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 = 'CF348C5' 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 = 'CF348C5' 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 CA131028008Circuit Breaker · failed(CAN) FOUND "RCCB MAIN BATTERY" CIRCUIT BREAKER POPPED, CBP1 D1. CB RESET BUT POPS WHEN MAIN BATTERY POWER WAS APPLIED, NO AC ONLINE. UPON SHUTDOWN OF ACFT IT WAS NOTED CB DID NOT POP BUT SMOKE WAS COMING FROM CB-CIRCUIT. BREAKER PULLED AND BATTERY MASTER SSDR REXA2013101702116Skin · chafedLEFT ENGINE AFT CORE COWL OUTER SKIN AT PYLON SEAL IS CHAFED. REPAIRED LEFT ENGINE AFT CORE COWL OUTER SKIN TO WITHIN LIMITS CONDITION IAW SRM 54-13-00.SDR CA131016003Controller · malfunctioned(CAN) ON TAXI OUT, RHE DOES NOT START WITH MSG RT START VALVE ON ED1. RETURN TO PARKING. RHE STARTED MANUALLY. ACFT RTS. THE START VALVE WAS REPLACED AFTER 2 SUBSEQUENT FLIGHTS.SDR MASA2013101516788Blade · lack of lubeENGINE 1 HIGH VIBRATION. ENGINE FAN BLADE INSPECTED, BLADE SHAKE, & VIBRATION CHECK ENGINE RUNS COMPLIED WITH. FAN BLADE LUBRICATION COMPLIED WITH ENGINE VIBRATION CHECK WITHIN LIMITS.SDR CA130930001Acm · seized(CAN) AFTER LANDING, DURING TAXI THE FLIGHT CREW REPORTED SMOKE IN THE CABIN. AT THE SAME TIME THEY RECEIVED A RT PACK HOT OR RT PACK FAIL MESSAGE AND THEY TURNED OFF THE RT PACK. THEY STOPPED ON THE TAXIWAY AND DID A RAPID DEPLANEMENT OF THE PASSENGERS. THSDR REXA2013092501958Blowout Door · chafedNR 1 ENGINE, LOWER CORE COWL BLOW OUT DOOR, STRIKER PLATE IS CHAFED. R & R NR 1 ENG LOWER CORE COWL CLOWOUT DOOR LATCH STRIKER IAW SRM 51-42-06 AND 51-42-13.SDR CA130926002Pin · dislodged(CAN) WHEN INSPECTING NOSE GEAR FOR NOSE GEAR SHIMMY. FOUND SCORING ON NOSE GEAR SLIDING MEMBER. LP 764670 POSSIBLY CAUSED BY PIN, DOWEL BECOMING DISLOGDED FROM PISTON/AXLE ASSY AND GETTING CAUGHT IN GLAND NUT AT BOTTOM OF PISTON, GLAND NUT SCORED AND PIN SHOSDR CA130920011Trim Panel · stuck(CAN) IN CRUISE FLIGHT, AT FL360 WITH THE A/P ON, THE ACFT HAD AN UN-COMMANDED RUDDER TRIM GOING FULL LEFT. THE FLIGHT CREW RETURNED THE RUDDER TRIM TO NEUTRAL AND THERE WERE NO FURTHER ISSUES. MAINTENANCE INVESTIGATION FOUND FROM THE FDR READOUT THAT THE RUSDR REXA2013090901716Hinge · wornRT UPPER RT UPPER TRANSCOWL ACCESS DOOR HINGE WORN. R & R RT UPPER TRANSCOWL ACCESS DOOR HINGE IAW SRM 51-24-18 AND SRM 51-42-21.SDR REXA2013090901717Structure · wornRIGHT LOWER TRANSCOWL COAMING AND DOUBLER WORN. REPLACED RT LOWER TRANSCOWL LOAMING AND DOUBLES IAW SRM 51-42-06 AND 51-42-13.SDR CA130909006Printer · smoke(CAN) DURING PASSENGER BOARDING, THE FLIGHT CREW NOTICED AN ELECTRICAL ODOR FOLLOWED BY SMOKE COMING FROM THE ACARS PRINTER WHICH RESULTED IN THE ACFT BEING DEPLANED. THE SMOKE DISSIPATED ONCE