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 = 'CF680C2B2' 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 = 'CF680C2B2' 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 UIEA200600222Fan Blade · lack of lubeN415MC AT PIK FOR MSG-3, C-4&A-4 CHECK. AS PER N/ROUTINE 154, NR 1 ENGINE S/N 704-916 FAN BLADES REMOVED FOR LUBRICATION. IT WAS FOUND, FAN DISKS HAVE NO EVIDENCE OF LUBRICANT. INSPECTION PERFORMED IAW MM 72-31-00, 206 TABLE 601 NR 1 DOVETAILS ON FAN DISK HSDR P5CA0601493Blades · damagedREPLACE NR 4 ENGINE DUE TO 7, 8, 9 STAGE BLADE DETERIORATION. REMOVED AND REPLACED NR 4 ENGINE IAW WORK CARDS ENG FUNCTION CHECK AND LEAK CHECK NORMAL.SDR P5CA0601449Bleed Valve · deactivatedRETURNED TO BLOCKS WITH -BLEED PRV ENGINE 3- MESSAGE. NR 3 ENG PRV BLEED VALVE DEACTIVATED PER MEL 36-11-86. ALSO REQUIRED TO LOCK OUT NR 3 REVERSER PER THE MEL.SDR BB06005Wire · disconnectedMAINTENANCE REPORTED THE EMERGENCY AISLE LIGHTS AT THE RT MID LAVATORY INOPERATIVE. MAINTENANCE FOUND WIRES DISCONNECTED AT LIGHT ASSEMBLY. RECONNECTED WIRES. OPERATIONAL CHECK GOOD.SDR BB06003Fuel Filter · bypassingFLIGHT 168, CLT-SJU: ON CLIMBOUT, RECEIVED EICAS MESSAGE -R ENG FUEL FILT-. RETURNED TO CLT. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL FILTER AND THE RIGHT ENGINE FUEL FILTER BYPASS SWITCH. NO FURTHER DIFFICULTIES NOTED.SDR USAABB05094Iru · failedFLIGHT 948, PHL-BCN: AFTER TAKEOFF, CREW RECEIVED CENTER IRS FAULT LIGHT WITH ASSOCIATED EICAS MESSAGE, DIVERTED. REPLACED THE CENTER IRS. NO FURTHER DIFFICULTIES.SDR TAMF20050007OSkin · dentedDURING INSPECTION CHECK, FOUND THE AIRPLANE HIT AT FUSELAGE SKIN, STA 172.5 STRINGER 21 RT BY A CARGO LOADING EQUIPMENT.REPAIR DOUBLER AS TEMPORARY REPAIR WAS INSTALLED IAW EWO 767-53-002, MFG SERVICE REQUEST NR 1-134757238 AND SRM 53-00-01 FIGURE 201. PERMANESDR TAMF20050006OSkin · crackedDURING TAKE OFF, THE CREW FELT A SUSPECTED BIRD STRIKE IN THE RIGHT PART OF THE AIRPLANE. DURING MAINTENANCE INSPECTION WAS FOUND A DENT AND CRACK ON THE NOSE SKIN AT SLAT NR 7. TIME LIMITED REPAIR WAS PERFORMED IAW EWO AND MFG APPROVAL NR 1-124395785-2 IN ORSDR AU510001729Cooling Fan · failedUPPER RECIRCULATION FAN FAILED. CIRCUIT BREAKER `OHD RECIRC FAN PWR 2` R7 ON P415 TRIPPED. INVESTIGATION FOUND FAN BEARINGS HAD FAILED.SDR DL764050322Warning Light · false indicationLT ENGINE EGT RED BOXED AT 975 ABORTED T/O AT 80KNTS - T/S PER FIM - NO EXCEEDENCES RECORDEDSDR UIEA200500058Hmu · unserviceableAFTER ROTATION UP TO 1000 FT, NR3 ENGINE N1 WOULD SURGE (ROLL BACK) BETWEEN 101.5 AND 98.0 N1. AT THRUST REDUCTION ALTITUDE, THE SURGE WOULD STOP. ALL PHASES OF FLIGHT WERE NORMAL. AFTER LANDING, DID A POWER RUN UP AND THE SAME AS ABOVE OCCURRED, NO EICAS OSDR UIEA200500059Fuel Filter · unserviceableAIR TURN BACK. STATUS MESSAGE: ENG 3 FUEL FILTER. THE AIRCRAFT RETURNED TO DEPARTURE. REMOVED AND REPLACED FUEL FILTER IAW MM, LEAK CHECKED SATISFACTORY. (K)SDR UIEA200500060Connector · contaminatedON TAXI OUT NR2 ENGINE OIL PRESSURE DROPPED BELOW RED LINE-ENGINE SHUTDOWN. T/S IAW MM. CLEANED OIL PRESSURE TRANSMITTER CONNECTOR. ENGINE GROUND RUN PERFORMED ALL WORKING NORMAL. (K)SDR DL764050225Compressor · stalledNR 1 ENGINE COMPRESSOR STALL. LOUD BANG HEARD. ABORTED T/O AT 5 KTS. MTC IN WORK REPLACING ENGINE. METAL IN TAILPIPE.SDR BB05023Pump · failedEN ROUTE, CREW RECEIVED THE EICAS MESSAGE R HYD PRIM PUMP AND NOTED DECREASING HYDRAULIC QUANTITY AND PRESSURE. CREW SECURED THE RIGHT EDP. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT EDP.SDR BB04095Pressure Switch · faultySJU - FL 1268 - EN ROUTE, THE CREW RECEIVED THE EICAS MESSAGE 'L OIL FILTER.' THE OIL PRESSURE AND QUANTITY WERE NORMAL. CREW REDUCED THRUST TO IDLE, BUT THE MESSAGE REMAINED. THE LEFT ENGINE WAS SECURED. FLIGHT CONTINUED TO SJU AND LANDED WITHOUT FURTHER SDR USAA040671Support Angle · crackedCRACK IN NR 7 SLAT SUPPORT ANGLE. NR 7 SLAT LOWER T/E, 54 INCHES FROM OB END. REPLACED WITH FABRICATED ANGLE IAW SRM 51-40-02.SDR USAA040667Floorbeam · corrodedFLOORBEAM BS 1480, LBL36, 5.5 INCHES X 3 INCHES, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-51.SDR BB04085Trim System · inoperativeAFTER TAKE-OFF, CREW NOTED THAT THE RUDDER TRIM WAS INOPERATIVE. CREW ALSO REPORTED THAT THE ANTI-SKID WAS INOPERATIVE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A RUDDER TRIM CHECK IAW THE FIM AND A VISUAL INSPECTIONSDR USA2004F00096Windshield · crackedEN ROUTE, AT FL380, THE CAPTAINS WINDSHIELD CRACKED. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WINDSHIELD.SDR USA2004F00091Pressure Switch · faultyINBOUND, THE CREW RECEIVED THE EICAS MESSAGE (R ENG OIL FILTER). THE MESSAGE REMAINED ILLUMINATED WHEN THE ENGINE THRUST WAS REDUCED. CREW SECURED THE ENGINE. FLIGHT LANDED, WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OIL FILTER DIFFERENTIAL PRESSURSDR USAABB04061Engine · making metalPHL - FLT 71 - INBOARD TO PHL, THE CREW RECEIVED THE EICAS MESSAGE 'R ENGINE OIL FILTER.' THE MESSAGE REMAINED ILLUMINATED WHTN THE ENGINE THRUST WAS REDUCED. CREW SECURED THE ENGINE. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE SDR USAABB04021Pressure Switch · faultySJU - FLT 134, EN ROUTE STT TO PHL, CREW RECEIVED THE EICAS MESSAGE 'L ENG FUEL FILT.' FLIGHT DIVERTED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE FILTER AND FOUND IT SATISFACTORY. THE FUEL DIFFERENTIAL PRESSURE SWITCH WAS REPLACED,SDR CA031020005Odor · detected(CAN) AFTER T/O THRU 8,000 FT HAD A STRONG ODOR OF SMOKE IN C/P CABIN. THE ODOR WAS SULPHERUS AND NOT ELECTRICAL. TURNED OFF RECERC AND GASPER FANS AND ODOR DISSAPPEARED. FLT CONTINUED TO DESTINATION AND NO FURTHER FAULT.SDR DL764030345Engine · failedON TAKEOFF ROLL, BETWEEN 30 AND 50 KTS, POWER STABILIZED AT ALTENATE 60, HEARD LOUD BANG AND CONTINUOUS RUMBLE. TAKEOFF ABORTED. ENGINE INSTRUMENTS LOOKED NORMAL. PASSENGERS REPORTED SEEING FLASH OF FLAME ON THE LEFT SIDE OF THE AIRCRAFT. FOUND METAL IN TAIL SDR S03J27006Control Cable · out of rigRUDDER DOES NOT FULL DEFLECT TO RT . RUDDER & RUDDER TRIM SYSTEM RIG CHECK FOUND CONTROL CABLE TENSION WAS OUT OF LIMIT. PERFORM RUDDER AND RUDDER TRIM CONTROL SYS ADJ IAW 27-21-00. PERFORM RUDDER TRIM SYS TEST NML. EON 744-27-632292-0017 