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 DJFA2006266Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION AS PART OF THE A / B LEVEL INSPECTION, THE RIGHT INBOARD HORIZONTAL STABILIZER ROLLER RIB STRUCTURE AND AN INTERNAL BRACKET WERE FOUND CRACKED. DETAILED INSDR CA060704012Engine · flamed out(CAN) DURING CRUISE AT FL380 (AND APPROACHING CLOUD TOP) BOTH ENGINES WERE THROTTLED BACK IN POWER BY THE CREW PRIOR TO ENGAGING ANTI-ICE. BOTH ENGINES FLAMED OUT. THE ENGINES WERE SUBSEQUENTLY RE-STARTED IN FLIGHT AND THE AIRCRAFT DIVERTED. POST-EVENT INSPESDR 2006FA0000648Connector · damagedINVESTIGATED REPORT OF FLAP ASYMMETRY ANNUNCIATOR LIGHT FLICKERING IN-FLIGHT. FOUND WIRE C458A22 ROUTED SO THAT EXCESSIVE WIRE TENSION AT P156 PLUG WAS CAUSING INTERMITTENT CONTACT WITH A156 PC BOARD J1 CONNECTOR. REROUTED WIRING AS REQUIRED FOR REVEALING WISDR DJFA2006264Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION AS PART OF THE A / B LEVEL INSPECTION THE RIGHT INBOARD HORIZONTAL STABILIZER ROLLER BRACKET RIB STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTSDR DXTA200601436Landing Gear · inoperativeGEAR WOULD NOT RETRACT AFTER TAKEOFF. ITEM IS UNDER INVESTIGATION.SDR DJFA2006263Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION AS PART OF THE (A) LEVEL INSPECTION BOTH THE LT AND RT IB HORIZONTAL STABILIZER ROLLER BRACKET RIB STRUCTURES AND BRACKETS WERE FOUND CRACKED. DETAILED INSSDR DJFA2006260Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT, WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION AS PART OF THE (B) LEVEL INSPECTION THE RT IB HORIZONTAL STABILIZER NOSE RIB STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARSDR DJFA2006261Odor · detectedTHE FLIGHT CREW REPORTED THAT THE AIRCRAFT CABIN TEMPERATURE HEAT WAS EXTREMELY HOT AND HARD TO CONTROL AND HAD AN ODOR SIMILAR TO BURNED RUBBER. MAINTENANCE TROUBLESHOT THE CABIN AND COCKPIT TEMPERATURE CONTROLS IAW MM CABIN TEMPERATURE SYSTEM CHECKS. NO DESDR DJFA2006259Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION AS PART OF THE (A) LEVEL INSPECTION BOTH THE LT AND RT IB HORIZONTAL STABILIZER ROLLER BRACKET RIB STRUCTURES WERE FOUND CRACKED. DETAILED INSPECTION INSTRSDR DJFA2006257Motor · burnedCREW REPORTED THAT THE AIR CONDITIONING SYSTEM FAILED DURING DESCENT AND THE REFRIGERANT COMPRESSOR CIRCUIT BREAKER POPPED. THERE WAS A STRONG SMOKE ODOR IN THE BAGGAGE COMPARTMENT. MAINTENANCE ISSUED MEL 21-16 FOR THE VAPOR CYCLE AIR CONDITIONING SYSTEM ANDSDR DXTA200601418Smoke · detectedUNKNOWN SOURCE OF SMOKE AND ODOR ENTERING CABIN THROUGH UPPER/REAR LAV AREA DURING FLIGHT FROM IAD TO ORF, DIVERTED TO NHK. AIR CONDITIONER AND GALLEY