N36911
Service difficulty reports · 21
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N36911' AND registry_match = 'registration' 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 n_number = 'N36911' AND registry_match = 'registration' 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 HYIA20220405001Rib · crackedWHILE PERFORMING THE SID 57-10-25 INSPECTION, THREE CRACKS WHERE IDENTIFIED IN THE RIGHT CLOSE-OUT RIB (P/N 5122155-56.) THESE CRACKS WERE FOUND ON THE FORWARD ROW OF AT THE REAR TRUNNION PLATE ATTACH POINT. THERE ARE 6 HI-LOK HOLES ALIGNED VERTICALLY IN THSDR HYIA20210625001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT SIDE OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY .097 LONG AND IS CONSISTENT WITH OTHER CRACKS FOUND USING THE LIGHTED BORESCOPE INSPECTION TESDR HYIA20181130001Crankshaft · fracturedPILOT REPORTED DURING CLIMB/CRUISE FLIGHT THE RIGHT HYDRAULIC FLOW LIGHT CAME ON AND RIGHT ENGINE LOST POWER. UPON INITIAL INSPECTION, THE ENGINE WAS FOUND TO BE SEIZED. PISTONS AT CYLINDERS 1-4 WERE FOUND TO BE IN THE TOP DEAD CENTER POSITION. CYLINDER #3 WSDR HYIA20170828002Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK IS APPROXIMATELY 1.208 INCHES IN LENGTH. OPENSDR HYIA20170828001Fitting · crackedWHILE CONDUCTING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS APPROXIMATELY 1.208 INCHES IN LENGTH.SDR HYIA201611081840Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20161108183Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160104001O-Ring · wornPILOT REPORTED NO RT BRAKE. INSPECTED & FOUND THE RT MASTER CYLINDER INTERNAL O RING WORN. REPLACED O RING IAW MM CH 32-40-01. OPERATIONALLY CHECKED GOOD.SDR HYIA20140624003Dimmer · malfunctionedSMOKE APPEARED FROM INSTRUMENT PANEL LIGHT, DIMMER ASSEMBLY. R & R DIMMER ASSEMBLY PN 5118424-1.SDR HYIA2012043002Spar Cap · fracturedDURING ROUTINE MX, A FRACTURE WAS FOUND IN 1 OF OUR ACFT LOCATED AT THE, RT WING AFT LOWER SPAR CAP, INBD FLAP WELL, AND ADJACENT TO LWR BELL CRANK SUPPORT AT WING STA 113.69.SDR HYIA36911KG102311Gyro · shortedCREW REPORTED, WHILE IN CRUISE CONFIGURATION, IFR CONDITIONS, CAPTAINS HEADING INDICATOR FAILED, REMOTE GYRO CIRCUIT BREAKER TRIPPED. EMERGENCY DECLARED, LANDING WAS UNEVENTFUL. MX INSPECTED ACFT, FOUND REMOTE GYRO CONTAMINATED WITH WATER. R & R GYRO, TESTED SDR HYIA36911RHAXLEAxle · crackedON TAXI, CREW REPORTED LOAD "POP" FROM RT GEAR, ACFT BECAME DIFFICULT TO TAXI. MX FOUND RT MAIN GEAR AXLE ASSY CRACKED AT LOWER HALF. R & R AXLE ASSY. RELEASED ACFT BACK TO SERVICE.SDR HYIA36911100709Ground Wire · brokenON APPROACH TO PVC FROM BOS, PILOT REPORTED RIGHT MAIN GEAR DOWNLOCK LIGHT DID NOT ILLUMINATE, PERFORMED EMERGENCY GEAR EXTENSION, STILL DID NOT ILLUMINATE.PRESS TO TEST OF LIGHT CHECKED OK. PILOT ELECTED TO DIVERT. DECLARED AN EMERGENCY, LANDED WITHOUT INCIDSDR HYIA3691193009Torque Tube · crackedDURING SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND PILOTS LEFT RUDDER PEDAL TO TORQUE TUBE LINKAGE CRACKED. MAINTENANCE REMOVED AND REPLACED RUDDER TORQUE TUBE. AIRCRAFT RELEASED TO SERVICE.SDR HYIA36911 625Master Switch · unserviceableCREW REPORTED AVIONIC MASTER SWITCH INOPERATIVE. MX REMOVED AND REPLACED SWITCH AND RETURNED ACFT TO SERVICESDR HYIA36911Gyro · malfunctionedCREW REPORTED HORIZONTAL SITUATION INDICATOR INOPERATIVE IN CLIMB-OUT AT 400 FT. CONTACTED LOCAL TOWER, DECLARED AN EMERGENCY, AND RETURNED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED REMOTE GYRO. AIRCRAFT RELEASED BACK TO SERVICESDR 1356911120307Actuator · intermittentNOSE GEAR DOWN AND LOCKED LIGHT CAME ON AND THEN WENT OFF DURING FINAL APPROACH. BLEW GEAR DOWN TESTED GEAR DOWN INDICATION WITH FLAP HANDLE, LANDED. MAINTENANCE FOUND UPLOCK ACTUATOR TO BE BAD REMOVED AND REPLACED ACTUATOR.SDR 1350603N36911Circuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.SDR YBS2003F00000Barrel · shearedUPON LANDING, PILOT REPORTED RT MLG COLLAPSED. MECHANIC FOUND RT MLG UPPER BARREL SHEARED ABOVE UPPER TORQUE LINK ATTACH POINT. MECHANIC REMOVED AND REPLACED MLG ASSY, RT PROP, RT ENGINE, C/W MINOR SHEET METAL REPAIRS TO FLAPS, AND REPLACED RT MLG DOOR. INSSDR 95ZZZW150Le Skin · corrodedCORROSION ON LEADING EDGE OF WING AT TOP AND BOTTOM OF FRONT SPAR AT WS 119.29 THROUGH 229.7. CORROSION AT BOTTOM OF WING JUST AFT OF EXHAUST PIPE ON LEFT AND RIGHT WINGS AT WS 119.29. (W)SDR 95ZZZW148Le Skin · corrodedCORROSION LEADING EDGE TO FRONT SPAR RT WING TOP AND BOTTOM AT WS 119.29 THROUGH 229.71. (W)
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