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 DXTA200802964Circuit Board · false indicationUPON GEAR RETRACTION,ALL GREEN DOWN AND LOCKED LIGHTS EXTINGUISHED. HOWEVER,RED IN TRANSIT LIGHT REMAINED ILLUMINATED. REPLACED GROUND SAFE PCB A161. OPS CHECK GOOD. IAW MM 32-60-00.SDR DXTA20082964Indicator · malfunctionedUPON GEAR RETRACTION, ALL GREEN DOWN AND LOCKED LIGHTS EXTINGUISHED. HOWEVER, RED IN TRANSIT LIGHT REMAINED ILLUMINATED. REPLACED GROUND SAFE PCB A161. OPS CHECK GOOD. IAW MM CH 32-60-00.SDR DJFA2008030Hmu · failedON TAXI FOR TAKE-OFF, WHILE PERFORMING THE EFC TEST, THE NR 2 ENGINE SHUT DOWN UNCOMMANDED. MAINTENANCE CHECKED RIGGING AND PERFORMED SEVERAL OPERATIONAL CHECKS. MAINTENANCE DETERMINED THAT THE HMU REQUIRED REPLACEMENT. THE HMU AND FLOW DIVIDER WERE REPLASDR DJFA2008029Inlet · crackedDURING A SCHEDULED INSP, MAINT DISCOVERED THE NR 2 ENGINE HEATED INLET CRACKED AT THE 4 O'CLOCK POSITION. MAINT REMOVED AND REPLACED THE INLET.SDR DJFA2008028Inlet · crackedDURING A SCHEDULED INSPECTION, MAINT DISCOVERED THE NR 2 ENGINE HEATED INLET CRACKED. MAINTENANCE REPLACED THE INLET.SDR DJFA2008027Connector · dirtyON TAXI TO TAKEOFF, DURING EFC TEST, CREW EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 2 ENGINE. MAINTENANCE CLEANED THE EFC CONNECTOR AND PERFORMED SEVERAL GROUND RUNS, EFC TESTS, AND A T/R CHECK WITHOUT FAILURE.SDR DXTA20082938Sensor · failedHORIZONTAL STAB FAILED IN FLIGHT. TROUBLESHOT IAW MM 30-12-00 FOUND LEFT STAB TEMP SENSOR TO HAVE SPLIT READINGS FROM P473 AT THE CONTROLLER, AT 238.3 OHMS AND ONE AT 203.2 OHMS. CLEANED TERMINAL STRIP 061. RECHECKED RESISTANCE FOUND GOOD AT 202 EACH. PERFORMSDR DJFA2008026Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70.SDR DJFA2008025Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MASDR DJFA2008024Rib · crackedDURING A SCHEDULED MAINT VISIT, WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED INCOMMUNIQUE' NR 70. MAINT INSDR DXTA20082911Squat Switch · defectiveSPEED BRAKES WORK INTERMITTENTLY IN FLIGHT. TROUBLE SHOT SPEED BRAKE SYSTEM & FOUND LH WOW SWITCH DEFECTIVE AND LT THROTTLE LEVER 85 PERCENT SWITCH OPERATING ARM OUT OF ADJUSTMENT. REMOVED UNSERVICEABLE LT WOW SWITCH & INSTALLED A NEW SWITCH. ADJUSTED LT THSDR DJFA2008023Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT AND RT IB RIBS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70.SDR DJFA2008022Support Bracket · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70.SDR DJFA2008021Support Bracket · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 7SDR DJFA2008020Downlock Switch · failedCREW REPORTED ON APPROACH THE LT MAIN GEAR DOWN LIGHT DID NOT ILLUMINATE. THE LIGHT ILLUMINATED DURING THE TEST. EMERGENCY PROCEDURES WERE FOLLOWED AND THE AC LANDED NORMALLY. THE DOWNLOCK SWITCH WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DJFA2008018Connector · damagedCREW REPORTED AFTER TAKEOFF UPON GEAR RETRACTION THE RED UNSAFE LANDING GEAR LIGHT REMAINED