POWER WAS REMOVED FROM THE PRINTER.SDR REXA2013090701703Stand Off · crackedLEFT UPPER TRANSCOWL INBD STANDOFF CRACKED. R & R LT UPPER TRANSCOWL INBD STANDOFF WET IAW SRM 51-42-14, 51-42-20 AND 51-23-00.SDR CA130910008Fan · lack of lube(CAN) STRANGE NOISE FROM ENGINE NR 1 AND VIBRATION. FAN LUBRICATION CARRIED OUT AFTER BOROSCOPE INSPECTION. ACFT RETURNED TO SERVICE.SDR CA130828013Engine · fluctuates(CAN) ITT FLUCTUATION AND IN FLIGHT SHUTDOWN DURING CLIMBOUT.SDR REXA2013082701502Engine · failedDURING CLIMB, LT ENGINE BEGAN TO FLUCTUATE, N1, N2, ITT AND FF. N1 APPROXIMATELY 15 PERCENT, ITT APPROXIMATELY 200 DEGREES. LT ENGINE WOULD NOT ACCELERATE ABOVE 60 PERCENT N1. ITT WAS NEVER HOT. CREW HAD NO CAS MESSAGES, PROCEEDED WITH ENGINE OSCILLATIONSSDR REXA2013081701529Rub Strip · wornRT ENGINE UPPER COWL INBD AFT RUB STRIP IS WORN. REMOVED DAMAGED SECTION OF RUBSTRIP AND INSTALLED NEW IAW SRM 53-23-00-201-007-A01. PN NAS1097AD4-6, CN624-3073-203.SDR REXA2013081601469Fuel Nozzle · leakingF/A REPORT A STRONG ODOR IN CABIN. ODOR BEGAN WHEN PACKS STARTED. STRONG "OILY" ODOR. ODOR IMPROVED AFTER A TIME, BUT REMAINED IN THE CABIN. ODOR SEEMED STRONGER IN SOME AREAS. PRIMARILY AROUND ROWS 5 AND 6. WHEN PACKS WERE OFF, ODOR WENT AWAY. FOUND LEAKSDR CA130828011Engine · flamed out(CAN) CREW HEARD A LOUD NOISE AND THE ACFT JOLTED. CREW RECEIVED RT ENGINE VIBRATION FOLLOWED BY RT ENGINE LOSS OF OIL PRESSURE AND UNCOMMANDED ENGINE SHUTDOWN, THEN FLAMEOUT. NO FIRE AND NO FIRE BOTTLES BLOWN.SDR CA130812005Windscreen · cracked(CAN) ENROUTE, ACFT DIVERTED DUE TO A CRACKED WINDSCREEN. FLIGHT CREW DID DECLARED AN EMERGENCY AND LANDED SAFELY. WINDSCREEN COVERED IN CRACKS.SDR CA130819012Line · cracked(CAN) AFTER ARRIVAL THE RAMP CREW NOTICED A HYDRAULIC LEAK AT THE NLG. HYDRAULIC LINE,WAS FOUND CRACKED AND LEAKING AT THE WELD. THE LINE WAS REPLACED. ACFT TSN 25401, CSN 12796.SDR REXA2013080101449Floorbeam · crackedFLOORBEAM IS CRACKED BS 274 RBL 12. REPAIRED FLOORBEAM IAW EO R53444.SDR REXA2013072501440Retainer · chafedLEFT LOWER TRANSCOWL RETAINER TABS CHAFED. REMOVED CHAFE FROM LT LOWER TRANSCOWL RETAINER TABS IAW SRM 51-12-00. TABS FOUND TO BE IN LIMITS IAW SRM 54-21-00.SDR CA130726009Line · cracked(CAN) AFTER LANDING, THE PILOT REPORTED A HYDRAULIC LEAK FROM THE NLG AREA. FOUND A HYDRAULIC LINE CRACKED. THE HYDRAULIC LINE, WAS REPLACED.SDR REXA2013071701419Fairing · crackedRT ENGINE UPPER AFT HINGE FAIRING CRACKED. R & R RT ENGINE UPPER AFT HINGE FAIRING IAW SRM 51-42-16, PN'S CR3212-4-2, MS20426A04-4, MS20426AD5-5, 0632024T-3.SDR REXA2013071701420Stand Off · crackedRT UPPER TRANSCOWL INBD STANDOFF CRACKED. REPLACED RT UPPER TRANSCOWL INBD STANDOFF IAW SRM 51-42-10.SDR CA130715013A/C