WERE SHUT OFF AND WE ISOLTED CABIN PRESSURE SOURCE TO RT ENGINE ONLY. ANY OR ALL 3 OF THESE ACTIONS CAUSED TSDR DJFA2006254Switch · failedDURING APPROACH AFTER LANDING GEAR WAS SELECTED DOWN, CREW RECEIVED INDICATION THAT MAIN GEAR WAS DOWN. SAME INDICATION WAS RECEIVED AFTER LANDING GEAR WAS CYCLED. FLY-BY WAS PERFORMED, CREW WAS INFORMED THAT GEAR APPEARED TO BE DOWN. DURING FLY-BY, CREW RESDR 2006FA0000601Fuse · failedFLIGHT CREW REPORTED NO BATTERY VOLTAGE INDICATION ON VOLTMETER WITH ALL DC BUSSES POWERED. TROUBLESHOOTING FOUND AIRCRAFT WOULD NOT GO INTO EMERGENCY POWER OR PERFORMED FEEDER FAULT TEST. FOUND 5A MICROFUSE F105 CONNECTED TO K005 EMERGENCY BUSS POWER RELAY SDR DJFA2006255Blower · burnedTHE CREW REPORTED THAT THE REAR EVAPORATOR BLOWER WAS MAKING A LOUD NOISE AND THERE WAS A STRONG SMELL / SMOKE OF SOMETHING BURNING. MAINTENANCE REPLACED THE REAR EVAPORATOR BLOWER ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVICE FOLLOWING SATISFACTORY OPERATISDR 2006FA0000603Servo · intermittentFLIGHT CREW REPORTED PILOTS CONTROL WHEEL TRIM INTERRUPT/AUTOPILOT DISENGAGE SWITCH NOT DISCONNECTING YAW DAMPER ON FINAL APPROACH. FOUND CONTROL WHEEL SWITCH OPERATIONS NORMAL. REPLACED SVO-85C YAW DAMPER SERVO WITH OVERHAULED UNIT. ALSO, REPLACED NR 1 FCCSDR 2006FA0000602Circuit Card · intermittentFLIGHT CREW REPORTED AUTOPILOT PITCH TRIM FAILURE ANNUNCIATION CAME ON DURING CLIMB WITH AUTO PILOT DISCONNECTED. AIRCRAFT REPPORTED TO HAVE PITCH-UP MOVEMENT. FOUND NR 1 FCC-850 CARD INTERMITTENTLY NOT CROSS-TALKING TO NR 2 FCC-850 CARD. REPLACED NR 1 FCC SDR DXTA200601413Pitot System · obstructedON TAKEOFF ROLL, COPILOTS AIRSPEED INDICATOR NEVER MOVED OFF OF 40 KTS. CAPTAINS AIRSPEED SHOWED 65 KTS MAX WHEN ABORT WAS INITIATED. STANBY AIRSPEED INDICATOR HAD MOVED FROM ITS MINIMUM 60 KTS. REPEAT WRITEUP. CHECKED PILOT AND COPILOT AIRSPEED INDICATORS WISDR DJFA2006252Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT, WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION AS PART OF THE (A) LEVEL INSPECTION THE LT AND RT IB HORIZONTAL STABILIZER RIB STRUCTURE WAS FOUND CRACKED NEXT TO THE SIDE ROLLER BRACKET. DETAILED INSPECTION INSDR DXTA200601405Pitot Tube · obstructedON T/O ROLL, L AIRSPEED INDICATOR WAS AT 80 KIAS WHILE R SIDE INDICATED 40 KIAS ( IT NEVER MOVED DURING ROLL). - CLEANED DEBRIS FROM RIGHT PITOT TUBE. OPERATIONAL CHECKS AND LEAK CHECKS OF THE PILOTS AND CO-PILOTS AIRSPEED INDICATOR SATISFACTORY IAW THE HAWKERSDR 0MKR20064Rib · crackedLT IB ROLLER SUPPORT RIB FOUND CRACKED. P/N 45A21104-641 WAS REMOVED AND REPLACED WITH NEW. DUE TO THE NUMBER OF THESE WE ARE SEEING, IT IS LIKELY THE ENTIRE 400A FLEET HAS A