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.

SDR AU961127Lever · broken(AUS) ENGINE FUEL CONTROL UNIT LEVER BROKEN OFF AT BASE - ENGINE RETURNED TO FLIGHT IDLE - SUSPECT PRE-EXISTING CRACK CAUSED BY IMPACTAug 6, 1996 · Emb EMB110P1 · Fuel Controlling SystemSDR AU961179Torque Tube · cracked(AUS) LH ELEVATOR TORQUE TUBE CRACKED FROM TAPER PLUG HOLES - FOUND DURING INSPECTION IAW SB110-027-0079Jul 9, 1996 · Emb EMB110P1 · Elevator Control SystemSDR AU961178Switch · faulty(AUS) LH MAIN LANDING GEAR DOWNLOCK MICROSWITCH FAULTY - FOUND DURING INSPECTION IAW AD/EMB110/42Jul 9, 1996 · Emb EMB110P1 · Landing Gear Retraction/Extension SystemSDR AU960818Actuator · faulty(AUS) LH MAIN LANDING GEAR DOWNLOCK ACTUATOR FAULTY - MICROSWITCH STRIKER NOT ACTIVATING MICROSWITCHJun 7, 1996 · Emb EMB110P1 · Landing Gear Retraction/Extension SystemSDR CA960625017Support · cracked(CAN) RIGHT AILERON BRACKET, CENTRE SUPPORT CRACKED ON CENTRE AILERON SPAR.Jun 6, 1996 · Emb EMB110P1 · AileronsSDR CA960620024Support · cracked(CAN) LEFT AILERON BRACKET, CENTRE SUPPORT CRACKED, ON CENTRE AILERON SPAR.Jun 6, 1996 · Emb EMB110P1 · AileronsSDR AU960680O-Ring · failed(AUS) LANDING GEAR HYDRAULC SYSTEM PRESSURE REDUCER VALVE 'O' RING SEAL FAILEDMay 16, 1996 · Emb EMB110P1 · Landing Gear Retraction/Extension SystemSDR 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 SEALMay 15, 1996 · Emb EMB110P1 · Hydraulic System, MainSDR AU960637Hose · ruptured(AUS) LH MAIN LANDING GEAR DOWNLOCK HOSE RUPTURED - LOSS OF HYDRAULIC FLUIDMay 15, 1996 · Emb EMB110P1 · Landing Gear Retraction/Extension SystemSDR 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 OVERSPEEDMay 1, 1996 · Emb EMB110P1 · Fuel Controlling SystemSDR BUHA2396001T Fitting · crackedLOSS OF HYDRAULIC PRESSURE DUE TO CRACKED T-FITTING. (X)Apr 25, 1996 · N34A · Emb EMB110P1 · Hydraulic System, MainSDR AU960473Wheel · failed(AUS) LH MAIN WHEEL TYRE RETAINING BEAD HAD SEPARATED FROM THE INNER WHEEL HALFApr 3, 1996 · Emb EMB110P1 · Wheel/Ski/FloatSDR 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.Apr 1, 1996 · Emb EMB110P1 · Landing Gear Retraction/Extension SystemSDR AU960408Motor · faulty(AUS) FLAP MOTOR ASSYMETRY WIRING BROKENMar 30, 1996 · Emb EMB110P1 · Trailing Edge Flap Control SystemSDR CA960311032Centering System · out of adjust(CAN)AFTER TAKEOFF PILOT COULD NOT SELECT GEAR UP. NOSE CENTERING SYSTEM ADJUSTMENT REQUIRED.Mar 4, 1996 · Emb EMB110P1 · Landing Gear Retraction/Extension SystemSDR AU960231Arm · cracked(AUS) LH ENGINE FUEL CONTROL UNIT (FCU) CONTROL ARM CRACKED AND FAILEDMar 3, 1996 · Emb EMB110P1 · Fuel Controlling SystemSDR AU960305Rod End · stiff(AUS) ENGINE FUEL CONTROL UNIT CONTROL ROD CONNECTOR ROD END STIFFFeb 1, 1996 · Emb EMB110P1 · Fuel Controlling SystemSDR AU960001Support · cracked(AUS) LANDING GEAR DOOR ACTUATOR SUPPORT ASSEMBLY CRACKED INTO THREE PARTS - DOOR ACTUATOR ROD PNO 110-2721-68-07 BENTJan 2, 1996 · Emb EMB110P1 · Landing Gear Door ActuatorSDR 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 INDICATIODec 13, 1995 · N110EM · Emb EMB110P1 · Cargo/Baggage DoorsSDR 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 Oct 15, 1995 · N621KC · Emb EMB110P1 · Rudder Control SystemSDR 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).Aug 11, 1995 · N621KC · Emb EMB110P1 · Main Landing Gear Strut/Axle/TruckSDR 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 THROJul 14, 1995 · N901FB · Emb EMB110P1 · Engine (Turbine/Turboprop)SDR 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 DJul 12, 1995 · N904FB · Emb EMB110P1 · Landing Gear Position and WarningSDR 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.Jul 3, 1995 · N216EB · Emb EMB110P1 · Landing Gear Door Retract SectionSDR 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.May 24, 1995 · N710NH · Emb EMB110P1 · Rudder Control SystemSDR 96ZZZX4695Hinge · crackedDURING ROUTINE 150-HOUR INSPECTION, FOUND LEFT AILERON CENTER HINGE CRACKED AT PIVOT BOLTS. CRACKED FROM ONE SIDE THROUGH THE OTHER.May 22, 1995 · N710NH · Emb EMB110P1 · Ailerons
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