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.

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 THMay 5, 2022 · N36911 · Cessna 402C · Wing StructureSDR 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 TEJun 25, 2021 · N36911 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR 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 WNov 28, 2018 · N36911 · Cessna 402C · Reciprocating Engine Power SectionSDR 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. OPENMar 8, 2017 · N36911 · Cessna 402C · Nacelle/Pylon, Main FrameSDR 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.Mar 8, 2017 · N36911 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA201611081840Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 21, 2016 · N36911 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108183Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 21, 2016 · N36911 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR 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.Dec 27, 2015 · N36911 · Cessna 402C · Master Cylinder/Brake ValveSDR HYIA20140624003Dimmer · malfunctionedSMOKE APPEARED FROM INSTRUMENT PANEL LIGHT, DIMMER ASSEMBLY. R & R DIMMER ASSEMBLY PN 5118424-1.Jun 22, 2014 · N36911 · Cessna 402C · Flight Compartment LightingSDR 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.Apr 30, 2012 · N36911 · Cessna 402C · Wing SparSDR 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 Mar 16, 2011 · N36911 · Cessna 402C · Directional Gyro and Indicating SystemSDR 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.Jun 18, 2010 · N36911 · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR 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 INCIDOct 7, 2009 · N36911 · Cessna 402C · Landing Gear System WiringSDR 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.Sep 30, 2009 · N36911 · Cessna 402C · Rudder Control SystemSDR HYIA36911 625Master Switch · unserviceableCREW REPORTED AVIONIC MASTER SWITCH INOPERATIVE. MX REMOVED AND REPLACED SWITCH AND RETURNED ACFT TO SERVICEJun 25, 2009 · N36911 · Cessna 402C · Electrical Power SystemSDR 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 SERVICEJun 23, 2009 · N36911 · Cessna 402C · Directional Gyro and Indicating SystemSDR 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.Dec 2, 2007 · N36911 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR 1350603N36911Circuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.Aug 3, 2006 · N36911 · Cessna 402C · Electrical Power SystemSDR 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. INSJul 24, 2003 · N36911 · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR 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)Jan 30, 1995 · N36911 · Cessna 402C · Wing, Plate/SkinSDR 95ZZZW148Le Skin · corrodedCORROSION LEADING EDGE TO FRONT SPAR RT WING TOP AND BOTTOM AT WS 119.29 THROUGH 229.71. (W)Jan 30, 1995 · N36911 · Cessna 402C · Wing, Plate/Skin
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