PROBLEM IN THIS AREA.SDR DJFA2006251Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION AS PART OF THE (B) LEVEL INSPECTION THE LT IB HORIZONTAL STABILIZER RIB STRUCTURE WAS FOUND CRACKED NEXT TO THE SIDE ROLLER BRACKET. DETAILED INSPECTION INSTRUCTIOSDR 2006FA0000634Link · wornDURING OPERATIONAL CHECK FLIGHT OF AIRCRAFT, PILOT ADVANCED POWER LEVERS FORWARD AND NOTED LT ENG (N) REACHED MAX OF 117 PERCENT N2, REACHED MAXIMUM OF 100 PERCENT. IT IS DETERMINED THAT PROBABLE CAUSE OF OVERSPEED WAS ACHIEVED BY WORN THROTTLE LEVER LINK NOTSDR DJFA2006250Duct · leakingTHE CREW REPORTED THAT THE SIDEWALL ON THE RIGHT SIDE OF THE AIRCRAFT WAS EXTREMELY HOT AND HAD A BURNING SMELL. MAINTENANCE REMOVED THE RT CABIN SIDEWALL AND INSPECTED THE DUCTING. A LOOSE CLAMP FOR THE AFT CONDITIONED AIR WAS RESECURED. NO LEAKS WERE NOTESDR DJFA2006249Control Valve · defectiveTHE CREW REPORTED THAT THE BRAKE PEDALS ON BOTH SIDES WENT TO THE FLOOR THREE TIMES UPON BRAKE APPLICATION. THE BRAKES HAD TO BE PUMPED TO RECEIVE ANY BRAKING ACTION. MAINTENANCE REPLACED THE POWER BRAKE CONTROL VALVE AND BLED THE BRAKE SYSTEM. NO FURTHER DSDR DJFA2006247Valve · inoperativeTHE CREW REPORTED LOUD CLUNKING SOUNDS WHILE IN CLIMB, CRUISE AND DESCENT. THE CABIN TEMPERATURE WAS REPORTED AS BEING HIGH AND A BURNING PAINT SMELL WAS NOTED WHEN THE WING ANTI-ICE HEAT WAS OPERATING. MAINTENANCE REPLACED THE FLOW INCREASING VALVE. SATISFSDR OMKR200600003Rib · crackedCRACKED ROLLER RIB SUPPORT.SDR OMKR200600002Rib · crackedCRACKED ROLLER RIB ASSEMBLY.SDR DJFA2006245Arm · brokenTHE CREW REPORTED THAT THE LEFT THRUST REVERSER LOWER CLAM EXTEND ARM HAD BROKEN WHERE IT BOLTS TO BUCKET CAUSING THE OVERLAP OF THE UPPER BUCKET FLANGE TO BEND UPWARD. MAINTENANCE REPLACED THE LEFT THRUST REVERSER ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVSDR DJFA2006244Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION AS PART OF THE 'B' LEVEL INSPECTION THE LEFT INBOARD HORIZONTAL STABILIZER NOSE RIB STRUCTURE WAS FOUND CRACKED NEXT TO THE SIDE ROLLER ATTACH BRACKET. DETSDR DXTA200601383Connector · dirtyON TAXI, LOST ALL BRAKES. THE ANTISKID WAS ARMED BUT BEGAN TO FLICKER A FAIL MESSAGE BUT NEVER STEADY. TURNING THE ANTISKID OFF, HAD FULL BRAKES. TROUBLESHOT BRAKE SYSTEM. INSPECTED AND CLEANED TRANSDUCERS. ACCESSED ANTI SKID CONTROL BOX AND CLEANED CONNESDR DJFA2006241Housing · leakingTHE CREW REPORTED A BURNING SMELL IN THE AIRCRAFT WHEN INITIATING HIGH POWER SETTINGS. THE BURNING WOOD SMELL WOULD DISSIPATE AFTER APPROXIMATELY 30 SECONDS. MAINTENANCE FOUND THE NR 4 BEARING HOUSING ON THE LEFT ENGINE LEAKING WHICH WAS CAUSING THE BURNING SDR DJFA2006243Rib · crackedDURING A