Walter M601E-11

Service difficulty reports · 24

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 engine_model_key = 'M601E11'
  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 CA140618003Engine · failed(CAN) SHORTLY AFTER TAKEOFF FROM OUR BASE OF OPERATION OUR DHC-3T OTTER ON FLOATS HAD FLAMES SHOOT OUT OF BOTH OF THE EXHAUST STACKS AND THEN THE PROPELLER RAPIDLY SLOWED TO A STOP AND THE AIRCRAFT MADE A SAFE EMERGENCY LANDING ON THE LAKE AND WAS TOWED BACK TJun 16, 2014 · Dhav DHC3 · Engine (Turbine/Turboprop)SDR CA140214006Skin · cracked(CAN) UPON COMPLETING WING INSPECTION ACCESS HOLES INSTALLATION 5 CORRUGATED SKINS WERE FOUND CRACKED.Feb 14, 2014 · Dhav DHC3 · Wing, Plate/SkinSDR CA140214008Spar · corroded(CAN) ON REPLACING WING CORRUGATIONS ON THE WINGS THE FRONT SPAR PLATE AT APPROXIMATELY BS 70 WAS FOUND CORRODED.Feb 12, 2014 · Dhav DHC3 · Wing SparSDR CA130627011Bar · cracked(CAN) UPON REPLACEMENT OF THE AFT SPREADER BAR, THE FRONT SPREADER BAR WAS FOUND TO BE CRACKED AT THE FLOAT ATTACH POINT. WE DECIDED TO REMOVE 1 FROM ANOTHER SET OF FLOATS TO REPLACE THE CRACKED ON AND FOUND THAT ON CRACKED IN THE SAME LOCATION.Jun 26, 2013 · Dhav DHC3 · Landing Gear SystemSDR 2013FA0000205Blades · brokenREPORTED THAT AFTER LANDING, PROPELLER SLOWED DOWN QUICKER THAN NORMAL. DURING SHUTDOWN THE PROPELLER DID NOT FEATHER AND CAME TO LOW SPEED STOP. INSPECTION OF THE ENGINES REVEALED GGT ROTOR BLADE SEPARATION. SUBJECT ENGINE WAS REMOVED FROM SERVICE AND SENApr 1, 2013 · Airtrc AT401 · Turbine SectionSDR CA121009012Bracket · broken(CAN) THE PART DESCRIBED IS A FLYING WIRE ATTACHMENT AT THE BASE OF THE LT FLOAT REAR STRUT POSITION. BEFORE THE FIRST FLIGHT OF THE DAY 1. PILOTS NOTICED THE LT REAR FLYING WIRE HANGING LOOSE. THE PILOT THAT FLEW THE ACFT LAST NOTED, HEARD A NOISE DURING COct 3, 2012 · Dhav DHC3 · Wheel/Ski/FloatSDR CA130306008Blade · damaged(CAN) PILOT REDUCED POWER TO IDLE AT TOUCHDOWN, HE NOTED PROP RPM DECAY BELOW NORMAL. ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED, PROP THEN STOPPED TURNING BUT DID NOT FEATHER. PILOT CARRIED OUT SHUTDOWN PROCEDURE. ACFT WAS TOWED FROM RUNWAY. INITIAL INSPECJun 6, 2012 · Airtrc AT401 · Turbine SectionSDR CA120405002Actuator · unserviceable(CAN) A FAILURE OF THE TRIM ACTUATOR, PN C3CF290-9, CAUSED A RUNAWAY TRIM CONDITION DURING THE ACFT INITIAL CLIMB. ADDITIONAL INFORMATION TO BE PROVIDED FOLLOWING INSPECTION OF THE ACFT AND PART INVOLVED. THE TRIM ACTUATOR HAD NOT BEEN GEARED ADEQUATELY AND Apr 5, 2012 · Dhav DHC3 · Elevator Tab Control SystemSDR CA110930010Bar · corroded(CAN) FLOAT INSTALLATION THE REAR SPREADER BAR EXHIBITED SIGNS OF CORROSION PRODUCT EXITING THE HOLLOW TUBE ASSY. FURTHER INTERNAL INVESTIGATION REVEALED SEVERE CORROSION INTERNALLY IN THE TUBE ASSY, D30511-1. SPREADER BAR REPLACED, FWD SPREADER BAR WAS REPSep 14, 2011 · Dhav DHC3 · Wheel/Ski/FloatSDR CA110929016Bracket · cracked(CAN) ON VISUAL INSP, THE LOWER RUDDER BRACKET FLANGE EXTRUSION WAS FOUND TO BE CRACKED AT THE REAR RADIUS ADJACENT TO THE RUDDER PUSH PULL ROD END ATTACH POINT. RUDDER REMOVED AND BOTTOM BRACKET, PN C3TR19-5, REPLACED.Jul 21, 2011 · Dhav DHC3 · Rudder StructureSDR CA101104013Bushing · corroded(CAN) REAR FUEL CELL SUMP PANEL HAS A CORRODED SUMP DRAIN PLUG BUSHING. PANEL REPLACED WITH NEW UNIT.Nov 2, 2010 · Dhav DHC3 · Fuel StorageSDR CA101115014Retainer · loose(CAN) RIVETS HOLDING THE ELEVATOR QUADRANT ASSEMBLY TOGETHER WERE FOUND LOOSE, ESPECIALLY AROUND THE BEARING