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 HYIA20240718003Axle · crackedDURING SCHEDULED NDT INSPECTION A CRACK WAS FOUND ON THE LEFT MAIN LANDING GEAR AXLE. THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20240718002Axle · brokenDURING TAXI OUT THE PILOT REPORTED THE LEFT MAIN LANDING GEAR AXLE BROKE. MAINTENANCE INSPECTED AND CONFIRMED THE AXLE WAS BROKEN, THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER ISSUES.SDR HYIA20240828001Fitting · crackedWHILE PERFORMING THE LIGHTED BORESCOPE PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02 R2 TO SATISFY AD2017-10-19, A CRACK WAS IDENTIFIED ON THE OUTBOARD SIDE OF THE LEFT-HAND OUTBOARD FITTING. THIS CRACK MEASURES .152 IN LENGTH AND IS CONSISTENT WITH OTHERS FOUNDSDR HYIA20240718001Trunnion · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT MAIN GEAR TRUNNION BARREL ABOVE THE ACTUATOR ATTACH POINT. UNIT WAS REPLACED WITH NO FURTHER DEFECTS.SDR HYIA20240711002Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB (P/N: 5122115-55) AT L.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS VERTICALLY TO ASDR HYIA20240711001Rib · crackedDURING MAINTENANCE THREE CRACKS WERE VISUALLY IDENTIFIED ON THE RIGHT HAND CLOSEOUT RIB (OEM P/N: 5122115-56). ALL CRACKS ARE LOCATED IN THE AREA OF FASTENERS COMMON TO THE FORWARD TRUNNION SUPPORT. THESE CRACKS ARE CONSISTENT WITH OTHERS THAT HAVE BEEN FOUND SDR HYIA20240607001Fitting · crackedDURING SCHEDULED NONDESTRUCTIVE TESTING AS NOTED IN CESSNA SUPPLEMENTAL INSPECTION DOCUMENT (SID) 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND OUTBOARD NACELLE FITTING (OEM P/N: 5292029-31) THIS CRACK MEASURES APPROXIMATELY .104 INCHES LONG ON THE LOWER OSDR HYIA20240524003Nut · excess playUPON REMOVAL OF AN ALTERNATOR FOR AN INTERNAL OIL LEAK, THE HUB NUT WAS FOUND TO BE LOOSE, ALLOWING THE THRUST WASHER TO ROTATE BY HAND. THE COTTER PIN REMAINED IN PLACE. THE UNIT WAS REMOVED FROM SERVICE PENDING FURTHER INVESTIGATION.SDR HYIA20240524002Nut · excess playUPON REMOVAL OF AN ALTERNATOR, THE HUB NUT WAS FOUND TO BE LOOSE, ALLOWING THE THRUST WASHER TO ROTATE BY HAND. THE COTTER PIN REMAINED IN PLACE. THE UNIT WAS REMOVED FROM SERVICE PENDING FURTHER INVESTIGATION.SDR HYIA20240521001Crossbeam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND CROSSOVER BEAM (OEM P/N: 5654104-12) OF N678JG. THIS CRACK IS LOCATED ON THE AFT FACE OF THE BEAM, COMMON TO THE TOP OUTBOARD BOLT HOLE FOR THE TURBOCHARGER SUPPORT BRACKET. THIS CRACK MEASURSDR HYIA20240514001Hub · excess playUPON REMOVAL OF AN ALTERNATOR, THE HUB NUT WAS FOUND TO BE LOOSE, ALLOWING THE THRUST WASHER TO ROTATE BY HAND. THE COTTER PIN REMAINED IN PLACE. THE UNIT WAS REMOVED FROM SERVICE PENDING FURTHER INVESTIGATION.SDR HYIA20240429001Attach Fitting · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE RIGHT HAND LOWER FUSELAGE ATTACH FITTING (P/N: 0811350-12). THIS CORROSION MEASURES APPROXIMATELY .313 INCHES TALL, .353 WIDE, AND HAS A MAXIMUM DEPTH OF .016. IT IS LOCATED ON THE FORWARD SDR HYIA20240426001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE OUTBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .100 