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 = '400A' 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 = '400A' 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 DJFA20120705001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT LEFT HORIZONTAL CANTED STATION 13.78, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. TSDR DJFA20120705002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT LEFT HORIZONTAL CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. TSDR DJFA20120705003Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT LEFT HORIZTONAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. TSDR DJFA20120705004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT LEFT HORIZTONAL CANTED STATION 62.20, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. TSDR DJFA20120705005Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT RIGHT HORIZTONAL CANTED STATION 13.78, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. SDR DJFA20120705006Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT RIGHT HORIZTONAL CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. SDR DJFA20120705007Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT RIGHT HORIZTONAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. SDR DJFA20120705008Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT RIGHT HORIZONTAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. SDR DJFA20120705009Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT RIGHT HORIZTONAL CANTED STATION 62.20, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. SDR DJFA20120702002Control Valve · failedON LANDING, CREW REPORTED LOSS OF BRAKING ACTION WITH THE ANTI-SKID SYSTEM ON. WITH ANTI-SKID SYSTEM TURNED OFF, THE BRAKES WORK NORMALLY. MX DETERMINED THE ANTI-SKID BRAKE CONTROL VALVE FAILED. THE VALVE WAS REPLACED.SDR DJFA20120702001Control Valve · failedON LANDING, CREW REPORTED LOSS OF BRAKING ACTION WITH THE ANTI-SKID SYSTEM ON. WITH ANTI-SKID SYSTEM TURNED OFF, THE BRAKES WORK NORMALLY. MAINTENANCE DETERMINED THE ANTI-SKID BRAKE CONTROL VALVE FAILED. THE VALVE WAS REPLACEDSDR DJFA20120701001Brake Sys · contaminatedWHILE TAXIING, CREW REPORTED EXCESSIVE PRESSURE REQUIRED TO OPERATE THE BRAKES WITH THE ANTI-SKID SYS ACTIVATED. DEACTIVATION OF THE ANTI-SKID SYSTEM RESULTED IN NORMAL BRAKING ACTION. MX FOUND THAT THERE WAS EXCESSIVE AIR IN THE LINES. SYS WAS BLED AND NO SDR CA120709001Engine · flamed out(CAN) IT WAS REPORTED THAT DURING FLIGHT AT 45,000 FT BOTH ENGINES FLAMED OUT AND RE-LIT IN-FLIGHT. FURTHER COMMUNICATION WITH THE OWNER REVEALED THAT BOTH ENGINES WERE NOT RUNNING WHEN THE ACFT LANDED. THE CREW PERFORMED A DEAD STICK LANDING SAFELY. TROULBSDR DJFA20120626001Bulb · inoperativeDURING PREFLIGHT INSPECTION, WITH ACFT POWER ON, THE CREW REPORTED A ZAPPING SOUND FOLLOWED BY A SMALL AMOUNT OF SMOKE NEAR THE PILOT'S YOKE. MX PERSONNEL FOUND THE BULB ON THE PILOT'S CHART HOLDER (ATTACHED TO THE YOKE) SEVERELY BURNED. THE BULB WAS REPLACESDR DXTA2012062505016Hinge · crackedDURING LANDING CHECKLIST, PUT LANDING GEAR DOWN WITH 3 POSITIVE GREEN LIGHT INDICATIONS WITH BOTH RED LIGHT IN THE GEAR HANDLE STAYED ILLUMINATED. EXECUTED CHECKLIST WITH NO POSITIVE RESULTS. BOTH RED LIGHT ON THE GEAR HANDLE STAYED ILLUMINATED AT ALL TIME.SDR DXTA2012062205009Landing Gear · malfunctionedON APPROACH, EXPERIENCED AN UNSAFE RED LIGHT IN THE GEAR HANDLE, ACCOMPANIED WITH THE AURAL GEAR-WARNING HORN AFTER SELECTING FLAPS FROM 20 TO 30 DEGREES. AFTER ABORTING THE APPROACH TO COMPLETE RELEVANT