PIVOT RETAINER. QUADRANT REPLACED WITH REPAIRED UNIT.Nov 2, 2010 · Dhav DHC3 · Elevator StructureSDR CA101115016Attach Bolt · bent(CAN) DURING QUADRANT INSPECTION/REPLACEMENT (CF-85-04) IT WAS NOTED THAT THE SPECIAL BOLT NAS1954-24D THAT ATTACHES THE ELEVATOR PUSH PULL ROD TO THE QUADRANT WAS BENT. THIS DEFECT WOULD BE NEARLY IMPOSSIBLE TO DETECT WITHOUT REMOVING THE PUSH PULL ROD DURINNov 2, 2010 · Dhav DHC3 · Elevator StructureSDR CA101115018Lug · worn(CAN) BOTH UPPER AND LOWER ATTACH LUGS WERE REPLACED DUE TO WEAR AT THE STRUT ATTACH BOLT HOLE. THE WEAR WAS NOTICEABLE IF YOU MOVED THE WING TIP FOR AND AFT WHILE THE FLOAT EQUIPPED AIRCRAFT WAS ON THE HARD.Nov 2, 2010 · Dhav DHC3 · Wing Miscellaneous StructureSDR CA101115019Bushing · corroded(CAN) FUEL SUMP DRAIN BUSHING CORRODED AT FUEL DRAIN COCK. FUEL SUMP ASSEMBLY REPLACED WITH NEW UNIT.Nov 2, 2010 · Dhav DHC3 · Fuel StorageSDR CA101115022Bar · cracked(CAN) CRACK LOCATED PARALLEL TO LUG ATTACHMENT ON FORWARD SPREADER BAR TUBE. NEW FORWARD SPREADER BAR ASSEMBLY INSTALLED.Nov 2, 2010 · Dhav DHC3 · Wheel/Ski/FloatSDR CA101104014Roll Pin · sheared(CAN) SEAT HEIGHT LOCK PIN FOUND SHEARED MID SHAFT AT ROLL PIN STOP LOCATION. LOCK PIN REPLACED WITH NEW UNIT.Oct 25, 2010 · Dhav DHC3 · Flight Compartment EquipmentSDR CA101013003Cooler · leakingCOOLER FOUND TO BE LEAKING DURING FLIGHT MODE. COOLER REPLACED WITH O/H UNIT.Oct 10, 2010 · Dhav DHC3 · Engine Fuel/Oil CoolerSDR CA100812020Display · unserviceableON START UP AT THE FIRST FLIGHT OF THE DAY, THE MULTIFUNCTION DISPLAY SCREEN WOULD NOT COME ON LINE. TROUBLESHOOTING INDICATED THAT THE SCREEN HAD POWER AND A GOOD GROUND. SCREEN REMOVED AND RETURNED TO MFR FOR REPAIR. NOTE: THE GLASS COCKPIT FORMS PART OF Aug 7, 2010 · Dhav DHC3 · Flight Management Computing Hardware SystemSDR 2010FA0000713Angle · crackedTHE CRACK DEVELOPED FROM THE TOP DOWN IN THE CORNER OF THE ANGLE FOR APPROX 1 INCH. IT HAS FLOWN FOR 91 HRS SINCE THE LAST INSP AT WHICH TIME NO CRACK WAS APPARENT. THE ACFT FLIES OUT OF A SMOOTH PAVED RUNWAY AND IS USED MOSTLY FRO GRANULAR FERTILIZER APPLICJun 17, 2010 · N10063 · Airtrc AT401 · Fuselage Miscellaneous StructureSDR 2010FA0000510Wheel Half · shearedWHEEL ASSY INNER FLANGE FAILED INFLT. FLANGE BROKE INTO SEVERAL PIECES. TIRE (TUBE TYPE) PUSHED INWARD & PUSHING THE FLANGE PIECES INTO BRAKE ROTOR & DEPRESSED THE CALIPER PISTON. DURING FLT, PILOT NOTICED RT BRAKE PEDAL FELT LOCKED & FLUID LEAKING FROM RT May 21, 2010 · N3633C · Scwzer G164B · Wheel/Ski/FloatSDR CA090611004Gear · failed(CAN) REAR CHIP DETECTIOR LIGHT ILLUMINATED 15 MINUTES PRIOR TO LANDING ACFT. METAL WAS FOUND IN REAR CHIP DETECTOR AND REAR CHIP DETECTOR SCREEN, ENGINE REMOVED FROM ACFT FOR REPAIR.May 30, 2009 · Dhav DHC3 · Starter-GeneratorSDR CA070606004Rod End · broken(CAN) PILOT COULD NOT GET GEAR DOWN INDICATION, BUT COULD GET GEAR UP AND LOCKED INDICATION. WATER LANDING CARRIED OUT. MAINT FOUND LT NOSE GEAR WOULD NOT EXTEND. ROD END FOUND BROKEN ON NOSE GEAR ACTUATOR, REPLACED AND ACFT RETURNED TO SERVICE. (TC NR 2007060Jun 5, 2007 · Dhav DHC3 · Landing Gear ActuatorSDR CA040923004Tie Rod · broken(CAN) PILOT NOTICED TIE ROD BROKEN UPON RETURN TO BASE. NO DIFFICULTY WITH THIS LANDING OR PREVIOUS LANDINGS WHERE NOTED BY PILOT. PART WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. PLEASE ADVISE WHERE PARTS CAN BE SENT FOR EXAMINATION. HAVE NOT SEEN A FSep 4, 2004 · Dhav DHC3 · Wheel/Ski/Float
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