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 RU92003F00000Squat Switch · failedON NOV. 13, 2002 GEAR FAILED TO RETRACT, SQUAT SWITCH FAILED. REPLACED SQUAT SWITCH. OPS CHECK, OK.SDR CA021115006Attach Angle · worn(CAN) DURING A SCHEDULED INSPECTION EVENT EXCESSIVE WEAR WAS NOTED AROUND THE BOLT HOLE OF THE UPPER RUDDER ATTACH BRACKET. THE RIVETS SECURING THE BUSHING BOSS IN THE BRACKET WERE ALSO WORKING.THE RUDDER ATTACH BRACKET ASSEMBLY PART NUMBER 4A-3441 WAS REPLACESDR CA021105007Starter Gen · failed(CAN) STARTER/GENERATOR SHAFT SHEARED WHILE MOTORING THE RT ENGINE FOR START. THE SHAFT BROKE AT 1/8 INCH BELOW THE SPLINE. INSTALLED NEW STARTER/GENERATOR ON RT ENGINE. GROUND RUN SERVICEABLE. AIRCRAFT RETURNED TO SERVICE.SDR CA021104007Extinguisher · loose(CAN) AT LAST FLIGHT OF THE DAY, PILOT NOTICED PRESSURE VERY LOW ON REAR CABIN HAND FIRE EXTINGUISHER AND REPORTED SNAG. UPON REMOVAL, MAINTENANCE PERSONNEL FOUND UNIT VERY LIGHT, AND PRESSURE ZERO. THE Q.A.CHECKED: BOTTLE LOOSELY UNSCREWED FROM HEAD. NOTE: SESDR CA021028004Torque Link · cracked(CAN) DURING A LANDING GEAR INSPECTION THE TECHNICAIAN FOUND THE CENTER POINT OF TORQUE LINK PART NUMBER 14470 CRACKED.SDR CA021101003Control Cable · frayed(CAN) AIRCRAFT AFTT: 22782.0 HOURS. CABLE FOUND FRAYED DURING INSPECTION OF ELEVATOR CABLE SYSTEM AS PER AD 82-09-08R2 AND SB 110-027-064-R2 AND C2 INSP SHEET, HENCE NECESSITY OF DISCONNECTING CABLES FOR PROPER INSPECTION. PULLEY MS 20220A2 ALSO REPLACED AS SHSDR CA021016037Switch · failed(CAN) GAP SHORT CAUSED BY POSSIBLE LOOSE AIR COLLECTOR WHEN OPEN/SHUT BY PASSENGER, COMING IN CONTACT WITH LIGHT ASSEMBLY. A SMALL PLASTIC TONGUE PROTRUDING FROM SWITCH TO ISOLATE N & P PROBES / LUGS ON SWITCH MAY HAVE BEEN BROKEN. POSSIBLE SIMPLY INSIDESDR CA020917004Case · cracked(CAN) DURING ROUTINE MAINTENANCE THE MAINTENANCE CREW NOTICED TWO SMALL CRACKS ON THE RT ENGINE GAS GENERATOR CASE. THESE CRACKS ARE LOCATED AT THE FIRE SEAL MOUNTING ANGLES. THE ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA020903002Fuel Nozzle · failed(CAN) AT TERMINATING A ROUTINE 7 DAYS INSPECTION ON THE AIRCRAFT, THE MECHANIC SPOTTED A ROUND DISCOLOURED 'DOT' ON THE ENGINE CASING, TWO FUEL NOZZLES WERE REMOVED TO INVESTIGATE WITH A BORESCOPE TO CONFIR M APPARENT DAMAGE IN THE FUEL COMBUSTION LINER. ENGINSDR CA020523009Clamp · loose(CAN) PILOT REPORTED THAT FLAPS WOULD NOT OPERATE WHEN SELECTED. MAINTENANCE CONFIRMED THE SNAG ON THE RAMP. INVESTIGATION REVEALED THAT THE AREA AROUND THE FLAP PROTECTION BOX, FLAP MOTOR AND ASSYMETRIC ASSEMBLY WAS VERY WARM. THESE ITEMS