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 engine_model_key = 'IO360' 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 engine_model_key = 'IO360' 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 2005FA0000777Spring · fracturedPROPELLER PITCH WENT UNCONTROLLABLE IN STRAIGHT AND LEVEL FLIGHT. SPRING HAD ONE COMPLETE FRACTURE AND AT LEAST 4 INCOMPLETE FRACTURES. (K)SDR 2005FA0001251Clamp · separatedEXHAUST PIPE TO TURBOCHARGER CLAMP FOR FRONT ENGINE CRACKED AT SPOT-WELD AND SEPARATED ON TAKEOFF. WHEN THIS HAPPENED, THE EXHAUST PIPE DEPARTED THE AIRCRAFT AND THE EXHAUST SCORCHED THE ENGINE COWLING AND FIREWALL. (K)SDR 2005FA0000700Magneto · shortedON A 500 HOUR MAGNETO INSPECTION, FOUND MAGNETO SPARKING INTERNALLY. AC RAN GOOD AND HAD A 100 RPM MAG DROP. INTERNAL SPARKING WAS BETWEEN COIL AND CARBON BRUSH. BRUSH AND SPRING DESTROYED AND PART OF DISTRIBUTOR BLOCK MISSING. RECOMMEND MANDATORY INTERNALSDR 2021092004Strut · crackedWHILE PERFORMING AN ANNUAL INSPECTION IT WAS NOTED THE NOSE LANDING GEAR STRUT ASSY P/N 11907-004 HAD TWO SMALL CRACKS. THE AREA IN QUESTION IS LOCATED JUST AFT OF THE INTERSECTION OF THE (ROUND) STRUT ASSEMBLY AND THE LT AND RT (BOXED) SECTIONS THAT ATTACH THSDR 2004FA0000785Pcu · frozenNEW PROP CONTROL INSTALLED IAW SRM, CONTROL OPERATED FINE, AIRCRAFT WAS FLOWN ONCE AFTER COOL DOWN. PROP CONTROL WAS FROZEN, WAS ABLE TO BREAK FREE, INSTALLATION AND RIGGING CHECKED, PROP GOVERNOR CHECKED, AIRCRAFT FLOWN AGAIN, PROP CONTROL FROZEN AGAIN AFTERSDR 2004FA0000687Receiver · interferenceWSI WEATHER RECEIVER CAUSES INTERFERENCE WITH COMS ON FREQS. 126.425 AND 126.450. THIS CONDITION MAY EXIST IN OTHER INSTALLATIONS AND SHOULD BE ADDRESSED IN THE MANUFACTURERS INSTALLATION MANUAL. (EA13200405796)SDR 2004FA0000566Control Cable · chafedMIXTURE CONTROL AND ALTERNATOR BATTERY AND CABLE ARE TIED TOGETHER. CONTROL AND CABLE CHAFED INSULATION OFF CABLE AND SHORTED TO MIXTURE CABLE, CAUSING MIXTURE CABLE TO FREEZE UP AT ITS CURRENT SETTING. WHEN TYING WIRES AND CABLE AND LINES OR HOSE TOGETHER USDR NF22004F00000Motor · failedPITCH TRIM MOTOR OUTPUT SHAFT SHEARED OFF ALLOWING TRIM CARTRIDGE AND ARM TO HANG LOOSELY IN THE TAIL POTENTIALLY JAMBING AND RESTRICTING ELEVATOR MOVEMENT.SDR CHQA000443Light · malfunctionedNO POWER LEFT TO EMERGENCY LIGHTS. MECHANIC TESTED LIGHTS IAW EMB-145 MM 33-50-00. FOUND TO BE WORKING OK.SDR CHQA000460Wire · exposedPROXIMITY STRIP HAS EXPOSED WIRES ON CONNECTOR AT261BF. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-50-08-4.SDR CHQA000457Wire · exposedPROXIMITY STRIP HAS EXPOSED WIRES ON CONNECTOR AT261BF. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-50-08-4.SDR CHQA000424Engine · malfunctionedDURING CLIMB OUT OF LGA HIGH ITT WAS NOTED ON NR 2 ENGINE. AT MAX CLIMB THRUST ITT WAS AMBER AND RISING ABOVE 290. WE PULLED POWER BACK 7 PERCENT N1 LOWER THAN NR 1 ENGIN FOR REST OF FLIGHT ITT ON NR 2 ENGINE RAN AT 880-890 DEGREES WHEN N1 WAS PULLED BACK 7 SDR 2003FA0001136Caliper · crackedAIRCRAFT BEGAN TO SHAKE WHILE TAXIING, FELT LIKE SOMEONE WAS TAPPING ON THE RIGHT BRAKE PEDAL. FLANGE AT THE BEAD CRACKED (ABOUT 5 INCHES LONG) AND WAS CATCHING ON BRAKE CALIPER. NO KNOWN HARD LANDINGS. POSSIBLE CAUSE: WHEEL TOO SMALL FOR AIRCRAFT. CORROSSDR 2003FA0000836Pin · shearedCOPILOTS DOOR WOULD NOT OPEN FROM INSIDE. OUTSIDE HANDLE WORKED OK. UPON DISASSEMBLY, THE PIN (CROSS PIN) FOR THE PILOTS WAS FOUND SHEARED. SAFETY HAZARED EVIDENT. REPLACED PIN FROM PN MS16562-224. NO FURTHER MALFUNCTIONS AT THIS TIME.SDR 2003FA0000831Bolt · shearedWHILE PERFORMING A COMPRESSION CHECK ON THE CYLINDER FOR THE 100 HOUR INSPECTION, HAPPENED TO LOOK AT THE CYLINDER BOLTS AND NOTICED ONE OF THE NUTS WAS MISSING ON THE TOP FORWARD THRU BOLT ON THE NR 2 CYLINDER. LOOKED AROUND ON THE BAFFLING AND FOUND THE OTHSDR AUS20030473Trunnion · cracked(AUS) NOSE LANDING GEAR UPPER TRUNNION CRACKED AT DRAG BRACE ATTACHMENT POINT. SUSPECT CAUSED BY EXCEEDING TURNING LIMITS DURING GROUND HANDLING.SDR 2003FA0000377Motor · damagedSHAFTED IN ROLL, TRIM MOTOR ASSEMBLY SHEARED IN FLIGHT, DURING LANDING APPROACH. THE PILOT RETAINED CONTROL AND A SAFE LANDING WAS ACCOMPLISHED. NO FURTHER DAMAGE WAS FOUND DURING INSPECTION OF THE TRIM SYSTEM, AILERON AND LEFT WING. THE CAUSE OF THIS FAILUSDR 2003FA0000292Baffle · brokenDURING VISUAL INSPECTION, FOUND FUEL TANK BAFFLE SPOT WELDS BROKEN LOOSE, ALLOWING BAFFLE TO MOVE AROUND FREELY INSIDE FUEL TANK. THIS CONDITION COULD CAUSE FUEL STARVATION DURING A DECENT WITH A LOW FUEL QUANTITY AND COULD CAUSE ERRONEOUS FUEL QUANTITY INDICASDR 2003FA0000200Bracket · crackedTHE PANT BRACKETS MOVE AND ALLOW THE WHEEL PANT TO MOVE AND CRACK OR COME APART. THE NEW WHEEL PANT BRACKETS COME WITH A BUSHED .2500 INCH HOLE INSTEAD OF THE NR 10 HOLE THAT IS THE SIZE NEEDED FOR THE NR 3 BOLT. WE HAVE BEEN MAKING UP PLASTIC BUSHINGS THAT SDR AUS20021072Filter · missing(AUS) ENGINE SUMP FITTED WITH NO SUCTION FILTER IN THE OIL SYSTEM. APIECE OF LOCKWIRE APPROXIMATELY 15.875MM (0.625IN) LONG WAS FOUND IN AN OIL GALLERY. DAMAGE TO OIL PUMP, CRANKSHAFT REAR BEARINGAND THRUST BEARING SURFACES. ALL PISTON SKIRTS SEVERELY SCORED.SDR AUS20021073Filter · unapproved part(AUS) UNAPPROVED OIL FILTER INSTALLED. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.SDR AUS20020930Hub · unapproved part(AUS) PROPELLER HUB IS A SUSPECT UNAPPROVED PART. INVESTIGATION FOUND THAT THE HUB SERIAL NUMBER IS NOT USED ON THIS TYPE OF AIRCRAFT. HUB FLANGE TYPE ALSO INCORRECT. FURTHER INVESTIGATION FOUND THAT THE ORIGINAL MODEL STAMPINGS HAD BEEN PREVIOUSLY REMOVED.SDR AUS20020931Blade · unapproved part(AUS) PROPELLER BLADE SUSPECT UNAPPROVED PART. INVESTIGATION FOUND THAT THE BLADE HAD ORIGINALLY BEEN AN FC7666A BLADE BUT HAD BEEN ILLEGALLY MODIFIED BY UNKNOWN PARTIES TO AN F7666A BLADE. THE BLADE MANUFACTURER WAS CONTACTED AND CONFIRMED THAT THE BLADE WISDR AUS20020545Injector · contaminated(AUS) REAR ENGINE FUEL