Embraer EMB-500

Service difficulty reports · 197

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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.

SDR E07A20151211001Engine · contaminatedON TAKEOFF, CREW NOTED SLIGHT SMOKE IN CABIN & SMELL OF BURNING OIL. RETURNED WITHOUT INCIDENT. THIS WAS FIRST FLIGHT AFTER OVERHAULED ENGS WERE INSTALLED. OPENED BLEED SYS & USED BORESCOPE TO INSPECTED ENG & BLEED SYS UP TO THE PRESS AFT PRESS BULKHEAD. NDec 8, 2015 · N620AS · Emb EMB500 · Engine (Turbine/Turboprop)SDR E07A20151207001Modulating Valve · stuckAFTER TAKEOFF, CREW NOTED HOT SMELL & A SMALL BIT OF SMOKE IN THE CABIN. TURNED OFF RT BLEED VLV, SMOKE & HOT SMELL DISSIPATED. DETERMINED RT CABIN TEMP MODULATING VLV WAS STUCK OPEN. INSTALLED NEW VLV, GND RUN & OPERATIONS CHECK WERE SATISFACTORY. ACFT WADec 3, 2015 · N665AS · Emb EMB500 · Cabin Temperature Control SystemSDR CA150811007Rivet · broken(CAN) DURING AN AIRWORTHINESS CONDITION CHECK, IT WAS DISCOVERED THAT A RIVET HEAD FOR THE TTO SENSOR ATTACHMENT MOUNT IN THE #1 ENGINE INLET HAD DEPARTED. ONLY ONE OF THE FIVE TOTAL WAS FOUND MISSING THE HEAD, THE AIRFRAME AND ENGINE HAD A TOTAL OF 3029.3 HRSAug 7, 2015 · Emb EMB500 · Engine Air Intake SystemSDR 2015FA0000348Clamp · leakingDUCT NR 2 OVERTEMP. PERFORMED QRH PROCEDURE AND RETURNED TO DEPARTURE. INSPECTED ACFT AND FOUND RT TMV DUCT CONNECTOR LEAKING. ADJUSTED CLAMP ON TMV AND SECURED. ACCOMPLISHED FULL POWER ENGINE RUNS IAW AMM 71-00-00. NO BLEED LEAKS OR INDICATIONS DURING RJul 23, 2015 · N100NV · Emb EMB500 · Pneumatic Distribution SystemSDR 2015FA0000330Attach Fitting · gougedDURING INSPECTION OF THE HORIZONTAL STABILIZER ATTACHMENT TO THE VERTICAL STABILIZER, FOUND THE 4 BARREL NUTS FOR THE FWD 4 ATTACH BOLTS WERE INSTALLED UPSIDE DOWN IN THE FITTING HOLES IN THE VERTICAL STABILIZER FITTING. THIS CAUSED DAMAGE TO THE FITTING FROMJul 23, 2015 · N514AF · Emb EMB500 · Vertical Stabilizer, Attach FittingsSDR CA150724004Control Cable · worn(CAN) DURING A SCHEDULED 3000 FH INSPECTION AN AILERON CONTROL CABLE IN THE L/H WING SHOWED WEAR BETWEEN RIBS 5 AND 6, THERE WAS NO VISIBLE CONTACT ON ADJACENT STRUCTURE.Jul 22, 2015 · Emb EMB500 · Aileron Control SystemSDR CA150724003Control Cable · worn(CAN) DURING A SCHEDULED 333FH INSPECTION AN AILERON CONTROL CABLE IN THE R/H WING SHOWED WEAR BETWEEN RIBS 5 AND 6. THERE WAS NOT VISIBLE CONTACT ON ADJACENT STRUCTURE.Jul 22, 2015 · Emb EMB500 · Aileron Control SystemSDR E07A20150819600Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1 TURN LOOSE ON 100% OF SCREWS.Jul 22, 2015 · N600AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819685Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 3/4 TURN LOOSE ON 80% OF SCREWS.Jul 20, 2015 · N685AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819669Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 