Embraer EMB-500
Service difficulty reports · 197
Newest first. General aviation reporting is voluntary.
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 = 'EMB500' 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 = 'EMB500' 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 2012FA0000741Gear · obstructedON APPROACH, PILOT UNABLE TO RETARD THE RT THROTTLE COMPLETELY. A SUCCESSFUL LANDING WAS ACCOMPLISHED. INSPECTION REVEALED ONE OF THE DUST COVER SEGMENTS FOR THAT THROTTLE WAS NOT MOVING IN SEQUENCE WITH THROTTLE MOVEMENT. ON FURTHER INVESTIGATION, IT WAS FSDR E07A201209280001Skin · bentAFTER LANDING, CREW NOTICED ON POSTFLIGHT INSPECTION THE LT LOWER WING SKIN/WHEEL WELL FAIRING WAS PEELED BACK.SDR E07A2012092000002Pressure Switch · defectiveON LANDING ROLL, BRAKES FADED THEN FAILED. ACFT WAS STOPPED USING EMERGENCY BRAKES. CREW NOTED HYDRAULIC PRESSURE INDICATED 0 ALSO HAS BRAKE FAIL MESSAGE AND LOW HYD PRESSURE CAS MESSAGE. DETERMINED FAULT TO BE PRESSURE SWITCH OR PUMP CONTROL RELAY.SDR E07A2012092000001Relay · defectiveBRAKES FADED AND THEN FAILED ON LANDING ROLL OUT. HYDRAULIC PRESSURE INDICATED 0. SUSPECT PRESSURE SWITCH OR HYDRAULIC PUMP RELAY FAILED.SDR CA120917019Shutoff Valve · failed(CAN) ON CLIMB OUT THE ACFT HAD A NR 1 BLEED AIR FAILURE. THE ACFT DIVERTED BACK AND LANDED WITHOUT INCIDENT. LT PYLON PRESSURE REGULATING SHUTOFF VALVE, PRSOV REPLACED.SDR CA120903003Engine · faulted(CAN) DURING TAKE OFF ROLL, THE PILOT RECEIVED A NR 1 ENGINE CONTROL FAULT, WARNING AND ABORTED TAKE OFF. TAXIED BACK TO THE TERMINAL AND RESET THE POWER AND FADEC CIRCUIT BREAKERS BEFORE MAKING A SUBSEQUENT NORMAL TAKE OFF. THE SAME PROBLEM, OCCURRED ON TSDR CA120717008Powerpack · failed(CAN) WHILE IN CLIMB THREW ABOUT 12,000, MLG DROPPED OUT AND AFTER WE REDUCED POWER AND BROUGHT A/S FROM 200 IAS TO 160 IAS THE ACFT WAS THEN LEVELED OFF AND RAN QRH FOR HYD LOW PRESSURE GEAR WAS SELECTED DOWN AND ACFT RETURNED. DURING THE TAXI THE HYD PUMP WSDR 6JPA20121212001Pump · failedUPON STOPPING THE AIRCRAFT ON THE RAMP TO PARK AT THE FBO AT KLNS (LANCASTER PA) THE HYDRAULIC PUMP FAILED AND BLEW THE HYDRAULIC POWER ELECTRICAL FUSE. MAINTENANCE CREW REMOVED AND REPLACED THE HYDRAULIC POWER PACK ASSEMBLY AND ELECTRICAL FUSE IAW PHENON 100SDR E07A20120521512Bleed Air Sys · contaminatedON CLIMBOUT, CREW SMELLED BURNED OIL AND OBSERVED LIGHT SMOKE IN THE AFT CABIN. LECTED TO RETURN FOR INSPECTION. SMOKE AND ODOR DISSIPATED WITHIN MINUTES. AFTER INSPECTION OF ACFT, DETERMINED ODOR AND SMOKE TO HAVE ORIGINATED FROM SMALL AMOUNT OF ENGINE SDR 2012FA0000145Pitot Tube · erodedDURING A POST FLIGHT INSPECTION, DISCOVERED PLATING MATERIAL ON THE INLET LIP SURFACE WAS SEPARATING FROM THE LIP AND HAD FLARED BACKWARDS INTO THE THROAT OF THE PITOT TUBE. THE PITOT TUBE WAS REMOVED FROM THE ACFT AND THE PITOT LINE WAS CLEARED OF DEBRIS. TSDR CA120125002Warning Message · illuminated(CAN) CAS MESSAGE GENERATOR NR 2 OFF BUSS.SDR 2012FA0000019Skin · crackedTHE RT WING LOWER WING