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 = 'CF348C1' 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 = 'CF348C1' 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 SIMA20131210009Engine · vibrationON FLIGHT 3604 DURING CLIMB OUT CREW REPORTED N1 FAN VIBRATION PEAKED AT 1.7 WITH THRUST LEVERS IN CLIMB DETENT. WHEN LEVEL AT FL340 N1 FAN VIBRATION EXCEEDED GREEN LIMITS & PEAKED AT 2.0 WITH THRUST LEVERS IN CRZ SETTING. THE VIBRATION FAULT THROUGH ENTIRE SDR CA131209005Gcu · failed(CAN) CAPTAIN STATED ALL PHASES OF THE FLIGHT WERE NORMAL, BOTH GENERATOR 1 & 2 ON LINE, BUT PASSING 11000 FT ON DESCENT, THE NR 1 IDG WENT OFFLINE AND THE ADG AUTO DEPLOYED. FOLLOWED QRH AND STARTED THE APU AND POWER RETURNED. THE NR 2 GENERATOR APPARENTLSDR CA131209012Actuator · failed(CAN) SLAT FAIL ON APPROACH.SDR SWIA201334690Fmu · failedWHILE ADVANCING POWER FOR TAKEOFF, N1 DID NOT INCREASE & ITT REACHED 1027° ON RT ENGINE. REJECTED THE TAKEOFF & RT ENGINE AUTO SHUTDOWN. RETURNED TO GATE. FLT#4963 REPLACED RT ENGINE FUEL METERING UNIT & OPERABILITY BLEED VALVE. PERFORMED BORESCOPE INSPECSDR SWIA201334555Link · damagedRT ENGINE FWD ENGINE MOUNT LINK ASSEMBLY HAS PITTING. C-CHECK REPLACED RT ENGINE FWD MOUNT LINK ASSEMBLY.SDR CA130912005Spoiler Sys · failed(CAN) TSB REPORTED ON SEPTEMBER 12, 2013 FLIGHT CREW RECEIVED EICAS CAUTION MESSAGES "INBD FLT SPOILERS" AND "INBD SPOILERONS". THE CREW FOLLOWED THE AOM VOL 1 PROCEDURES AND DECLARED AN EMERGENCY. THE ACFT PERFORMED AN UNEVENTFUL LANDING WITH ARFF STANDING SDR CA130820006Hose · failed(CAN) DURING APPROACH, CREW NOTICED ON EICAS THE HYDRAULIC NR 3 LEVEL AT 10 PERCENT. AFTER NORMAL GEAR EXTENSION, THE LEVEL WAS AT ZERO. CREW COMPLIED WITH QRH AND DECLARED PAN/PAN. ACFT GAINED PARKING POINT. DURING WALK-AROUND CREW NOTICED A LARGE HYD LEAKSDR CA130828010Bleed Valve · malfunctioned(CAN) RIGHT ENGINE FLAMED OUT ON LANDING DURING APPLICATION OF THRUST REVERSER. ENGINE WAS REPLACED.SDR CA140218011Cotter Pin · sheared(CAN) DURING SB 670BA-53-042 INSPECTION, A SHEARED OFF COTTER PIN WAS DETECTED AT CENTER FUSELAGE AREA RT FWD. KEEL-BEAM LINK, AFT ATTACHMENT, NUT IS LIGHTLY LOOSENED. IAW STANDARD PRACTICE, NUT WAS RE-TORQUED AND A NEW COTTER PIN WAS INSTALLED.SDR SWIA201333711Plug · leakingOIL LEVEL DROPPED TO 17 PERCENT DURING FLIGHT. REPLACED SPLINE PLUG, RAN LT ENGINE AT 85 PERCENT N2 AND SHUTDOWN ENGINE TO CHECK FOR LEAKS. COMPLIED WITH LEAK CHECK OF LT ENGINE BOTH OIL AND HYD WITH NO LEAKS NOTED.SDR MASA2013061852487Engine · fodFOD EVENT DURING GROUND OPERATIONS, ENGINE WAS INSPECTED AND ACFT FERRIED TO MX BASE FOR ENGINE REPLACEMENT.SDR N6WA2013052203Engine · malfunctionedOBSERVED POWER LOSS ON NR 2 ENGINE AT ROTATION. OBSERVED ENGINE SURGING N1 FROM 80 TO 70 PERCENT, HEARD POPPING SOUND, SHUTDOWN ENGINE IAW QRH. R & R NR 2 ENGINE IAW AMM 71-00-00, SP-09 FOR COMPLETION OF RUNS AND RII'S.SDR CA130429004Door · out of rig(CAN) SHORTLY AFTER TAKEOFF THE CREW HEARD A LOUD MECHANICAL NOISE FROM THE NOSE LANDING GEAR AREA. THE NOISE WAS REPEATED APPROXIMATELY EVERY 7 SECONDS. ALL INDICATIONS AND THE FLIGHT BEHAVIOR OF THE ACFT WAS NORMAL. THE PILOT DECLARED EMERGENCY AND DECIDEDSDR CA130508005Flap System · failed(CAN) CREW REPORTED ENROUTE AFTER FLYING AT FL 390 