ARE LOCATED UNDER THSDR AUS20020875Hose · failed(AUS) HYDRAULIC HOSE FAILED IN AN AREA APPROXIMATELY 200MM (8IN) ALONGTHE LENGTH ALONG THE HOSE. LOSS OF HYDRAULIC FLUID. SUSPECT HOSEHAD SUFFERED SOME DISTRESS DURING ITS LIFE.SDR CA020605003Bracket · cracked(CAN) DURING A SCHEDULED INSPECTION THE UPPER RUDDER ATTACHMENT BRACKET WAS FOUND CRACKED.SDR CA020326011Hinge · cracked(CAN) THE PILOT REPORTED INTEMITTENT ELEVATOR CONTROL ABNORMALITY. INSPECTION REVEALED THAT THE RT OUTBOARD ELEVATOR HINGE POINT WAS CRACKED. THE EFFECTED PARTS WHERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR AUS20020236Duct · cracked(AUS) EXHAUST DUCT CONTAINED HAIRLINE CRACKS.SDR CA020222003Valve · leaking(CAN) 1) AN OVERHAULED PARKING BRAKE VALVE WAS INSTALLED TO REPLACE A UNIT "ROBBED" TO SERVICE ANOTHER AIRCRAFT. NOTE: AIRCRAFT HANGARED MORE THAN TWO (2) DAYS, THUS WARM FLUID AND SYSTEM. 2) OVERHAULED VALVE INSTALLED. 3) UPON FIRST PRESSURE TEST FOLLOWING ISDR CA011121014Downlock Switch · failed(CAN) DURING DESCENT INTO YMO THE CREW SELECTED GEAR DOWN AND DID NOT GET A LT MAIN GEAR DOWN AND LOCKED INDICATION. THE LANDING GEAR WAS CYCLED A FEW TIMES AND GEAR DOWN AND LOCKED WAS CONFIRMED WITH INDICATION OF DOWN AND LOCKED. AS A PRECAUTION THE CREW ELESDR CA011018013Boot · damaged(CAN) ON APPROACH A VIBRATION WAS FELT BY THE FLIGHT CREW. VISUAL INSPECTION BY THE FLIGHT CREW REVEALED THE OB LEFT HAND WING DEICE BOOT WAS RIPPED AND FLAPING AGAINST THE WING. THE AIRCRAFT LANDED WITH OUT INCIDENT, HOWEVER A PORTION OF THE DEICE BOOT SEPERASDR CA011029001Ball Joint · damaged(CAN) ON ROLL OUT FOLLOWING LANDING THE BALL JOIINT ASSEMBLEY PULLED OUT OF THE UPPER TORQUE LINK. THIS CAUSED THE RIGHT MAIN WHEEL TO TURN 180 DEGREES. REPAIRS REQUIRED THE REPLACEMENT OF BOTH THE UPPER TORQUE LINK AND THE BALL JOINT ASSEMBLYSDR CA011109014Fastener · sheared(CAN) DURING A 12C INSPECTION (7200 HOUR) MAINTENANCE PERSONNEL FOUND SEVERAL SHEARED HILOCKS ON THE LEFT HAND WING AT RIB NR 6.THE LEFT HAND LANDING GEAR WAS REMOVED AND AREA INSPECTED, NO STRUCTURAL DAMAGE WAS FOUND. 22 HILOCKS WERE REPLACED AND GEAR REINSTASDR CA010622037Light · sparks(CAN) CUSTOMER REPORTED SPARKS FROM LOOSE OVERHEAD LIGHT IN 7TH ROW, LEFT SIDE.SDR CA010621024Hose · blocked(CAN) BRAKES ON 4TH SIDE WERE REPORTED GRABBING AND OCCASSIONALLY NOT RELEASING PROPERLY. BRAKE UNIT, SHUTTLE VALVE AND BRAKE PRESSURE REDUCER WERE ALL REPLACED WITH NO SUCCESSFUL RESULT. IT WAS DISCOVERED THAT THE ABOVE BRAKE HOSE HAD DETERIORATED INSIDE AND SDR CA010504005Wheel · separated(CAN) WHILE TAXIING OFF RUNWAY AFTER