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 DJFA2005119Downlock Switch · out of adjustKSMO - KCOS THE CREW REPORTED WHEN EXTENDING THE LANDING GEAR THE RIGHT MAIN GEAR GREEN INDICATION WAS NOT RECEIVED. THE GEAR WAS CYCLED AND THE CREW RECEIVED THE SAME INDICATION. A LIGHT TEST CONFIRMED THE LAMP WAS WORKING. THE CHECKLIST PROCEDURES WERE FSDR DJFA2005118Smoke · detectedCREW REPORTED A WHITE HAZY SMOKE LIKE VAPOR EMITTING INTO THE COCKPIT. SOON AFTER COMPLETING THE REQUIRED CHECKLISTS THE SMOKE HAD DISSIPATED AND DID NOT RETURN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED.SDR DJFA2005114Bonding Jumper · out of positionON DESCENT, THE SPEED BRAKES WERE USED TO INCREASE THE DESCENT RATE FOR APPROACH. LT YOKE WAS APPLIED TO COUNTER ACT A TURBULENCE INDUCED ROLL. THE CREW DISCOVERED THEY ONLY HAD ABOUT .2500 LT OR RT ROLL CONTROL MOVEMENT OF THE YOKE. WHEN THE SPOILERS WERE RSDR DXTA200500794Bulb · burned outLEFT GEAR GREEN DOWN LOCK INDICATOR INOPERATIVE (LIGHT BULB INOPERATIVE). REMOVED AND REPLACED ALL DOWN AND LOCKED INDICATOR BULBS, OPS CHECK GOOD.SDR AJC2005F00008Control Panel · defectiveAFTER TAKEOFF, CREW REPORTED THAT LANDING GEAR HANDLE WAS LOCKED IN DOWN POSITION AND THEY COULD NOT RETRACT GEAR. LANDING GEAR DOWNLOCK OVERRIDE WAS ENGAGED AND THE GEAR RETRACTED NORMALLY. ON DESCENT THE CREW REPORTED THAT THE SPEED BRAKES WOULD NOT DEPLOSDR DJFA2005110Wire · burnedTHE CREW REPORTED A SMELL OF BURNING WIRES AND NOTICED SMOKE COMING FROM THE GLARESHIELD AND FROM THE FRONT OF THE WINDSHIELD. THE CREW ALSO NOTICED THAT THE NR 1 RADIO TRANSFER UNIT WAS INOPERATIVE. PULLED THE RTU CIRCUIT BREAKER TO STOP THE SMOKE. THE AIRSDR DXTA200500768Warning Light · intermittentDURING T/O ROLL & TAXI BACK TO FBO THE RIGHT WINDSHIELD OVERHEAT & MASTER WARNING LIGHTS ILLUMINATED ON & OFF INTERMITTENTLY. ITEM IS UNDER INVESTIGATION.SDR DJFA2005105Coalescer Bag · contaminatedDURING CRUISE WITH ANTI-ICE SYS ON, NOTICED A STRANGE ODOR IN CABIN. WHILE LOOKING INTO CABIN THERE WAS A HAZY SMOKE EMANATING FROM REAR CABIN AROUND LAV AREA. CREW SELECTED RT ENG AS BLEED AIR SOURCE SMOKE APPEARED TO DECREASE. ACFT DIVERTED TO KAGS & MADESDR 2005FA0000864Clamp · defectiveDURING FLIGHT, THE CREW HEARD A POP AFTER WING DEICE HAD BEEN TURNED ON. THEY PERFORMED THE NESSARY PROCEDURES ACCORDING TO THE CHECKLIST. DETAILED INSPECTION REVEALED THAT THE SUSPECT CLAMP HAD SEPARATED AND CAUSED ENGINE BLEED AIR TO DUMP INTO THE AFT EQUISDR DJFA2005099Wire · damagedCREW REPORTED THAT AFTER GEAR WAS SELECTED DOWN THEY HAD ONLY RECEIVED INDICATION FOR THE NOSE AND LEFT MAIN GEAR AND THE RED GEAR HANDLE LIGHT RAN THROUGH THE PROPER SEQUENCE. THE INDICATOR LIGHTS WERE CHECKED AND THE RIGHT BULB DID TEST GOOD. THE GEAR WAS SDR DJFA2005097Switch · defectiveCREW REPORTED THAT FOLLOWING GEAR EXTENSION THEY RECEIVED 3 GREEN LIGHTS ALONG WITH 2 RED LIGHTS IN