FOR 20 MINUTES WE RECEIVED CAUTION MESSAGE, FLAPS FAIL, IT NEVER WENT AWAY. ACFT DID A ZERO FLAPS LANDING. MAINTENANCE CLEARED FLAPS INHIBITS THROUGH THE MDC AND PERFORMED AN OPS CHECK OF THE FLAPS IAW AMM 27SDR CA130508006Flap System · failed(CAN) CREW REPORTED "FLAPS FAIL" CAUTION MESSAGE RIGHT AFTER LEVEL OFF AT FL 380 A/C PREFORMED A ZERO FLAPS LANDING. PART REMOVED: DETECTOR, SKEW, FLAP TRACK, INBD PN 5915549 REMOVED.SDR CA130429003Grommet · unsecure(CAN) RT AILERON WAS BLOCKED A SHORT TIME. MAINTENANCE PERFORMED A DETAILED INSPECTION OF THE RT AILERON CONTROL CIRCUIT, AILERON QUADRANT AND AILERON HINGES. NEAR THE RT BPSU THERE WAS A GROMMET MISSING. THIS MISSING GROMMET WAS FOUND ON THE AILERON CABLE NSDR CA130417004Window · cracked(CAN) LEFT SIDE WINDOW CRACKED DURING FLIGHT.SDR SWIA201333138Engine · overtempLIGHTNING STRIKE ON RIGHT SIDE, ITT IMMEDIATELY WENT ABOVE RED LINE AND NUMBER 2 ENGINE SHUT DOWN. (FLT 4756) PERFORMED BOROSCOPE INSP AND OVERTEMP INSP. ALL PARAMETERS NORMAL AT THIS TIME. OPS CHECK GOOD.SDR CA130325010Acm · failed(CAN) CREW REPORTS LT PACK AUTO FAIL CAUTION MESSAGE ON TAKEOFF. MESSAGE CLEARED SHORTLY AFTER ROTATION. SMOKE IN FLIGHT DECK AND CABIN. ACFT RETURNED TO THE FIELD.SDR V0XR20130219J0166Attach Fitting · gougedLT ENGINE LOWER C DUCT HINGE ATTACH POINT GOUGED. REO 670-78-34-989 REV NC HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RIIS HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTSDR CA130122008Idg · failed(CAN) ON APPROACH, BOTH GENERATORS DROPPED OFFLINE AND ADG DEPLOYED. CREW DECLARED AN EMERGENCY. THERE WAS ALSO REPORT OF SMOKE AFT LAV MSG. NTSB IS INVESTIGATING. FDR/CVR ARE IN QUARANTINE. RT IDG WAS R & R. THE NR 1 GCU WAS R & R.SDR CA130109003Unknown · smoke(CAN) SMOKE IN LAVATORY INDICATION AND ODOR OF ELECTRICAL BURNING IN CABIN.SDR CA130107009Torque Tube · corroded(CAN) TROUBLESHOOTING FLAP FAIL CAUTION, FOUND FLAP TOQUE TUBE INBD OF LT NR 2 ACTUATOR SEVERLY CORRODED AND NEARLY SHEARED.SDR N6WA20121226001Engine · malfunctionedRIGHT ENGINE DEGRADED, CAUTION MESSAGE ON TAKEOFF. PERFORMED 3 ENGINE STARTS AND CLEARED FAULTS IAW AMM 72-00-00.SDR N6WA20120701Fmu · failedRIGHT FADEC MESSAGE ON TAKE OFF ROLL. REMOVED & REPLACED NR 2 ENGINE FMU PER AMM. OP'S CHECKED GOOD AT THIS TIME.SDR SWIA201232303Engine · vibrationNR 2 ENGINE VIB 1.7 - 1.9 IN CLIMB, C 38.000 FEET, VIB JUMPED TO 3.5 - 3.7, DECLARED EMERGENCY. (FLT 6209) SHOOK OUT RT ENGINE FAN BLADES IAW AMM, GROUND RUN ENGINE VIB ARE NORMAL.SDR CA121205006Acm · failed(CAN) AFTER REACHING THE PARKING POSITION AND AFTER ENGINE SHUTDOWN AND APU RUNNING THERE WAS STRONG SMOKE DEVELOPMENT IN THE COCKPIT AND THE CABIN. THE PIC DECIDED TO EVACUATE THE CABIN. AFTER INVESTIGATION THE ACM WAS FOUND STUCK. THE LT ACM WAS REPLACED SDR CA121112002Light · overheated(CAN) ELECTRICAL ODOR IN COCKPIT. FLOOD LIGHT FOUND AT FAULT 2LA006913 & 8722,00.SDR ASOA2012101102342Sill · corrodedPAX DOOR SILL ANGLE HAS CORROSION AROUND FASTENER HOLES. REMOVED CORRODED PAX DOOR SILL ANGLE. LOCATED DRILLED NEW PARTS IAW SRM 51-40-11-001-001-A01, INSTALLED NEW PARTS IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-45-00-001-001-A01.SDR V0XR20120924J0104Floor Support · corrodedFS 279 FLOOR SUPPORT CORRODED AT BL 0 BEYOUND