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXSDR HYIA20230425001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE OUTBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .250 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXSDR HYIA20240718006Axle · crackedDURING SCHEDULED NDT INSPECTION A CRACK WAS FOUND ON THE LEFT MAIN LANDING GEAR AXLE. THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20240405001Chain · brokenPILOT REPORTED SLAPS WILL NOT RETRACT AFTER LANDING, AND EXPERIENCED A SPLIT FLAP ON FINAL. MAINTENANCE INSPECTED AND FOUND THE RIGHT FLAP CABLE CHAIN AT GEARBOX SNAPPED. THE CHAIN, CABLE & GEARBOX ARE BEING REPLACED.SDR HYIA20240321002Alternator · failedPILOT REPORTED RIGHT ALTERNATOR INOPERATIVE. MAINTENANCE INSPECTED AND FOUND THE ALTERNATOR HUB NUT MISSING, FLY WHEEL BOLTS MISSING AND DAMAGE TO THE FLY WHEEL. THE ENGINE IS BEING REPLACED DUE TO METAL CONTAMINATION.SDR HYIA20240221001Engine · failedON APPROACH PILOT NOTICED A SUDDEN "BANG" ACCOMPANIED BY SLIGHT POWER & RPM LOSS ON THE LEFT ENGINE. SMOKE AND OIL BEGAN COMING FROM LEFT ENGINE. OIL PRESSURE DROPPED AND PILOT SECURED THE ENGINE PER COMPANY PROCEDURES. INITIAL INSPECTION FOUND THE NUMBER 6 CYSDR HYIA20240221002Pump · leakingPILOT REPORTED STRONG SMELL OF FUEL IN THE CABIN WITH THE HEATER ON. MAINTENANCE INSPECTED AND FOUND THE HEATER FUEL PUMP TO BE LEAKING. THE PUMP WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20240131001Fitting · crackedWHILE PERFORMING THE LIGHTED BORESCOPE PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02 R2 TO SATISFY AS2017-10-19, A CRACK WAS IDENTIFIED ON THE OUTBOARD SIDE OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES .0799 IN LENGTH AND ITS LOCATION IS CONSISDR HYIA20231219001Spar Cap · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE RH AFT LOWER OUTBOARD SPAR CAP, OEM P/N: 5122041-24. THIS CORROSION IS LOCATED ON THE FORWARD FACE OF THE VERTICAL LEG AT APPROXIMATE RWS 229.71. THIS CORROSION MEASURES APPROXIMATELY .020 SDR HYIA20240321001Alternator · failedPILOT REPORTED RIGHT ALTERNATOR OUT LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND FOUND ALTERNATOR HUB NUT MISSING AND METAL CONTAMINATION IN THE ENGINE. THE ENGINE WAS REPLACED.SDR 2023FA0000765Unknown · unknownAFTER DEPARTURE RETRACTED THE MLG AND CONFIRMED THE GEAR WAS UP WHEN THE UNLOCK LIGHT EXTINGUISHED AND 3 GREEN MLG DOWN LIGHTS WERE ALSO EXTINGUISHED. NOTICED THAT THE AIRSPEED WAS SLOWER THAN NORMAL & CLIMB RATE WAS SLOWER THAN NORMAL. ALONG WITH SLOWER SPEESDR HYIA20231031001Throttle Body · backed outPILOT REPORTED LEFT THROTTLE STUCK AT APPROXIMATELY 34 INCHES MP WHEN REDUCING FROM TAKE OFF POWER TO CLIMB POWER. MAINTENANCE INSPECTED AND FOUND THE LEFT THROTTLE BODY LEVER PIN HAD BACKED OUT AND WAS CONTACTING THE IDLE STOP. THE PIN WAS REPLACED AND NO FURSDR HYIA20231031002Gps · failedPILOT REPORTED THE GARMIN 430 STOPPED WORKING, SCREEN WENT BLANK AND NOTED ELECTRICAL BURNING SMELL. MAINTENANCE REPLACED THE GPS 430W UNIT IN ACCORDANCE WITH GARMIN 430W INSTALLATION MANUAL WITH NO FURTHER DEFECTS NOTED.SDR HYIA20231027002Display · failedPILOT REPORTED WEATHER RADAR WOULD NOT TURN ON AND HAD ELECTRIC BURNING SMELL IN FLIGHT. MAINTENANCE INSPECTED AND FOUND RADAR DISPLAY BURNED SMELL DURING INSPECTION. REMOVED AND REPLACED RADAR DISPLAY AND ANTENNA.SDR HYIA20231006002Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB (P/N: 5122115-55) AT L.