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 = '340B' 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 = '340B' 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 NSVA2010235Smoke Detector · faultyAVIONICS SMOKE LIGHT ILLUMINATED. REPLACED AVIONICS SMOKE DETECTOR.SDR NSVA2010236Control Valve · malfunctionedLT DUCT OVERTEMP ILLUM SENT ROAD TRIP, REMOVED AND REPLACED DUAL TEMP CONTROL VALVE. OPENED MEL 21-60-2 FOR AUTO MODE BEING INOP.SDR MALA100207Uplock · icedAFTER TAKEOFF LANDING GEAR "IN TRANSIT" LIGHT REMAINED ON. RECYCLED GEAR IAW NON-NORMAL CHECKLIST. LIGHT REMAINED ON AFTER GEAR SELECTED UP AGAIN. COMPLETED REMAINDER OF FLIGHT WITH GEAR DOWN IAW CHECKLIST. ALL HYD INDICATIONS NORMAL. UPLOCK PADS WERE CHESDR NSVA2010234Valve · malfunctionedLOSS OF BRAKE PRESSURE ON FINAL. REMOVED AND REPLACED BRAKE VALVE, LANDING GEAR CONTROL VALVE AND NR 4 WHEEL SPEED TRANSDUCER.SDR NSVA2010233Wire · disconnectedDURING APPROACH CREW DID NOT GET THE 3 LANDING GEAR SAFE INDICATION. CREW COMPLIED WITH QRH AND DID GET THE 3 GREEN INDICATION. DCA TOWER REQUESTED A FLYBY AND CLEARED THE AIRCRAFT TO LAND, BUT DID DISPATCH EMERGENCY EQUIPMENT AS PRECAUTION. THE FLIGHT LANDSDR NSVA2010232Frame · crackedPERFORM PERMANENT REAIR OF CRACK DAMAGE IN FRAME FLANGE IAW TD 340-55-10-15.SDR MALA100206Pump · inoperativeDURING LANDING GEAR EXTENSION, HYD CAUTION LIGHT CAME ON WITH ZERO MAIN ACCUMULATOR PRESSURE AND ZERO HYD QUANTITY. OTHER ACCUMULATORS SHOWED ABOUT 2800 PSI. REPLACED HYD LINE AS REQ. REPLACED HYD PUMP AS PRECAUTIONARY PN ON/OFF 40185-02, SN ON KG73, SN OFFSDR NSVA2010230Pressure Switch · malfunctionedGEAR TOOK ABOUT 4 MINUTES TO COME UP HYD PUMP RAN CONTINOUSLY. RAN QRH CYCLED GEAR THEN CAME UP NORMALLY. COULD NOT DUPLICATE DISCREPENCY. REPLACED HYDRAULIC AUTO PRESSURE SWITCH. REPLACED HYDRAULIC RESEVOIR, BLED SYS AND SERVICED; PERFORMED NUMEROUS GEAR SDR NSVA2010229Skin · damagedPERFORM PERMANENT REPAIR MULTIPLE FUSELAGE DAMAGES IAW TD 340-51-10-11.SDR NSVA2010228Structure · damagedPERFORMED PERMANENT REPAIR MISC RIVET DEVIATION ON RT INBOARD NACELLE IAW TD 340-54-09-15.SDR MALA100200Cdu · malfunctionedSMOKE FROM FMS AREA, ON GROUND PULLED "AREA NAV" CIRCUIT BREAKER TURNED OFF LT AND RT AVIONICS. SMOKE STOPPED. R & R FMS CDU IAW 34-60, ALL CHECKS GOOD PN ON/OFF F1014-21, SN OFF 470, SN ON 417.SDR MALA100196Uplock Switch · out of adjustGEAR UNSAFE INDICATION AFTER DEPARTURE. ALL LDG GEAR LIGHTS EXTINGUISHED. ENNC COMPLETED. GEAR UNSAFE LIGHT EXTINGUISHED. FOUND LT & RT MLG UPLOCKS WERE PREVIOUSLY ADJUSTED TOO TIGHT. READJUSTED WITHIN LIMITS IAW AMM 32-32-00-05. PERFORMED ADJUSTMENT OF LTSDR MALA100195Door · out of rigGEAR UNSAFE LIGHT WITH GEAR