R1 IS ISSUED SDR S03J27004Control Cable · out of rigB-18701 RUDDER DOES NOT FULL DEFECT TO RT (SHORT OF ABOUT 15-20 PERCENT). RUDDER & RUDDER TRIM SYSTEM RIG CHECK FOUND CONTROL CABLE. TENSION WAS OUT OF LIMIT. PERFORM RUDDER AND RUDDER TRIM CONTROL SYS ADJ IAW AMM 27-21-00. PERFORM RUDDER RATIO GROUND TSDR USAABB02161Idg · malfunctionedLAX - FLT 48 - FLIGHT DEPARTED LAX WITH THE LEFT IDG ON MEL. DURING CLIMB, THE CREW NOTED THE EICAS MESSAGE 'R GEN DRIVE' AND THE 'DRIVE' LIGHT FLICKERING. FLIGHT RETURNED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH IDG'S. (M)SDR CA020315007Tube · cracked(CAN) ON CLIMB, EICAS ENGINE OVERHEAT NR 2 NAC. FLIGHT CREW FOLLOWED THE CHECK LIST, BLEED OFF, MESSAGE REMAINED. REDUCED THRUST TO APPROX 75 PERCENT POWER, MESSAGE DISAPPEARED. AIRCRAFT RETURNED TO HAWAII. FOUND CRACK AT UPPER BEND OF NR 2 HP TURBINE COOLINSDR EVAS91004Hmu · failedDURING TAKE OFF, NR 1 ENGINE LOW N2 THEN FLAME OUT. ON GROUND REPLACED EEC & HMU, OPR CHECKED NORMAL.SDR CA010815004Warning System · false activation(CAN) 1. DURING TAKEOFF, ECAM WARNING FOR BULK CARGO DOOR INDICATION. AIRCRAFT RETURNED TO GATE. SYSTEM CHECKED AND MEL 52-7-0 APPLIED. AIRCRAFT RELEASED FOR FLIGHT. 2. NO PROBLEM DURING SUBSEQUENT FLIGHT. 3. UPON ARRIVAL TO HOME BASE, BULK CARGO DOOR INDICATISDR USAABB01066Manifold · leakingPIT - FLT 48 - ON TAKEOFF ROLL IN PIT, THE LEFT ENGINE REACHED 80 PERCENT N1 AND THEN FAILED. THE TAKEOFF WAS ABORTED AT 60 KNOTS. THE FLIGHT RETURNED TO THE GATE, WHERE IT WAS NOTED THAT FUEL WAS LEAKING FROM THE LEFT ENGINE. MAINTENANCE FOUND A FUEL PRESSSDR USAABB01054Manifold · cloggedPHL - FLT 14, AFTER TAKEOFF, THE LEFT ENGINE WAS REPORTED TO HAVE LOST OIL PRESSURE AND THE N2 WAS AT 0 PERCENT. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED ENGINE. ENGINE TEARDOWN REVEALED THAT THE OIL MANIFOLD THAT FEEDS ISDR CA010815005Controller · failed(CAN) 1. AT CRUISE, ECAM CONTROLLER SHOWED SIGNS OF BEING ERRATIC, FLASHING THEN TURNED BLACK. SMOKE STARTED FOR 10 SECONDS WITH ELECTRICAL SMELL. CB POPPED AND SMOKE STOPPED. NOT ENOUGH SMOKE TO DON O2 MASKS. 2. PHONE PATCH MADE TO DISPATCH REGARDING PROBLEM.SDR USAABB01037Engine · malfunctionedLAX - DESCENT THRU FL170 INTO LAX, CREW REPORTED THE NR 2 ENGINE HAD UNSPOOLED AND HAD NO THROTTLE RESPONSE DURING A 1,500 FPM DESCENT. NO RESTART WAS ATTEMPTED. NO OTHER ENGINE ABNORMAL INDICATIONS NOTED. CREW SHUT DOWN THE ENGINE, DECLARED AN EMERGENCY. LANSDR CA010511028Heater · failed(CAN) DURING FLIGHT, SMOKE WAS OBSERVED COMING FROM FORWARD GALLEY NR 2 BOILER. ALL CB PULLED & GALLEY POWER SHEDDED. NO MORE SMOKE OBSERVED & FLIGHT CONTINUED WITHOUT INCIDENT. NR 2 WATER BOILER CHANGED IAW MM 25-30 & CHECKED SERVICEABLE. NO FURTHER INCIDENTSDR DL764010566Line · failedNR 1 ENGINE OIL QTY DECREASED TO ZERO AND WITH OIL PRESSURE FLUX DECREASED TO 23 PSI PULLED ENG BACK TO IDLE AND DIVERTED TO ABQ. ENGINE WAS SHUTDOWN ON THE GROUND WHEN OIL PRESSURE DROPPED TO 10 PSI. FOUND C SUMP SCAVENGE LINE DAMAGED BY BROKEN STARTER PIECESDR USAABB01007Pressure Switch · faultyCLT - FLT 192 - SHORTLY AFTER