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS FORWARD AN APPRSDR HYIA20231006001Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT R.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS FORWARD AN APPSDR HYIA20230901001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND CROSSOVER BEAM (OEM P/N: 5654104-12) OF N401SX (402C0447). THIS CRACK IS LOCATED ON THE AFT FACE OF THE BEAM, COMMON TO THE TOP OUTBOARD BOLT HOLE FOR THE TURBOCHARGER SUPPORT BRACKET. THIS CSDR HYIA20230724001Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE AFT FACE OF THE FWD RH UPPER FUSELAGE ATTACH FITTING PN: 0811350-9. THIS CORROSION MEASURES .275 WIDE, AND .226 TALL, WITH AN APPROXIMATE DEPTH OF .018 AND IS CONSISTENT WITH OTHER CORROSIONSDR HYIA20230707001Fitting · crackedWHILE PERFORMING LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R3 TO SATISFY AD2017-10-09, A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD VERTICAL LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY .138 INSDR HYIA20230525001Fitting · crackedDURING SCHEDULED NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS NOTED ON THE RIGHT HAND INBOARD NACELLE FITTING P/N: 5292029-30. THE CRACK MEASURES .125 INCHES LONG AND IS CONSISTENT WITH OTHERS FOUND USING THE LIGHTED BORESCOPE INSPECTION TECHNIQUE (TEXSDR HYIA20230526001Trunnion · failedPILOT REPORTED RIGHT MAIN LANDING GEAR CAME OUT OF THE AIRCRAFT AFTER LANDING. INITIAL INSPECTION FOUND THE RIGHT MAIN LANDING GEAR TRUNNION FAILED. AIRCRAFT IS UNDER REPAIR.SDR HYIA20230501001Intake Valve · damagedPILOT REPORTED RIGHT ENGINE NTO PRIMARY/SECONDARY LIGHTS ILLUMINATED DURING CRUISE AND NOTED A CONTINUOUS POP/SURGE SOUND FROM THE ENGINE. THE ENGINE DIED WHEN POWER WAS BROUGHT NEAR IDLE. INITIAL INSPECTION FOUND THE # CYLINDER INTAKE VALVE HEAD MISSING. ADDISDR HYIA20230421001Unknown · unknownPILOT REPORTED BURNING SMELL FROM CABIN HEATER IN CRUISE, WHICH STOPPED WITH HEATER WAS TURNED OFF. MAINTENANCE IS INSPECTING AND WILL ADDRESS THE ISSUE PRIOR TO NEXT FLIGHT.SDR HYIA20230413001Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT R.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS FORWARD AN APPSDR HYIA20230410001Blower · failedPILOT REPORTED ELECTRICAL BURNING SMELL FROM HEATER. MAINTENANCE INSPECTED AND DETERMINED THE HEATER BLOWER FAN TO BE INOPERATIVE. THE BLOWER WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20230321001Fitting · crackedDURING SCHEDULED NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS NOTED ON THE LEFT HAND INBOARD NACELLE FITTING P/N: 5292029-21. THE CRACK MEASURES .125 INCHES LONG AND IS CONSISTENT WITH OTHERS FOUND USING THE LIGHTED BORESCOPE INSPECTION TECHNIQUE (TEXTSDR 2023F00185Line · blew outLINE ASSY, GEAR RETRACTION HOSE P/N 58 0108-1 HAD ITS FLAIR SPLIT UPON INITIAL GEAR RETRACTION DEPOSITING ALL HYDRAULIC FLUID OVERBOARD. NOSE GEAR