IN UP POSITION JUST AFTER TAKEOFF. EMER NON-NORMAL CHECKLIST COMPLETED. PERFORMED RIGGING OF UPLOCK AND RELEASE ON LT LANDING GEAR IAW AMM 32-32-00. PERFORMED FUNCTIONAL TEST OF EXTENSION RETRACTION SYS 32-30-00. FUNCTIONAL TESTSDR NSVA2010221Spinner · malfunctionedJUST AFTER LEVELING OFF IN CRUISE THE FLIGHT ATTENDANT REPORTED TO THE CAPTAIN THAT PASSENGER SEATED IN 5F INFORMED HER THAT SPARKS APPEARS TO BE COMING FROM THE NUMBER 2 ENGINE. SHE THEN VISUALLY VERIFIED THAT SPARKS ARE COMING FROM THE INTAKE AREA. THE CAPSDR MALA100188Control Unit · malfunctionedON DEPARTURE, WE RECEIVED GEAR UNSAFE INDICATIONS WITH GEAR HANDLE IN THE UP POSITION AND HANDLE ILLUMINATED. RAN CHECK LIST ON BOTH OCCASIONS AND RECYCLED GEAR. LIGHT EXTINGUISHED. PERFORMED GEAR SWINGS. UNABLE TO DUPLICATE. R & R LANDING GEAR CONTROL UNSDR NSVA2010218Boot · damagedAT 9000FT, CREW ENCOUNTERED STAB TIMER LIGHT. CREW CONTACTED DISPATCH AND ADVISED OF SITUATION. DISPATCH INFORMED CREW OF CURRENT CONDITIONS ALONG THE PLANNED ROUTE AND RECOMMENDED RETURN TO IAD. CAPTAIN CONCURRED, SHOULD BE ABLE TO AVOID ICING CONDITIONS RSDR NSVA2010217Structure · crackedPERFORM PERMANENT REPAIR OF CRACK DAMAGE ON LT NACELLE IAW TD 340-54-10-20.SDR NSVA2010216Unknown · malfunctionedBRAKES STOPPED WORKING. AIRCRAFT NEEDED TO GET TUGGED BACK TO THE GATE. ANTI-SKID BOX OPS CHECKED GOOD.SDR MALA100183Control Unit · malfunctionedIN-TRANSIT LIGHT REMAINS ILLUMINATED WHEN GEAR HANDLE SELECTED UP, 3 GEAR LIGHTS OUT. RECYCLED WITH SAME RESULTS. REPLACED LANDING GEAR CONTROL UNIT AND PERFORMED FUNCTIONAL TEST OF EXTENSION & RETRACTION SYS IAW AMM 32-31-05-02. ALL CHECKS GOOD.SDR NSVA2010215Structure · damagedINSTALL PERMANENT REPAIR DOUBLER ON CARGO DOOR IAW TD 340-52-10-14.SDR PNSA101101Line · crackedWHILE ON CLIMBOUT AT 1000FT AGL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL IMMEDIATELY FOLLOWING A POWER REDUCTION FOR CLIMB POWER. THERE WAS 2 "BANGS" AND THE ENGINE WENT INTO AUTO COARSENING AND THE ENGINE WAS SHUT DOWN BY THE FLIGHT CREW AND NO TEMPERSDR NSVA2010209Pump · failedHYDRAULIC PUMP FAILED IN FLIGHT, RETURNED TO FIELD. REPLACED HYDRAULIC PUMP, OPS CHECKED GOOD.SDR NSVA2010208Boot · damagedRETURNED TO FIELD DUE TO DEICE TIMER LIGHT ON DURING CONTINUOUS MODE. THERE WERE ICING CONDITIONS IN WISCONSIN. PATCHED LEFT WING BOOT. RT HORIZONTAL STAB BOOT, AND ONE ON VERTICAL STAB BOOT. OPS CHECKED GOOD.SDR 2010F00238Indicator · burnedWHILE IN CRUISE, PILOTS SAY THE CABIN PRESSURE INDICATOR STOP WORKING. CREW THEN SMELLED A FAINT ELECTRICAL BURNING SMELL, NO SMOKE WAS REPORTED. ACFT RETURNED, NO OTHER PROBLEMS WERE NOTED. MX FOUND THAT THE CABIN PRESSURE CONTROLLER HAD FAILED AND WAS THESDR