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 CA101111003Seat Back · cracked(CAN) CONTOUR J-CLASS SEATBACK PNS231010-001-001 FAILED AND REQUIRED REPLACEMENT. SEATBACK HAD ALREADY BEEN MODIFIED BY CONTOUR SB25-3379 INSTALLATION OF DOUBLERS TO SEATBACK SUPPORT ARMS. AIR CANADA SAFETY REPORT NR 12892 RAISED.SDR CA101004006Hose · leakingTHE ACFT DEVELOPED LOW CTR HYD PRESSURE AFTER TAKEOFF. WITH NO INDICATIONS OF IMPROVEMENT, THE FLIGHT DIVERTED. AS A PRECAUTION, CFR WAS CALLED OUT TO MEET THE FLIGHT, HOWEVER THE ACFT WAS ABLE TO TAXI INTO THE GATE WITHOUT ASSISTANCE. THERE WAS NO ADVERSE PSDR CA100719004Brake Assy · fireON THE TAXI INBD TO THE GATE, THE CREW REPORTED THAT THEY HAD HOT BRAKES. WHEN THE ACFT ARRIVED ON THE GATE, AN ATTENDANT NOTICED SMOKE COMING FROM THE RT MAIN OTBD GEAR FOLLOWED BY A SMALL FLAME. ATTENDANT EXTINGUISHED THE FLAME USING THE PCA (AIR CONDITIONSDR AALA20100603PHL01Compressor · stalledPHL - INFLIGHT JFK-STI. CREW REPORTED RIGHT ENGINE COMPRESSOR STALLED INFLIGHT. EMERGENCY DECLARED DIVERTED PHL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BOROSCOPE AND ENGINE CHANGE DECLARED. REPLACED RIGHT ENGINE ON 06/04/2010 SDR IPXA10660202Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR4 SLAT L/E INBD AT OSS572.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1455", DAMAGED CUTOUT IS 0.500" DIA. SDR IPXA10660203Skin · crackedINSP TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E OTBD AT OSS641.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1530", DAMAGED CUTOUT IS 0.500" DIA. THISDR IPXA10659951Connector · intermittentINSPECTION TYPE: L3, WINDOW WORKS ONLY INTERMITTENT. T/S C/O FOUND J9 CONNNECTION INTERMITTENT ON L3 WINDOW. CLEANED CONNECTION ON WINDOW AND RETAPED WINDOW THREAD. INSTALLED NEW SCREW AND WASHER. C/O TEST IAW AMM 30-41-00-5. BITE TEST OK AND OPS SATIS. THIS SDR AALA20100513BOS01Decoder · inoperativeBOS - FLIGHT ATTENDANTS OBSERVED AN ELECTRICAL ODOR IN CABIN AT ROW 25. PILOTS PULLED THE ENTERTAINMENT SYSTEM CIRCUIT BREAKER ON OVERHEAD PANEL AND SMELL DISSIPATED. FLIGHT LANDED BOS WITHOUT INCIDENT. FOUND CIRCUIT BREAKER FOR AFT COLUMN TIME DECODER POPPSDR DL76G101304Bulb · inoperativeEMERGENCY LIGHT ROW 31F ON SIDE SEAT DAMAGED. MX REPLACED LIGHT LENS BULB. SYS OPS IS NORMAL.SDR AALA20100323SJU01Pressure Switch · inoperativeSJU - INFLIGHT STI-JFK. CREW REPORTED EICAS AMBER LEFT ENGINE FUEL FILTER. ENGINE PERFORMED NORMALLY. EMERGENCY DECLARED DIVERTED SJU LANDED WITHOUT INCIDENT. REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH AND FUEL FILTER. SYSTEM GROUND CHECK NORMAL OPSDR IPXA10658551Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 930 TO 975, L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10658552Floor Panel · puncturedINSP TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 731 TO 833, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR CA100126002Duct · damaged(CAN) UPON ARRIVAL, MX DISCOVERED THAT THE L/E SLAT NR 4 (LT WING) OVERPRESSURE PANEL WAS OPEN. FURTHER INSP REVEALED THAT THE THERMAL ANTI-ICE INSTERSTITIAL DUCT WAS DAMAGED AND HAD IN FACT SEPARATED AT THE JOINT WITH THE ADJOINING SLAT ANTI-ICE DUCT WHILE ISDR AALA20091011MIA01O-Ring · leakingON TAKEOFF ROLL AIRCRAFT CABIN SMELL OF AIR CONDITIONING WATER SEPARATOR ODOR. RECIRCULATION FANS WERE TURNED OFF TO ACCOMPLISH ODOR REMOVAL. ODOR DISSIPATED AFTER 5 MINUTES. TURNED RECIRCULATION FANS BACK ON AND HAD A DIFFERENT ODOR. ON DESCENT BOTH ODORSSDR CA090818003Lug · damaged90 MINUTES AFTER TAKEOFF, AT 34,000 FT, RED CABIN ALTITUDE WARNING AND BELL SOUNDED. CABIN ALT SHOWED 10,000 FT WITH CABIN ALTITUDE CLIMBING AT 800-1000 FT/MIN. PRESS CHECK LIST ACCOMPLISHED, MASKS DEPLOYED AND CREW DECLARED A PAN PAN. FLIGHT DESCENDED TO 8,0SDR DL76G091256Engine · overtempRT ENGINE OVERTEMP DURING ENGINE START. EGT EXCEEDANCE CAT D OPENED ENGINE FOR BORO PER M/M 72-00-00-60 273001. C/W NR 2 ENG 695446 BOROSCOPE FOR HOT START ABOVE PER M/M 72-00-00-601. NO DAMAGE FOUND QC 1510. RE-INSTALLED BORO PLUGS AND CRANK PAD COVER. LSDR DL76G091188Engine · leakingNR 1 ENGINE HIG OIL USAGE, OIL COMING OUT OF RECOUP DUCT. REPLACING NR 1 ENGINE.SDR DL76G091081Warning Message · illuminatedRT IDG VALVE MSG. FWD TO MCO/PLAC PER MEL 75-21-01B DISCONNECTED AND STOWED VALVE CONNECTOR PER MEL PROCEDURES. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPSSDR DL75E091057Coffeemaker · sparksF/A REPORTED SPARKS COMING FROM LOW WATER BUTTON FROM AFT NR 2 COFFEEMAKER 1ST CLASS GALLET/ REMOVED AND REPLACED F/C COFFEEMAKER OPS CHECKS NORMAL.SDR AALA2009060300005Clamp · brokenSJU - INFLIGHT SDQ-JFK. RIGHT DUCT LEAK ILLUMINATED. EMERGENCY DECLARED, LANDED SJU WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BROKEN CLAMP ON RIGHT ENGINE THERMAL ANTI-ICE VALVE DUCTING. SYSTEM GROUND CHECK NORMAL OPERATION.SDR AALA2009051400003Valve · inoperativeRIGHT ENGINE BLEED OVERHEAT INDICATION. EMERGENCY DECLARED RETURNED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT ENGINE HP VALVE AND CONTROLLER. REPLACED FAN AIR VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)SDR DL76G090845Connector · dirtyNO OIL PRESS ON EICAS AND L ENG OIL PRESS LIGHT REMAINED ILLUMINATED ON LT ENG START ATTEMPT. TROUBLESHOT AND COMPLIED WITH QRH. CLEANED CONNECTORS OIL PRESSURE TRANSMITTER AND LOW OIL PRESSURE SWITCH. PERFORMED ENGINE RUN. ALL INDICATIONS NORMAL.SDR AALA2009040200002Line · leakingINFLIGHT RDU-LHR. NO ANTI-ICE ON LT ENGINE GOING INTO ICY CONDITIONS. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PRV MUSCLE LINE LEAKING. RESEATED TIGHTENED LINE. SYSTEM GROUND CHECK NORMAL OPERATION.SDR DL76G090582Shutoff Valve · failedLT BLEED LIGHT ILLUMINATED WHEN THROTTLE RETARDED FOR CRUISE POWER, DEACTIVATED LT HPSOV PER MM AND FWD TO MCO AND PLACARD PER M 36-11-02.SDR DL76G090380Pump · malfunctionedAT FL340 DURING A CROSS FEED OPS TO CORRECT MINOR FUEL IMBALANCE THE LEFT ENG ROLLED BACK TO 52 PERCENT N1. LEFT MAIN BOOST PUMP WERE TURNED BACK ON AND X-FEED VLV CLOSED. ACFT RETRIMMED AND A/T ARM SW TURNED OFF. INITIALLY ENG WAS UNRESPONSIVE TO CHANGES ISDR DL76G090318Lead · misinstalledON RIGHT ENGINE START UP HAD FOLLOWING ELECTRICAL SYSTEM INDICATIONS RT AC BUSS OFF EICAS ON OVERHEAD R BUS TIE ISLN RBUS OFF AND RT GENERATOR CONTROL OFF. BIT BPCU FAULT WAS DP TRIP MAIN BUSS/OVERLAP ZONE. REPLACED BPCU AND RT GCU. RAN ENG NO HELP. REINSTSDR DL76G090002Throttle · stuckLEFT ENGINE THROTLE WILL NOT ADVANCE. REPLACED LOWER CABLE FROM PYLON TO HMU PER AMM. INSPECTED ALL OTHER AREAS. NO TROUBLE FOUND. PULL TEST NOW AT 3 POUNDS. BEFORE WAS 6 POUNDS.SDR DL76L090003Smoke Detector · false activationMID LAV 219 SMOKE ALARM SOUNDED. NO SMOKE OR BURNING ODOR NOTED. LAVATORY INSPECTED FOR BURNS OR DISCREPANCY NIL FOUND. LAVATORY WASTE FLAP AND LAVATORY FIRE EXTINGUISHER BOTTLE INSPECTED OK. SMOKE DETECTOR OPS CHECKED OK FOR SERVICE.SDR AALA200802544ASeal · leakingINFLIGHT FCF - APPROXIMATELY FIVE MINUTES AFTER LEVEL OFF AT 40000 FEET OIL QUANTITY INDICATION ILLUMINATED OR NUMBER TWO ENGINE THEN WENT RAPIDLY TO ZERO. OIL PRESSURE BEGAN TO DROP AND OIL TEMPERATURE BEGAN TO RISE. REDUCED ENGINE TO IDLE. ON DESCENT OIL SDR AALA200802350Engine · leakingJFK INFLIGHT, CREW REPORTED SMOKE IN CABIN. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. FOUND OIL IN EIGHTH STAGE AREA OF NUMBER TWO ENGINE. REPLACED NUMBER TWO ENGINE ON 19 OCT 2008 AT JFK. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DL76G081342Starter · failedNR 2 ENGINE FAILED TO START ON TAXI OUT. MANUALLY OPENED START VALVE. ENGINE DIDN'T ROTATE. REMOVED DAMAGED STARTER. DUE TO STARTER VALVE MAY HAVE CLOSED DURING START AND REOPENED. REPLACED VALVE ALSO AS PRECAUTION. STARTER AND VALVE REPLACED PER AMM.SDR UIE2008F00031Skin · dentedDENT WAS FOUND AT THE AFTER LOWER CORNER OF BULK CARGO DOOR. INSPECTED IAW SRM 51-10-00 AND SR ID NR 1949639862. (K)SDR UIE2008F00032Skin · crackedFOUND NR 3 ENGINE RT CORE COWL LOWER FACE CRACKED. 0.3 INCH AT NAC STA 288. REPAIRED IAW FORM NR E8207.4. (K)SDR UIE2008F00033Fairing · damagedFOUND NR 4 ENGINE SKIRT FAIRING SUPPORT BRACKET ATTACHED BOLT IB SIDE HOLE ENLARGED NEAR FAIRING DOOR NR 4 HINGE. REPAIR ACCOMPLISHED IAW SR ID NR 1945402461 AND EO NR 4464A066. (K)SDR UIE2008F00034Skin · damagedDURING PFM J/C: MCIA016, REPLACE 6 BLIND FASTENER FOUND DEVIATION FOR STA 380, 440, S-1R MISS DRILLING HOLE. ACCOMPLISHED THE SEA DOUBLER HOLES ON SKIN COMMON TO THE STRAP AT BS 380, 440, AND 480 BETWEEN S1R AND A2R. (K)SDR AALA200802282Eec · inoperativeBDL INFLIGHT T160/06 SEP SAN TO JFK. CREW REPORTED UNCOMMANDED SHUTDOWN OF NR 1 ENGINE. LANDED BDL WITHOUT INCIDENT. REPLACED NR 1 ENGINE ELECTRONIC ENGINE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPS.SDR DL76G080218Engine · failedENGINE FAILED BORO-ENGINE REPLACED.SDR DL76G090028Hose · leakingRIGHT HYD QTY EICAS MESSAGE WITH RT HYD QTY LIGHT. RT SYSTEM QTY INDICATING 0.47 WITH RF AND DECREASING SLOWLY 5 HOURS AND 20 MIN INTO FLIGHT. REPLACED LINE WITH BORROW PART FROM AIR FRANCE. FOUND RT ENG EDP HYDRAULIC PRESS HOSE ASSEMBLY LEAKING. REPLACED SDR AALA20072176Control Unit · inoperativeGRU INFLIGHT T942/09NOV - RIGHT ENGINE FUEL SHUTOFF VALVE CIRCUIT BREAKER POPPED AFTER LEVEL OFF. RETURNED TO GRU AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE MAIN FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DL76G071304Engine · making metalWHILE PERFORMING OPN 4050 ON NR 2 ENGINE, FOUND FERROUS MATERIAL ON MAG CHIP DETECTOR MATERIAL SENT TO SHOP FOR EVALUATION. DUE TO LAB FINDINGS, RECOMMEND ENGINE CHANGE. REPLACED NR 2 ENGINE PER TRANS 1T161.SDR DL76S071305Acm · frozenLEFT A/C PACK TRIPPED ON TAKEOFF ROLL. RETURNED FOR LANDING DUE TO SMOKE AND FUMES IN THE CABIN AFTER TAKEOFF. FOUND LEFT AIR CYCLE MACHINE SEIZED. REPLACED LT ACM PER M/M 21-51-03-004. LEFT PACK CKS OK, RAN BOTH ENGS. NO SMOKE OR ODOR NOTED.SDR AALA20071827Engine · vibrationLAX INFLIGHT T297/28SEP - CREW REPORTED NUMBER TWO ENGINE N2 VIBRATION INDICATING 3.7 ON CLIMB. NUMBER TWO ENGINE FIRE LOOP ONE ILLUMINATED FIVE TO TEN MINUTES THEN EXTINGUISHED. LANDED LAX WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 30 SEP 2007 AT LAX SDR DL76G071161Engine · malfunctionedDURING ENGINE START, LT ENGINE, AS THE L FUEL CONTROL SWITCH WAS PLACED ON, THESE INDICATIONS APPEARED - 1 EICAS L ENG FUEL VLV MSG 2 ENG VLV LIGHT ON PEDESTAL ENGINE WOULD NOT START NO EGT RISE FUEL CONTROL SWITCH WAS PLACED OFF APPROX 2 MINUTES LATER THE ABOSDR DL76G071158Engine · damagedNR 1 ENG FAILED BORO ENGINE CHANGE.SDR DL76G071081Controller · malfunctionedLEFT ENG PRV MESSAGE REMOVED AND REPLACED PRV CONTROLLER GRD, OPS CK GOOD.SDR DL76G070967Engine · hot startPENDING HOT START IN STR. PRECAUTIONARY BORO SHOWED DAMAGE TO 10 BLADES OF HPC. CHANGED NR 2 ENGINE PER ROUTINE TRANSMITTAL 1T161.SDR DL76G070710Engine · unknownRTB - RIGHT ENGINE NR 2 ENGINE FUEL CONTROL VALVE LIGHT. NO START VALVE EXCERCISED BY OPERATING FIRE HANDLE. ENGINE GROUND RUN CARRIED OUT. NIL DEFECTS.SDR DL76G070699Engine · inoperativeR ENGINE WOULD NOT START. R ENG FUEL VLV LIGHT ON PEDESTAL ILLUM. RTB, CYCLED VALVE RAN RT ENG. CHKS GOOD.SDR DL76G070054Line · cloggedNO THROTTLE RESPONCE TO THROTTLE MOVEMENT AFTER ENG START. ALL PARAMETERS NORMAL. FOUND BURNER PRESSURE SENSE LINE CLOGGED. CLEARED LINE, OPS CK NORMAL.SDR DLM88070056Clamp · looseAFTER T/O OUT OF LGA. GOT A TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR. RAN QRH AND LIGHT EXTINGUISHED WHEN LEFT THROTTLE RETARDED TO IDLE. DIVERTED TO JFK. REPOSITION CLAMPS ON LT AUGMENTATION VALVE, RETORQUE SAME. AS PER MM, PERFORM PROC 36-00-00201. AUG V
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