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 = 'PA42' 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 = 'PA42' 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 IL7A2017062800001Shaft · shearedLEFT ENGINE SHUTDOWN AT APPROXIMATELY 1500. JUST BEFORE DESCENT, THE LEFT ENGINE LOST TORQUE AND % RPM AND LOW OIL PRESSURE WAS INDICATED. CROSSED CHECKED THE ENGINE INSTRUMENTS TO DETERMINE IF IT WAS A FAULTY INDICATOR, THEN FEATHERED THE LEFT ENGINE AND FOSDR PQG2014F00000Shuttle Valve · inoperativeVALVE PARTIALLY OPENED ALLOWS FLUID THROUGH TO PNUMATIC SIDE. IT IS SUSPECT OF WIND/SIDE LOAD TO PUSH AGAINST IB GEAR DOOR, FORCING HYDRAULIC FLUID PAST VALVE TO PNUMATIC SIDE.SDR 2013FA0000002Actuator · inoperativeDURING LANDING, THE LEFT MLG ACTUATOR LOCKED UP INTERNALLY CREATING A GEAR UNSAFE CONDITION.SDR GBBRN8RYATA24Connector · meltedDURING CRUISE FLIGHT THE PIC NOTED A HOT ELECTRICAL ODOR AND MINOR SMOKE IN THE RT SIDE COCKPIT AREA. THE PIC EXECUTED AN EMERGENCY DECENT AND DEPRESSURIZED THE CABIN FOR VENTILATION. THE FLIGHT WAS DIVERTED TO AN ALTERNATE (CLOSER) AIRPORT AND LANDED UNEVENTFSDR ZFD2007F00000Pump · malfunctionedPILOT STATED THAT THE LT FUEL PRESSURE WOULD GO TO ZERO IF THE ELECTRIC PUMPS WERE TURNED OFF. FOUND AIRFRAME MFG INSTALLED ENGINE DRIVEN PUMP INOPERATIVE.. THE PUMP DRIVE WAS FOUND TO BE SLIPPING. INSPECTED THE PUMP AND NO OTHER DEFECTS WERE NOTED. THE PUSDR CA030926002Shaft · cracked(CAN) PILOT REPORTED LACK OF NOSE WHEEL STEERING CONTROL. UPON INSPECTION, THE NOSE WHEEL STEERING SHAFT WAS FOUND CRACKED LONGITUDINALLY BETWEEN BOLT HOLES.SDR CA030708001Door · buckled(CAN) ON DESCENT AT 8500 FT, LT WING LOCKER DOOR BUCKLED UP IN MIDDLE APPROX 4-5 INCHES, THEN CAME LOOSE FROM DOOR PIN AND POPPED OPEN & STARTED FLAPPING. AIRCRAFT SPEED WAS REDUCED TO 140 KTS & AIRCRAFT LANDING WAS UNEVENTFUL. DETERMINED THAT WING LOCKER WASSDR FTU2002F00000Bracket · mismanufacturedRECEIVED TWO NEW MAIN LANDING GEAR DOWN LOCK PIVOT BRACKETS, FOUND THE SLOT SUED TO CREATE THE PIVOT CAPABILITY WAS IMPROPERLY MACHINED. WHEN INSTALLED ON THE AIRCRAFT, THE PART WOULD NOT PIVOT DUE TO CLEARANCE PROBLEM REPLACEMENT ITEM ON THIS AIRCRAFT, ALONGSDR 2002FA0001269Screen · crackedDURING A SCHEDULED EVENT INSPECTION, BOTH ENGINE AIR INLET SCOOP SCREENS WERE FOUND CRACKED IN BOTH FORWARD CORNERS FOR EACH ENGINE. REPAIR WAS NOT FEASABLE DUE TO THE LOCATION DAMAGE. BOTH INLET SCREEN HAD TO BE REPLACED WITH NEW PARTS.SDR AUS20021193Trunnion · cracked(AUS) LANDING GEAR TRUNNION CRACKED THROUGH VERTICAL WEB. CRACK LENGTHAPPROXIMATELY 12.7MM (0.5IN). AIRCRAFT OPERATES FROM ROUGHSTRIPS.SDR AUS20021192Bulkhead · cracked(AUS) LH ENGINE NACELLE BULKHEAD CRACKED.SDR ESM2002F00000Tire · splitPILOT NOTED AFTER LAST LANDING, SPLITS/TEARS APPROXIMATELY 1 