TAKEOFF, CREW RECEIVED THE EICAS MESSAGE ''R ENG FUEL FILTER.'' FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL FILTER AN FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. (M)SDR CA010301017Engine · failed(CAN) ON FINAL INTO YYZ, RIGHT ENGINE SHUTDOWN, 4 MINUTES TO LANDING. ENGINE SHUTDOWN CHECKLIST COMPLETED. LANDED WITHOUT INCIDENT. ON INSPECTION OF RT ENGINE METAL FOUND IN TAILPIPE. RT ENGINE REPLACED. OFF PART NUMBER 6-7200-9-0002, SERIAL NUMBER 2611.2001-0SDR USAABB00100Turbine Wheel · failedPHL - ON ENGINE RUN-UP AFTER IDG MAINTENANCE, ONE OF THE LEFT ENGINE TURBINES FAILED. MECHANICS DISCHARGED BOTH BOTTLES WHICH PROVED INEFFECTIVE IN BATTLING THE FIRE. CFR WAS CALLED TO EXTINGUISH THE FIRE. DAMAGE INCLUDES THE WING, PYLON, FLAP AND AILERON ASDR CA000118018Blade · seized(CAN) ENGINE WAS SHUTDOWN DUE TO VIBRATION. INSPECTION REVEALED LPT BLADES DAMAGED AND ENGINE SEIZED. SECONDARY DAMAGE TO OUTBRD AILERON WAS EXPERIENCED. REPORT TO FOLLOW.SDR CA000110019Blade · seized(CAN) ENGINE WAS SHUTDOWN DUE TO VIBRATION. INSPECTION REVEALED LPT BLADES DAMAGED AND ENGINE SEIZED. SECONDARY DAMAGE TO OUTBRD AILERON WAS EXPERIENCED. REPORT TO FOLLOW.SDR USAABB99023O-Ring · rupturedPHL - FLT 12 - EN ROUTE PHL-MAD, AT APPROXIMATELY 50W LONGITUDE, THE CREW NOTED THAT THE LEFT ENGINE OIL PRESSURE WAS LOW AND THAT THE QTY WAS FLUCTUATING BETWEEN 13 AND 14. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A BAD SDR DL76K990061Engine · failedCOMPRESSOR STALL ON TAKEOFF RETARDED THROTTLE AIR TURN BACK, FOUND METAL IN TAIL PIPE ON INSPECTION. CHANGING NR 2 ENGINE.SDR CA990119028Engine · leaking(CAN) NR 1 ENGINE OIL QUANTITY DECREASED RAPIDLY IN CLIMB, 15 MINUTES AFTER TAKEOFF. THE FLIGHT WAS DIVERTED. POST -FLIGHT INSPECTION FOUND AN OIL LEAK AT THE 6 O'CLOCK POSITION. THE SCAVENGE O-RING WAS REPLACED AND A GROUND RUN INDICATED THE OIL LEAK WAS STSDR CA981125022B Nut · loose(CAN) AIR RETURN DUE RT ENGINE BLEED OVERHEAT EICAS MESSAGE ON TAKEOFF. REPLACED BLEED CONTROL CARD PER MM. FOUND B-NUT ON DUCT PRESSURE SENSE LINE LOOSE, TIGHTENED.SDR CA981125019Transmitter · failed(CAN) ON ENGINE START, OIL PRESSURE SYSTEM NR 3 DISPLAYED ON EICAS DUE TO NO OIL PRESSURE INDICATION NR 3 ENGINE. REPLACED NR 3 OIL PRESSURE TRANSMITTER. PART TC: 4,547.SDR AU981350Light · malfunctioned(AUS) CABIN LIGHTING FAULTY. SIDEWALL FLUORESCENT TUBE LOCATED AT SEAT 5JK FAULTY CAUSING FAILURE OF UPPER EICAS DISPLAY AND THE FIRST OFFICER'S CLOCK.SDR CA980928031Sensor · faulty(CAN) DURING DESCENT, THE POWER WAS INCREASED TO MAINTAIN AIRSPEED TARGET. NR 1 ENGINE PARAMETERS DID NOT CHANGE, BUT REMAINED INDICATING LOWER THAN NORMAL IDLE. PRECAUTIONARY ENGINE SHUTDOWN CARRIED OUT. POST-FLIGHT, THE N1 HYDROMECHANICAL SENSOR WAS CHANGSDR USAABB98084Blades · damagedPHL - FLT 42 - AT TAKEOFF FROM PHL, CAPTAIN SAW A BIRD PASS BENEATH THE AIRCRAFT. AS THE GEAR RETRACTED, THE CREW NOTED A STRANGE NOISE FROM THE RIGHT ENGINE. ALL INDICATIONS WERE NORMAL, BUT THE NOISE CONTINUED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FU
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