Pack · failed(CAN) AIRCRAFT RETURNED TO GATE AFTER SMOKE REPORT IN THE CABIN FOLLOWED BY A LT PACK TEMP" C, MSG ON ED1 AFTER LT ENGINE START. MAINTENANCE DEFERRED NR 1 PACK IAW MEL 21-51-1.SDR REXA2013070801289Structure · chafedLEFT LOWER TRANSCOWL CHAFED. REPAIRED IAW REO 670-54-21-1028.SDR REXA2013070801290Structure · chafedLEFT UPPER TRANSCOWL CHAFED. REPAIRED IAW REO 670-54-21-1028.SDR REXA2013070801291Stand Off · crackedLEFT UPPER TRANSCOWL HAS A CRACKED STANDOFF. R & R IAW SRM 51-42-14 AND 51-42-21.SDR REXA2013062601219Riser · crackedPAX DOOR AFT RISER IS CRACKED AT SECOND STEP. A251-010. REPAIRED PAX DOOR AFT STAIR RISER AT SECOND STEP IAW REO 670-52-11-104. OPS CHECK OF PAX DOOR GOOD IAW AMM 52-11-00.SDR REXA2013062501259Stand Off · crackedRT LOWER, LT UPPER TRANSCOWL HAS A CRACKED STANDOFF. R & R CRACKED STANDOFF IAW SRM 51-42-14.SDR REXA2013062401218Skin · chafedFLAP PANEL 684ET CHAFED. FABRICATED NEW PANEL IAW SRM 51-40-11.SDR REXA2013062001459Pad · chafedLEFT UPPER TRANSCOWL HAS TWO CHAFED LATCH PADS. R & R PADS IAW SRM 51-42-06.SDR REXA2013061601000Housing · gougedUPON REMOVAL OF LT ENGINE AFT THRUST MOUNT SPHERICAL BUSHING HOUSING, FOUND OTBD RIB HOUSING BORE GOUGED. REPAIRED LT ENG AFT THRUST MOUNT SPHERICAL BUSHING HOUSING ON OTBD RIB IAW REO 690-54-51-010 AND EO R54093.SDR REXA2013061601001Exhaust Pipe · chafedNR 2 EXAUST NOZZLE INBD OUTER SKIN CHAFED. REPAIRED NR 2 EXHAUST NOZZLE INBD OUTER SKIN IAW REO 690-71-13-008.SDR REXA2013060800986Stand Off · crackedLEFT LOWER, LEFT UPPER TRANSCOWL INBD STANDOFF CRACKED. R & R LEFT UPPER TRANSCOWL INBD STAND OFF IAW SRM 51-42-14 AND SRM 51-42-21. AAR-R S/M 4, AAR A-263.SDR REXA2013060800987Pad · wornNR 2 NOZZLE STAND OFF PAD WORN. R & R IAW SRM 54-13-00, 54-13-01.SDR CA130603016Control Valve · failed(CAN) CREW REPORTED STRONG BURNING SMELL IN FLIGHT DECK AND CABIN ON FINAL APPROACH FLIGHT ATTENDANT REPORTED LIGHT HAZE OR SMOKE IN THE CABIN. MAINTENANCE FOUND RIGHT FLOW CONTROL VALVE INOP. ACS CONTROLLER NOT ABLE TO CONTROL FLOW CONTROL VALVE. MAINTENANCESDR CA130529006Floorbeam · corroded(CAN) DURING A HEAVY MAINTENANCE VISIT, THE FLOOR BEAM (LEFT HAND SIDE, BEHIND THE CAPTAIN`S SEAT) AT FS 280 WAS FOUND TO BE CORRODED. THE CORROSION WAS CLASSIFIED AS LEVEL 2 AND MEASURED 10" LENGTH X 1" WIDTH AND .018" DEPTH. THIS BEAM ITSELF IS .040" THE CORSDR CA130514005Tire · failed(CAN) AT 120 KNOTS, THE CREW FELT A BUFFET AND THEY REJECTED THE TAKEOFF. THE BUFFET WAS DUE TO THE FACT THAT BOTH LT MAIN TIRES BLEW. CREW STOPPED ON RUNWAY AND IT WAS CLOSED. BOTH LT TIRES WERE COMPLETELY GONE AND THEY WERE ON THE RIMS. ACFT WAS TOWED OFSDR CA130515003Computer · failed(CAN) DURING APPROACH, TERRAIN NOT AVAIL, EICAS MESSAGE IS