INCH IN LENGTH, BETWEEN OUTBOARD TREAD IN GROOVE OF TIRE.SDR CA020405005Bolt · cracked(CAN) DURING MAIN WHEEL ASSEMBLY TIRE REPLACEMENT, THREE TIE BOLTS OUT OF EIGHT SHEARED WHEN RECOMMENDED TORQUE WAS APPLIED. PRIOR TO ASSEMBLY ALL BOLTS WERE VISUALLY INSPETED AND NO EVIDENCE OF CRACKS WERE NOTED. ALL EIGHT BOLTS WERE REPLACED.SDR CA020108003Pump · stripped(CAN) ENGINE SHUT DOWN IN CRUISE FLIGHT. AIRCRAFT MADE AN UNSCHEDULED LANDING TROUBLESHOOTING REVEALED NO FUEL FLOW TO DIVIDER. HIGH PRESSURE FUEL PUMP REMOVED. FUEL PUMP SPLINES FUND TO BE STRIPPED. PUMP REPLACED.SDR CA010809018Outflow Valve · dirty(CAN) AT FLIGHT LEVEL 22000, CABIN LOST PRESSURE. AN EMERGENCY DESCENT WAS CARRIED OUT AND THE REMAINDER OF THE FLIGHT WAS NORMAL. UPON INSPECTION THE OUTFLOW VALVE WAS FOUND TO BE LOOSE AND DIRTY. THE VALVE WAS CLEANED & TIGHTENED, THEN A SATISFACTORY TEST FLSDR 20000911SH018Tire · shearedTIRE SHREADED ON LANDING. (X)SDR CA000516024Valve · failed(CAN) PILOTS CHECKED FOR BRAKE PRESSURE DURING CRUISE FLIGHT AT 33,000 FEET. BRAKES WERE VERY SOFT. PARKING BRAKE VALVE FOUND TO HAVE LEAKING O-RINGS. SEALS REPLACED.SDR CA000218001Bearing · broken(CAN) OUTER WHEEL HALF BEARING WAS FOUND LOOSE. THIS ALLOWED WHEEL TO MOVE AND LOCK BRAKE DISC IN CALIPERS. IT APPEARS THAT THE OUTER BEARING SEIZED OR JAMMED AND THE OUTER RACE SPUN IN THE ALUMINIUM WHEEL HALF WEARING THE WHEEL HALF AND DEFORMING IT. GREASSDR 20000523SH017Connector · damagedCREW REPORTED SMOKE SMELL IN THE COCKPIT AND THEN NUMEROUS CIRCUIT BREAKERS STARTED TRIPPING. AFTER AIRCRAFT SHUT DOWN AFTER LANDING, THE BATTERY POWER COULD NOT BE SHUT OFF. THE BATTERY WAS DISCONNECTED AND AN INVESTIGATION REVEALED THE ELECTRICAL CONNECTORSDR 99ZZZX4235Spring · brokenFIVE OUT OF SIX SPRING STEEL PLATES WERE BROKEN ON LEFT SIDE OF ASSEMBLY AND CHAFING ON PITOT/STATIC RIGID LINES AND LEFT SIDE OF WHEELWELL.SDR 99ZZZX4234Spring · brokenFIVE OUT OF SIX SPRING STEEL PLATES WERE BROKEN ON LEFT SIDE OF ASSEMBLY AND CHAFING ON PITOT/STATIC RIGID LINES AND LEFT SIDE OF WHEELWELL.SDR 99ZZZX4241Valve · stickingDURING LANDING GEAR EXTENSION, LEFT AND RIGHT LANDING GEAR WOULD NOT EXTEND. AN ATTEMPT TO EXTEND THE GEAR WAS MADE USING EMERGENCY BLOW-DOWN SYSTEM. THE RIGHT GEAR CAME DOWN, BUT NOT THE LEFT. THE LEFT GEAR EVENTUALLY CAME DOWN. ACFT WAS PLACED ON JACKS ASDR 99ZZZX1559Tire · mismanufacturedTIRE WAS RE-CAPPED BY HAWKINS AIRCRAFT TIRE CO. TIRE WOULD NOT ALLOW GEAR DOOR TO FULLY CLOSE.SDR 99ZZZX1573Washer · missingCABIN COULD NOT PRESSURIZE ABOVE 2.5 PSI. FOUND CARGO DOOR SEAL, SEALING WASHER MISSING. INSTALLED NEW SEALING WASHER.SDR 99ZZZX970Rod · brokenLEFT MAIN GEAR DOOR ACTUATOR ROD END BROKE OFF 1.50 INCHES FROM END OF ROD END.SDR 99ZZZX488Engine · failedCATASTROPHIC FAILURE OF LEFT ENGINE. AIRCRAFT WAS