SERVICEABLE LIMITS. R & R FLOOR SUPPORT AT FS 279 BL 0 IAW SRM 51-42-06.SDR N6WA2012092001Warning Light · false activationSTALL FAIL MASTER CAUTION. PERFORMED OPS TEST OF STALL PROTECTION SYS IAW AMM 27-35-00. OP'S CHECKED GOOD.SDR N6WA2012092002Light · inoperativeCEILING EMERGENCY FLOOD LIGHT ROW 15 INOPERATIVE.SDR N6WA2012092003Light · inoperativeCEILING EMERGENCY FLOOD LIGHT ROW 17 INOPERATIVE.SDR V0XR20120921J0098Angle · corrodedPASSENGER DOOR MID CAP ANGLE IS CORRODED. R & R PASSENGER MID CAP ANGLE IAW SRM 51-42-06 AND 51-40-11.SDR V0XR20120921J0099Floor Support · corrodedRT FORWARD FLOOR SUPPORT CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-06 AND 51-40-11.SDR V0XR20120921J0100Stringer · corrodedSTRINGER 27 IS CORRODED FROM STA 333 TO 364. R & R STRINGER 27 FROM BS 333 TO 364 IAW SRM 51-42-06.SDR V0XR20120921J0101Fitting · corrodedLT OTBD INTERCOSTAL FLOOR MOUNT MACHINE FITTING IS CORRODED. R & R LT OTBD INTERCOSTAL FLOORMOUNT MACHINE FITTING IAW SRM 51-40-11 AND 51-42-21.SDR V0XR20120921J0102Angle · corrodedPASSENGER DOOR AFT CLOSING ANGLE IS CORRODED. R & R AFT PASSENGER DOOR CLOSING ANGLE IAW SRM 51-40-11,51-42-06, AND 51-42-21.SDR V0XR20120921J0103Fitting · corrodedPASSENGER DOOR THRESHOLD FORWARD CLOSING FITTING IS CORRODED. R & R FORWARD CLOSING FITTING IAW SRM 51-42-06,51-40-11,51-42-21, AND51-21-11.SDR N6WA2012091902Light · unknownEMERGENCY EXIT SIGN LIGHT INOPERATIVE. OP'S CHECKED GOOD AT THIS TIME.SDR N6WA2012091903Sign · inoperativeFORWARD LOWER LT EMERGENCY EXIT SIGN INOPERATIVE. OP'S CHECK GOOD AT THIS TIME.SDR N6WA20120904Light · inoperativeROW 9 CEILING EMEGENCY LIGHT INOPERATIVE. R & R EMERGENCY POWER SUPPLY UNIT, IAW AMM 33-51-17, OP'S CHECKED GOOD AT THIS TIME.SDR CA120928007Hinge · failed(CAN) WHEN THE PASSENGERS WERE DISEMBARKING, THE TOP DOOR STEP COLLAPSED AND 1 PASSENGER FELL AND HURT HIS KNEE DOOR HINGE.SDR V0XR20120918J0096Stringer · crackedMAIN PASSENGER DOOR CRACKED AT STRINGER 3L. FOUND DURING COMPLIANCE OF SB 670BA-53-040, INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR ,HAVING SB REV A, AND SPECIFIC TO SB CONTENT PARA (PART B) METHOD, TECHNIQUES AND PRACTICES. ASDR V0XR201209180097Stringer · crackedLINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR IS CRACKED. COMPLIED WITH MFG SB 670BA-53-040, INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, HAVING SB REV A, AND SPECIFIC TO SB CONTENT PARA (PART B) METHOD, TECHNIQUES AND PRACTISDR N6WA2012091601Seal · dirtyPAX DOOR SQUEAL. CLEANED PAX DOOR SEAL AND OPS CHECK IAW AMM 52-11-07, OP'S CHECKED GOOD AT THIS TIME.SDR N6WA2012091402Door · out of adjustLOWER GREEN LOCK INDICATOR NOT ALIGNED WHEN MAIN CABIN DOOR IS CLOSED AND LOCKED. ADJUSTED DOOR RIG IAW AMM 52-11-00. FUNCTIONAL TEST OF PAX DOOR GOOD.SDR N6WA2012091201Controller · defectiveBOTH PACKS 1 & 2 CYCLING ON AND OFF IN FLIGHT. R & R AIR CONDITIONING CONTROLLER, OP'S CHECKED GOOD, IAW AMM 21-61-00. NO FURTHER DEFECTS NOTED.SDR N6WA2012091002Light · inoperativeROW 10 CEILING FLOOD LIGHT INOPERATIVE.SDR V0XR2012091288Fitting · corrodedINTERCOSTAL FLOOR MOUNT FITTING CORRODED. LT OTBD FITTING STA 282. R & R FLOOR MOUNT FITTING LT OTBD FITTING STA 282 IAW SRM 51-40-11, 51-42-06, 51-42-21.
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