LANDING LT MAIN WHEEL FAILED. APPROXIMATELY 12 INCHES OF BEAD SEAT SEPARATED FROM INBOARD WHEEL HALF INSTANTLY DEPRESSURIZING TIRE. AIRCRAFT TAXIED TO SAFE ZONE. MAINTENANCE REPLACED WHEEL ON TAXI WAY AND AIRCRAFT WAS RETURSDR CA010508015Line · cracked(CAN) DURING CLIMB, HYDRAULIC FLUID LOW LEVEL WARNING LIGHT ILLUMINATED. MANUAL GEAR EXTENSION PERFORMED, AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND A CRACKED HYDRAULIC LINE IN THE L/H MAIN WHEEL BAY HYDRAULIC LINE REPLACED, HYDRAULIC SYSTEM SERVICED. HYDRAULICSDR CA010411003Taper Pin · corroded(CAN) AIRCRAFT TT: 18965.4 HRS CYC: 24946 PART TT: APP. 7200 HRS. IF REPLACED AT LAST C12 INSP. TAPER PIN CONE BUSHINGS ALSO AFFECTED. PIN DID NOT COME OUT WITH MANUFACTURERS SPECIAL TOOL PRESS. NEW PINS AND CONES REQUIRED. PIN HAD TO BE DRILLED AND CUT BY MASDR CA010222007Light · failed(CAN) IN FLT AFTER LEVELING OFF AT 9000 ODOUR STARTED COMING FROM HEATING VENTS. CREW OPTED TO SHUT AIR-COND SYS OFF TO FIND OUT WHERE SMELL COMING FROM. AT SAME TIME CREW CHECKED OP OF SMOKE ALARMS. THEY FUNCTIONED NORMALLY. CREW HAD THOUGHT THAT GLYCOL COULDSDR AU010224Relief Valve · contaminated(AUS) RT ENGINE OIL PRESSURE RELIEF VALVE CONTAMINATED BY A PIECE OF O-RING SEAL.SDR AU010191Engine · damaged(AUS) ENGINE SKI JUMP SEVERELY CRACKED AND DISTORTED IN AREA AROUND NR 3 BEARING COVER. SOME PIECES OF THE EXHAUST CASING HAVE COMPLETELY BROKEN AWAY CAUSING DAMAGE TO THE POWER TURBINE DISC AND BLADES. POWER TURBINE STATOR CRACKED THROUGH THE INNER BAND.SDR CA001214016Bracket · cracked(CAN) THE HORIZONTAL STABILIZER UPPER AND LOWER SKIN AT THE RIGHT HAND ELEVATOR ATTACH BRACKET WERE FOUND DENTED AND CRACKED. THE DAMAGED AREA WAS OUT AWAY AND REPAIRED BY INSTALLING AN INNER SPLICE PLATE AND AN EXTERNAL DOUBLERS PLATE PATCH OF 2024T3 ALUMINUMSDR CA001005008Pin · broken(CAN) BROKEN PIN HEAD ON ADJUSTER ASSEMBLY. CAUSED ADJUSTER TO LOOSEN.SDR AU000760Wheel · cracked(AUS) LT MAIN WHEEL INNER HALF CRACKED IN THE TIRE BEAD SEAT AREA RESULTING IN A SECTION BREAKING AWAY AND CAUSING THE TIRE TO DEFLATE.SDR AU000556Bracket · cracked(AUS) NOSE LANDING GEAR ACTUATOR SUPPORT BRACKET CRACKED. CRACK LENGTH28.5MM (1.125IN). FOUND DURING INSPECTION IAW SB 110-53-0027. CRACK COULD BE SEEN VISUALLY.SDR CA000719029Bolt · sheared(CAN) A/C ON LANDING ROLLOUT PULLED TO R/H WHEN STOPPED. RT GEAR 90 DEGS TO DIRECTION OF FLT. MAINT HALF OF P/N 16469 CENTRE TORQUE LINK BOLT STILL IN PLACE. REPLACED BOLT FERRIED A/C TO MAINBASE. INSP CARRIED OUT USING MAINTENANCE MANUAL & 625 APPENDIX G. ABNSDR CA000621022Gear · failed(CAN) PILOT REPORTED