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 = '95B55' 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 = '95B55' 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 2025FA0000751Wire · shortedWE TURNED THE BATTERY MASTER ON TO TEST A LANDING LIGHT THAT WAS REPORTED TO BE OUT. AFTER ABOUT ONE MINUTE OF THE BATTERY MASTER BEING ON, LARGE AMOUNTS OF SMOKE CAME FROM THE LEFT ENGINE. TROUBLESHOOTING FOUND THAT THE ALTERNATOR OUTPUT WIRE WAS SHIELDED ANDSDR 2022FA0000276Vacuum Sys · failedTWO VACUUM PUMPS WERE INSTALLED AT ENGINE CHANGE. THEY BOTH FAILED IN UNDER 25 HOURS. BOTH INTERNAL FAILURES. SHEARING THE DRIVE COUPLING. BOTH PURCHASED FROM MAFARLANE AVIATION ON 2/8/22. INVOICE 0453567IN.SDR 2022FA0000275Vacuum Sys · failedTWO VACUUM PUMPS WERE INSTALLED AT ENGINE CHANGE THEY BOTH FAILED AT 25 HOURS PUMPS WERE PURCHASED FROM MCFARLAND AVIATION ON 2/8/22 MCFARLAND INVOICE 0453567-INSDR 2022FA0000244Filter Adapter · failedOIL FILTER ADAPTER IS AN F&M ENTERPRISES ADAPTER INSTALLED UNDER AN STC. IT IS AFFECTED BY A STRATUS MANDATORY SERVICE BULLETIN NO. SB-001, REV B AND AN AIRWORTHINESS DIRECTIVE AD22-04-04. A FIBER GASKET WAS INSTALLED BETWEEN THE ADAPTER NUT AND OIL PUMP BODY.SDR 2021FA0000115Line · leakingCUSTOMER REPORTED SMELLING PAINT THINNER WHILE TAXYING BY AN AIRCRAFT PAINTING CENTER. THOUGHT NOTHING OF IT AND MADE 2 HR FLIGHT. AFTER LANDING AND DURING TAXI THE ODOR WAS ONCE AGAIN NOTED RAISING SUSPICION. AIRCRAFT USES A FUEL PRESSURE GAGE CALIBRATED IN GSDR CA190731020Fuel Control · malfunctioned(CAN) RH ENGINE WAS SURGING ON TAKE OFF. PILOT ABORTED TAKE OFF AND MAINTENANCE TROUBLESHOT THE PROBLEM AND FOUND THAT THE MIXTURE SETTING ON THE RH ENGINE WAS EXCESSIVELY RICH. MAINTENANCE SET THE MIXTURE AS PER MAINTENANCE MANUAL AND AIRCRAFT WAS GROUND RUN SDR CA190731022Door · malfunctioned(CAN) DURING TAKEOFF CABIN ENTRANCE DOOR OPENED AND PILOT RETURNED TO AIRPORT. THE PILOT PROPERLY CLOSED THE DOOR AND ENSURED IT WAS LATCHED. HE THEN RETURNED TO THE RUNWAY TO CONTINUE THE INTENDED FLIGHT. (TC# 20190731022)SDR 2019FA0000192Bearing · failedUPON INITIAL TAKEOFF, A LOUD NOISE WAS HEARD WHEN LANDING GEAR CAME UP. WHEN PLANNING FOR LANDING, GEAR WAS SELECTED DOWN, IT MOVED DOWN FOR A SPLIT SECOND AND THEN THE CIRCUIT BREAKER FOR THE LANDING GEAR MOTOR POPPED AND THERE WAS A SMELL OF SMOKE OR BURNINGSDR 2019FA0000089Actuator Cable · unsecureDURING ANNUAL INSPECTION HEIM JOINT USED TO CONNECT THROTTLE CABLE TO THROTTLE BODY WAS FOUND TO BE PARTIALLY UNSCREWED FROM THROTTLE CABLE. THE WITNESS HOLE ALLOWED A WIRE TO PASS THROUGH, INDICATING INSUFFICIENT ATTACHMENT.SDR 2019FA0000043Connecting Rod · brokenPILOT