SKIN, AFT OF THE RT MLG, WAS FOUND CRACKED AT THE FORWARD RIVET HOLE FOR THE SKIN ATTACHMENT TO THE MIDDLE RIB DURING A VISUAL INSPECTION.SDR 2012FA0000017Pitot Tube · erodedEROSION OF THE "PLATING MATERIAL" ON THE FACE/INLET OF THE TUBE WHICH THEN PROCEEDS TO MIGRATE DOWN THE BARREL OF THE TUBE. PITOT TUBE HAS THEN BEEN INSTALLED AND THE CORRESPONDING RECONNECT/LEAK AND CERTIFICATION CHECKS HAVE BEEN PERFORMED TO RETURN THE ACFTSDR CA111123012Control Unit · failed(CAN) UPON LANDING, SKIDDED DUE TO THE RNWY BEING WET. THE WX AT TIME OF LANDING WAS HEAVY RAIN. WHEN THE ACFT STARTED TO SKID, THE CREW DEPLOYED THE EMER BRAKE. BOTH MAIN GEAR TIRES HAVE BEEN FLAT SPOTTED. UPDATED BY THE CREW NOT EXACTLY, WE LANDED & APPLSDR 2011FA0000552Static Port · misrepairedPRIOR TO INSTALLATION OF AN OVERHAULED DUAL STATIC PORT IT WAS NOTED THAT 1 OF THE AN FITTINGS THAT CONNECTS TO 1 OF THE STATIC LINES WAS DAMAGED ON THE SEATING SURFACE. A BENCH LEAK CHECK WAS PERFORMED AND THE LEAK RATE WAS BEYOND LIMITS. MFG SUPPLIED INSTALLSDR E07A20110730001Brake · intermittentAFTER TOUCHDOWN, SPEED AND APPLYING BOTH BRAKE PEDALS WITH EQUAL PRESSURE, THE ACFT STARTED IMMEDIATELY VEERING QUICKLY TO THE LT OF THE RUNWAY. AFTER RELEASING PRESSURE FROM BOTH BRAKE PEDALS, THE BRK FAIL CAS MESSAGE ILLUMINATED. NO BRAKES WERE AVAILABLE ASDR 2011FA0000460Fuel Filter · missingDURING THE FIRST SCHEDULED INSP (600HR/12 MONTH) THE RT ENGINE FUEL FILTER WAS FOUND TO HAVE NEVER BEEN INSTALLED AT THE FACTORY. THE MFG WAS NOTIFIED AND THEY REQUESTED AN ENGINE HOT SECTION BOROSCOPE INSP BE PERFORMED. NO ENGINE DISTRESS WAS OBSERVED AND COSDR E07A20110708001Pump · inoperativeON REPOSITION FLIGHT, CREW HAD A HYD PUMP FAILURE. THIS ALSO CAUSED THE BRAKE FAILED CAS MESSAGE TO ILLUMINATE. THE CREW ELECTED TO FLY TO AIRPORT WHICH HAS A LONGER RUNWAY. ON ROLL OUT CREW USED EMEREGANCY BRAKES CAUSING RT MAIN TO FLAT SPOT AND LOOSE ALL SDR 2011F00164Control Valve · failedAFTER LANDING GEAR EXTENSION FOR LANDING AT KMSO THE CREW WAS NOTIFIED OF A BRAKE SYSTEM FAILURE VIA THE CAS SYSTEM. AIRCRAFT LANDED WITHOUT INCIDENT AND THE CREW IDENTIFIED THEY DID NOT HAVE NORMAL BRAKES AVAILABLE. AIRCRAFT WAS SLOWED TO A STOP USING THE ESDR E07A557TCStarter Gen · failedON FLIGHT, CREW NOTED VIBRATION AND THEN LT GEN FAIL INDICATION. ACFT WAS DIVERTED AND LANDED WITHOUT INCIDENT. UPON INSPECTION IT WAS DETERMIND BEARINGS ON LT GEN HAD FAILED. THIS ALSO DAMAGED THE SPLINE DRIVE ADAPTER IN THE ENGINE. PN CT3983-01SDR 2011FA0000213Starter Gen · failedDURING CRUISE FLIGHT THE PILOT NOTICED AN INCREASING NOISE AND VIBRATION COMING FROM THE RT ENGINE. SHORTLY AFTER, THE NR 2 GENERATOR WENT OFF LINE AND COULD NOT BE RESET. BEFORE HE COULD MAKE A PRECAUTIONARY LANDING THE NOISE AND VIBRATION CONTINUED TO INCRESDR E07A645ASAStarter Gen · failedON DESCENT CREW NOTICED NR 2 GEN INOP LIGHT ILLUMINATED. THE GENERATOR WAS SELECTED OFF AND THE ACFT LANDED WITHOUT INCIDENT. ON FUTHER INSP IT APPEARS THAT THE BEARING IN THE STARTER/GEN