Embraer EMB-110P1
Service difficulty reports · 176
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 = 'EMB110P1' 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 = 'EMB110P1' 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 CA991007069Wire · shorted(CAN) DURING FLIGHT, PILOT REPORTED SMOKE AROUND MASTER COMPASS AND LOSS OF OTHER LIGHTING IN THE COCKPIT. COMPASS LIGHT WIRES FOUND SHORTED AT CONNECTOR AND INSULATION BURNT. CIRCUIT BREAKER DID NOT TRIP.SDR CA991209087Switch · out of adjust(CAN) AFTER TAKEOFF WHEN GEAR SELECTED UP, CREW DIDN'T GET NOSE GEAR UP INDICATION THAT THE NOSE GEAR HAD MOVED. GEAR CYCLED WITH NO INDICATION. RETURNED HANDL E TO DOWN POSITION WITH 3 GREEN LIGHTS. NOSE GEAR CENTERING ACCUMULATOR WAS BELOW MINIMUM PRESSUSDR AU990721Rib · corroded(AUS) RIGHT WING INBOARD RIB CORRODED IN THE AREA BETWEEN THE FRONT AND REAR SPARS. FOLLOWING REMOVAL OF THE RIB A SMALL AMOUNT OF INTERGRANULAR/FILIFORM CORROSION WAS FOUND ON THE REAR SPAR WEB UNDER THE STAINLESS STEEL SHIMS LOCATED BETWEEN THE RIB REAR FLASDR AU990796Accumulator · faulty(AUS) NOSE LANDING GEAR CENTERING ACCUMULATOR FOUND TO HAVE NIL CHARGE.SDR CA990812012Bolt · striped(CAN) REMOVAL OF CT BOLT AT FIRST HSI DIFFICULT TO REMOVE. THREADS PULLED FROM END OF BOLT, WHICH WAS A POST SB 1439R2 BOLT.SDR AU990797Rod · broken(AUS) NOSE LANDING GEAR DOOR ROD BROKEN.SDR AU990704Fcu · faulty(AUS) FUEL CONTROL UNIT SUSPECT FAULTY.SDR AU990372Fire Detector · broken(AUS) LEFT ENGINE FIRE DETECTOR LOCATED IN THE COMPRESSOR INLET AREA FOUND TO HAVE A FAULTY TERMINAL POST (POST BROKE WHEN THE WIRE WAS REMOVED). SUSPECT MOISTURE INGRESS CAUSED A SHORT CIRCUIT CAUSING THE FIRE WARNING TO ACTIVATE.SDR AU990363Fire Detector · contaminated(AUS) LEFT ENGINE FIRE WARNING DETECTORS CONTAMINATED WITH MOISTURE. AIRCRAFT FLEW THROUGH LIGHT RAIN.SDR AU990362Fire Detector · contaminated(AUS) LEFT ENGINE FIRE DETECTORS CONTAMINATED WITH MOISTURE.SDR CA990318073Window · leaking(CAN) GLYCOL PENATRATED CABIN WINDOW SOAKING INSULATION. WHEN HEATER APPLIED, VAPORS VISIBLE ON INTERIOR. WINDOW RESEALED AND INSULATION REPLACED.SDR 20000424AP042Wheel · crackedWHILE REPORTING FROM UPS RAMP TO FBO RAMP IN BUF A GRINDING NOISE WAS HEARD WHEN TURNING AIRCRAFT WHILE TAXIING. THE NOSE WHEEL HALF BROKE LEAVING THE AXLE BOLT AND TWO WHEEL BEARINGS ON THE AXLE. BEARINGS WERE FOUND TO BE CORRODED. PROBABLE CAUSE, FREQUENTSDR CA990115012Accumulator · leaking(CAN) WHEN GEAR SELECTED UP AFTER TAKEOFF, ALL BUT THE