HORIZ STAB ROLLER BRACKET INSP (AS PART OF THE 'D' LEVEL INSP) BOTH THE RT AND LT INBD HORIZ STAB RIB STRUCTURES WERE CRACKED NEXT TO THE SIDE ROLLER BRACKET. THE HORIZONTAL STABILIZERS WERE REMOVED AND BOTH LEFT AND RIGHT LEADING EDGE ROLLER SUPPORSDR DXTA200601380Controller · noneDURING CLIMBOUT AN UNUSUAL ODOR WAS PRESENT IN THE COCKPIT. ODOR BECAME STRONG ENOUGH THAT AN IMMEDIATE LANDING WAS MADE. NO SMELL ON GROUND OR DURING RUNUP. POWER SETTINGS MADE NO DIFFERENCE IN INTENSITY. UPON INSPECTION, FOUND CABIN VIP SEAT TEMP CONTROLSDR DJFA2006237Brake Assy · leakingTRIP ID NR 1013020, THE CREW REPORTED THAT THE BRAKES FAILED ON LANDING WHILE SLOWING THROUGH APPROXIMATELY 20 KNOTS. AFTER A FEW SECONDS POWER BRAKING OPERATED NORMALLY. NO DISCREPANCIES WERE NOTED WHEN MAINTENANCE PERFORMED ANTI-SKID RESPONSE SYSTEM CHECSDR DJFA2006236Odor · detectedTHE CREW REPORTED A BURNING OR HOT WOOD SMELL IN THE CABIN. THE ODOR LASTED FOR 30 SEC TO 1 MINUTE THEN DISSIPATED. MAINTENANCE COMPLIED WITH RAYTHEON CUSTOMER SERVICE LETTER BJ-CSL-1011 WHICH REPLACES THE WRAPPING MATERIAL ON THE WING ANTI-ICE DUCTING AND COSDR DJFA2006235Switch · out of adjustTRIP ID NR 1010703, FOLLOWING SELECTION OF FLAPS FROM (0) DEGREES TO (10) DEGREES WHILE ON APPROACH, THE CREW RECEIVED A FLAP ASYMMETRY LIGHT AND FLAPS REMAINED AT (0) DEGREES. CREW AGREED TO HAVE CFR TRUCKS ROLLED WHEN THE AC LANDED. BEFORE FLAP HANDLE WAS SDR DJFA2006233Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION AS PART OF THE (B) LEVEL INSPECTION THE RT IB HORIZONTAL STABILIZER RIB STRUCTURE WAS FOUND CRACKED NEXT TO THE SIDE ROLLER BRACKET. THE HORIZONTAL STABILIZER WAS SDR DXTA200601349Fuel Control · malfunctionedRT ENGINE EFC CAME OFF LINE WHEN POWER WAS SET, SLOW SPEED ABOUT. THEY CLEARED RUNWAY AND RESET EFC. DISPATCH GAVE VERBAL RELEASE AND ENGINE POWER WAS MADE FOR TAKEOFF.SDR DJFA2006231Thrust Reverser · brokenCREW REPORTED THAT RT THRUST REVERSER DID NOT RESEAT PROPERLY. THERE WAS A .5 INCH OPENING ON THE LT BOTTOM AND A .75 INCH GAP ON THE BOTTOM RT. ONE EXTERIOR OB STANG FLANGE WAS BENT AND THE BOTTOM LOWER OB STANG WAS GOUGED. MEL 78-1 WAS ISSUED FOR THE THRUSDR DJFA2006230Bulb · burned outKPIA - KRSW TRIP ID NR 1004447 THE CREW REPORTED THAT WHILE THEY WERE ON FINAL APPROACH THEY DID NOT RECEIVE THE RT MLG DOWN INDICATION. A LOW PASS WAS MADE PAST THE TOWER TO CONFIRM THE LANDING GEAR POSITION. AN EMERGENCY WAS DECLARED AND CFR RESPONSE WASDR 071106KTRScrew · shearedUPON REMOVAL OF THE PLUNGER TUBE ASSEMBLY FROM THE LANDING GEAR CYLINDER, FOUND THE2 AN501A10-5 SCREWS THAT SECURE THE PLUNGER TUBE HEAD TO THE PLUNGER TUBE HAD SHEARED. THE CONDITION RESULTED IN LOOSE