RETRACTED BUT THE MAIN LANDING GEAR REMAINED IN THE DOWN POSITION. AFTER COMPANY WAS CALLED AND ADVISED OF THE SISDR 2023F00092Line · blew outLINE ASSY GEAR RETRACTION HOSE PN 58 0108-1 HAD ITS FLAIR SPLIT UPON INITIAL GEAR RETRACTION ALLOWING THE DEPLETION OF ALL HYDRAULIC FLUID. AIRCRAFT EMERGENCY PROCEDURE WAS USED TO BLOW DOWN THE GEAR AND RETURN FOR REPAIRS.SDR 2023F00088Line · blew outLINE ASSY GEAR RETRACTION HOSE P/N 58 0108-1 HAD ITS FLAIR SPLIT UPON INITIAL GEAR RETRACTION DEPOSITING ALL HYDRAULIC FLUID OVERBOARD. NOSE GEAR RETRACTED BUT THE MAIN LANDING GEAR REMAINED IN THE DOWN POSITION. AFTER COMPANY WAS CALLED AND ADVISED OF THE SITSDR KW7R2023011228002Clevis Bolt · wornDURING SCHEDULED INSPECTION OF RUDDER PEDAL TORQUE TUBE AND ATTACHING ARMS PER CESSNA INSPECTION OPERATION 73 USING SUPPLEMENTAL INSPECTION NUMBER 27-20-05 INSPECTION PROCEDURES: UPON REMOVAL OF THE RUDDER PEDAL ASSEMBLY, THE CLEVIS BOLTS (ITEM #90 IN IPC) SECSDR HYIA20230210001Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT R.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS FORWARD AN APPSDR HYIA20230124001Indicator · failedPILOT REPORTED BURNING/ELECTRICAL SMELL IN THE CABIN IN FLIGHT. MAINTENANCE INSPECTED AND FOUND THE WEATHER RADAR TO HAVE AN ELECTRICAL SMELL IN STANDBY MODE. MAINTENANCE REPLACED THE RADAR INDICATOR AND ANTENNA WITH NO FURTHER DEFECTS NOTED.SDR HYIA20230113001Fitting · damagedDURING MAINTENANCE, A SPOT OF DAMAGE WAS VISUALLY IDENTIFIED ON THE RH FWD WING ATTACH FITTING (PN: 082550-46). THIS DAMAGE IS LOCATED ON THE TOP EDGE OF THE FITTING AS SEEN THROUGH THE WING GAP PANEL 611AT INBOARD OF RWS 58.94. THIS DAMAGE MEASURES APPROXIMASDR HYIA20230124002Blower Motor · failedPILOT REPORTED BURNING SMELL IN CABIN, THEY TURNED THE HEATER OFF AND SMELL DISSIPATED. MAINTENANCE INSPECTED AND FOUND THE COMBUSTION BLOWER INOPERATIVE. MAINTENANCE REPLACED THE COMBUSTION BLOWER WITH NO FURTHER DEFECTS NOTED.SDR HYIA20221215001Circuit Breaker · failedPILOT REPORTED SMOKE OBSERVED FROM SIDE PANEL. MAINTENANCE INSPECTED ANTI-COLLISION CIRCUIT BREAKER SWITCH AND WIRING, FOUND SWITCH INOP AND WIRE INSULATION BURNT ON LOAD SIDE OF SWITCH. REPAIRED DAMAGED ANTI-COLLISION LIGHT SWITCH WIRE IAW 402C WDM CHAPTER 20SDR HYIA20221205001Fitting · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE TOP EDGE OF THE VERTICAL LEG OF THE FORWARD LEFT HAND LOWER AFT WING FITTING. CORROSION MEASURES APPROXIMATELY 1.25 INCHES LONG, WITH A MAX DEPTH OF APPROXIMATELY .017 INCHES DEEP AND IS CSDR HYIA20221128001Spar Cap · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RH UPPER FWD SPAR CAP PN: 5122031-6. THIS CRACK IS LOCATED NEAR THE FORWARD RADIUS OF THE SPAR CAP AT APPROXIMATE RWS 70.94. THIS CRACK WAS CONFIRMED BY SURFACE EDDY CURRENT, MEASURES APPROXIMATELY 1 INSDR HYIA20221114002Crossbeam · crackedDURING MAINTENANCE ON N223PB, A MULTIPLE CRACKS WERE VISUALLY IDENTIFIED ON THE RH NACELLE CROSSOVER BEAM (P/N: 5654104-2). ONE CRACK ON THE FRONT FACE OF THE BEAM AT APPROXIMATE RWS 87.44 WITH AN APPROXIMATE LENGTH OF 3.780 INCHES. A SECOND CRACK WAS IDENTIFI
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