NOSE GEAR INDICATED UP AND LOCKED. DOWN SELECTION MADE AND ALL GREENS. CREW RETURNED AND LANDING OK. THE NOSE LANDING GEAR CENTERING ACCUMULATOR FOUND LOW IN NITROGEN BECAUSE OF A LEAKING SCHRAEDER VALVSDR CA981230036Actuator · cracked(CAN) FLAP ACTUATOR DUST COVER FOUND DAMAGED. NO REPORTED FLAP OPERATION SNAGS. PART TC: 5,015.SDR CA981216006Lamp Socket · failed(CAN) SHORTLY AFTER TAKEOFF, THE CREW REPORTED A SMELL OF BURNING ELECTRICAL INSULATION, WITH A STRONGER SMELL IN CABIN. AIRCRAFT RETURNED TO BASE. INVESTIGATION FOUND THAT THE FLUORESCENT LIGHT SOCKET IN THE CARGO AREA HAD COME APART CAUSING IT TO SHORT OUTSDR CA981209001O-Ring · failed(CAN) PILOT SHUT DOWN NR 2 ENGINE DUE TO LOW OIL PRESSURE. POST-FLIGHT INSPECTION FOUND OIL LEAKING FROM THE OIL PRESSURE TUBE AT THE C-FLANGE, WHEN THE ENGINE WAS BEING MOTORED. THE OIL PRESSURE TUBES WERE REMOVED AND INSPECTED FOR DAMAGE. THE TUBES WERE RESDR CA981209005Control Cable · worn(CAN) TRIM JAMMED BELOW NEUTRAL POSITION, TRIM WORKS FROM NEUTRAL TO NOSE DOWN. DURING REPLACEMENT OF TELEFLEX CABLE, FOUND BOX TRANSMISSION GEAR LOOSE, TRANSMISSION REPLACED AND SYSTEM RIGGED. IT WAS DETERMINED THAT THE WEAR ON THE CABLE AT THE TRANSMISSIONSDR AU981450Switch · failed(AUS) NOSE LANDING GEAR UPLOCK MICROSWITCH FAULTY.SDR AU981353Shaft · broken(AUS) ENGINE FUEL CONTROL UNIT THROTTLE SHAFT BROKEN AT THE CAM.SDR 99ZZZM286Latch · wornBUFFALO-BINGHAMTON - WHILE EN ROUTE THE FLIGHT CREW DIVERTED TO ROCHESTER NY AFTER EXPERIENCING RIGHT ENGINE TORQUE FLUCTUATIONS. AFTER LANDING, THE CREW DISCOVERED THE RIGHT ENGINE TOP COWL HAD BECOME PARTIALLY UNLATCHED. THE ENGINE INLET WAS INSPECTED AND SDR CA981001002Blower · shorted(CAN) CREW REPORTED SMOKE IN THE CABIN AND CREW SHED UNNECESSARY ELECTRICAL LOADS. SMOKE DISSIPATED. AIRCRAFT LANDED OK. BLOWER MOTOR FOUND SHORTED.SDR CA980827010Bleed Valve · sticking(CAN) PILOT REPORTED NR 2 ENGINE PARAMETERS BEGAN TO FLUCTUATE DURING SHORT FINAL. POST-FLIGHT INSPECTION FOUND THE COMPRESSOR BLEED VALVE STICKING. THE VALVE WAS REPLACED AND THE ENGINE WAS GROUND RUN SERVICEABLE.SDR CA980825010Switch · out of adjust(CAN) ON APPROACH, GEAR SELECTED DOWN AND DID NOT RECEIVE GREEN DOWN AND LOCKED FOR THE RIGHT HAND MAIN. GEAR CYCLED AND WAS OK. GEAR MICROSWITCH FOUND OUT OF ADJUSTMENT.SDR AU980945Switch · sticking(AUS) RIGHT MAIN LANDING GEAR MICROSWITCH STICKING.SDR AU980761Fitting · cracked(AUS) HYDRAULIC PUMP PRESSURE SYSTEM ALUMINUM `T' FITTING LOCATED ON LT FIREWALL CRACKED. FITTING