PARTS, WHICH CAUSED ONLY MINIMAL INTERNAL STRUT DAMAGE, ANSDR 2006FA0000422Tube · brokenDURING RECURRING 400 HR INSPECTION REQUIRED BY AD, FOUND AFT FUSELAGE RT BLEED AIR DUCT ASSY. BELLOWS BRAIDED WIRE MESH BLOWN OUT OF END FITTINGS. SUSPECTED TO BE CAUSED BY BLEED AIR LEAK FROM EITHER CRACKED BELLOWS OR FATIGUE/TUBING MIS-ALIGNMENT STRESS. RSDR 2006FA0000421Screw · wrong partDURING INSPECTION IAW MFG SB, FOUND BRAKE HYDRAULIC LINE DAMAGED BY FLOOR PANEL ATTACHING SCREW. REPAIRED TUBING AND MODIFIED FLOOR PANELS IAW SB. HAVE FOUND THIS SAME CONDITION ON OTHER AIRCRAFT. (K)SDR 2006FA0000375Connector · wrong partDURING SCHEDULED INSPECTION FOUND SEVERAL INCORRECT TYPE SPLICE CONNECTORS AND REPAIRS IN CABIN COLD CATHODE LIGHTING WIRING. HAVE FOUND THIS TO BE THE APPARENT CAUSE OF MINOR FIRES AND OVERHEATING ABOVE THE HEADLINER IN SEVERAL AIRCRAFT PREVIOUSLY.. SEVERALSDR DJFA2006224Strut · malfunctionedAFTER TAKEOFF ON A NORMAL CLIMBOUT THE CREW EXPERIENCED AN UNCOMMANDED NOSE GEAR EXTENSION AT 4,000 FT AND 220 KTS WHILE MAKING A RIGHT TURN. POWER WAS REDUCED AND THE AIRCRAFT WAS LEVELED OFF AT 7,000 FT. THE NOSE LANDING GEAR INDICATED DOWN AND LOCKED. THSDR DJFA2006225Blower · inoperativeTHE CREW REPORTED A BURNING WOOD SMELL IN THE CABIN AND THE CABIN TEMPERATURE CONTROL WOULD NOT ADJUST CABIN TEMPERATURE. MAINTENANCE DISCOVERED THAT THE CABIN TEMPERATURE SENSOR BLOWER WAS NOT WORKING. THE CABIN TEMPERATURE SENSOR BLOWER WAS REPLACED. NO DSDR DXTA200601304Downlock Switch · out of adjustNO RIGHT LANDING GEAR GREEN DOWN AND LOCKED INDICATION UNTIL THIRD CYCLING. NO RED UNSAFE LIGHT OR WARNING HORN, EXECUTED ABNORMAL CHECKLIST. ADJUSTED MAIN GEAR DOWNLOCK SWITCH IAW HAWKER 400XP MM 32-10-00. OPERATIONAL CHECK SATISFACTORY.SDR DJFA2006220Odor · detectedTHE CREW REPORTED, DETECTED A STRONG ELECTRICAL BURNING ODOR COMING FROM THE LAVATORY AREA. MAINTENANCE RAN THE AIRCRAFT ENGINES AND DID NOT NOTICE AN ODOR UNTIL THE BLEED AIR WAS TURNED ON. THE ODOR WAS DETERMINED TO BE COMING FROM HOT BLEED AIR ON NEW DUCTSDR DJFA2006219Switch · shortedDURING CLIMB AT 15K FT, RUMBLING SOUND HEARD AND LT ENG N1 IND 84.8% WITH A SPLIT IN ENG THROTTLES. LT THROTTLE COULD NOT BE PUSHED BACK UP, SO RT THROTTLE WAS PULLED BACK TO MATCH LT ENG'S N1 SPEED. A/C RETURNED FOR MX. LT THRUST REVERSER INBOARD UNLOCK SWSDR DJFA2006215Idler Assy · brokenTHE CREW REPORTED THAT THE RIGHT THRUST REVERSER ACTUATING ARM HAD SHEARED OFF AT THE FORWARD END OF THE ACTUATOR LINKAGE ARM. MAINTENANCE REPLACED THE RIGHT THRUST REVERSER IDLER LINK, AND REPAIRED SKIN DAMAGE ON THE UPPER THRUST REVERSER BUCKET IN ACCORDANC
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