FELT A SHUDDER OF THE LEFT ENGINE AND IT SHUT DOWN ON ITS OWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION WE FOUND THAT THE PROP DID NOT FEATHER, THE ENGINE SEIZED, THERE ARE THREE HOLES IN THE TOP ON THE LEFT ENGINE CASE HALF, OBSERVED THROUGSDR E5ZR20180613001Connecting Rod · failedAFTER TEARING DOWN THE ENGINE IN QUESTION IT IS OUR OPINION THAT THE FAILURE WAS DO TO OIL STARVATION OF THE NR 5 CYLINDER CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNS SDR E5ZR2018061300178Connecting Rod · failedAFTER TEARING DOWN OF THE ENGINE IN QUESTION IT IS OUR OPINION THAT THE FAILURE WAS DO TO OIL STARVATION OF THE #5 CYLINDER CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNSSDR E5ZR2018061300177Connecting Rod · oil starvationAFTER TEARING DOWN OF THE ENGINE, THE NR 5 CYLINDER FAILED DUE TO OIL STARVATION OF THE CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNS OF BURN MARKS.SDR JZRR2015011200004Adapter · corrodedWHILE COMPLETING AN ANNUAL INSPECTION, REMOVED FUEL CAPS TO INSPECT THE CAPS, SEALS AND ADAPTERS. FOUND THE LEFT WING MAIN TANK FUEL CAP ADAPTER HEAVILY CORRODED AND PITTED. WITH THE EXTENT OF CORROSION ON THE ADAPTER, THE CAP WOULD NOT SEAL ALLOWING WATER TO SDR PAIR201510131457Mount · chafedDURING SCHEDULED ENGINE CHANGE FOUND LT ENGINE MOUNT CHAFED BY EXHAUST PIPE AT LOWER INBD ATTACH FITTING. FOUND RT ENGINE MOUNT CHAFED BY EXHAUST PIPE AT LOWER OTBD ATTACH FITTING. AIRCRAFT HAS BEEN MODIFIED BY STC SA432SO, REPLACEMENT OF ENGINES WITH DIFFERSDR 2015FA0000456Attach Fitting · crackedDURING ANNUAL INSPECTION, LT AFT LOWER WING ATTACH FITTING WAS FOUND TO BE CRACKED ALONG LOWER SURFACE, AND VERIFIED BY DYE PENETRANT INSPECTION. CRACK MEASURES APPROXIMATELY 0.85" IN LENGTH AND 0.35" DEEP, AS MEASURED ON INBD SURFACE OF FITTING. REPLACEMENTSDR CA150831012Gear · worn(CAN) LEFT ENGINE LOST POWER IN FLIGHT. APPROXIMATELY 25 MINUTES AFTER DEPARTING, WHILE IN CRUISE AT 8000 FT, THE LT ENGINE QUIT. FUEL PUMP REMOVED AND FOUND THE COUPLING SHAFT, PN: 631683 ROUNDED INTERNALLY AND DRIVE GEAR, PN: 631684 WORN. DRIVE GEAR AND CSDR CA150831011Drive Coupling · worn(CAN) LEFT ENGINE LOST POWER IN FLIGHT, APPROXIMATELY 25 MINUTES AFTER DEPARTING, WHILE IN CRUISE AT 8000`, THE LT ENGINE QUIT. FUEL PUMP REMOVED AND FOUND THE COUPLING SHAFT PN: 631683 ROUNDED INTERNALLY AND DRIVE GEAR, PN: 631684 WORN. DRIVE GEAR AND COUPLINSDR 2015FA0000063Bearing · failedPILOT REPORTED THAT HE HAD GREEN GEAR DOWN AND LOCKED LIGHTS PRIOR TO LANDING AND WHEN THE NOSE TOUCHED DOWN IT FOLDED. FOUND THAT THE AFT RETRACT ROD,ROD-END AT THE EXTENSION IDLER FAILED CAUSING THE COLLAPSE. ONLY MINOR AIRFRAME DAMAGE TO THE NOSE