SHOWN. LATER ON, AURAL WARNING, TOO LOW TERRAIN, IS HEARD. ABORTED APPROACH DUE TO BAD WEATHER AND RETURN TO ORIGIN AIRPORT. ACFT RELEASED TO SERVICE. EGPWS COMPUTER REPLACED AFTER 2 SUBSEQUENT FSDR CA130418003Ballast · overheated(CAN) CLIMBING THROUGH 12000, THE F/A REPORTED AN ELECTRICAL ODOR AROUND ROW 17. ACFT RETURNED TO DEPARTURE POINT. MAINTENANCE ACTION DETERMINED THAT THE SIDEWALL LIGHTING BALLAST AT ROW 18 TO BE AT FAULT. THE BALLAST WAS THEN REMOVED, THE CONNECTORS WERE STSDR CA130411003Proximity Sensor · out of rig(CAN) ON CLIMBOUT, DURING GEAR RETRACTION THE CREW GOT A GEAR DISAGREE MSG AND THE GEAR DID NOT RETRACT. THE CREW ACTIONED THE QRH AND THE GEAR WAS PUT DOWN IN THE LOCKED POSITION WITH 3 GREEN. AFTER TALKING TO MAINTENANCE, THE CREW TRIED TO RETRACT THE GEARSDR CA130410004Acm · failed(CAN) CREW REPORTED ODOR AND SMOKE IN CABIN DURING TAXI. SMOKE DISSIPATED. ACFT RETURNED TO GATE. ON TAXI BACK TO GATE RT PACK, AUTO FAIL, CAUTION CAME ON.SDR REXA2013040500727Blade · lack of lubeON FLIGHT 3814 (ATL TO IAD) ON TAKEOFF CREW NOTICED THAT THE LEFT ENG FAN VIBE IN YELLOW (1.9) HAD TO KEEP POWER BELOW 76% N1 TO KEEP VIBRATION IN GREEN RANGE. CREW ACCOMPLISHED QRH AND PERFORMED AIR RETURN TO ATL. APPLIED LUBRICATION ON THE FAN BLADE IAW CRSDR CA130403004Cable · frayed(CAN) DURING MAINTENANCE INSPECTION OF THE MAIN CABIN DOOR THE PRESSURE VENT FLAP ICE BREAKER CABLE WAS FOUND TO HAVE MANY BROKEN STRANDS AT THE SWAGED END. CABLE TO BE REPLACED IAW THE AMM.SDR UHLA2013040200111Compressor · damagedAT FL180 E1 SURGED REPEATEDLY. ENGINE 1 CONTROL FAULT CAME ON EICAS. FOLLOWED QRH AND THRUST WAS UNSTABLE. PERFORMED INFLIGHT SHUTDOWN OF ENGINE 1 AND RETURNED TO DTW. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MTX PERFORMED BOROSCOPE OF ENG 1 IAW GE MMSDR CA130403001Acm · seized(CAN) DURING TAXI OUT, SMOKE AND AN ABNORMAL ODOR WAS NOTICED IN THE CABIN AND COCKPIT. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO THE GATE WHERE PASSENGERS WERE DEPLANED. DURING TROUBLESHOOTING, THE MAINTENANCE DIAGNOSTIC COMPUTER, MDC, REVEALED AN OVER TSDR CA130325012Duct · ruptured(CAN) AFTER TAKEOFF THE CREW RECEIVED A RT COWL ANTI-ICE DUCT WARNING MESSAGE. THE ACFT RETURNED TO THE DEPARTURE AIRPORT. CONTRACT MAINTENANCE INSPECTED THE ACFT AND FOUND A LOOSE CLAMP AT THE WING ANTI-ICE VALVE. THE CLAMP WAS TIGHTENED AND THE ACFT RETURSDR CA130326005Hose · ruptured(CAN) AFTER DEPARTURE THE ACFT LOST ALL OF THE NR 3 HYDR SYS FLUID AND RECEIVED THE ASSOCIATED SYS CAUTION MESSAGES. THE ACFT RETURNED TO THE DEPARTURE AIRPORT AND CARRIED OUT AN ALTERNATE LANDING GEAR EXTENSION AND LANDED SAFELY. MAINTENANCE INVESTIGATION FO
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