FAILED. EXCHANGE STARTER/GEN WAS INSTALLED AND THE ACFT WAS RETURNED SDR CA110223006Heater · failedSTANDBY PITOT/STATIC TUBE HEATER FAILED IN FLIGHT CAUSING THE"STBY HTR FAIL CAS MESSAGE TO ILLUMINATE. TROUBLESHOOTING CONFIRMS THAT THE HEATER ELEMENT HAD BURNED OUT IN THE PROBE. THIS IS THE SECOND PROBE THAT HAS BEEN CHANGED IN THE LAST 3 WEEKS. THE 1STSDR CA110214004Fmu · failedPOWER ROLLBACK, PILOT REPORTED THAT JUST AFTER TAKEOFF (WHILE IN CLIMB), THE LT SIDE ENGINE ROLLED BACK TO 60 PERCENT N2. THE RT SIDE ENGINE REMAINED NORMAL. PILOT PERFORMED AN UNEVENTFUL LANDING AT AIRPORT OF ORIGIN. TROUBLESHOOTING IS ONGOING WITH MFG ASSISSDR DJFA2011007Inlet · crackedDURING ACCOMPLISHMENT OF REPETATIVE INLET INSP REQUIRED BY SB 505-71-0001, MX FOUND MULTIPLE CRACKS ON THE LT ENGINE INLET. CRACKS WERE REPAIRED IAW THE ACFT MFG INSTRUCTIONS.SDR CA110125001Engine · failedIFSD AFTER A NORMAL START THE GROUND CREW SHUTDOWN THE ENG AFTER THE ENGINE EXHIBITED FLAMES OUT OF THE EXHAUST AND THE CABIN FILLED WITH SMOKE. AFTER THE SHUTDOWN THE PILOT FOUND A PUDDLE OF ENGINE OIL ON THE GROUND BELOW THE ENGINE. NO ABNORMAL ENGINE PARAMESDR E07A20101221001Skin · bentDURING DESCENT, GEAR UP, FLAPS ZERO, AT APPROX 10, 000 FT THE CREW FELT A RUMBLE. DISCONNECTED AUTOPILOT AND FELT A LT ROLL. CONTINUED DESCENT, LANDED UNEVENTFUL. POSTFLIGHT INVESTIGATION REVEALED THE SKIN AFT OF THE LT GEAR WELL FOLDED BACK.SDR E07A20101220001Inlet · crackedDURING POSTFLIGHT, IT WAS DISCOVERED THAT THE INLET LIP ON THE NR2 ENGINE IS COMING APART. IT HAS A SEGMENT OF MATERIAL MISSING. CRACKED IN 2 OTHER LOCATIONS AND 3 RIVET HEADS MISSING IN ANOTHER LOCATION.SDR E07A600AS1210Starter Gen · vibrationCREW EXPERIENCED A VIBRATION IN CRUISE FLIGHT. WITHIN SEVERAL MINUTES A NR2 GEN OFF BUS CAS WAS ILLUMINATED. STARTER/GEN WAS REPLACED AND ACFT WAS RETURNED TO SERVICE.SDR E07A 392AS 1110Probe · inoperativeON TAKEOFF ROLL CREW HAD CAS MESSAGE INDICATING AP FAIL AND YD FAILED . TAKEOFF WAS ABORTED AND ACFT WAS RETURNED TO FBO. RT SMART PROBE WAS REPLACED AND ACFT WAS RETURNED TO SERVICE.SDR E07A645ASStarter Gen · malfunctionedIN CRUSE FLIGHT, CREW HEARD LOUD NOISE AND NOTICED VIBRATION. CREW LANDED ACFT WITHOUT INCIDENT. ON FINAL APPROACH CREW NOTICED FEN 1 FAIL LIGHT. LT STARTER/GENERATOR WAS REPLACED AND ACFT FINISH TRIP TO DESTINATION.SDR E07A557TC001Shuttle Valve · bindingEXPERIENCED A BRAKE FAIL CAS MESSAGE WITH ASSOCIATED LOSS OF BRAKING. PERFORMED A QUICK TURN APPROX 15 MIN AFTER ARRIVAL. AFTER RELEASING PARK BRAKE NOTICED CAS MESSAGE BRAKE FAIL. APPLIED NORMAL BRAKES AND HAD NO BRAKING ON THE RT SIDE. REAPPLIED PARK BRAKE,SDR E07A20100917001Shuttle Valve · stickingACFT ARRIVED AT DESTINATION. PASSENGERS WERE DROPPED OFF AND ACFT WAST TAXING FOR TAKEOFF. CREW NOTED LIMITED BRAKING. ACFT RETURNED TO MX BASE. BRAKES WERE BLED IAW MM 32-40-00-870-801-A. ACFT WAS RETURNED TO SERVICE.SDR 2010FA0001040Shuttle Valve · stickingACFT ARRIVED AT DESTINATION AFTER DROPPING OFF PASSENGERS, PILOTS