EN ROUTE TO DESTINATION WHEN AN IN-FLIGHT FAILURE OF LEFT ENGINE OCCURRED. DESTRUCTION AND SEPARATION OF TURBINE BLADES AFT OF HOT SECTION OCCURRED. PIECES OF BLADES WENT THROUGH AND DESTROYED BOTH EXHAUST SSDR 98ZZZX4782Angle · crackedON A ROUTINE INSPECTION, A 2 INCH CRACK WAS FOUND ON THE RT ENGINE FIREWALL COMING OUT FROM UNDER OUTBOARD LOWER MOUNT FLANGE. THE MOUNT BOLT APPEARED TO BE TORQUED CORRECTLY. WHILE DOING REPAIR TO FIREWALL, FOUND A CRACK IN ANGLE ON AFT SIDE OF FIREWALL. 7SDR 98ZZZX4480Line · leakingRIGHT BRAKE SOFT. FOUND THE STEEL BRAIDED LINE RUBBING ON STEEL HARD LINE AND WORE A HOLE IN STEEL LINE. SUBMITTER RECOMMENDED THE LINES UNDER INSTRUMENT PANEL BE CHECKED FOR CHAFING.SDR 98ZZZX4524Nipple · crackedRUBBER NIPPLE AT OUTBOARD END OF TANK FROM TIP TANK CRACKED AND ALLOWED FUEL TO LEAK FROM WING. DEFECT WAS FOUND AFTER REPLACING FORWARD FUEL CELL AND FILLING WING WITH FUEL TO LEAK CHECK. SUBMITTER SUGGESTED POSSIBLE CAUSE OF FAILURE, AGE OF FUEL CELL CAUSISDR 98ZZZX2660Window · crackedCOPILOT WINDOW HAS CRACKED.SDR 98ZZZX2445Connector · smokedELECTRICAL PLUG CODE E357 MALE P/N 206037-1, FEMALE, P/N 206036-3. WHILE IN CRUISE FLIGHT, SMOKE WITH AN 'ELECTRICAL SMELL' BEGAN COMING OUT OF OVERHEAD SWITCH PANEL. PILOT INITIATED A SHUTDOWN OF ELEC SYS. SMOKE LASTED ABOUT 10 SECONDS, 3 EXTERIOR LIGHTINGSDR AU980283Engine · failed(AUS) ENGINE POWER SECTION FAILED.SDR AU980220Gear · failed(AUS) RT ENGINE REDUCTION GEARBOX PLANETARY GEAR FAILURE. METAL CONTAMINATION OF GEARBOX. GEARBOX DECOUPLED FROM POWER TURBINE. SECOND STAGE TURBINE SHED ALL BLADES CAUSING INTERNAL DAMAGE.SDR 98ZZZX828Link Assy · failedJANUARY 8, AIRCRAFT LANDED AND THE NOSE GEAR COLLAPSED. INITIAL INVESTIGATION REVEALED A LINK ASSY FAILURE. THE MECHANICAL LINKAGE OF NOSE GEAR ASSY IS SUCH THAT IT WILL NOT INDICATE A GEAR UNSAFE CONDITION. SUBMITTER RECOMMENDED A SPECIAL INSPECTION FOR LISDR 98ZZZX235Retract Link · crackedDURING ROUTINE INSPECTION, 250-HOUR MAGNAFLUX INSPECTION PERFORMED ON RETRACT ARM LINK. LEFT LINK WAS FOUND CRACKED. TIME SINCE LAST INSPECTION, 107 HOURS. NOTE: PA42 MM CONTAINS NO NDT INSTRUCTIONS OR WHAT TYPE OF NDT TO BE USED DURING THIS INSPECTION. LSDR 98ZZZX31Auxiliary Lock · failedJUST PRIOR TO VR, DOOR HANDLE ROTATED AND DISENGAGED PINS. PILOT ABORTED TAKEOFF, CLOSED DOOR, AND TAXIED BACK TO PARKING. INITIAL INSPECTION REVEALED THAT AUXILIARY LOCK DID NOT ENGAGE.SDR 97ZZZX4630Connector · burnedCONNECTOR E324 WAS FOUND SEVERELY OVERHEATED IN SWITCH PANEL OVERHEAD. CONTROLS PITOT STALL/HEAT. SUSPECT UNDERRATED CONNECTOR FOR AMPERAGE.SDR 97ZZZX2905Clamp · missingFUEL FLOW TRANSMITTER IS MOUNTED TO ENGINE WITH 2 STAINLESS LINES PN 3032010 AND PN 3026779 B1; AND, IF SUPPORT CLAMP PN 30006614 IS NOT INSTALLED, LINES WILL CRACK AT WELDS