GEAR HANDLE. GEAR WAS CYCLED, AND THE SAME INDICATION WAS OBSERVED. AIRCRAFT PERFORMED A GO-AROUND AND TOWER COMMUNICATED THAT THE GEAR AND GEAR DOORS APPEAREDSDR 2005FA0000786Tube · unserviceableDURING INSPECTION FOUND FLEXIBLE BELLOWS EXTENDED DUE TO THE WIRE BRAID FAILURE. INTEGRITY OF THE BLEED AIR SUPPLY TUBE WAS INTACT. INSPECTION OF THE LT ENGINE TUBE FOUND BRAID PARTIALLY FAILED. BOTH BLEED AIR SUPPLY TUBES WERE REPLACED WITH NEW. (K)SDR DJFA2005092Transfer Tube · malfunctionedCREW FOUND FUEL CROSSFEED NOT MAINTAINING A BALANCED CONDITION AS RT WING TANK CONTINUED TO DEPLETE. CROSSFEED SWITCHES CYCLED & CIRCUIT BREAKERS CHKD. REPORTED FUSELAGE FUEL NOT TRANSFERRING TO WING TANKS. ACFT PREVIOUSLY ISSUED MEL 28-2-2 FOR DISCREPANCY SDR DJFA2005094Speed Brake · malfunctionedCREW REPORTED; ON APPROACH ABOVE 10,000 FT SPEEDBRAKES WERE EXTENDED & A YAWING / ROLLING MOVEMENT OF ACFT OCCURRED WITH NOSE MOVING 15-20 DEG. SPEEDBRAKES RETRACTED & CREW DISCONNECTED AUTOPILOT & PERFORMED A CONTROL CHK OF ACFT. ACFT THEN BEHAVED NORMAL. SDR DJFA2005090Switch · false indicationDURING CLIMB FROM 28,000 FT TO 33,000 FT, RIGHT THRUST REVERSER DEPLOY LIGHT ILLUMINATED. THE ARM AND UNLOCK LIGHTS REMAINED EXTINGUISHED. CREW PUSHED BOTH THRUST REVERSER EMERGENCY STOW BUTTONS. THE DEPLOY LIGHT EXTINGUISHED AT 9,000 FT AND 190 KTS. AN UNSDR E812005F00000Computer · malfunctionedTROUBLESHOT PILOT REPORT OF TAWS SYSTEM AND RADAR INOPERATIVE. FOUND TAWS8000 SYSTEM LOCKED UP. NO RESPONSE WHEN COMPUTER CONNECTED FOR TROUBLESHOOTING. REPLACED TAWS8000 UNIT WITH REPAIRED UNIT, SYSTEM OPERATIONS NORMAL. FOUND RADAR INOPERATIVE DUE TO REMSDR DJFA2005087Lever · splitCREW REPORTED THAT WHILE AT CRUISE FLIGHT 380, WITH ENGINE SYNCRONIZATION ON, BOTH ENGINES ROLLED BACK FROM N1 AT 98.0 TO 90.9, OAT WAS -63 DEGREES. THE ENGINE SYNCHRONIZATION WAS TURNED OFF AND ENGINE IGNITERS WERE TURNED ON. THE CREW WAS THEN ABLE TO INCRESDR OMKR200600001Rib · crackedROLLER RIB AT INBOARD END CRACKED (ASSY P/N 45A21104-642) IN THREE PLACES. RIB, AND BOTH CLIPS. CRACKING IS FROM RIB MATERIAL BEING TOO THIN, IMPROPER RIGGING, OR EXCESSIVE WEAR OF HORIZONTAL STABILIZER HINGE POINTS. SUSPECT RIB MATERIAL IS JUST TOO THIN TOSDR 2005FA0000664Starter Gen · inoperativeINVESTIGATED PILOT REPORT OF LT ENGINE NOT ROTATING WHEN STARTER BUTTON DEPRESSED. FOUND STARTER GEN NOT ROTATING WITH POWER APPLIED. REPLACED STARTER GEN WITH OVERHAULED UNIT IAW MM. ENGINE START AND GENERATOR OPERATIONS NORMAL. TRANSIENT AIRCRAFT AT OFF-SDR DJFA2005083Switch · failedCREW REPORTED THAT WHILE IN CRUISE FLIGHT AT FL 360, THE AIR CONDITIONING FAIL LIGHT ILLUMINATED AND THE EMERGENCY PRESSURIZATION SYSTEM ACTIVATED. AN EMERGENCY WAS DECLARED AND CREW DIVERTED TO KSBA. DURING THE EMERGENCY DESCENT, SMOKE WAS NOTICED IN THE AISDR DJFA2005081Bulb · burned outKIND - KACY TRIP ID NR 815740 CREW REPORTED THAT