILE ENROUTE. THE AIRCRAFT WAS RETURNED TO LGW. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND OPERATION CHECKED GOOD. *S/D* INSPECTION OF THE ENGINE FOUND THAT THE ENTIRE COMPRESSOR HAD SUFSDR 97UAL900348Fuel Inlet Tube · looseNR 1 ENGINE FLAMED OUT ON DECENT AFTER ANTI-ICE TURNED ON. DID NOT RESTART ON RESTART ATTEMPT. DURING INSPECTION, MAINTENANCE FOUND THAT THE FUEL INLET TUBE TO THE FUEL FLOW TRANSMITTER WAS LOOSE AND LEAKING. THE BOLTS THAT ATTACH THE TUBE HAD BACKED OFF SDR 97UAL900341Packing · damagedLANDING GEAR MADE AN EXTREMELY LOUD NOISE WHEN IT WAS LOWERED. A BANG WAS HEARD THROUGHOUT THE AIRPLANE. WHILE TAXIING, BRAKES CHATTERED AT SLOW TAXI SPEEDS. CENTER GEAR WAS FOUND TO HAVE LOST ALL AIR AND FLUID. FOUND CENTER LANDING GEAR DIAPHRAGM PACKINGSDR 97UAL900324O-Ring · damagedNOSE GEAR WILL NOT FULLY RETRACT, RED LIGHT ON. VISUAL INSPECTION SHOWS GEAR DOORS HANGING OPEN ABOUT SIX INCHES. GEAR RECYCLE NO HELP AND AIRCRAFT VIBRATES WITH SPEEDS AT 250 KNOTS. ON GEAR EXTENSION GOT A VERY LOUD BANG FROM NOSE GEAR. *S/D* THE NOSE LASDR CA970421019Squib · no discharge(CAN) INADVERTANT FIRING OF APU FIRE BOTTLE. SQUIB ACTIVATED BUT FAILED TO DISCHARGE EXTINGUISHANT. SQUIB AND BOTTLE SENT TO SHOP FOR FURTHER INVESTIGATION. NEW SQUIB AND BOTTLE ASSEMBLY INSTALLED.SDR 97UAL900265Slat · crackedDURING L-CHECK, 8 BY 12 INCH PIECE OF THE LT NR 1 SLAT WAS FOUND MISSING. THE MISSING SECTION WAS LOCATED ON THE UNDERSIDE OF THE SLAT ALONG THE TRAILING EDGE WEDGE, EXTENDING FROM THE INBOARD EDGE APPROX 12 INCHES. CAUSE OF DAMAGE UNKNOWN. REPAIRED PER SRMSDR CALA9700440Turbine Liner · failedTHE NR 2 MANIFOLD LIGHT AND FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. THE FIRE BOTTLE WAS DISCHARGED AND THE NR 2 ENGINE WAS SHUT DOWN. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/D* SDR 97UAL900234Ceiling Panel · looseCONTROL WHEEL VIBRATING, POSSIBLY DUE TO AILERON OR SPOILER FLOATING AND ELEVATOR IS VERY STIFF. FOUND CEILING PANEL LAYING ON FLIGHT CONTROL CABLES. REINSTALLED PANEL AND ACCOMPLISHED FLIGHT CONTROLS CHECK. ALL O.K.SDR 97UAL900193Hydraulic Pump · failedNR THREE HYDRAULIC QUANTITY DECREASED TO ZERO. DIVERTED TO HNL. 1-3 REVERSIBLE MOTOR PUMP SHAFT BEARINGS FAILED, DAMAGING THE SHAFT SEAL. REPLACED MOTOR PUMP AND ENGINE DRIVEN HYDRAULIC PUMPS ON NR 3 ENGINE. PART TOTAL CYCLES, 4,500.SDR 97UAL900191Engine · failedNR ONE ENGINE FAILED AT 1000 FEET DURING DEPARTURE. NR 1 ENGINE FLAMED OUT IN CRUISE. FUEL PRESSURE DROPPED JUST PRIOR TO FLAME OUT. LABORATORY ANALYSIS HAS SHOWN THAT THE TUBE FAILURE WAS A RESULT OF A LATERAL OVERSTRESS BENDING FORCE, NOT A COMMON FAILUSDR AU970470Fitting · cracked(AUS) RUDDER ACTUATOR HINGE FITTING CRACKED ON OUTER FLANGE RADIUS AND INNER WEBSDR CA970318001Actuator Rod · cracked(CAN) DURING ROUTINE ISOTOPE INSPECTION A CRACK AND CORROSION WAS DETECTED