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 = '402C' 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 = '402C' 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 HYIA20181003002Rib · crackedDURING MAINTENANCE A CRACK WAS FOUND ON THE RIGHT HAND CLOSE OUT RIB LOCATED AT RIGHT WING STATION 106.79 (P/N: 5122115-56). THIS CRACK STARTS FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT TRUNNION PLATE AND TRAVELS FORWARD APPROXIMATELY .595 ISDR HYIA20181003001Spar Cap · corrodedDURING MAINTENANCE CORROSION DAMAGE WAS FOUND ON THE RIGHT WING AFT LOWER CAP (P/N: 5122041-24). THIS CORROSION IS LOCATED AT APPROXIMATE RIGHT WING STATION 204.71 AND MEASURES APPROXIMATELY .019 DEEP. THIS IS GREATER THAN REMOVABLE LIMITS ALLOWED UNDER MEB95-SDR HYIA20180928001Pushrod · brokenPILOT REPORTED THE LEFT ENGINE RUNNING ROUGH IN FLIGHT AND OIL PRESSURE WENT TO ZERO PSI. PRELIMINARY INSPECTION FOUND METAL CONTAMINATION IN OIL FILTER, #4 CYLINDER INTAKE PUSH ROD BROKEN AND A LARGE GAP AT THE EXHAUST ROCKER ARM. THE ENGINE IS BEING REPLACEDSDR HYIA20180927001Indicator · failedPILOT REPORTED "RIGHT LANDING GEAR LIGHT BURNT OUT. REPLACED WITH BULB AND WHEN REPLACED, 3 GREEN APPEARED BUT THEN SPARKED AND WENT OUT." MAINTENANCE INSPECTED AND DETERMINE THE LANDING GEAR INDICATOR BLOCK TO BE AT FAULT. THE LANDING GEAR INDICATOR BLOCK WASSDR HYIA20180926001Engine · making metalPILOT REPORTED RIGHT ENGINE OIL PRESSURE DROPPED TO 20 PSI IN FLIGHT AND TO ZERO PSI AT IDLE ON THE GROUND. MAINTENANCE INSPECTED AND FOUND METAL PARTICLES AT THE OIL PRESSURE RELIEF VALVE, FURTHER INSPECTION FOUND THE STARTER ADAPTER NEEDLE BEARING DAMAGED. TSDR HYIA20180914001Beam · crackedDURING NDT TESTING DONE TO SATISFY AD 2015-07-03, A CRACK WAS DISCOVERED ON THE LEFT NACELLE INBOARD ENGINE BEAM P/N: 5654109-6. THIS CRACK IS TRAVELING LEFT TO RIGHT ACROSS THE TOP OF THE BEAM ORIGINATING FROM A FASTENER HOLE ON THE TOP OF THE BEAM TRAVELLINGSDR HYIA20180906001Door Frame · corrodedWHILE CONDUCTING OTHER MAINTENANCE, AN AREA OF CORROSION WAS NOTED ON THE FUSELAGE FRAME ASSEMBLY AT FS 214.00, JUST ABOVE THE 501110-12 STRIKER PLATE FOR THE LOWER PASSENGER DOOR PIN. THE 501110-12 STRIKER PLATE WAS REMOVED FOR FURTHER INSPECTION. UPON REMOVASDR HYIA20180827002Fitting · corrodedDURING MAINTENANCE, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE RIGHT NACELLE OUTBOARD FITTING, AROUND THE FASTENER HOLES OF THE TOP FORWARD FACE OF THE FITTING, JUST FORWARD OF THE FIREWALL. THE DEPTH OF THIS CORROSION IS .019 IN. THE FITTING WAS REPLACESDR HYIA20180827001Crossbeam · chafedDURING MAINTENANCE, CHAFING DAMAGE WAS FOUND ON THE RIGHT NACELLE CROSSOVER BEAM.SDR HYIA20180831001Oil System · low pressurePILOT REPORTED IN CRUISE, BOTH ENGINES