ILLUMINATED. EMERGENCY GEAR EXTENSION WAS PERFORMED WITH NORMAL INDICATION AFTERWARD. THE AC DIVERTED, MAINT FOUND PIN M OF THE RT DOOR UPLOCK SWITCH PUSHED BACK. THSDR 68JV02AAdapter · failedAFTER DEPARTING MKE THE LEFT GENERATOR DROPPED OFF LINE AND RESET WITHOUT ANY ACTION FROM CREW. AIRCRAFT RETURNED TO MKE. LANDING WAS UNEVENTFUL. INSPECTION OF LEFT STARTER/GENERATOR FOUND THE THREADS ON THE STARTER/GENERATOR GROUND TERMINAL ADAPTER HAD FAISDR DXTA20082900Unknown · odorELECTRICAL ODOR IN LAVATORY. REMOVED ALL PANELS IN LAV AREA. COULD NOT DUPLICATE ODOR. INSPECTED ALL WIRES, PC BOARDS TERMINALS ETC. FOR SIGNS OF DAMAGE. NO DEFECTS NOTED. SUPPLIED GROUND POWER TO AIRCRAFT THROUGHOUT ENTIRE INSPECTION PROCESS. SUPPLIED GROSDR DJFA2008019Uplock Switch · out of adjustCREW REPORTED AFTER TAKE OFF DURING GEAR RETRACTION THE UNSAFE GEAR LIGHT ILLUMINATED. THE GEAR WAS EXTENDED WITH NO DOWN AND LOCKED INDICATION. EMERGENCY PROCEDURES WERE TAKEN AND LANDING WAS NORMAL. MAINT FOUND LT AND RT LANDING GEAR DOOR UPLOCK SWITCHES SDR 68JV02Computer · failedON CLIMBOUT FROM DSM CREW RECEIVED AUTOPILOT PITCH TRIM FAIL ANNUNCIATOR. AIRCRAFT RETURNED TO DSM, LANDING WAS UNEVENTFUL. AFTER LANDING, CREW PERFORMED PREFLIGHT OPS CHECKS OF AUTOPILOT SYSTEM AND COULD NOT DUPLICATE FAILURE. REPOSITIONED AIRCRAFT FROM DSSDR DXTA20082888Trim System · malfunctionedLT AND RT AP TRIM PITCH TRIM FAIL LIGHTS ON TRIM INDICATIONS WERE FINE, BUT NOSE DOWN PITCH WHEN AP DISENGAGED. INSPECTED PITCH TRIM SERVO, VERIFIED NO DEFECTS. PERFORMED PITCH TRIM SERVO SPIN UP TEST WITH NO DEFECTS NOTED. SYSTEM OPERATES NORMAL IAW SRM PUB SDR DXTA20082879Control Switch · inoperativeRED LANDING GEAR UNSAFE LIGHT REMAINS ON AFTER GEAR RETRACTION. REPLACED LANDING GEAR CONTROL SWITCH ASSY WITH NEW UNIT. PERFORMED LANDING GEAR FUNCTIONAL CHECK - SWUNG GEAR 5 TIMES WITH NO DEFECTS. OPS CHECKS GOOD. MX IAW MM CH 32-30-00.SDR 2008FA0000155Rib · crackedFOUND SEVERAL CRACKS (25) IN RIB TO LOWER SKIN ATTACH FLANGES, AT RIVET HOLES , IN 3 LT , AND 4 RT HORIZONTAL STABILIZER INNER SPAR RIBS. RIBS NR 234 ON LT SIDE, AND NR 2345 ON RT SIDE AFFECTED.SDR 2008FA0000154Rib · crackedFOUND SEVERAL CRACKS (25) IN RIB TO LOWER SKIN ATTACH FLANGES, AT RIVET HOLES , IN 3 LT, AND 4 RT HORIZONTAL STABILIZER INNER SPAR RIBS. RIBS NR 234 ON LT SIDE, AND NR 2345 ON RT SIDE. AFFECTED.SDR DXTA20082878Wire · broken(H) STAB FAIL) LIGHT ILLUMINATED IN FLIGHT. INSPECTED AND FOUND BROKEN WIRE AT P540 CONNECTOR PLUG. REPAIRED WIRE IAW MM 20-20-04. PERFORMED PITOT TEST, SYSTEM PASSED. PERFORMED GROUND CHECK, OPS CHECK GOOD. DONE IAW AMM 30-12-00.SDR DXTA200802866Bumper Block · damagedUPON LANDING GEAR RETRACTION, THE 3 GREEN LIGHTS EXTINGUISHED BUT THE RED GEAR HANDLE UNSAFE LIGHTS REMAINED ILLUMINATED. REMOVED EXCESS MATERIAL FROM RUBBER NOSE GEAR BUMPERS IN NOSE WHEEL WELL. OPERATIONAL CHECK NOW SATISFACTORY. CYCLED GEAR & CHECKED NOSE GSDR DJFA2008015Coalescer Bag · odorDURING CRUISE, CREW