AND NOSE SDR CA141231002Relay · failed(CAN) WHILE GEAR OPERATION SWITCH WAS IN THE UP POSITION, GEAR LOWERED VIA THE MOTOR ON ITS OWN. PIC NOTED THAT SWITCH WAS UP AND LOCKED AND NO BREAKERS HAS "POPPED", HOWEVER BOTH PIC AND PASSENGER ALSO NOTICED THAT THE 3 GREEN WERE INDICATING. UPON TROUBLESHSDR CA141203006Indicator · leaking(CAN) DURING FLIGHT, PILOT NOTICED THE FACE OF THE FUEL PRESSURE INDICATOR HAD FLUID POOLING IN THE BOTTOM OF IT. IT WAS REPORTED TO MAINTENANCE AND THE INDICATOR WAS REPLACED.SDR 2013FA0000503Cylinder · failedENGINE RAN INTERMITTENTLY ROUGH . NR 1 CYLINDER SHOWED VERY LOW EGT AND CHT. PERFORMED COMPRESSION TEST ON NR 1 CYLINDER. COMPRESSION WAS LOW AND AIR WAS ESCAPING PAST EXHAUST VALVE INTO EXHAUST STACK. R & R CYLINDER WITH REPAIRED AND INSPECTED UNIT. REPOSDR CA130807012Line · cracked(CAN) DURING A DAILY INSPECTION ON THE RT ENGINE, THE FUEL INJECTOR LINE AT THE NR 3 CYLINDER FUEL INJECTOR WAS FOUND FUEL/SOOT STAINED. A QUICK LEAK CHECK WITH THE FUEL BOOST PUMP RUNNING REVEALED A LEAK NEAR THE FITTING ATTACHING THE LINE TO THE FUEL INJECTSDR 2013FA0000372Tube · defectiveNOSE TIRE WENT FLAT ON LANDING. TUBE HAD PIN HOLE.SDR CA120809014Control Cable · crossed(CAN) IN CRUISE, PILOT ATTEMPTED TO CENTER THE BALL IN THE TURN AND BANK INDICATOR BY APPLYING RUDDER TRIM. WHEN APPLIED, AFFECT WAS OPPOSITE TO NORMAL, TURNED TRIM WHEEL LT AND RT RUDDER TRIM WAS NOTED. PILOT LANDED AND ADVISED MAINTENANCE. MAINTENANCE DISCSDR 2012FA0000540Motor · failedLANDING GEAR MOTOR WOULD TRIP CIRCUIT BREAKER DURING ALL ATTEMPTS AT LOWERING LANDING GEAR. EMERGENCY PROCEDURES FOR LANDING GEAR EXTENSION FAILURE AND MANUAL GEAR EXTENSION UNSUCCESSFUL RESULTING IN A GEAR-UP LANDING. ON INSPECTION OF LANDING GEAR COMPONENTSDR CA110503006Aileron · misinstalled(CAN) RT AILERON OUTBOARD ATTACH DISCONNECTED IN FLIGHT DUE TO IMPROPER INSTALLATION. ON INSPECTION PICK UP POINTS FOR AILERON ATTACH HAD BEEN MISSED INTERNALLY DUE TO DIFFICULTY IN VISUAL ALIGNMENT IN BETWEEN SKINS WHERE ATTACH HARDWARE PURCHASE AILERON ATTACSDR 2010FA0001234Line · corrodedACCESSED & CLOSELY INSPECTED RT FUEL FLOW/PRESSURE GAGE LINE WHERE IT CROSSED DEFROST DUCT BECAUSE IT LOOKED LIKE THEY MAY BE CONTACTING. FOUND EXTENSIVE CORROSION AT POINT OF CONTACT. AFTER LINE WAS REMOVED, SLIGHT BENDING PRESSURE CRACKED AREA WIDE OPEN ANSDR 2010FA0001103Control Cable · detachedDURING FLIGHT, THE RT ENGINE MIXTURE CONTROL FAILED AND THE ENGINE QUIT. AFTER LANDING, FOUND THE SWAGGED END OF THE MIXTURE CONTROL CABLE (PN 50-389010-21) HAD SEPARATED AT THE FUEL CONTROL UNIT.SDR 2010FA0000249Lifter · spalledENGINE CYLINDERS HAD LOW COMPRESSION. REMOVED CYLINDERS