NOTICED THAT THEY HAD LIMITED BRAKING WHILE TAXI OUT FOR DEPARTURE. ACFT RETURNED TO MX BASE AND BRAKE BLEEDING PROCEDURES WAS ACCOMPLISHED IAW MM 32-40-00-870-801-A. ACFT WAS RETURNED TO SERVSDR 2010FA0001052Actuator · malfunctioned(MV5R) FLIGHT CREW REPORTED STRONG ROLL TENDENCIES TO THE RT WHEN POSITIONING THE FLAPS TO FLAPS 3 OR FULL. BUT NO ROLL IN POSITION 1 OR 2. A FLAP RIGGING CHECK WAS PERFORMED WITH NO DEFECTS NOTED. THE RT FLAP LINEAR ACTUATOR WAS REPLACED, RIGGED AND THE ACSDR 2010FA0000721Actuator · failedNUMEROUS SYS FAILURES WERE INDICATED AT THE SAME TIME. THE SYS CONTINUED TO OPERATE NORMALLY. THE PILOT DIVERTED FOR REPAIR. THE PILOT DECLARED AN EMERGENCY DUE TO AN UNSAFE RT LANDING GEAR INDICATION. THE ACFT LANDED AND TAXIED TO THE SERVICE CENTER SAFELY. TSDR 2010FA0000471Cooling Fan · inoperativeTHE HYD POWER PACK COOLING FAN WAS FOUND INOPERATIVE.SDR 2010FA0000469Servo · out of toleranceRUDDER AUTO PILOT SERVO MOUNT SLIP CLUTCH COULD NOT BE ADJUSTED TO AMM LIMITS.SDR 2010FA0000468Transducer · intermittentDURING TAXI, ACFT PULLS TO THE LT DURING APPLICATION OF THE BRAKES. THE RT WHEEL SPEED TRANSDUCER WAS DISPLAYING 0 KTS INTERMITTENTLY WHILE ACFT WAS IN MOTION.SDR 2010FA0000450Electrical Sys · malfunctionedRECEIVE AN "ELEC XFR FAIL" CAS MESSAGE DURING EVERY ENGINE START, THEN GOES AWAY AFTER A FEW MOMENTS.SDR 2010FA0000449Control Unit · intermittentDURING ENGINE START, "BRAKE FAIL" CAS MESSAGE WAS DISPLAYED FOR A FEW MOMENTS THEN WOULD EXTINGUISH. BRAKES WERE ALWAYS OPERATIONAL.SDR 2010FA0000448Stall Warning · malfunctionedDURING PREFLIGHT STICK PUSHER WOULD NOT TEST THE FIRST TIME THE STALL WARNING SYSTEM WAS TESTED AFTER APPLYING ELECTRICAL POWER TO THE AIRPLANE. SUBSEQUENT TESTS WERE NORMAL.SDR E07A620AS410Pitot Tube · delaminatedON POST FLIGHT INSPECTION IT WAS NOTICED THAT THE INSIDE OF THE RT PITOT TUBE WAS PEELING (DELAMINATED). NEW PITOT TUBE WAS INSTALLED BEFORE FLIGHT.SDR 2009FA0001025Outflow Valve · defectiveDURING APPROACH AT 4000MSL THE PILOT LOST PRESSURIZATION CONTROL IN THE AUTO AND MANUAL MODE. A "MAX DIFF" CAS MESSAGE WAS DISPLAYED.SDR 2009FA0000952Control Unit · malfunctionedFLIGHT CREW REPORTED BRAKE FAIL CAS MESSAGE, BRAKE CONTROL CIRCUIT BREAKER POPPED IN FLIGHT. CREW WAS ABLE TO RESET BREAKER IN FLIGHT. UPON LANDING ACFT NORMAL BRAKING WAS UNAVAILABLE. CREW USED EMERGENCY BRAKE TO STOP ACFT.SDR 2009FA0000837Hinge · seizedTHE MAIN CABIN DOOR AFT HINGE PIN PARTIALLY SEIZED IN THE HINGE HALF MOUNTED ON THE DOOR. THE DOOR WAS VERY HARD TO OPEN AND CLOSE AND MADE A LOUD NOISE WHEN OPENING. THE HINGE PIN HAD TO BE CUT TO BE REMOVED FROM THE DOOR. A VISUAL AND EDDY CURRENT INSPECTIONSDR CA090828006Metering Unit · damagedON CLIMB, FOLLOWING TAKEOFF, ENG EXPERIENCED AN UNCOMMANDED PWR ROLLBACK AND FLUCTUATIONS. INVESTIGATION REVEALED A DAMAGED FUEL METERING UNIT. CAUSE OF DAMAGE REMAINS UNDER INVESTIGATION. WILL CLOSE THIS SDR WHEN ROOT CAUSE HAS BEEN ESTABLISHED.
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