WHILE PREPARING FOR LANDING THEY DID NOT RECEIVE THE LEFT MAIN GEAR GREEN INDICATION. FIRE/RESCUE RESPONSE AND PRIORITY HANDLING WAS GIVEN. AIRCRAFT PERFORMED A FLY-BY PAST THE TOWER TO CONFIRM THE GEAR WAS DOSDR DJFA2005080Valve · malfunctionedKTEB TRIP ID NR814487 CREW REPORTED THAT AFTER TAKEOFF WHILE ATTEMPTING TO RETRACT THE LANDING GEAR, THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AN ALTERNATE GEAR EXTENSION WAS INITIATED, AND THREE GREEN AND NO RED INDICATIONS WERE RECEIVED. A FLY-BY PAST THSDR DJFA2005078Switch · no indicationKDAL TRIP ID NR 813053, CREW REPORTED THAT THEY RECEIVED A UNSAFE GEAR INDICATION FOR THE RIGHT MAIN GEAR WITH NO GREEN LIGHT ILLUMINATING. THE GEAR HANDLE LIGHT WAS EXTINGUISHED. GEAR WAS CYCLED ONCE WITH NO CHANGE IN GEAR DOWN INDICATION. AN ALTERNATE GEASDR DJFA2005075Line · reversedKTEB - KBWI TRIP ID NR 807676 CREW REPORTED THAT WHILE ON LANDING ROLL OUT AT APPROXIMATELY 60 KTS, WHEN THE BRAKES WERE APPLIED THEY WOULD CATCH AND THE AIRCRAFT WOULD MOVE LEFT AND RIGHT OF THE CENTERLINE. WHILE AT TAXI SPEEDS THE AIRCRAFT WAS REPORTED AS HSDR DJFA2005071Landing Gear · malfunctionedCREW REPORTED THAT DURING DESCENT THROUGH FL 250 AT APPROXIMATELY 300 KTS THE NOSE GEAR EXTENDED AND LOCKED DOWN. THE CREW SLOWED THE AIRCRAFT TO 200 KTS AND EXTENDED THE GEAR. THE MAIN GEAR EXTENDED NORMALLY. A FLY-BY WAS PERFORMED SO TOWER COULD VISUALLY SDR DJFA2005068Heater · contaminatedCREW REPORTED THAT THEY NOTICED A HAZE AND A BURNING SMELL IN THE CABIN. THE CREW BELIEVED THAT SOMETHING MAY HAVE BEEN PLACED INTO A HEATER VENT THAT WAS CAUSING THE SMOKE. THE HEAT WAS THEN TURNED OFF AND THE HAZE HAD DISSIPATED. WHEN THE HEAT WAS TURNED BSDR DJFA2005066Bulb · inoperativeCREW REPORTED THAT WHILE ON APPROACH TO KVNY, AFTER LOWERING THE LANDING GEAR, THE NOSE GEAR DID NOT INDICATE GREEN. THE RED GEAR HANDLE LIGHT WAS EXTINGUISHED. THE LANDING GEAR WAS CYCLED AND CREW RECEIVED THE SAME INDICATION. A MASTER LIGHT TEST INDICATEDSDR 2005FA0000446Bracket · brokenFLIGHT CREW REPORTED LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION FOLLOWING DEPARTURE. CREW ELECTED TO RETURN TO AIRPORT. OBTAINED DOWN AND LOCKED INDICATION ON ALL 3 LANDING GEAR AND LANDED UNEVENTFULLY. UPON JACKING AC FOR SDR DJFA2005063Switch · false activationKDET - KIND DURING APPROACH TO RUNWAY 32 IN KIND, THE GEAR HANDLE LIGHT REMAINED ILLUMINATED RED WITH ALL THREE GEAR INDICATORS SHOWING DOWN AND LOCKED. GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULTS. THE TOWER HAD CONFIRMED AT LEAST ONE MAIN GEAR DOOR WSDR MXI2005F00001Switch · failedTHE LANDING GEAR WOULD NOT EXTEND WITH GEAR HANDLE DOWN. THE LANDING GEAR WAS LOWERED USING THE MANUAL EMERGENCY EXTENSION AND THE GEAR DOORS WERE CLOSED USING THE PNEUMATIC GEAR BOTTLE. PROBABLE CAUSE WAS THE HIGH RESISTANCE IN THIS SWITCH AND THE GEAR DOORSDR MXI2005F00000Switch · failedTHE LANDING GEAR WOULD NOT EXTEND WITH GEAR HANDLE DOWN. GEAR WAS LOWERED USING THE MANUAL EMERGENCY EXTENSION AND THE GEAR DOORS WERE CLOSED USING THE PNEUMATIC GEAR BOTTLE. PROBABLE CAUSE WAS THE HIGH RESISTANCE IN THIS SWITCH AND THE GEAR DOOR CLOSED SWITSDR DJFA2005067Rib · crackedDURING A ROUTINE MAINTENANCE VISIT WHILE PERFORMING PHASE A AND PHASE B INSPECTIONS A CRACKED RIB WAS DISCOVERED ON THE LEFT HORIZONTAL STABILIZER AT THE LEFT ROLLER ASSEMBLY. THE RIB WAS REPLACED ALONG WITH SUPPORT BRACKETS. THE AIRCRAFT WAS RETURNED TO SERSDR 2005FA0000356Wire · brokenREMOVED BATTERY FROM ELT 110-406 FOR VISUAL INSPECTION IAW WITH MFG MM. UPON INITIAL INSPECTION FOUND ONE WIRING TERMINAL BROKEN OFF OF ONE BATTERY CELL. BATTERY EXPIRATION DATE 6/2006. (K)SDR DJFA2005060Switch · faultyKMIA - KMCO CREW REPORTED AFTER DESCENDING TO FL 270 FELT ACFT YAW TO LEFT. PARTIAL LT T/R DEPLOYMENT, NO WARNING INDICATION RECEIVED. AIRSPEED REDUCED & LT & RT T/R EMERGENCY STOW BUTTONS ACTIVATED. LT ENG SHUT DOWN, ACFT LANDED. MX INSPECTED LT T/R & FOSDR DJFA2005058Fuel Sys · contaminatedKMIA - KCVG CREW REPORTED THAT WHILE DESCENDING FROM 19,000 TO 11,000 FEET THE LEFT FUEL FILTER BYPASS LIGHT ILLUMINATED MOMENTARILY, THEN RE-ILLUMINATED AFTER APPROXIMATELY ONE MINUTE. SEVERAL MINUTES LATER THE RIGHT FUEL FILTER BYPASS LIGHT ILLUMINATED, ANSDR DJFA2005057Display · malfunctionedSHORTLY AFTER TAKEOFF CREW NOTICED AN INCREASING TREND OF A BURNING ELECTRICAL SMELL. AFTER APROXIMATELY 15 MINUTES THE NR 2 PRIMARY FLIGHT DISPLAY FAILED WITH A "DISPLAY TEMP" FLAG. THE APPROPRIATE CIRCUIT BREAKER WAS PULLED, AND AIRCRAFT RETURNED TO KAPA WSDR DJFA2005059Squat Switch · out of adjustKPBI CREW REPORTED THAT JUST AFTER ROTATION THE LEFT AND RIGHT THRUST REVERSER ARM LIGHTS HAD ILLUMINATED. THE EMERGENCY STOW BUTTONS WERE IMMEDIATELY PRESSED. THE AIRCRAFT RETURNED TO KPBI AND LANDED WITHOUT FURTHER INCIDENT. THE ARM LIGHTS HAD REMAINED ISDR DJFA2005055Brake Assy · wornCREW REPORTED, AFTER LANDING THE BRAKES FAILED AFTER 50 KTS. EMERGENCY BRAKING SYSTEM WAS USED TO STOP THE AIRCRAFT. MAINTENANCE FOUND THE LEFT AND RIGHT BRAKE ASSEMBLIES TO BE WORN. THE LEFT AND RIGHT BRAKE ASSEMBLIES WERE REPLACED. MANUAL AND POWER BRAKESDR DJFA2005054Sensor · malfunctionedIN CRUISE FLT CREW NOTICED AN ELECTRICAL ODOR IN COCKPIT. ODOR SEEMED TO DISSIPATE AFTER BATTERY & MASTER GENERATOR SWITCHES WERE PLACED IN EMERGENCY POSITIONS. EMERGENCY DECLARED & ACFT LANDED. MX INSPECTED BATTERY WIRING, AREA BEHIND LAV PANEL, AND THE DUSDR 2005FA0000630Relay · looseCREW SQUAWKED ELEC FUMES AND FOUL ODOR IN COCKPIT. ODOR SEEMED TO LET UP AFTER BATTERY PLACED IN EMERG AND BOTH GENERATORS PLACED IN EMERG. MAINT FOUND RT WINDSHIELD HEAT CURRENT SENSE RELAY (L102S) TERMINAL B AND APPROX 2 INCHES OF WIRE INSULATION TO OVERHESDR DJFA2005052Actuator · failedCREW REPORTED MX TEST FLT GEAR