HAS AN INTERNAL FLARE SEAL. LOSS OF HYDRAULIC FLUID. PART TOTAL CYCLES: 18,318.SDR 98ZZZX3396Pump · failedAT APPROXIMATELY 6:30 P.M. ON 6-25-98 WHILE EN ROUTE TO SYRACUSE, THE LT HYD SYSTEM PRESSURE DROPPED TO ZERO PSIG. A NORMAL LANDING ACCOMPLISHED AT SYRACUSE. THE HYD SYS FILTER AND PRESSURE AND SUCTION LINES WERE EXAMINED FOR METAL. NONE FOUND. THE LT PUMPSDR AU980946Py Line · cracked(AUS) ENGINE PY LINE CRACKED AT END FITTING FERRULE.SDR CA980318046Uplock Switch · failed(CAN) ON PREFLIGHT CREW NOTICED THE GEAR INTRANSIT LIGHT ON AS WELL AS THE THREE GREENS. THE RIGHT HAND UPLOCK SWITCH HAD FAILED.SDR AU980293Channel · cracked(AUS) FUSELAGE LT UPPER HORIZONTAL STABILIZER SUPPORT ATTACHMENT CHANNEL CRACKED THROUGH TWO BOLT HOLES. FURTHER INVESTIGATION FOUND SEVERE FRETTING ON THE LT CHANNEL TO REAR BULKHEAD ATTACHMENT FACE.SDR 98ZZZM444Bracket · crackedELEVATOR TRIM TAB ACTUATOR SUPPORT, PART NR 110-3210-04, FOUND CRACKED DURING INSPECTION PER AD 91-25-09. BRACKET WAS REPLACED. (M)SDR AU980058Bus Bar · failed(AUS) RH ENGINE T5 BUS BAR LUG BROKEN OFF.SDR AU980089Switch · failed(AUS) LH MAIN LANDING GEAR DOWN MICROSWITCH FAULTY.SDR AU980195Cover · misinstalled(AUS) NO2 BEARING COVER INCORRECTLY SEATED. PERSONNEL/MAINTENANCE ERROR.SDR 98ZZZM443Bracket · crackedAT FRAME STATION 33, LEFT FORWARD UPPR SUPPORT BRACKET, P/N 110-1411-07-31, FOUND CRACKED DURING DYE PENETRANT INSPECTION PER AD 83-14-09. CRACK EXTENDED APPROXIMATELY .125 INCH THROUGH .1875 INCH FROM BOLT HOLE. BRACKET WAS REPLACED.SDR AU980006Bleed Valve · malfunction(AUS) LH ENGINE BLEED VALVE DIRTY CAUSING THE BLEED VALVE TO STICK WHEN CLOSING RESULTING IN COMPRESSOR STALLS. AIRCRAFT OPERATES FROM UNSEALED AIRSTRIPS.SDR 98ZZZX217Wire Terminal · brokenWHILE ON SHORT FINAL, LEFT FIRE WARNING ILLUMINATED. MAINTENANCE INSPECTED AND FOUND BROKEN WIRE AT TERMINAL END AT OUTBOARD FORWARD THERMOCOUPLE. REPLACED TERMINAL END SYSTEM. OPS CHECKED OK.SDR CA971216044Guide · missing(CAN) TAXIING TO RAMP, PILOT NOTICED UNVEVEN BRAKING ON ONE SIDE. THE GUIDE, WHICH IS NORMALLY ATTACHED TO THE CIRCUMFERENCE OF THE DISC WAS MISSING AND THE DISC WAS SCORED. SUBMITTER NOTES THAT SOMETIMES THE SCREWS WHICH ATTACH GUIDE TO DISC HAVE BEEN FOUNDSDR 97ZZZX3374Wheel · crackedLEFT MLG INBOARD WHEEL HALF, BEAD AREA BROKE OFF (80 PERCENT). A PIECE OF WHEEL HIT PROPELLER CAUSING LEFT PROPELLER BLADE DAMAGE.SDR CA970624008Exhaust Duct · cracked(CAN) DURING ROUTINE MAINTENANCE, WHEN THE EXHAUST STACKS WERE