INJECTOR NOZZLES (4OFF) CONTAMINATED WITH AN UNKNOWN SUBSTANCE. NO CONTAMINATION WAS FOUND IN THE UPSTREAM FILTER.SDR 2002FA0000525Cable · brokenON FINAL APPROACH, AIRCRAFT EXPERIENCED A SPLIT FLAP CONDITION, CAUSED BY BROKEN CABLE ASSEMBLY. FLAP ACTUATOR INBOARD (PN 14601007). CABLE HAD BROKEN ON RIGHT SIDE, 1 INCH FROM CABLE END, AT BELLCRANK ENTRY POINT. INSPECTION OF LEFT SIDE FLAP CABLE ASSEMBLSDR AUS20020382Control Rod · cracked(AUS) LT AND RT AILERON CONTROL LINKS CRACKED. FOUND IAW AD/M20/52 & MOONEY SB M20-264.SDR AUS20011214Bearing · cracked(AUS) NOSE LANDING GEAR ACTUATOR BEARING CRACKED AND BROKEN.SDR V5MR198Y1Bracket · elongatedNOSE WHEEL PANT BRACKETS, QTY2, FOUND WITH ELONGATED MOUNTING HOLES UNDER NORMAL USE. AIRCRAFT HAS BEEN OPERATED BY A SINGLE INDIVIDUAL WITH MINIMAL TAKEOFFS AND LANDING IN APPROXIMATELY ONE YEARS TIME. FURTHERMORE, THE MOUNTING HOLES IN THE NEW REPLACEMENT SDR V5MR198Y2Bumper Block · deterioratedREBOUND BUMPERS, QTY 2, FOUND VERY DETERIORATED UNDER NORMAL USE. THEY WERE IN SERVICE FOR 344.4 HOURS IN LESS THAN ONE YEAR. THE AIRCRAFT IS OPERATED AS PART OF A CLUB AND SEES MANY TAKEOFF AND LANDING CYCLES. THE DETERIORATION COULD BE DUE TO INTERACTION SDR V5MR198Y3Bracket · elongatedNOSE WHEEL PANT BRACKETS, QTY 2, FOUND WITH ELONGATED MOUNTING HOLES UNDER NORMAL USE. AIRCRAFT HAS BEEN OPERATED AS A CLUB AIRCRAFT WITH MANY TAKEOFFS AND LANDING IN LESS THAN ONE YEARS TIME. FURTHERMORE, THE MOUNING HOLES IN THE NEW REPLACEMENT PART ARE APSDR V5MR198Y5Bumper Block · deterioratedREBOUND BUMPERS, QTY 2, FOUND MISSING SINCE LAST INSPECTION. THEY WERE IN NORMAL SERVICE FOR 223.7 HOURS IN LESS THAN ONE YEAR. AIRCRAFT SEES MINIMAL TAKEOFF AND LANDING CYCLES. THE DETERIORATION AND SUBSEQUENT LOSS OF THE PARTS IN QUESTION COULD BE DUE TO SDR 2001FA0000120Swivel · separatedINSTALLED BALL JOINT OR SWIVEL PN S2999-1 ON MIXTURE CONTROL CABLE FRONT AND REAR ENGINES AT TIME OF ENGINE INSTALLATION. A/C WAS TEST FLOWN AND FERRIED TO PAINT SHOP AND RETURNED. PREVIOUS TO ANY ADDITIONAL ADJUSTMENT AND WHILE IN THE COCKPIT PERFORMING A MSDR 20010501CW020Coupling · slippedAT ENGINE CHANGE, FRESH OVERHAUL ALT INSTALLED AFTER 9.0 HOURS OF OPERATION NOTED ERATIC ALTERNATOR OUTPUT. INSPECTED ALTERNATOR AND DETERMINED ALTERNATOR DRIVE COUPLING SLIPPING. REPLACED ALTERNATOR DRIVE COUPLING WITH OVERHAULED LIKE ITEM AND REINSTALLED SDR 2001FA0000688Pump · failedON 16 MAR O1 BPA RETURNED TO SERVICE (PN IO360, SN 966336A) AFTER SATISFACTORY TEST AFTER OVERHAUL. THE ENGINE WAS SUBSEQUENTLY INSTALLED AT ANOTHER FACILITY. THE MECHANIC NOTIFIED US BY PHONE THAT FUEL WOULD NOT FLOW THRU THE FUEL PUMP EVEN WITH THE USE OF SDR 20001012SH005Bearing · making metalFOUND METAL IN FILTER. SENT SAMPLE OF FILTER TO LYCOMING. THEY SAID IT WAS BEARING MATERIAL AND RECOMMENDED TAKING OUT OF SERVICE. (X)SDR EY2R56619Hub · corrodedEXTERIOR SURFACE OF HUB CORRODED BEYOND LIMITS.
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