REPORTED BURNING ODOR WITH HEAT IN AUTO OR MANUAL. AIRCRAFT LANDED SAFELY AT INTENDED DESTINATION. MAINTENANCE RAN THE ENGINES AND NOTED A MOLDY SMELL BUT NOT A BURNING SMELL. THE COALESCER BAG WAS REPLACED AND ALL SMELLS WENT AWAY.SDR DXTA200802835Indicator · inoperativeON TAKEOFF LT OIL TEMP WENT TO 0, ABORTED TAKEOFF. SWAPPED GAUGES FROM RT TO LT, STARTED ENGINES, DID FIND OIL TEMP NEEDLE DID NOT RISE TAPPED ON GAUGE AND IT CAME UP. SWAPPED GAUGES TO THE ORIGINAL POSITION, RAN ENGINES AGAIN PROBLEM STILL FOLLOWED. REPLACEDSDR DJFA2008014Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB BRACKET WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. BOTHSDR DXTA200802823Uplock Switch · out of adjustRED LANDING GEAR UNSAFE REMAINS ON AFTER GEAR RETRACTION. (M2B) PERFORMED GEAR SWINGS WITH NO ADVERSE INDICATIONS CHECKED CLEARANCES OF GEAR DOOR UPLOCK ROLLERS. NO DEFECTS FOUND, CHECKED MLG DOOR UPLOCK SW FOR PLUNGER OVERTRAVEL. FOUND RH SW. OUT OF ADJUSTMENSDR DJFA2008013Ring · crackedDURING INSP, MAINT FOUND THE RT ENGINE INLET RING CRACKED BETWEEN THE 1200 AND 0100 O CLOCK POSITION. MAINTENANCE REPLACED THE INLET RING.SDR DJFA2008012Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. OPENSDR 433858831Fmc · faultedUNCOMMANDED 360 DEGREE TURN AS COMMANDED BY THE FMS. REF SB 0057-05 DATED DECEMBER 21, 2005 DELETING A WAYPOINT MAY CAUSE THE FMS TO INSERT AND FLY AN UNINTENDED TURN. KNOWN PROBLEM WITH OPTIONAL SOLUTION FOR FMS6000 INSTALLED IN AC, NO SOLUTION FOR FMS5000 SDR DJFA2008011Hmu · malfunctionedDURING CRUISE, CREW NOTED LT ENGINE ROLL BACK FROM 95.7 TO 91.0 WITH SIMULTANEOUS FUEL FLOW AND ITT FLUX. AC WAS AT FL 380 WITH AN OAT OF -33 C IN CLEAR AIR. ENGINE ANTI-ICE WAS OFF. MAINTENANCE FOUND THE LEFT HMU FAILED. IT WAS REPLACEDSDR DJFA2008009Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENASDR DXTA200802798Bellcrank · out of adjustNR2 ENGINE WOULD NOT MAINTAIN TAKEOFF TARGET N1 OF 96.9. INITIALLY NR2 N1 INDICATED 96.9 WITH POWER LEVER AT FULL FWD BUT IMMEDIATELY DROPPED TO AND MAINTAINED 94.4. NR1 ENGINE MAINTAINED 96.9 WITH FULL POWER APPLIED. ADJUSTED NR2 ENGINE BELL CRANK ASSY IN REASDR DJFA2008010Duct · obstructedIN FLIGHT, CREW REPORTED CABIN HEAT INOP AND BURNING SMELL IN REAR OF CABIN. MAINT FOUND THE CARPET IMPROPERLY TUCKED BEHIND THE SIDEWALLS AND BLOCKING THE HEAT DUCT HOLES. THE CARPET WAS ADJUSTED AND THE SYS CHECKED SATISFACTORILY.SDR DXTA200802797Warning Light · illuminatedON GEAR RETRACTION, RED LIGHT IN LANDING GEAR HANDLE REMAINED ILLUMINATED AND ALL GREEN LIGHTS EXTINGUISHED. CYCLED LANDING GEAR DOWN AND ALL GREEN AND RED LIGHTS FUNCTIONED PROPERLY. RETRACTED GEAR AGAIN + RED GEAR HANDLE LIGHT REMAINED ILLUMINATED.SDR DJFA2008007Sensor · inoperativeDURING CRUISE CREW REPORTED BURNING ODOR NEAR THE LAV AREA. CREW CONTINUED TO DESTINATION. MAINTENANCE FOUND THE CABIN TEMP SENSOR FAILED. THE TEMP SENSOR WAS REPLACED.SDR DJFA2008008Unknown · odorIN FLIGHT, CREW REPORTED