REMOVED, A PIECE OF THE EXHAUST DUCT WAS FOUND MISSING AND THE REMAINDER WAS CRACKED. MAINTENANCE INSTALLED AN IMPROVED EXHAUST DUCT ASEEMBLY AS PER SERVICE BULLETIN 1430.SDR 97ZZZX3340Bellcrank · crackedLEFT ELEVATOR BELLCRANK CRACKED ON FLANGE. CRACK CAUSED BY TELEFLEX CABLE BOUNCING ON FLANGE AREA. THIS BELLCRANK WAS REPLACED. REPOSITIONED CLAMP FOR TELEFLEX CABLE.SDR AU970657Switch · incorrect wired(AUS) LH MAIN LANDING GEAR DOWNLOCK SWITCH FAULTY - FAILED INSULATION TEST IAW SB/110/32-0052 REV3 - INVESTIGATION FOUND THAT THE SWITCH HAD BEEN WIRED DIRECTLY INTO THE LOOM INSTEAD OF THROUGH THE PLUG - THE WIRING SPLICES HAD EVENTUALLY CORRODED CAUSING CRACSDR 97ZZZM872Bracket · crackedRIGHT AILERON CENTER HINGE BRACKET WAS FOUND CRACKED AT HOLE FOR MOUNTING TO WING. REPLACED HINGE BRACKET.SDR CA970521004Bolt · sheared(CAN) AFTER TAKEOFF THE PILOT REPORT GEAR WOULD NOT RETRACT. VISUAL INDICATED THAT RH MAIN LANDING GEAR WAS CANTED. AIRCRAFT LANDED OK. TORQUE LINK BOLT FOUND SHEARED. SUBMITTER SUSPECTS FAILURE CAUSED BY GAS BUBBLE IN BOLT. BOLT SENT TO LAB FOR ANALYSIS.SDR AU970473Hose · leaking(AUS) MAIN LANDING GEAR DOWNLOCK HOSE LEAKING FROM FITTINGSDR AU970268Selector Switch · broken(AUS) AFTER TOUCH DOWN THE COPILOTS KNEE ACCIDENTLY BROKE THE FLAP SELECTOR LEVER - INVESTIGATION LATER FOUND THE LEVER EXCESSIVELY WORN AND WEAKENED DUE TO THE CONTINUAL SLIDING CONTACT WITH THE DETENT PLATESDR AU970136Hydraulic System · contaminated(AUS) LANDING GEAR HYDRAULIC SYSTEM CONTAMINATED WITH AIRSDR AU970079Wiper Arm · bird strike(AUS) AIRCRAFT SUFFERED BIRDSTRIKE - IMPACT DAMAGE ON NLG LEG AND IN AREA OF COPILOTS WINDSCREEN WIPER ARM ACTUATOR POST RESULTING IN MINOR BENDING OF THE WIPER ARM - NIL OTHER DAMAGESDR AU970088Support · cracked(AUS) WING FLAP SUPPORT ASSEMBLY CRACKED - FOUND DURING INSPECTION IAWOSIP 2706 - SUSPECT ORIGINAL FITMENT PNO 4A-2621-46SDR CA970107004Reducing Valve · out of adjust(CAN) ON TAKEOFF LANDING GEAR SELECTED TO RETRACT. RED IN TRANSIT LIGHT WOULD NOT GO OUT. GEAR LEVER TO EXTEND AND THREE GREEN INDICATED. PRESSURE REDUCING VALVE FOUND TO BE LOW AT 1300 PSI. VALVE ADJUSTED TO 1400+/-50 PSI.SDR CA961203014Rods · mis adjusted(CAN) ON TAKEOFF GEAR SELECTED UP. GEAR INSTRANSIT LIGHT REMAINED ON. INSPECTION FOUND THAT THE NOSE LANDING GEAR DOOR WERE ADJUSTED TOO TIGHT AND WITH THE AIR LOADS IN FLIGHT WOULD PULL GEAR DOWN ENOUGH TO BREAK THE UP SWITCH GIVING THE INTRANSIT LIGHT. DOOR
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