LOST OIL PRESSURE AND STARTED TO RUN ROUGH. NO LEAKS WERE NOTED, BUT LOW OIL LEVELS WERE NOTED ON BOTH SIDES OIL DIPSTICKS. ENGINES ARE BEING REPLACED.SDR HYIA20180823002Strap · corrodedDURING MAINTNENANCE, CORROSION WAS FOUND ON THE LEFT WING SPAR STRAP, LT WS 136.54. THE DIMENSIONS FOR THIS CORROSION ARE: 1.320 INCHES LONG, .884 INCHES WIDE, AND .050 INCHES DEEP. REPLACED THE SPAR STRAP.SDR HYIA20180823001Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS FOUND ON THE RIGHT REAR LOWER SPAR CAP, AT RT WS. 215.71. THE DIMENSIONS FOR THIS CORROSION ARE .391 INCHES LONG, .375 INCHES WIDE, AND .020 INCHES DEEP. THIS IS GREATER THAN REMOVEABLE LIMITS ALLOWED UNDER MEB95-11R1 SEC. 3. SDR HYIA20180823003Engine · making metalPILOT REPORTED THE LEFT ENGINE OIL PRESSURE DROPPED TO BOTTOM OF GREEN ARC DURING CRUISE. MAINTENANCE INSPECTED AND FOUND METAL PARTICLES IN OIL SYSTEM. THE ENGINE HAS BEEN REPLACED.SDR HYIA20180815001Angle · corrodedCORROSION WAS DISCOVERED ON ONE OF THE LEFT SIDE VERTICAL STABILIZER AFT ANGLES. REMOVED AND REPLACED THE ANGLE.SDR HYIA20180813001Engine · surgesPILOT REPORTED THE ENGINE SURGED TO A POINT OF UNCONTROLLABLE AFTER TAKE-OFF. THE ENGINE WAS INTENTIONALLY SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE ISSUE. OPENSDR HYIA20180803002Engine · making metalPILOT REPORTED LT ENGINE HAD PARTIAL POWER, THEN NOTICED OIL COMING FORM COWLING UNDER THE TURBO. MAINTENANCE INSPECTED AND FOUND METAL CONTAMINATION IN ENGINE OIL FILTER AND THE #5 CYLINDER SHOWING SIGNS OF
PRE-IGNITION. THE ENGINE IS TO BE REPLACED.SDR HYIA20180803001Cylinder · damagedPILOT REPORTED THE LEFT ENGINE STARTED TO RUN ROUGH DURING FLIGHT AND THE OIL PRESSURE SLOWLY DROPPED. AFTER LANDING, THE CREW REPORTED OIL DRIPPING OFF THE COWL. MAINTENANCE INSPECTED AND FOUND METAL CONTAMINATION IN ENGINE OIL SYSTEM AND THE NR 5 CYLINDER SDR HYIA20180717002Frame · corrodedWHILE CONDUCTION OTHER MAINTENANCE, AN AREA OF CORROSION WAS NOTED ON THE FUSELAGE FRAME ASSEMBLY AT FS 214.00, JUST ABOVE THE 501110-12 STRIKER PLATE FOR THE LOWER PASSENGER DOOR PIN. THE 501110-12 STRIKER PLATE WAS REMOVED FOR FURTHER INSPECTION. UPON REMOSDR HYIA20180717001Spar Cap · corrodedWHILE CONDUCTING OTHER MAINTENANCE, CORROSION WAS NOTED ON THE HORIZONTAL LEG OF THE LOWER LEFT AFT OUTBOARD SPAR CAP, AT WS 222.46. THE CORROSION AREA MEASURED .218 BY .086. THE DEPTH OF THE CORROSION MEASURED AT .022, WHICH IS DEEPER THAN THE ALLOWABLE REMSDR HYIA201808031001Dimmer · failedDURING CLIMB OUT, THE CAPTAIN'S FLIGHT INSTRUMENT ILLUMINATION FAILED. SHORTLY AFTER, SMELLED A BURNING ELECTRICAL AND LIGHT SMOKE. MAINTENANCE INSPECTED AND FOUND THE INSTRUMENT LIGHT DIMMER ASSEMBLY AT FAULT. REPLACED THE DIMMER AND TRANSISTOR Q4 WITH NO FUSDR