CHECKLIST, RETRACTED THE FLAPS, WHICH SILENCED HORN, BSDR 9JLA201271904219Motor · defectiveCREW REPORTED THAT THE AIR CONDITIONING WAS INOPERATIVE. TROUBLESHOOTING IDENTIFIED THE AIR CON COMPRESSOR MOTOR AS DEFECTIVE. A MODIFIED MOTOR WAS INSTALLED, FUNCTIONAL CHECKED SATISFACTORY.SDR 9JLA2012071704219Motor · overheatedTHE CREW REPORTED THE AIR CONDITIONING SYSTEM INOPERATIVE. TROUBLESHOOTING FOUND THE AIR CONDITIONER COMPRESSOR MOTOR DEFECTIVE. A MODIFIED MOTOR WAS INSTALLED. OPS CHECKS GOOD.SDR DJFA201206150001Wire · meltedWHILE CARRYING OUT A D-CHECK INSPECTION, THE WIRING AT THE RT GCU WIRE BUNDLE S220 IT WAS NOTED THAT THE SHIELDED WIRE HAD MELTED INTO THE HARNESS AT THE CONNECTOR GOING INTO THE RT GCU. THIS WIRE WAS REPLACED.SDR DJFA20120604008Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSEMBLY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT LEFT HORIZTONAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLSDR DJFA20120610001Windshield · crackedDURING CRUISE FLIGHT, CREW REPORTED THE RT MAIN WINDSHIELD CRACKED. CREW INITIATED EMERGENCY DESCENT AND LANDED SAFELY. MX PERSONNEL REPLACED THE FAILED WINDSHIELD.SDR UG8A201206190001Oxygen Mask · separatedDURING A DECLARED EMERGENCY FOR SMOKE AND HEAT IN COCKPIT, THE PILOT OXYGEN MASK BROKE UPON DEPLOYMENT. IT APPEARS THE MASK WAS DEFECTIVE. IT WAS IN DUE O/H BY THE END OF JUNE 2012. THE MASK WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE.SDR UG8A20120610660A/C Pack · failedSMOKE AND UNCOMMANDED HEAT IN COCKPIT SHORTLY AFTER TAKEOFF. THE FREON AIR CONDITIONING SYS HAD BEEN DEFERRED DUE TO A DAMAGED DRIVE BELT REQUIRING REPLACEMENT. THE (M) PROCEDURE 21-50.1 CALLED FOR THE "AIR COND" CIRCUIT BREAKER TO BE PULLED/COLLARED. WITH SDR DXTA2012061104995Landing Gear · unknownLANDING GEAR HANDLE PLACED DOWN, GEAR DID NOT EXTEND SLOW TO EXTEND. REMOVED CONNECTOR PLUG AND CHECKED PINS AND PLUG WITH NO DISCREPANCIES NOTED. CLEANED AND LUBRICATED SELECTOR HANDLE, SECURED CONNECTOR PLUG, AND PERFORMED MLG FUNCTIONAL CHECK. OPS CHECKESDR 2012FA0000446Wire · chafedACFT EXPERIENCED LOSS OF ALL NORMAL ELECTRICAL POWER AT FL400. EMERGENCY POWER WAS AVAILABLE AND OPERATED NORMALLY. BOTH ENGINES AND ASSOC FADEC ENGINE CONTROLS CONTINUED TO OPERATE NORMALLY. CREW HEARD A LOUD POP IN THE AREA OF THE CIRCUIT BREAKER PANEL ASDR DJFA20120607009Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT LT HORIZONTAL CANTED STA 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RSDR DJFA20120607008Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STA 13.78, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE SDR DJFA20120607007Rib · crackedDURING INSP FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STA 62.20, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBS WSDR DJFA20120607006Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT LT HORIZONTAL CANTED STA 13.78, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RSDR DJFA20120607005Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT LT HORIZONTAL CANTED STA 29.92, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBS WESDR DJFA20120607004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STA 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBS WESDR DJFA20120607003Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT LT HORIZ CANTED STA 62.20, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBS WERE RESDR DJFA20120607002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STA 29.92, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RSDR