CREATING A HEAVY FUEL LEAKING ENGINE COMPARTMENT AND ONTO WING.SDR 97ZZZX1706Mount Bracket · brokenDURING SCHEDULED MAINTENANCE, PASSENGER SEAT AFT FACING BEHIND COPILOT, WRITTEN UP AS 'LOOSE IN TRACK'. DISCOVERED FRONT FLOOR MOUNTED BRACKET CRACKED AND TORN FROM SEAT FRAME. SUSPECT CAUSE, SEAT BACK USED AS LEVERAGE INTO COCKPIT: ALSO, AIRCRAFT TYPE CERTSDR CA970318005Fuel Contrl Unit · faulty(CAN) ENGINE TORQUE AND TEMPERATURE CONTINUED TO INCREASE AS THROTTLE WAS RETARDED. PILOT SELECTED THROTTLE TO OFF POSITION, TEMPERATURE STILL INCREASED. ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION FOUND FUEL CONTROL UNIT FAULTY. FCU WAS REPLACED.SDR 97ZZZX1076Snap Rings · missingLEFT HAND ENGINE WILL NOT MAINTAIN FULL RPM ON TAKEOFF. WILL NOT GO ABOVE 1850 RPM AND THEN DROPS OFF TO 1600 RPM. RPM RECOVERS TO 2000 RPM AFTER 2-3 MINUTES IN FLIGHT. FOUND LEFT PROP HAD TWO BETA FOLLOW-UP TUBE BUSHINGS, MISSING SNAP RINGS. REMOVED PROP SDR 96ZZZX5734Bolt · fracturedDURING ROUTINE INSPECTION THE LEFT ENGINE, LEFT OUTBOARD UPPER ENGINE MOUNT TO FIREWALL RETENTION BOLT, P/N 553-344 WAS FOUND FRACTURED. PART TOTAL TIME WAS 5338.1 HRS. LIFE LIMIT FOR THE PART PER PIPER MTC. MANUAL (P/N 761.523 CHAPTER 5 IS 7,500 HRS. IT WASDR 96ZZZX5075Shuttle Valve · damagedNIPPLE OF VALVE TO MAIN GEAR ACTUATOR BROKE OFF CAUSING LOSS OF FLUID AND FAILURE OF RIGHT GEAR TO DOWNLOCK.SDR CA960925001O-Ring · worn flat(CAN) WITH SYSTEM PRESSURE ON, EMERGENCY UPLOCK ACTUATOR O-RINGS LEAK FLUID INTO THE RIGHT HAND GEAR WELL. WITH NO SYSTEM PRESSURE THERE IS NO LEAK.SDR 96ZZZX4703Web · crackedINSPECTION FOUND A CRACKED WEB AT BOTH ENGINE FIREWALLS AT ENGINE MOUNT AREA.SDR AU961028Housing · cracked(AUS) RH MAIN LANDING GEAR OLEO HOUSING ASSEMBLY CRACKED FROM TOP TO BOTTOM THROUGH THE SHARP RADIUS AT THE BASE OF THE SIDE BRACE ATTACHMENT LUG - LOSS OF OLEO PRESSURESDR 96ZZZX3826Connector · burntPILOT REPORTED ERRONEOUS RIGHT STALL WARNING AND A MOMENTARY 'PUFF' OF SMOKE FROM RT INSTRUMENT PANEL. INSPECTION REVEALED PRESSURE BULKHEAD AREA BURNED. (CONNECTOR NR E339/439.) CONNECTOR WAS REPLACED AND GOLD PLATED PINS AND SOCKETS INSTALLED.SDR AU960645Bracket · cracked(AUS) LH ENGINE UPPER OUTBOARD ENGINE MOUNT TO FIREWALL ATTACHMENT BRACKET CRACKED THROUGH VERTICAL FACE FROM TOP WELD LINE EXTENDING DOWN BETWEEN RIVET HOLES - CRACK LENGTH 9MM (0.35IN)SDR CA960527001Tire · burst(CAN) ON LANDING, LEFT MAIN TIRE BLEW UP. NO OTHER DAMAGE.SDR CA960304010Bracket Support · cracked(CAN) INDICATION WAS A 1/2 INCH CRACK IN THE EDGE OF THE DOOR SKIN WHICH HAD PREVIOUSLY BEEN STOP DRILLED. INSPECTION FOUND PART TO HAVE A 3 INCH CRACK ACROSS FOUR RIVET HOLES. A CRACK WAS ALSO FOUND AT TWO OF THE FOUR RIVET HOLES WHICH PICK UP THE HINGE IN TH
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