CYCLED TO DOWN POSITION RESULTING IN TWO GREEN & ONE RED LIGHT. LEFT MAIN GEAR DID NOT SHOW DOWN AND LOCKED, WHICH WAS CONFIRMED BY RETARDING THE THROTTLE TO ACTIVATE THE LANDING GEAR WARNING HORN. AFTER SEVERAL UNSUCCESSFUL GESDR DJFA2005048Cowling · detachedCREW REPORTED THAT DURING CLIMB-OUT OF KTEB AT APPROXIMATELY 5,000 FT, THEY HAD FELT A SMALL BUMP. THE REST OF THE FLIGHT WAS WITHOUT INCIDENT. WHILE PERFORMING THE POSTFLIGHT INSPECTION IT WAS DISCOVERED THAT THE LOWER HALF OF THE RIGHT COWLING HAD BEEN TORSDR DJFA2005049Cable Assy · bindingCREW REPORTED THAT WHILE AT CRUISE FL390 FOR APPROXIMATELY 15 MINUTES, THEY WERE UNABLE TO ADJUST THE LEFT POWER LEVER AS IT WOULD NOT MOVE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS DIVERTED TO KELP. WHILE DESCENDING THROUGH FL220 THE LEFT POWER LEVER HAD SDR DJFA2005050Actuator · defectiveCREW REPORTED, AFTER NUMEROUS ATTEMPTS TO LOWER THE GEAR, DID NOT RECEIVE 3 GREEN LIGHTS. AN ALTERNATE EXTENSION WAS PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH MAIN LANDING GEAR DOWNLOCK SWITCHES, AND INSTALLED A NEW COSDR DJFA2005046Panel · meltedKPSP - KLAS TRIP ID# 743429 CREW REPORTED THAT THEY HEARD A POPPING SOUND COMING FROM THE CIRCUIT BREAKER PANEL. ARCHING HAD OCCURED FROM THE BOTTOM OF THE CIRCUIT BREAKER PANEL FOLLOWED BY A NOTICABLE SMOKEY SMELL. APPROXIMATELY TEN SECONDS LATER THE ARCHING SDR DJFA2004046Control Panel · arcedCREW REPORTED THAT THEY HEARD A POPPING SOUND COMING FROM THE CIRCUIT BREAKER PANEL. ARCING HAD OCCURRED FROM THE BOTTOM OF THE CIRCUIT BREAKER PANEL FOLLOWED BY A NOTICEABLE SMOKY SMELL. APPROXIMATELY TEN SECONDS LATER THE ARCING HAD EXTINGUISHED AND VAPOR SDR DJFA2004045Engine · underservicedAFTER T/O, THE LT ENGINE OIL PRESS GAUGE HAD DROPPED TO ZERO IND. WHEN POWER WAS REDUCED THE LT ENGINE OIL TEMP HAD INCREASED. THE LT ENGINE WAS SHUT DOWN AND AN EMERG DECLARED. NO YELLOW OR RED ANNUNCIATORS HAD ILLUMINATED. A/C HAD DIVERTED TO KPFN AND LANDSDR 2005FA0000703Connector · looseINVESTIGATED LANDING GEAR RETRACT SYSTEM FAULT (LANDING GEAR WOULD NOT RETRACT WHEN GEAR HANDLE SELECTED (UP) AFTER TAKEOFF) FOUND P162 CONNECTOR LOOSE, NOT FULLY SEATED ON A162 PC BOARD ASSY. J1 CONNECTOR, RESEATED P162 CONNECTOR TO A162J1 CONNECTOR, LANDINGSDR 2005FA0000702Nut · wornDURING A AND B INSPECTION NOTICED CLUNK IN PITCH TRIM. FOUND ACTUATOR IN FULL NOSE DOWN POSITION CONTACTING VERTICAL FIN CAP SUPPORT. UPON FURTHER INVESTIGATION FOUND JACKSCREW FREEPLAY MEASURED .075 MAX ALLOWABLE FREEPLAY IS .020. ACTUATOR OVERHAUL INTERVSDR DJFA2004041Duct · leakingCLIMBING TO 10,000 FT, LT BLEED AIR DUCT FAIL ANNUNCIATOR HAD ILLUMINATED. ENG THRUST REDUCED, AND CABIN PRESSURIZATION SOURCE TURNED OFF. TWO MINS LATER COCKPIT & CABIN HAD FILLED WITH SMOKE FOLLOWED BY EMERGENCY PRESSURIZATION VALVE OPENING. CREW DONNED O
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