DJFA20120607001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STA 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RSDR DJFA20120604009Fitting · crackedDURING INSPECTION OF THE HORIZONTAL STABILIZER, THE AFT PIVOT FITTING WAS FOUND CRACKED AT THE LOWER BOLT HOLE. THE AFT PIVOT FITTING WAS REPLACED.SDR DJFA20120604001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSEMBLY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT RIGHT HORIZTONAL CANTED STATION 13.78, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOSDR DJFA20120604002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSEMBLY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT LEFT HORIZTONAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLSDR DJFA20120604003Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSEMBLY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT LEFT HORIZTONAL CANTED STATION 62.20, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLSDR DJFA20120604004Rib · crackedDURING INSPECTION, FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSEMBLY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT RIGHT HORIZTONAL CANTED STATION 62.20, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOSDR DJFA20120604005Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED. ON THE LOWER FLANGE AT LEFT HORIZTONAL CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. SDR DJFA20120604006Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EA RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STA 29.92, BETWEEN SDR DJFA20120604007Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZONTAL CANTED STA 13.78, BETWEESDR DXTA2012052404978Wire · burnedDURING APPROACH, CREW SMELLED ELECTRICAL SMOKE (NOT VISIBLE). ON LANDING, DISCOVERED "PWR FDR" 1/2A BREAKER (ON STBY PWR PANEL) POPPED. T/S & FOUND RCCB 8 & 107 REMAINING OPEN R & R. ALSO FOUND BURNED WIRE H131A8 & BURNED CONTACT ON CURRENT SENSOR. R & R WSDR BP5A20120525001Rib · crackedWHILE AIRCRAFT UNDERGOING A/B SCHEDULED CHECK, PERFORMED BOROSCOPE INSPECTION OF HORIZONTAL STABILIZER RIBS FOR CRACKS IAW 400A ALM 04-00-02-001. FOUND NUMEROUS CRACKS FROM FASTENER HOLES AT 12 LOCATIONS ON LEFT STABILIZER RIBS, LOWER ATTACH LEGS. REMOVED SSDR DJFA20120517001Diffuser · brokenPRIOR TO FLIGHT, A CREW NOTICED DAMAGE TO THE RT ENGINE NOISE SUPPRESSOR (DIFFUSER). MX VERIFIED THE FAILURE. AN ENGINE BOROSCOPE INSPECTION WAS PERFORMED AND NO ADDITIONAL DAMAGE WAS FOUND. THE NOISE SUPPRESSOR WAS REPLACED AND THE FAILED UNIT SENT BACK FOSDR 2012FA0000340Wire · shortedDURING A D-CHECK INSPECTION, WIRING IN AFT BAGGAGE LT LOWER AREA, IT WAS NOTED THAT THERE WERE SOME BURNED WIRES ON THE P489 CONNECTOR. THESE HAD SHORTED OUT AND HAD BURNED THRU THE INSULATION. THE GROUNDED SHIED WIRE W811 HAD MELTED INSULATION AND FUSED TO SDR 2012FA0000339Wire · shortedDURING A D-CHECK INSPECTION, WIRING IN THE AFT BAGGAGE RT LOWER AREA IT WAS NOTED THAT THERE WERE SOME BURNED WIRES ON THE P490 CONNECTOR. THESE HAD SHORTED OUT AND HAD BURNED THRU THE INSULATION. THE GROUND SHIELD WIRE W812 HAD MELTED INSULATION AND FUSED SDR DJFA20120508002Rib · crackedDURING SCHDULED INSPECTION, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPSDR DJFA20120508003Rib · crackedDURING SCHDULED INSP, MX TECH FOUND 8 RIBS CRACKED IN THE HORIZ STAB. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPLACED ISDR DJFA20120508004Rib · crackedDURING SCHDULED INSP, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPLACED
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