NSVA2010203Skin Panel · corrodedREPAIR CORROSION ON RT FUSELAGE SIDE PANEL IAW TD 340-53-10-65.SDR NSVA2010202Warning Light · illuminatedA REPOSITION FLIGHT RETURNED TO FIELD DUE TO BLEED AIR FAULT LIGHT AND DUCT OVER TEMP LIGHT ILLUMINATED. OPENSDR NSVA2010200Skin · damagedPERFORM REPAIR OF COLLISION DAMAGE ON LT REAR FUSELAGE IAW TD 340-53-10-62.SDR NSVA2010199Generator · failedCLIMBING THROUGH 5000 FT RIGHT DC GENERATOR FAIL RAN THE QRH RESET NO FIX RETURN BACK TO BOS. REPLACED RIGHT DC GENERATOR.SDR NSVA2010197Control Valve · malfunctionedCREW WAS UNABLE TO RETRACT GEAR AFTER TAKEOFF. FOLLOWED QRH CHECKLIST AND LEFT THE GEAR DOWN. BY THE TIME CREW WAS ABLE TO ESTABLISH CONTACT WITH DISPATCH, THEY WERE 36 NL FROM IAH AND IT WAS AGREED THAT THEY SHOULD CONTINUE TO IAH. THE AIRCRAFT LANDED WITHSDR NSVA2010196Skin · damagedPERFORMED PERM PATCH REPAIR IN AFT FUSELAGE SKIN IAW TD 340-53-10-55.SDR NSVA2010195Tail Cone · dentedPERFORMED PERM REPAIR OF LEFT TAIL CONE DENT IAW TD 340-53-10-60.SDR NSVA2010198Dpu · malfunctionedLT EADI FAILED IN FLIGHT. SLIGHT ELECTRICAL BURNING SMELL, PULLED CB G18 LT EADI SCREEN BLACKED OUT. REPLACED LT EADI SCREEN IAW SAAB AMM 34-24-10, REPLACED LT DPU IAW SAAB AMM 34-24-20.SDR NSVA2010191Unknown · damagedPERFORMED TEMP REPAIR FOR FERRY FLIGHT IAW TD 340-53-10-59.SDR NSVA2010188Skin · damagedAIRCRAFT PARKED AT GATE WHEN GPU / AIR CART WAS UNDER TOW WHEN MADE CONTACT WITH AIRCRAFT SKIN AFT OF CARGO DOOR. MAINTENANCE WILL DO FORMAL INSPECTION OF DAMAGE, AND SUBMIT TO SAAB FOR MAJOR REPAIR.SDR NSVA2010185Skin Panel · dentedPERFORMED PERMANENT REPAIR OF THREE DENTS IN A ROW ON THE CABIN AND REAR FUSELAGE BOTTOM PANEL JUST AFT OF STA. 631.112 AND BETWEEN SL 1527 - SL 1627 IAW TD 340-53-10-55.SDR NSVA2010186Seal · damagedLEFT MASTER CAUTION ILLUMINATED ON TAKEOFF BUT QUICKLY EXTINGUISHED. DURING EN ROUTE CLIMB THE LEFT ENGINE OIL PRESSURE STARTED TO FLUCTUATE 40-50 PSI INTO THE YELLOW ARC. CAPTAIN ELECTED TO RETURN TO FIELD AS A PRECAUTION. CAPTAIN INFORMED DISPATCH THROUGH SDR NSVA2010184Warning System · false activationCONFIG WARNING ON TAKEOFF ROLL, LIGHT MINIMAL BRAKING DUE TO RW LENGTH. PERFORMED OPERATIONAL CHECK PER AMM, NO DEFECTS NOTED.SDR NSVA2010182Stall Warning · malfunctionedDURING FIRST FLIGHT OF THE DAY CHECKS STALL 2 DID NOT TEST PROPERLY AND WHEN BOTH STALL TEST SWITCHES ARE PUSHED UP THE PUSHER DID NOT ACTUATE. PERFORMED STICK PUSHER RESET PROCEDURE AND PERFORMED OPS CHECK, FOUND GOOD IAW AMM 27-35-00-05.SDR NSVA2010181Engine · malfunctionedTHE APPROACH WAS NOT STABLE AT 500 FEET CAPTAIN INITIALIZED GO-AROUND. CREW APPLIED GO-AROUND POWER AND THAT'S WHEN THE RIGHT ENGINE FAILED (ENGINE AUTOCOARSENED). CREW DECLARED