AND FUND LIFTERS HAD SPALLING AND CAM SHAFT WAS WORN. LIFTER PN 653888 AND PN 653877 INSTALLED. THESE PN ARE DESIGNATED AS NOT AFFECTED BY MSB 09-8 OR AD 2009-24-52.SDR 2008FA0000847Spring · brokenSTARTER ADAPTER P/N 635050-A4, STARTER SPRING FAILED. STARTER ADAPTER OVERHAULED, RETURNED TO SERVICE AFTER OVERHAUL. PART SOLD, STARTER ADAPTER INSPECTED AND RETAGGED AND SOLD TO MFG. MAINT INSTALLED STARTER ADAPTER AND SPRING FAILED 14 HOURS LATER.SDR 2008FA0000710Tube · chafedALUMINUM TUBING TO PROP GOVERNOR FOUND CHAFED DUE TO TIE RAP RUBBING TUBE. FABRICATED NEW TUBE, INSTALLED AND LEAK CHECKED.SDR 2007FA0001088Rib · crackedAT ANNUAL INSPECTION FOUND CRACK ON FLAP RIB. (FLAP ROD ATTACH POINT) BOTH LT AND RT FLAPS. (K)SDR CA071002005Piston · damaged(CAN) DURING CRUISE FLT, RT ENGINE BEGAN TO LOOSE OIL PRESSURE. OIL TEMP & CHT INCREASED. PILOT ELECTED TO SHUTDOWN ENGINE AS A VIBRATION BECAME APPARENT & OIL PRESSURE DECREASED TO NEAR ZERO. AN EMERGENCY DECLARED & AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. USDR CA071212002Spar · cracked(CAN) DURING ANNUAL INSPECTION, VISUAL INSPECTION OF AREA REVEALED A SUSPECTED CRACK. NOT OF DYE PENETRANT AND EDDY CURRENT CONFIRMED. MFG SERVICE KIT TO INSTALLED. PART LAST NDT INSPECTED 22.1 HRS PREVIOUS AND NO INDICATIONS. (TC NR 20071212002)SDR CA070801001Fuel Cell · deteriorated(CAN) THE RT WING LEADING EDGE FUEL CELL WAS REMOVED BECAUSE OF A FUEL LEAK. A REPLACEMENT FUEL CELL WAS ORDERED. PRIOR TO INSTALLATION OF THE NEW (OVERHAULED) CELL, IT WAS INSPECTED AND FOUND TO CONTAIN A LARGE QUANTITY OF SAWDUST-LIKE PARTICLES. ON FURTHER ISDR ATL07LA057Fuel Cell · leakingDURING START OF RT ENGINE, PILOT REPORTED HEARING A LOUD THUMP, NOTED FIRE COMING FROM THE BOTTOM OF THE RT COWLING. SHUTDOWN ENGINES, EVACUATED AIRCRAFT, AND NOTED APPARENT EXPLOSION HAD OCCURRED IN RT WING. VISUAL INSPECTION DID NOT REVEAL CAUSE OF EVENTSDR 2007FA0000030Valve · failedFOUND THERMOSTAT WORKING, BUT FUEL SOLENOID NOT STOPPING FUEL DELIVERY EVEN WITH POWER TO VALVE DISTUPTED. CABIN HEATER ONLY SHUTDOWN WHEN OVERHEAT SWITCH OPENED. VALVE INFO: MODEL NR 4400B.SDR CA060624001Bolt · loose(CAN) AILERON TRIM BOLT FOUND MIGRATING OUT OF LINKAGE ARM ON LT AILERON TRIM TAB ASSEMBLY. BOLT WAS NOTED TO BE FINGER-TIGHT ONLY AND NOT SET INTO LOCKING DEVICE. NOTE: BOLT WAS FOUND IN THIS CONDITION AFTER FLIGHT CONTROLS WERE INSTALLED AFTER AIRCRAFT WAS PSDR PAI5200604049Plate · crackedDURING ANNUAL INSPECTION FOUND RT BRAKE TORQUE PLATE CRACKED .7500 OF THE LENGTH OF THE CALIPER PIN BORE.SDR 2006FA0000327Impulse Coupling · rustedDURING A ROUTINE INSP, ALL MAGNETOS WERE REMOVED FOR POINTS AND CONDENSER REPLACEMENT. RUST