HYIA20180712001Switch · burnedPILOT REPORTED, WHEN NAV SWITCH ACTUATED SMOKE CAME OUT OF SWITCH WHILE MASTER SWITCH ON. INSPECTION FOUND THE NAV LIGHT SWITCH BURNT. MAINTENANCE REPAIRED WIRING IN LEFT WING TIP AND REPLACED NAV LIGHT SWITCH WITH NO FURTHER DEFECTS NOTED.SDR HYIA20180627001Strap · corrodedWHILE CONDUCTING A VISUAL INSPECTION, CORROSION WAS NOTED ON THE LEFT SPAR STRAP. ONE AREA OF CORROSION WAS FOUND AT LWS 127.04 TO 129.04 AT THE AFT ROW OF FASTENERS. CORROSION MEASURED .50 IN WIDTH AT IT'S WIDEST POINT. A SMALL PORTION OF THIS AREA WAS BLESDR HYIA20180613001Cylinder · separatedDURING POWER REDUCTION AT 20" LEFT ENGINE STARTED TO SHUTTER AND VIBRATE MAP INDICATION FLUCTUATED BETWEEN 20 AND 24" INCHES. ENGINE WAS NEVER SHUT DOWN AIRCRAFT WAS ON SHORT FINAL AND LANDED WITHOUT ISSUE. POSTFLIGHT INSPECTION REVEALED THE HEAD PORTION OF TSDR HYIA20180605001Spar Cap · corrodedCORROSION WAS DISCOVERED ON THE LT AFT LOWER OUTBOARD SPAR CAP WS 221.71 ON THE FORWARD SIDE OF THE CAP, INSIDE THE FUEL TANK, NEAR THE RADIUS. THE CORRODED AREA MEASURED .075 TALL, .243 IN WIDTH, AND .063 IN DEPTH. OUT OF LIMITS IAW MEB 95-11, R1, SECTION 3SDR HYIA20180525001Axle · crackedDURING TAXI FOR DEPARTURE, THE CREW REPORTED THE AIRCRAFT PULLED TO THE RIGHT AS IF THE TIRE HAD GONE FLAT. THE AIRCRAFT BECAME DISABLED ON THE TAXIWAY. THE RT AXLE ASSEMBLY HAD FAILED CAUSING THE WHEEL ASSEMBLY TO RUB AGAINST THE RT LANDING GEAR STRUT. UPSDR HYIA20180430001Exhaust Valve · brokenPILOT REPORTED IN CLIMB POWER, AIRCRAFT YAWED AND SEVERE ENGINE VIBRATION ENSUED. UPON INSPECTION MAINTENANCE FOUND THE CYLINDER TO HAVE ZERO COMPRESSION AND THE EXHAUST VALVE BROKEN AT THE STEM. THE CYLINDER WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20180427002Channel · corrodedWHILE PERFORMING A BORE SCOPE VISUAL INSPECTION OF THE THE NACELLE FITTINGS IAW AD2017-10-19, CORROSION WAS NOTED ON THE RT OUTBOARD NACELLE FITTING. DISASSEMBLE THE STACK UP AT THE BACK OF THE ENGINE BEAM CAP AND DOUBLERS, FOR FURTHER INSPECTION. NOTED THSDR HYIA20180427001Fitting · corrodedWHILE PERFORMING A BORE SCOPE VISUAL INSPECTION OF THE THE NACELLE FITTINGS IAW AD2017-10-19, CORROSION WAS NOTED ON THE RT OUTBOARD NACELLE FITTING. DISASSEMBLE THE STACK UP AT THE BACK OF THE ENGINE BEAM CAP AND DOUBLERS, FOR FURTHER INSPECTION. NOTED THSDR HYIA20180403001Crossbeam · crackedA CRACK WAS DISCOVERED IN THE CROSSBEAM ON THE AFT LEFT SIDE, AROUND ONE OF THE TURBO BRACKET MOUNTING HOLES. THE CRACK MEASURED 1.304 INCHES IN LENGTH. THE TURBO BRACKET WAS INSTALLED TO CHECK FOR PRELOADING. NO PRELOADING WAS NOTED. BEAM WAS REPLACED.SDR HYIA20180404001Cylinder · damagedPILOT REPORTED LEFT ENGINE VIBRATION DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE NR 3 