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 aircraft_model_key = 'AW139' 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 aircraft_model_key = 'AW139' 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 DT1R2011102701Window · departedCO-PILOT DOOR WINDOW DEPARTED IN FLIGHT AT APPROX 150 KNTS. ACFT WAS SLOWED AND RETURNED TO FIELD WITHOUT INCIDENT. DOOR AND ACFT WERE NOT DAMAGED. WINDOW WAS NOT FOUND. DOOR WAS REMOVED, WIDOW SEAL AREA WAS INSPECTED AND REPAIRED TO PROPER THICKNESS FOR SSDR CA110922013Servo · faulty(CAN) ENROUTE, THE NR 2 HYDRAULIC SERVO CAS MESSAGE ILLUMINATED INTERMITTENTLY. ACFT DIVERTED, AFTER LANDING THE NR 2 HYDRAULIC SERVO CAS MESSAGE WAS ON STEADY. SYSTEM WAS TROUBLESHOT AND FAULTY SWITCH ON THE NR 3 SERVO, LOWER POSITION, WAS REPLACED WITH NEW SDR AC2A9DS08292011Warning Light · illuminatedSHORTLY AFTER DEPARTURE, "1 HYD MIN" AND "EMER LDG PRESS" ILLUMINATED. REFERENCED THE SYNOPTIC PAGE AND STARTED THE RETURN TRIP. APPROX 90 SECONDS LATER, "1 HYD OIL PRESS", "1 SERVO" AND "1 HYD PUMP" ILLUMINATED.SDR CA120306002Exhaust Duct · buckled(CAN) EXHAUST NOZZLE SUSTANED EXTENSIVE BUCKLING DAMAGE ON THE BODY OF UNKNOWN CAUSE. RULED OUT GROUND MISHANDLING.SDR CA110727001Gearbox · damagedTAIL ROTOR FIPS SLIP RING WAS FOUND SEPARATED FROM THE GEARBOX AT THE DI. DAMAGE ALSO FOUND TO T/R GEARBOX.SDR CA110629001B-Nut · leakingWHILE CARRYING OUT THE DAILY INSPECTION, A SMALL POOL OF HYD FLUID WAS NOTICED ON UPPER DECK. ON INVESTIGATION, HYD FLUID FOUND AROUND THE B-NUT ON NR 1 HYD PUMP PRESURE LINE. A SERVICABLE LINE FROM ANOTHER ACFT WAS USED. HYD SYS BLEED AND LEAK CHECKED. ACFTSDR CA110531010O-Ring · leakingWHILE TAXIING OUT PRIOR TO DEPARTURE CREW NOTICED A CAS, " NR2/ NR4 HYD LOW". ACFT WAS TURNED AROUND AND RETURNED TO THE FBO AND ENGINES WERE SHUTDOWN. INVESTIGATION REVEALED NR 2 HYD SYS HAD DRAINED OUT. LEAKAGE WAS NOTED AT THE FITTING END OF THE NR 2 HYD SDR CA110509003Line · leakingDAILY INSPECTION FOUND HYD PRESSURE HOSE TO BE LEAKING. NR 2 SYS PRESSURE HOSE FROM THE TEE FITTING TO THE RT SERVO FOUND TO BE LEAKING FROM A PIN HOLE IN THE RUBBERIZED OUTER COVER. ACFT GROUNDED, DOM INFORMED AND PARTS PLACED ON ORDER.SDR DT1R20110328001Wire · misrepairedDURING THE INSPECTION, CUSTOMER FOUND 63 OUT OF 92 SOLDER SPLICES INSTALLED ON THE ACFT WERE BAD. ALL THE SPLICES HAD FAILED FOR THE SAME REASON, SOLDER HAD NOT FLOWED TO THE STUB WIRE SIDE OF THE CONNECTION. OF THE FAILURES THE NR 2 MAU, THE NR 2 MRC, THE PSDR AC2R9JP03062011Link · crackedFOUND MAIN ROTOR TENSION LINK CRACKED DURING VISUAL INSPECTION. REPLACED TENSION LINK.SDR CA110106011Smoke Detector · failedDURING UNSCHEDULED MAINTENANCE, THE SMOKE DETECTOR HAD TO BE DISCONNECTED FOR ACCESS. AN HIGHER THAN NORMAL FORCE WAS REQUIRED TO DISCONNECT THE CONNECTOR FROM THE UNIT. ONCE THE CONNECTOR WAS REMOVED, PIN NR 7 ON SMOKE DETECTOR UNIT WAS NOTICED TO BE BENT 9SDR CA101018001Engine · failed(CAN) IFSD ON APPROACH TO LANDING, OPERATOR EXPERIENCED HEAVY VIBRATION THEN A RISE IN ITT AND TQ. ENGINE WAS SHUTDOWN AND SECURED. A SINGLE ENGINE LANDING WAS MADE WITH NO ISSUES. TROUBLESHOOTING IS ON GOING.SDR 2010FA0000922Skin · delaminatedWHILE CONDUCTING A POST FLIGHT INSP, THE FLIGHT CREW NOTICED THAT THE TAILBOOM HAD AN AREA THAT WAS DELAMINATED ON THE RT SIDE OF THE TAILBOOM. THIS IS IN THE SAME CRITICAL AREA THAT HAS BEEN ADDRESSED BY AD 2009-19-51. IN ADDITION TO THE DELAMINATED AREA, THESDR ULXR2009091683124Blade · debondedTAIL ROTOR BLADE LEADING EDGE STRIP DEBONDING.SDR U0GA2009080782739Fitting · crackedDURING INSP FOUND CRACKED TAILBOOM FITTING.SDR ULXR2009080483136Indicator · malfunctionedIN FLIGHT CAS MESSAGE INTERMITTANTLY ILLUMINATED: NR 1 AHRS FAIL, NR 1 AP FAIL, AFCS DEGRADED, AVIONICS FAIL. REPLACEMENT OF AHRU CORRECTED THE SQUAWK.SDR ULXR2009070882607Probe · inoperativeRT SECONDARY FUEL PROBE FAILED, SYS INDICATED ZERO. CAS MESSAGE NR2 FUEL PROBE. PROBE REPLACEMENT FIXED PROBLEM.SDR ULXR2009070282608Unknown · multiple failLOW TORQUE INDICATION (30-40 PERCENT) ON BOTH PILOT'S AND COPILOT'S PFD/MFD DURING MAX GROSS WEIGHT TAKEOFF. CAS INDICATIONS: 1 AP FAIL, AVIONIC FAULT, 1 AHRS FAIL, AFCS DEGRADED.SDR ULXR2009062682285Hook · unserviceablePERFORMED SB 42315-489-01, THE HOOK HAS UNACCEPTABLE IRREGULARITIES AND DISCONTINUITIES. REMOVED HOOK FROM SERVICE.SDR ULXR2009062682284Hook · unserviceablePERFORMED SB 42315-489-01, THE HOOK HAS UNACCEPTABLE IRREGULARITIES AND DISCONTINUITIES. REMOVED HOOK FROM SERVICE.SDR ULXR2009050581806Sleeve · wornSLEEVE INTERNAL BORE WORN BEYOND LIMITS.SDR U0GA120488Fire Warning · activatedMULTIPLE CAS MESSAGES TO INCLUDE ENG FIRE, BAG FIRE, EEC FAILS NUMEROUS OTHERS. CAPTAINS A/S, VSI AND ALTIMETER AND NR 2 PI INDICATION FAILED. (K)
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