WAS FOUND ON THE FLYWEIGHT/AXLE AREA OF THE IMPULSE COUPLING. A WEAR CHECK WAS MADE AND IT WAS DETERMINED THAT ALL COUPLINGS FAILED IAW MSB. NOTE: THE FLYWEIGHT/ AXSDR 2006FA0000265Baffle · deterioratedFOUND FUEL SYSTEM CONTAMINATED WITH AN UNKNOWN SUBSTANCE. AFTER HAVE THE ENTIRE SYSTEM DRAINED, FLUSHED AND THE ENGINE FUEL INJECTION SYSTEM OVERHAULED, THE AIRCRAFT WAS REFUELED AND FLOWN. AFTER A SHORT FLIGHT, THE SUMPS WERE CHECKED AGAIN AND THE SUBSTANCESDR 2006FA0000262Fuel Cell · deterioratedFOUND FUEL SYTEM CONTAMINATED WITH AN UNKNOWN SUBSTANCE. AFTER HAVING THE ENTIRE SYSTEM DRAINED, FLUSHED AND THE ENGINE FUEL INJECTION SYSTEM OVERHAULED, THE AIRCRAFT WAS REFUELED AND FLOWN. AFTER A SHORT FLIGHT, THE SUMPS WERE CHECKED AGAIN AND THE SUBSTANCSDR 2005FA0001364Spar Cap · corrodedDURING AN ANNUAL INSPECTION, SOME CORROSION WAS FOUND IN THE AREA OF THE RT WING TIE DOWN ASSY, UPON FURTHER INVESTIGATION AN AREA OF APPROXIMATELY 8 INCHES IN LENGTH WITH SEVERE INTERGRANULAR CORROSION WAS DISCOVERED ON THE LOWER SPAR CAP POSSIBLY CAUSED BY DSDR CA050617007Doubler · cracked(CAN) DURING ROUTINE LPI INSPECTION OF THE FRONT WING SPAR CARRY THRU STRUCTURE AND REPAIR DOUBLERS IN ACCORDANCE WITH AD90-08-14, THE LT FWD REPAIR DOUBLER WAS FOUNDCRACKED IN THE LOWER BEND RADIUS IN THE SAME SPOT AS THE ACTUAL WING SPAR WHICH THE DOUBLER WASDR 2005FA0000794Door · delaminatedIB LANDING GEAR DOORS HAD CORROSION DUE TO DELAMINATION OF FORWARD EDGE OF GEAR DOORS.SDR IS4R200500003Combustion Head · wornHEATER CORE RECEIVED FROM CUSTOMER. UPON TEARDOWN, FOUND INTERIOR OF THE COMBUSTION HEAD SEVERELY WORN FROM FLAME EROSION. PREVIOUS INSPECTIONS BY THIS REPAIR STATION HAVE FOUND SMALL HOLES APPEARING IN THE WALL OF THE COMBUSTION HEAD. FROM THE OUTSIDE, THESDR IS4R200500002Tube · crackedHEATER COR RECEIVED FROM CUSTOMER. COMBUSTION TUBE FOUND CRACKED AT CROSSOVER PART WHICH CONNECTS THE INNER COMBUSTION TUBE TO THE OUTER COMBUSTION TUBE. MALFUNCTION FOUND USING A PRESSURE DECAY TEST, EVEN THOUGH THIS TEST IS NOT REQUIRED ON THE D83A28 HEATESDR CA050512009Coupling · wornAIRCRAFT IN CRUISE, ENGINE SPUTTERED AND DIED. BOOST PUMP ACTIVATED AND ENGINE RESTARTED. PART IS AN ON-CONDITION ITEM. THE SQUARE DRIVE ROUNDED OFF UNTIL IT WOULD NO LONGER ENGAGE THE DRIVE GEAR P/N 631684. THIS CAUSED THE FUEL PUMP TO STOP ROTATING RESULSDR CA041215003Relay · malfunctioned(CAN) DURING A MISSED APPROACH PILOT INITIATED A TURN TO RETURN FOR A 2ND APPROACH WHEN MLG EXTENDED UNCOMMANDED WITH NO DOWN OR UP INDICATION LIGHTS. PILOT SLOWED ACRFT & CONTINUED TO DESTINATION WITH MLG SELECTED DOWN & CONFIRMED MLG DOWN WITH EMERGENCY GEAR
Back to Beech 95-B55