CYLINDER WITH A COLLAPSED EXHAUST LIFTER, BROKEN VALVE GUIDE AND THE PISTON PIN BUSHING DAMAGED AND CRACKED. THE CYLINDER AND CONNECTING ROD HAS BEEN CHASDR HYIA20180316001Fitting · crackedWHILE PREPPING FOR A SID 57-10-16 INSPECTION OF THE SPAR STRAP AND NACELLE FITTINGS, A CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE RIGHT OUTBOARD FITTING, JUST FORWARD OF THE SPAR STRAP.SDR HYIA20180316002Control Cable · brokenPILOT REPORTED THE LEFT RUDDER DOES NOT MOVE, A SNAP WAS HEARD WHEN MAKING A LEFT TURN. MAINTENANCE INSPECTED AND FOUND THE FORWARD LEFT RUDDER CABLE BROKEN NEAR THE FORWARD PULLEY. LAST VISUAL INSPECTION OF AREA OCCURRED 134.8 HOURS PRIOR TO FAILURE. CABLE SDR HYIA20180314002Heater · odorPILOT REPORTED SMOKE SMELL IN COCKPIT. TURNED HEATER OFF AND SMELL STOPPED. MAINTENANCE INSPECTED AND AFTER TROUBLESHOOTING DETERMINED THE HEATER ASSEMBLY WAS TO BE REPLACED. REPLACED HEATER WITH NO FURTHER DEFECTS NOTED.SDR HYIA20180314001Blower · seizedPILOT REPORTED, HEATER GIVES A MELTING PLASTIC SMELL IN FLIGHT. MAINTENANCE INSPECTED AND FOUND THE HEATER COMBUSTION BLOWER HAD SEIZED, THE BLOWER WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20180220001Piston · damagedPILOT REPORTED AN EXCESSIVE AIR FRAME VIBRATION ASSOCIATED WITH PROP RPM. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE NR 6 CYLINDER PISTON HEAD TO BE DAMAGED, AND FOREIGN MATTER ON THE CYLINDER UPPER SPARK PLUG. THE DAMAGE TO THE PISTON APPEARED TO BE CSDR HYIA20180215002Beam · crackedWHILE PERFORMING OTHER MAINTENANCE, A CRACK WAS DISCOVERED IN THE RT CANTED BEAM ASSEMBLY (CROSSOVER BEAM) ON THE AFT RIGHT HAND SIDE, AROUND ONE OF THE TURBO BRACKET MOUNTING HOLES. IT APPEARS THE CRACK WAS CAUSED BY PRE-LOADING OF THE TURBO BRACKET. BEAM ASSDR HYIA20180215001Switch · failedPILOT REPORTED CABIN HEATER CIRCUIT BREAKER TRIPPED AND A STRONG ODOR IN THE CABIN. DURING INSPECTION THE HEATER OVERHEAT SWITCH WAS FOUND TO BE DAMAGED AND BURNED.SDR HYIA20180202001Bearing · fragmentedPILOT REPORTED THE LEFT ENGINE HAD LOW OIL PRESSURE, BELOW GREEN ARC AT 1700 RPM. DEBRIS WAS FOUND IN THE OIL FILTER, FURTHER INSPECTION DISCOVERED THE STARTER ADAPTER SHAFT NEEDLE BEARING TO BE SEVERELY DAMAGED. THE ENGINE WAS REPLACED.SDR HYIA20180110001Attach Fitting · crackedWHILE PREFORMING OTHER MAINTENANCE IN THE IMMEDIATE AREA, A CRACK WAS NOTED LENGTH WISE ALONG THE RADIUS OF THE FORWARD LOWER, OUTBOARD AFT SIDE WING FITTING (SEE ATTACHMENT FOR PICTURES AND DIMENSIONS.) A .065 THICK SHIM WAS INSTALLED BETWEEN THE LOWER HORIZOSDR HYIA2017010500001Engine · shutdownPILOT REPORTED THE RIGHT ENGINE SHUTDOWN IN FLIGHT. OPENSDR HYIA20171226001Cylinder · failedPILOT REPORTED RIGHT ENGINE RUNNING ROUGH. UPON INSPECTION FOUND THE RIGHT ENGINE