AN EMERGENCY PASSENGER WERE BRIEFED OF THE ENGINE FAILURE. FLIGHT CAME AROUND ASDR NSVA2010180Unknown · malfunctionedDURING MAINTENANCE TAXI/RUN THE AIRCRAFT VEERED RIGHT INTO A DITCH ON TAXIWAY ZULU. THE CAUSE IS UNKNOWN AT THIS TIME. IAD FIRE DEPARTMENT AND LAW ENFORCEMENT PERSONNEL WAS DISPATCHED TO ASSIST. THERE IS NO FIRE OR INJURIES REPORTED. THE FULL EXTENT OF THESDR MALA100148Power Supply · failed21LN FAILED CAPACITY TEST. R & R 21LN EMERGENCY BATTERY PN 3301-51 IAW SF340 AMM 24-35-10 SN OFF 1288 SN ON 1405. OPS CHECK GOOD.SDR NSVA2010179Ahrs · malfunctionedCREW RECEIVED RED HEADING FLAG WHICH IS A POSSIBLE AHRS PROBLEM PER MAINTENCE. DUE TO POTENTIAL EXTENSIVE DELAY IF CREW LANDED IN SHD ADVISED OVERFLY TO IAD TO GET THE PROBLEM RESOLVED QUICKER WITH LEAST AMOUNT OF PASSENGER INCONVENIENCE. REPLACED RT AHRS COSDR MALA100147Switch · inoperativeWHILE PERFORMING MX, FOUND EMERGENCY LIGHT SWITCH BAD. REPLACED EMERGENCY LIGHT SWITCH IN COCKPIT. REF AMM 39-40-15-02. P/N ON&OFF MS27406-1. OPS CHECK GOOD REF AMM 33-50-00.SDR MALA100146Power Supply · failedDURING PERFORMANCE OF JOB CARD 335003 BATTERY PACKS 21LN & 24LN INDICATED FAILURE. R & R EMERGENCY LIGHT POWER SUPPLIES 24LN AND 21LN IAW AMM 33-50-10. OPS TEST GOOD.SDR MALA100145Power Supply · failedEMERGENCY POWER SUPPLY 23LN & 20LN FAILED CAP CHECK. REPLACED EMERGENCY POWER SUPPLY 23LN IAW SF3 AMM 33-50-10. OPS CHECK GOOD. OPS CHECK GOOD.SDR NSVA2010176Engine · failedRIGHT ENGINE ABNORMAL INDICATIONS IN FLIGHT. CREW SHUT DOWN THE ENGINE AFTER FOLLOWING THE CHECKLIST. LANDED NORMAL, TAXIED TO GATE ON IT'S OWN POWER. PASSENGERS AND CREW ARE ALL RIGHT WITH NO KNOWN COMPLICATIONS AT THIS TIME. PERFORMED FDR DOWNLOAD FOUND ESDR NSVA2010175Loop · malfunctionedRETURNED TO FIELD DUE TO ENGINE INTAKE LIGHT ILLUMINATED AFTER TAKEOFF. COULD NOT CONTINUE DO TO ICING CONDITIONS. REPLACED LT INTAKE LOOP AND REPLACED WHITE HARNESS FROM LOWER DUCT.SDR MALA100142Seat Track · corrodedRT CTR AISLE SEAT TRACK HAS A SPOT OF CORROSION AT STATION 296. CUT OUT 12 INCH SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION IAW EO S53060. THIS EO PROVIDES INSTRUCTIONS FOR REPAIR OF DAMAGE TO SEAT TRACKS FROM TOP TO BOTTOM IAW SRM CHAPTER 53-70-60, SPECSDR MALA100143Power Supply · failedDURING TC 335003 POWER SUPPLY 21LN FAILED CAPACITY CHECK. REPLACED POWER SUPPLY 21LN IAW AMM 33-50-10, PN 3301-51, SN OFF 2056, SN ON 1355. EMERGENCY LIGHTING SYSTEM OPS CHECKS GOOD IAW AMM 33-50-00.SDR MALA100141Battery Pack · failedDURING TC NR335003 EMERGENCY BATTERY PACK 21LN FAILED CAPACITY CHECK. REPLACED EMERGENCY BATTERY PACK 21LN IAW AMM 33-50-10. EMERGENCY LIGHTING SYS OPS CHECKS GOOD IAW AMM 33-50-00.
Back to Saab 340B