30% OF SCREWS.Jul 20, 2015 · N669AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819723Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 50% OF SCREWS.Jul 17, 2015 · N723GB · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819639Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 20% OF SCREWS.Jul 16, 2015 · N639AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819645Screw · looseFOUND TORQUE ON WINDSHIELD SCREWS 1/4 TURN LOOSE ON 15% OF SCREWS.Jul 15, 2015 · N645AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819611Screw · backed outFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 5% OF SCREWS.Jul 15, 2015 · N611EC · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819102Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 40% OF SCREWS.Jul 15, 2015 · N102EP · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819620Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 15% OF SCREWS.Jul 14, 2015 · N620AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819605Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 15% OF SCREWS.Jul 11, 2015 · N605AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819670Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 100% OF SCREWS.Jul 10, 2015 · N670AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819630Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1 TURN LOOSE ON 50% OF SCREWS.Jul 10, 2015 · N630AS · Emb EMB500 · Flight Compartment WindowsSDR E07A20150819637Screw · looseFOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1 TURN LOOSE ON 50% OF SCREWS.Jul 8, 2015 · N637AS · Emb EMB500 · Flight Compartment WindowsSDR CA150615003Engine · faulty(CAN) PILOTS REPORTED SMOKE IN CABIN AFTER TAKEOFF, 1500 - 2000 FEET. CREW PUT MASK ON & LANDED. ENG HAD A RECENT HSI. THE TROUBLESHOOTING SHOWED OIL AROUND THE INNER DIAMETER OF THE FAN DISC & IN THE EXHAUST BREATHER OUT PORT & ON THE FMU DRAIN. OIL CONSUJun 2, 2015 · Emb EMB500 · Engine (Turbine/Turboprop)SDR MV5D2015052600001Tire · peelingUPON LANDING, THE RT MLG TIRE HAD TREAD SEPARATION. THE TIRE AND WHEEL ASSEMBLY WAS REPLACED WITH AN O/H ASSEMBLY, WHICH INCLUDED A NEW TIRE. VISUAL INSPECTION OF THE RT LANDING GEAR AND FLAP REVEALED DENTS IN THE RT FLAP LOWER SURFACE. PRODUCT SUPPORT ENGIMay 26, 2015 · N250Y · Emb EMB500 · TireSDR 9SUA2015FA0000221Carbon Seal · failedSMOKE IN COCKPIT RIGHT AFTER TAKEOFF. SMOKE ENTERED FROM UNDER AVIONICS, POSSIBLY FLOOR/RUDDER AREA. ENTERED CABIN AS WELL. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. RAN ACFT AT TAKEOFF POWER FOR 30 MIN. OPERATED BLEED SYSTEMS. PERFORMED CABIN/ May 14, 2015 · N575JS · Emb EMB500 · Turbine Engine Oil SystemSDR CA150306009Indication Sys · stuck(CAN) THE AIRCRAFT TOOK OFF & AFTER CROSSING 1500 FT THE ENGINE 2 LOW OIL PRESS CAS CAME ON. WHEN THE PILOT CHECKED THE RIGHT HAND OIL PRESS IT WAS SHOWING 75 PSI, IN RED, WITH ENGINE EXCEEDANCE CAS MESSAGE. THE AIRCRAFT LANDED AT DEPARTURE AIRPORT, DURING AMar 2, 2015 · Emb EMB500 · Engine Oil PressureSDR 9SUA201411070004Wire Harness · kinkedEXPERIENCED INTERMITTENT BRAKING ON LANDING ROLL. CREW NOTICED ANTI-SKID FAIL CAS MSG ON TAXI. DOWNLOADED THE COCKPIT VOICE DATA RECORDER. DATA SENT FOR EVALUATION. AFTER EVALUATION, CENTER RECOMMENDED WE INSPECT THE RT WHEEL SPEED TRANSDUCER & THE ASSOCIAJan 5, 2015 · N574JS · Emb EMB500 · Landing Gear System WiringSDR 2014FA0000715Pump · failedAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT FOLLOWED BY LOW HYDRAULIC CAS MESSAGE.Dec 5, 2014 · N665AS · Emb EMB500 · Hydraulic Pump (Electric/Engine), MainSDR CA141203009Bolt · damaged(CAN) DURING FLAP REMOVAL IT WAS DISCOVERED THAT BOTH FLAP ACTUATOR ATTACHING BOLTS WERE DAMAGED. THE LT BOLT APPEARS TO HAVE BEEN OVER TORQUED ON INSTALL, WHILE THE RT BOLT HAS A COUPLE GOUGE MARKS AROUND THE CIRCUMFERENCE OF THE BOLT.Dec 2, 2014 · Emb EMB500 · Trailing Edge FlapsSDR CA141203008Control Cable · worn(CAN) DURING INSPECTION THE LT AND RT FWD AILERON CABLES LOCATED IN THE WING WERE DISCOVERED TO HAVE 40% BLENDING OF THE CABLE WHERE IT PASSES OVER THE PULLEYS.Nov 29, 2014 · Emb EMB500 · Aileron Control SystemSDR CA141203007Torque Tube · worn(CAN) DURING INSPECTION IT WAS NOTED THAT THERE WAS EXCESSIVE PLAY IN THE RT ELEVATOR FITTING AND ATTACHING TORQUE TUBE. UPON DISASSEMBLY SOME WEAR WAS NOTED ON BOTH THE TORQUE AND THE R/H ELEVATOR FITTING.Nov 26, 2014 · Emb EMB500 · Elevator StructureSDR RT5R2014101084123Carbon Seal · failedIT WAS REPORTED THAT THE ACFT MADE AN UNSCHEDULED LANDING AND A PILOT COMMANDED SHUTDOWN NR 1 ENGINE DUE TO LOW OR LOSS OF OIL PRESSURE INDICATION.Oct 8, 2014 · N777JQ · Emb EMB500 · Turbine Engine Oil SystemSDR CA141024012Oil System · low pressure(CAN) WHILE IN CLIMB, 25 MINUTES AFTER T/O, PILOT NOTED ENGINE 1 LOW OIL PRESSURE WARNING AND ENGINE EXCEEDANCE MESSAGE. OIL PRESSURE GRADUALLY DECREASING AND PILOT INITIATED ENGINE SHUTDOWN WHEN PRESSURE REACHED 60 PSI, LOWEST 47 PSI. EMERGENCY WAS DECLAREDOct 6, 2014 · Emb EMB500 · Engine Oil Indicating SystemSDR 1MBD20140822001Cooling Fan · chatteringVCS SYSTEM WAS FAILING AND HAD A ODOR IN THE CABIN. WHEN MAINTENANCE PERSONNEL TURNED ON VCS SYSTEM, IT WAS NOTED EXCESSIVE NOISE AND VIBRATION COMING FROM THE GROUND COOLING FAN. ALSO, NOTICED ELECTRICAL BURNING ODOR IN COCKPIT AND GROUND COOLING FAN INLET.Aug 18, 2014 · N389MW · Emb EMB500 · Air Distribution FanSDR 9SUA201407180002Exhaust Duct · crackedTURBINE EXHAUST COWL ASSY CRACKED ON NR1 ENGINE. REMOVED TURBINE EXHAUST COWL ASSY, PN 35C4655-01, DUE TO CRACK. INSTALLED NEW TURBINE EXHAUST COWL ASSY, PN 35C4655-01. ALL WORK PERFORMED IAW MM PN 3072162, REV NR 11, DATED MAY 17, 2014. WORK PERFORMED BY Jul 8, 2014 · N582JS · Emb EMB500 · Engine Collector/Tailpipe/NozzleSDR 9SUA201407180001Control Valve · failedBRAKE FAIL CAS MESSAGE OCCURRED AT 23,000 FT ENROUTE TO 36000 FT CLEARED TO LEVEL OFF AT 24,000. DIVERTED. CREW RAN CHECKLIST FOR THE BRAKE FAIL. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED BRAKE SYSTEM FUNCTIONAL TEST IAW 32-41-00-720-80Jul 2, 2014 · N580JS · Emb EMB500 · Landing Gear Brake SystemSDR 2014FA0000395Shutoff Valve · misinstalledDURING INSTALLATION OF THE CREW OXYGEN BOTTLE AFTER HYDRO TEST, THE COCKPIT OXYGEN SHUTOFF CONTROL CABLE WAS CONNECTED TO THE BOTTLE WHEN THE SHUTOFF VALVE ASSY ON THE BOTTLE REGULATOR WAS ROTATED 180 DEGREES FROM THE CORRECT POSITION. THIS RESULTED IN THE BJun 20, 2014 · N142TL · Emb EMB500 · Crew Oxygen SystemSDR CA140619014Engine · power loss(CAN) DURING CRUISE, THE ENGINE SUFFERED AN UNCOMMANDED POWER LOSS AND IMMEDIATELY RECOVERED. P&WCÏ¿½S LOCAL FIELD SUPPORT REPRESENTATIVE WILL ANALYSE THE POST FLIGHT DATA DOWNLOAD TO TROUBLESHOOT.Jun 4, 2014 · Emb EMB500 · Engine (Turbine/Turboprop)SDR CA131105004Engine · unknown(CAN) DURING FLIGHT, THE ACFT ENCOUNTERED LIGHT RIME ICE CONDITION. ONCE ABOVE FL260, THE PILOT NOTICED THE ACFT WAS CLIMBING AT AN ANEMIC OR ZERO RATE. AFTER CROSSING FL290, THE PILOT NOTICED THAT THERE WAS A SIGNIFICANT DISCREPANCY BETWEEN BOTH ENGINES, TOOct 29, 2013 · Emb EMB500 · Engine (Turbine/Turboprop)SDR CA131007006Oil System · low pressureDURING FLIGHT, THE ENGINE OIL PRESSURE DROPPED, FORCING THE PILOT TO SHUT THE ENGINE DOWN. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGHT INSPECTION FOUND ENGINE EXTERNALS TO BE DRY BUT NO OIL ON THE SIGHT GLASS. THE ENGINE IS BEING REPLACED.Sep 25, 2013 · Emb EMB500 · Engine Oil PressureSDR CA130921001Oil System · fluctuates(CAN) OIL PRESSURE FLUCTUATIONS WERE FOLLOWED BY LOW OIL PRESSURE LIGHT AFTER THROTTLE BACK OF THE ENGINE. THE CREW ELECTED TO SHUTDOWN THE ENGINE. AN UNEVENTFUL SINGLE-ENGINE LANDING WAS ACCOMPLISHED.Sep 11, 2013 · Emb EMB500 · Engine Oil PressureSDR CA130819003Oil System · leaking(CAN) AFTER FLYING FOR .5 HOUR THE ENGINE NR 2 LOST OIL PRESSURE. THE PILOTS ELECTED TO SHUTDOWN THE ENGINE AND LANDED SAFELY. JUST BEFORE THE FLIGHT THE ENGINE OIL LEVEL WAS RECORDED TO BE 75 PERCENT AT THE SIGHT GLASS. THE ON GROUND INVESTIGATION REVEALED Aug 8, 2013 · Emb EMB500 · Turbine Engine Oil SystemSDR CA130805014Engine · faulted(CAN) DURING TAKEOFF ROLL, THE PILOT REPORTED E2 CONTROL FAULT AND ENGINE 2 FADEC FMU TORQUE MOTOR FAULTS. THE CREW ELECTED TO ABORT TAKEOFF. NO INJURIES REPORTED. EDCU MEMORY DOWNLOAD WAS SEND TO CFIRST. TROUBLESHOOTING ONGOING.Aug 1, 2013 · Emb EMB500 · Engine (Turbine/Turboprop)SDR CA130716003Tire · bulged(CAN) IN THE PAST MONTH WE HAVE REMOVED 2 MAIN WHEEL TIRES