NR 3 CYLINDER TO HAVE LOW COMPRESSION AND THE CYLINDER EXHAUST VALVE TO HAVE EVIDENCE OF A BURNING. THE CYLINDER WAS REPLACED.SDR HYIA20171227001Torque Tube · crackedDURING A SCHEDULED INSPECTION, THE RT RUDDER PEDAL TORQUE TUBE WAS CRACKED AND FAILED AT THE WELD INTERSECTION OF THE RT PEDAL 'POST'. THIS FINDING IS A RESULT OF A RECENTLY IMPLEMENTED MAGNIFIED VISUAL INSPECTION OF THESE WELDS AT EACH 180 FLIGHT HOURS OF OPSDR HYIA20171222001Indicator · failedDURING FLIGHT THE PILOT REPORTED THE WEATHER RADAR SHUT OFF BY ITSELF ACCOMPANIED BY A BURNED PLASTIC ODOR IN THE COCKPIT FOR A SHORT TIME. THE COMPONENT WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20171213001Fitting · crackedTHE RT OB NACELLE FITTING PART NUMBER 5292029-24 WAS FOUND TO BE CRACKED DURING BORESCOPE INSPECTION PRESCRIBED BY TEXTRON MULTI-ENGINE SERVICE LETTER MEL-54-02R2 DATED MARCH 29, 2017 AS CONTINUING ACTION REQUIRED BY AD2017-10-09. THE CRACK IS FAINT BUT VSDR HYIA20171205001Bulkhead · crackedAFTER DEPARTURE AND CLIMBING THROUGH 800 FT MSL THE AIRCRAFT FLEW THROUGH A FLOCK OF BIRDS. BOTH WINDSHIELDS WERE DAMAGED AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING. SUBSEQUENT INSPECTION FOUND THE FUSELAGE BULKHEAD AT STATION 14.25 (OEM PN 5213025-21) IS SSDR HYIA20171201001Socket · deterioratedDURING DESCENT FOR LANDING AT SCHEDULED DESTINATION, THE LWR PANEL LIGHT RHEOSTAT WAS ACTUATED. AFTER 2-3 SECONDS A STRONG ELECTRICAL ODOR WAS NOTED. THE PANEL LIGHTS WERE EXTINGUISHED AND THE ODOR RECEEDED. NO EMERGENCY WAS DECLARED AND THE LANDING WAS UNSDR HYIA20171121001Exhaust Valve · brokenPILOT REPORTED RIGHT ENGINE VIBRATING ON FINAL APPROACH AND TAXI. MAINTENANCE INSPECTED AND FOUND NO COMPRESSION ON THE RIGHT ENGINE NR 4 CYLINDER. UPON REMOVAL DISCOVERED THE EXHAUST VALVE HAD CRACKED AND BROKEN. THE CYLINDER WAS REPLACED WITH NO FURTHER DEFESDR HYIA20171117001Torque Tube · failedWHILE IN CRUISE, THE RT RUDDER PEDAL WENT TO THE FLOOR, FULL FORWARD. THE PILOT DID NOT HAVE ANY RUDDER AUTHORITY, BUT THE AIRCRAFT REMAINED IN STRAIGHT AND LEVEL FLIGHT. DIVERTED AND LANDED SAFELY WITH NO ISSUES. THE AIRCRAFT WAS UNABLE TO TAXI FROM THE RUSDR HYIA20171113001Cylinder · damagedAT CRUISE POWER SETTING, CREW REPORTED A ROUGH RUNNING RT ENGINE ALONG WITH A CONTINUOUS MODERATE VIBRATION THROUGHOUT RANGE OF POWER SETTINGS. THE FLIGHT DIVERTED AND LANDED SAFELY. INSPECTION REVEALED THE NR 6 CYLINDER AND PISTON ASSEMBLY WERE SEVERELY DASDR HYIA20171109001Fitting · corrodedDURING A ROUTINE VISUAL INSPECTION OF THE WING ATTACH FITTINGS, CORROSION WAS DISCOVERED ON THE LEFT OUTBOARD FORWARD, AFT SIDE WING ATTACH FITTING. THE FITTING WAS REMOVED AND REPLACED WITH FACTORY NEW PARTS.
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