IN THE LT ELEVATOR ACTUATOR ROD. THE POSITION OF THE CRACK DID NOT SHEAR THE SECONDARY LOAD PATH AS 50 PERCENT OF THE THREADS REMAINED ENGAGED. IF NEGLECTED THE CRACK WOULD HAVE RESULSDR CA970528004Bolt · cracked(CAN) REDUNDANT BOLT FOUND CRACKED AT CENTRAL AREA OF THE EXTERNAL THREAD SECTION THE RADIOGRAPHIC TECHNIQUE IS DESIGNED TO DETECT CRACKS IN THE BOLT HEAD TO SHANK RADIUS OR REDUNDANT ROD THE DOUGLAS "GAMMA RAY" INSPECTION PROCEDURE CONTAINED IN SB 72-172, RESDR AU970720Slide · faulty(AUS) DOOR 1L AND 1R ESCAPE SLIDES HAD MAINTENANCE PINS FITTED -PERSONNEL/MAINTENANCE ERRORSDR 9702121232Press Tubing · obstructedDURING CLIMB AT 1000 FEET, NR 1 ENGINE ROLLED BACK TO FLIGHT IDLE. AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE INSPECTION OF ENGINE FOUND THE COMPRESSOR DISCHARGE TUBING TO BE OBSTRUCTED. CLEARED OBSTRUCTION AND PSDR G6OA005Garloc Seal · damagedGVA - APPROXIMATELY 90 MINUTES AFTER TAKEOFF, CREW REPORTED LOSS OF NR 1 ENGINE OIL QUANTITY AND OIL PRESSURE FLUCTUATION OF 30-40 PSIG. ENGINE NR 1 WAS SHUT DOWN AND AIRCRAFT DIVERTED TO LYS AND LANDED WITHOUT FURTHER INCIDENTS. NO EMERGENCY WAS DECLARED. SDR AU970097Stringer · cracked(AUS) FUSELAGE FRAME 40 STRINGER 27 RHS CRACKED - FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION IAW SB A300-53-0310SDR 97UAL900014Dump Act · failedDIVERTED TO LAX DUE TO AN APPARENT WATER LEAK. HELD OVER LAX AREA TO BURN FUEL DOWN TO MAXIMUM LANDING WEIGHT DUE TO FUEL JETTISON PROBLEM. RT FUEL DUMP ACTUATOR MOTOR SHORTED. REPLACED ACTUATOR.SDR 97UAL900049Fitting · crackedDURING ROUTINE L-CHECK, THE LT SLAT NR 1 FAIRING ATTACH FITTING WAS FOUND CRACKED AND NOT REPAIRABLE. MANUFACTURED A NEW FITTING PER DRAWING ARB7131501. INSTALLED FITTING ON AIRCRAFT.SDR CA961205014Fuse Body · cracked(CAN) ON LANDING AUTO BRAKE SYSTEM ACTIVATED AND #3 HYDRAULIC SYSTEM LOST FLUID IMMEDIATELY AIRCRAFT TOWED TO GATE MAINTENANCE FOUND BODY OF HYDRAULIC FUSE CRACKED FUSE REPLACED AND #3 HYDRAULIC SYSTEM SERVICED.SDR 96UAL900908Relay · inoperativeON CLEARING RUNWAY COULD NOT TAXI BECAUSE OF LOCKED BRAKES . FOUND PARKING BRAKE VALVE NOT GETTING POWER TO OPEN VALVE. REPLACED PARKING BRAKE MOTOR VALVE RELAY. SYSTEM CHECKED OKAY.SDR CA961220009Duct Clamp · broken(CAN) ON TAKEOFF ROLL PRESSURE REGULATOR DUCT #2 ENGINE FAILED CAUSING EXCESSIVE DAMAGE TO PNEUMATIC DUCTING, SENSING LINES, OIL SCAVANGE AND OIL DUMP LINES. ALSO THERE WAS DAMAGE TO SUROUNDING STRUCTURE. NACELLE TEMPERATURE ROSE TO 240 DEGREES C AND FOLLOWED SDR 96UAL900879Fan Rotor · out of balanceNR 1 ENGINE VIBRATES STARTING AROUND 92 PERCENT N1 AND INCREASES IN INTENSITY. AROUND 95-96 PERCENT NI, IT APPEARS TO HAVE A PHASE OR OUT OF SYNC. BEAT. TURNING OFF BLEEDS, HYDRAULIC OR ELECTRICAL POWER HAS NO EFFECT. VIBRATION WAS ISOLATED TO THE FAN ROTO
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