FROM ACFT FOR SIDEWALL AND TREAD BULGES. THE TIRES ARE 21 X 6.5 X 10, PN 215K26-1. THE FIRST TIRE WAS REMOVED FROM THE LT POSITION OF ACFT. TIRE: PN 215K26-1, SN 22712476, TSN 292.7. THE SECOND TIRJul 14, 2013 · Emb EMB500 · TireSDR CA130705005Heater · failed(CAN) ON ENGINE START CAS MESSAGE, SWPS HTR 2 FAIL, APPEARED. TROUBLESHOOTING REVEALED THE NR 2 AOA VANE HEATER HAS FAILED. NR 2 AOA VANE BASE ASSEMBLY TO BE REPLACED.Jul 5, 2013 · Emb EMB500 · Ice/Rain Protection SystemSDR CA130628007Hose · leaking(CAN) DURING POST FLIGHT INSPECTION FOUND LT MLG ACTUATOR RETRACTION LINE LEAKING. HOSE ASSEMBLY, PN A11011-1, REPLACED.Jun 26, 2013 · Emb EMB500 · Hydraulic System, MainSDR 2013FA0000315Anti-Skid Sys · failedSHORTLY AFTER TOUCHDOWN, ACFT DISPLAYED CAS ALERT "ANTISKID FAIL." PILOT APPLIED BRAKES AND AFTER DECELERATION, NOTED A VIBRATION CONSISTENT WITH FLAT OR LOCKED WHEEL. MX DOWNLOADED THE ACFT CENTRAL MX COMPUTER (CMC) AND FORWARDED THE FILES TO ENGINEERING. May 28, 2013 · N917MM · Emb EMB500 · Brake Anti-Skid SectionSDR K5SR2013041425122Cooling Fan · vibrationVAPOR CYCLE SYSTEM GROUND COOLING FAN DEVELOPED LOUD NOISE AND VIBRATION THAT WAS FELT AND HEARD IN CABIN. MX TROUBLESHOT AND FOUND THAT THE COOLING FAN ASSY HAD COME LOOSE INSIDE OF UNIT AND BANGED AROUND IN CASE. VAPOR CYCLE SYSTEM AND GROUND COOLING FAN INOApr 17, 2013 · N450JF · Emb EMB500 · Air Distribution FanSDR CA130415004Powerpack · failed(CAN) BRAKE FAIL CAS FOLLOWED BY HYD FAIL CAS DURING TAXI OUT. HYDRAULIC PRESSURE RETURNED, BUT BRAKE FAIL CAS REMAINED. ACFT TAXIED BACK TO CHOCKS. CMC/CVFDR DOWNLOADS PERFORMED. FORWARDED TO MFG ENGINEERS, SUGGEST REPLACEMENT OF HYDRAULIC POWER PACK.Apr 11, 2013 · Emb EMB500 · Hydraulic System, MainSDR CA130328003Pressure Switch · malfunctioned(CAN) DURING A TIGHT LT 180 DEGREE TURN, CREW NOTICED A REDUCTION IN LT BRAKE EFFECTIVENESS, ACFT ACCELERATED THEN EMERGENCY PARK BRAKE WAS ACTIONED TO STOP THE ACFT, THEN CREW WAS PRESENTED WITH A BRAKE FAIL CAS MESSAGE AND THE HYD PRESSURE WAS INDICATING ZERMar 24, 2013 · Emb EMB500 · Landing Gear Brake SystemSDR CA131105010Manifold · blocked(CAN) FUEL MANIFOLD DETERMINED TO EXHIBIT CARBON BLOCKAGE OF INTERNAL PASSAGES DISRUPTING FUEL FLOW TO INTEGRAL FUEL NOZZLES AND LIMITING MAXIMUM AVAILABLE FLOW. THIS RESULTS IN PRESSURE RELIEF VALVE ACTIVATION AND APR HEADROOM FAULT INDICATIONS. MFG IS INVESTMar 16, 2013 · Emb EMB500 · Engine Fuel DistributionSDR CA121206008Lead · failed(CAN) MOC RECEIVED A CALL FROM THE FLIGHT CREW. THE CREW REPORTED DURING THE START OF ENGINE NR 1 THERE WAS NO ITT INCREASE ABOVE 12 DEGREE DURING ROTATION. CREW RESET THE ACFT AND CYCLED THE IGNITION SWITCH TO OFF AND ATTEMPTED ANOTHER START. ON THE 2ND ATDec 3, 2012 · Emb EMB500 · Ignition System Wiring
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