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 AU961127Lever · broken(AUS) ENGINE FUEL CONTROL UNIT LEVER BROKEN OFF AT BASE - ENGINE RETURNED TO FLIGHT IDLE - SUSPECT PRE-EXISTING CRACK CAUSED BY IMPACTSDR AU961179Torque Tube · cracked(AUS) LH ELEVATOR TORQUE TUBE CRACKED FROM TAPER PLUG HOLES - FOUND DURING INSPECTION IAW SB110-027-0079SDR AU961178Switch · faulty(AUS) LH MAIN LANDING GEAR DOWNLOCK MICROSWITCH FAULTY - FOUND DURING INSPECTION IAW AD/EMB110/42SDR AU960818Actuator · faulty(AUS) LH MAIN LANDING GEAR DOWNLOCK ACTUATOR FAULTY - MICROSWITCH STRIKER NOT ACTIVATING MICROSWITCHSDR CA960625017Support · cracked(CAN) RIGHT AILERON BRACKET, CENTRE SUPPORT CRACKED ON CENTRE AILERON SPAR.SDR CA960620024Support · cracked(CAN) LEFT AILERON BRACKET, CENTRE SUPPORT CRACKED, ON CENTRE AILERON SPAR.SDR AU960680O-Ring · failed(AUS) LANDING GEAR HYDRAULC SYSTEM PRESSURE REDUCER VALVE 'O' RING SEAL FAILEDSDR AU960639Seal · distorted(AUS) RH MAIN LANDING GEAR DOOR DROPPED INTO AIRFLOW - INVESTIGATION FOUND PRESSURE SIDE HYDRAULIC SERVICE COUPLING LEAKING UNDER PRESSURE DUE TO FLATTENED 'O' RING SEALSDR AU960637Hose · ruptured(AUS) LH MAIN LANDING GEAR DOWNLOCK HOSE RUPTURED - LOSS OF HYDRAULIC FLUIDSDR AU960994Coupling · sheared(AUS) RH ENGINE DRIVEN FUEL PUMP TO FCU DRIVE COUPLING SHEARED - SUSPECT CAUSED BY FAILURE OF FCU FRONT BEARING - ENGINE SUFFERED A MAJOR OVERTEMPERATURE, OVERTORQUE AND OVERSPEEDSDR BUHA2396001T Fitting · crackedLOSS OF HYDRAULIC PRESSURE DUE TO CRACKED T-FITTING. (X)SDR AU960473Wheel · failed(AUS) LH MAIN WHEEL TYRE RETAINING BEAD HAD SEPARATED FROM THE INNER WHEEL HALFSDR AU960409Cylinder · cracked(AUS) NOSE LANDING GEAR ROTATING CYLINDER CRACKED ON RH SIDE UPPER WELDED AREA - CRACK LENGTH 15MM (0.59IN) - TWO SMALLER CRACKS WERE ALSO FOUND IN THE SAME AREA - FOUND DURING INSPECTION IAW SB110-032-0053 REV 7 PT 2 PARA 2.2.6.SDR AU960408Motor · faulty(AUS) FLAP MOTOR ASSYMETRY WIRING BROKENSDR CA960311032Centering System · out of adjust(CAN)AFTER TAKEOFF PILOT COULD NOT SELECT GEAR UP. NOSE CENTERING SYSTEM ADJUSTMENT REQUIRED.SDR AU960231Arm · cracked(AUS) LH ENGINE FUEL CONTROL UNIT (FCU) CONTROL ARM CRACKED AND FAILEDSDR AU960305Rod End · stiff(AUS) ENGINE FUEL CONTROL UNIT CONTROL ROD CONNECTOR ROD END STIFFSDR AU960001Support · cracked(AUS) LANDING GEAR DOOR ACTUATOR SUPPORT ASSEMBLY CRACKED INTO THREE PARTS - DOOR ACTUATOR ROD PNO 110-2721-68-07 BENTSDR 96ZZZX145Door · openedAFTER TAKEOFF, THE AFT CARGO DOOR CAME OPEN CAUSING THE CARGO DOOR LINING TO COME OFF AND THE AIRCRAFT TO BUFFET. THE DOOR WAS CHECKED SECURE AT PRE-FLIGHT AND THE 'DOOR OPEN' CAUTION LIGHTS ON THE PILOT'S PANEL WERE CHECKED PRIOR TO TAKEOFF WITH NO INDICATIOSDR 95ZZZX6124Hinge · looseDURING FLIGHT, PILOT REPORTED SEVERE VIBRATION FROM RUDDER. UPON INSPECTION, FOUND UPPER RUDDER HINGE CRACKED WHERE BOLT PASSES THROUGH TOP AND BOTTOM. RUDDER TRIM TAB HINGE WHERE ACTUATOR ARM ATTACHES WAS FOUND LOOSE (WORKING CHERRYMAX RIVETS). THIS DAMAGE SDR 95ZZZX6102Torque Link · brokenRT MLG UPPER TORQUE LINK FAILED AT CENTER PIVOT POINT. THIS WAS CAUSED BY A LOCKING PIN FAILURE (ITEM 66A) AND (ITEM 67A).SDR ASOA95017Engine · failedDFW/TXK - FLT 7457 - AFTER TAKEOFF, RIGHT ENGINE AUTO SHUT DOWN. FLIGHT RETURNED TO DFW WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. ENGINE WAS CONFIRMED TO HAVE LOST SOME PIECES WHICH EXITED THROUGH THE EXHAUST AND BURNER CANS. NO PIECES EXITED THROSDR ASOA95016Switch · out of adjustSPS/DFW - FLT 7455 - DURING APPROACH FROM SPS/DFW, THE CREW REPORTED THE RIGHT MAIN GEAR LIGHT WAS SLOW TO ILLUMINATE AND REQUESTED EMERGENCY VEHICLES TO STAND BY DURING LANDING. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT AT DFW. ADJUSTED RIGHT MAIN GEAR DSDR 96ZZZX5267Rod Assy · detachedAFTER SELECTING GEAR, GEAR UNSAFE LIGHT REMAINED ON. INSPECTION REVEALED NOSE GEAR DOOR LINKAGE ROD END DETACHED FROM BELLCRANK BALL JOINT. INSPECTED ROD END AND BALL JOINT. NO DEFECTS NOTED. PERFORMED GEAR RETRACTION TEST THROUGH 10 FAULT FREE CYCLES.SDR 95ZZZX3153Bushing · crackedWHEN C/W SB 110-027-0080, RUDDER PEDAL PIVOT BUSHINGS, FOUND ALL 8 BUSHINGS ON PILOT'S SIDE WITH CRACKS, 2 OF THESE BUSHINGS WERE BROKEN IN HALF. TIME ON PARTS UNKNOWN. ACFT TT: 14,778.1 HOURS. P/N OF BUSHINGS: PE64004-2.SDR 96ZZZX4695Hinge · crackedDURING ROUTINE 150-HOUR INSPECTION, FOUND LEFT AILERON CENTER HINGE CRACKED AT PIVOT BOLTS. CRACKED FROM ONE SIDE THROUGH THE OTHER.
Back to Embraer EMB-110P1