A WOBBLY NOSE GEAR SHIMMY ON LANDING ROLL-OUT WITH LIMITED RT TURNING CAPACITY. MAINTENANCE FOUND TEETH MISSING OFF THE SECTOR GEAR JAMMING ON THE RACK FOR LIMITED TRAVEL WITH A GAP IN THE CENTER CAUSING THE SEVERE SHIMMY. THE GEAR WAS SDR 20000620SH029Seal · leakingGARLOCK SEAL FAILED CAUSING OIL TO DRAIN IN REAR OF ACCESSORY CASE. OIL THEN GOING FORWARD INTO COMPRESSOR AND DRAINING ON RAMP. (X)SDR AU000319Hinge · corroded(AUS) RIGHT ELEVATOR CENTER HINGE CORRODED.SDR AU000318Hinge · corroded(AUS) CENTER RUDDER HINGE BRACKET CORRODED BEYOND REPAIR.SDR CA000331010Line · cracked(CAN) FUEL LINE CRACK AT B-NUT FOUND TO BE THE CAUSE OF FUEL ODOR, AT FCU. FEEDBACK.SDR AU000321Hinge · corroded(AUS) RT AILERON INBOARD HINGE CORRODED.SDR AU000320Bellcrank · corroded(AUS) LEFT AND RIGHT ELEVATOR BELLCRANKS PN 4A-3224-02 (LT) AND PN 4A-3214-02 (RT) AND BELLCRANK STOPS PN 110-3010-26 AND PN 110-3010-27 CORRODED.SDR AU000317Control Cable · corroded(AUS) AFT ELEVATOR CABLES (4 OFF) AND AFT RUDDER CABLES CORRODED IN THE AREA LOCATED BETWEEN FRAME 19 AND FRAME 21.SDR AU000316Seat · cracked(AUS) CABIN SEAT LEGS DEFORMED AND CRACKED IN THE AREA OF ATTACHMENT TO THE MAIN SEAT TUBE.SDR AU000315Seat Track · corroded(AUS) ALL CABIN SEAT TRACKS SEVERELY CORRODED.SDR AU000314Fitting · worn(AUS) ELEVATOR TRIM FITTING AND HINGE HAD EXCESSIVE PLAY. FURTHER INVESTIGATION FOUND THE TRIM FITTING CRACKED.SDR AU000313Fitting · corroded(AUS) LEFT INBOARD NACELLE TO FORWARD SPAR ATTACHMENT CASTING UPPER LUG CORRODED IN THE AREA AROUND HI-LOC FASTENER.SDR AU000312Control Cable · worn(AUS) RIGHT WING FORWARD INBOARD AILERON CABLE AND LEFT WING AFT INBOARD AILERON CABLE SEVERELY ERODED IN THE AREA WHERE THEY EXIT THE FUSELAGE.SDR AU000308Structure · misrepaired(AUS) STRUCTURE AT THE BASE OF THE COPILOT''S CONTROL COLUMN CUT AND GROUND AWAY IN THE AREA OF THE ELEVATOR PUSH-PULL ROD ATTACHMENT. UNAPPROVED MODIFICATION. .SDR AU000092Switch · intermittent(AUS) RIGHT MAIN LANDING GEAR DOWNLOCK MICROSWITCH INTERMITTENT IN OPERATION.SDR CA000218012Support Bracket · cracked(CAN) DURING CRUISE, CREW HEARD A KNOCKING SOUND ACCOMPANIED BY A NOISE THAT PULSATED LOUDER AS AIRSPEED INCREASED. AFTER LANDING, CREW NOTICED RT INBOARD MLG DOOR HAD PULLED FREE OF THE DOOR ROD. THE DOOR ROD RECEIVING BALL HAD PULLED THROUGH THE SUPPORT ASSSDR CA991116003Pump · failed(CAN) RIGHT HYDRAULIC PUMP FAILED AFTER TAKEOFF. PUMP REPLACED. LINES FLUSHED, FILTERS REPLACED.SDR CA991103069Bearing · failed(CAN) OIL FOUND CONTAMINATED, SUSPECT NR 1 BEARING.
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