BURNING RUBBER SMELL WHEN AIR IS HOT. MAINT RAN BOTH ENGINES AND BLEED AIR SYSTEM WITH CABIN TEMP TO FULL HOT BUT COULD NOT DUPLICATE THE DISCREPANCY.SDR DXTA200802786Switch · out of adjustINITIAL SELECTION OF FLAPS 10DEG AT 200KIAS FLAP ASYM CAUTION LIGHT CAME ON. TROUBLESHOT, ADJUSTED LT AND RT FLAP FOLLOW UP SWITCHES, AND LT FLAP POSITION TRANSMITTER, ALSO ADJUSTED RT FLAP FOLLOW UP SWITCH LINK AREA AND CHECKED FLAP TRAVEL ANGLES. ALL CHECKESDR DJFA2008006Hmu · out of adjustDURING TAXI, PRIOR TO FLIGHT, WHILE PERFORMING THE EFC AUTHORITY CHECK THE NR1 ENGINE SHUTDOWN. MAINT FOUND THE NR1 HMU OUT OF ADJUSTMENT. THE HMU WAS ADJUSTED IAW THE MM AND THE ENGINE OPERATIONAL CHECK WAS SUCCESSFUL.SDR DJFA2008005Bumper Block · out of adjustON TAKEOFF, AFTER RAISING THE GEAR, THE RED LIGHT IN THE GEAR HANDLE STAYED ILLUMINATED. CREW RECYCLED THE GEAR AND SAME INDICATIONS RETURNED. FLY-BY OF TOWER CONFIRMED GEAR WAS UP AND MAIN GEAR DOORS WERE DEPLOYED. CREW RETURNED TO FTY WHERE MAINT FOUND THE SDR DXTA200802780Warning Light · illuminatedAFTER TAKEOFF, RED WARNING LIGHT IN GEAR HANDLE REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED. INSPECTED LANDING GEAR AND PERFORMED OPERATION CHECK OF LANDING GEAR SYSTEM. NO DEFECTS FOUND OPS CK GOOD IAW MM CH 32-10.SDR E0X2008F00000Engine · bird ingestionAFTER FULLY CONFIGURING AC FOR LANDING, ON APPROACH, AT APPROX 1500 FT, AGL AND 5 MILES FROM RUNWAY, AC SUFFERED A BIRD INGESTION AND CATASTROPHIC RT ENGINE FAILURE. THIS WAS FOLLOWED BY A SUCCESSFUL EMERGENCY LANDING WITH NO INJURIES TO PASSENGERS OR CREW. SDR DJFA2008004Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE BOTH IB RIBS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINSDR EOX2008F00001Sealant · smokeAC EXPERIENCED SMOKE IN THE CABIN AT FL 22 ENROUTE, FLIGHT CREW FOLLOWED PROCEDURE WITH CAPTAIN DAWNING O2 MASK AND 2ND OFFICER INSPECTING CABIN. NO DISCREPANCIES WERE NOTED OTHER THAN SMOKE IN CABIN, WHICH WAS DISSIPATING. FLIGHT CREW FELT THAT THE ISSUE WASDR DXTA200802748Brake Assy · malfunctionedUPON LANDING WITH NORMAL BRAKING ON DRY RUNWAY THE BRAKES PULSED HEAVILY CAUSING THE A/C TO SKID CONTINUALLY. INSPECTED WHEELS, TIRES, BRAKES, PERFORMED HUB CAP INSPECTION, CHECKED BRAKE ACCUMULATOR. TAXIED AIRCRAFT, NO DEFECTS FOUND, WORK DONE IAW MM 32-00-SDR DXTA200802742Uplock · out of adjustLANDING GEAR IN TRANSIT / UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER LANDING GEAR RETREACTION. ACCESSED CONNECTORS P271 AND P272. OHMED OUT DOOR CLOSED SWITCH & UPLOCK SWITCH PER WDM 32-61-01-02 NO DEFECTS NOTED. JACKED ACFT & INSTALLED HYDRAULIC MULE. ACCOMPLISDR DJFA2008001Uplock Switch · erraticDURING CLIMB-OUT CREW REPORTED RED LIGHTS IN GEAR SELECT HANDLE ILLUMINATED FOLLOWED BY SLIGHT DECELERATION AND A THUMP. CREW SUSPECTS THE GEAR EXTENDED AND RETRACTED UNCOMMANDED. MAINTENANCE FOUND THE LT MLG UPLOCK SWITCH ERRATIC IN COLD TEMPERATURES. THE
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