NTSB investigations · 1
Matched to this aircraft by N300ED and the event date: up to this one’s cancellation.
FAA incident reports · 4
FAA accident and incident reports matched to this aircraft by N300ED and the event date: up to this one’s cancellation.
Accident 20111208029059ALanding: Touchdown · Kaltag, AKOn December 8, 2011 at 1450 AKST, pilot elected to approach the Kaltag Airport (pakv) VFR with weather conditions reporting 1 3/4SM ovc 010. Pilot operated GPS direct from pfku. Pilot started before landing checklist 5 miles from pakv and saw he was picking…Incident 19980529014149IClimb · Fairbanks, AKNarrative: aircraft departed Fairbanks enroute to fort yukon. 20 miles north of Fairbanks the right engine failed. The pilot shut down the engine and returned to Fairbanks. Inspection revealed the #5 cylinder had separated from the engine case. The engine…Incident 19880202009169IClimb · Aniak, AKLeft engine failed on climb. Engine was shut down. Returned. Found a cracked cylinder.Incident 19800702059179IGround Taxi, Other Airplane · Boise, IDDuring taxi to takeoff, smelled smoke. A loose connection in terminal had caused a short.
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR WVBA2003003Fitting · crackedLANDING GEAR WOULD NOT EXTEND WITH GEAR HANDLE. GEAR LOWERED AND LOCKED WITH EMERGENCY PUMP HANDLE. UPON EXAMINATION FOUND LOWER FITTING ON LEFT INNER GEAR DOOR ACTUATOR CRACKED AND HOSE CHAFED TO BOTTOM FITTING. THE PROBLEM SEEMED TO COME FROM A ACTUATOR HSDR WVBA2002003Channel · crackedDURING INSPECTION THIS AREA WAS LOOKED AT AFTER FINDING OTHER AIRCRAFT WITH THIS CHANNEL CRACKED THE PART WAS REMOVED AND REPLACED. IT MAY BE THAT THE CUT OUT NOT BEING. DRESSED TO BELIEVE THE STRESS CAUSED THE PART TO FAIL AS EXTRA STRESS. IS INDUCED FROM TSDR WVBA2001040Pump · stuckDURING PREINSPECTION RUN, IT WAS NOTED THAT THE ENGINE DRIVEN FUEL PUMP PRESSURE WAS LOW AFTER ADJUSTMENTS WERE MADE THE DESIRED PRESSURE SETTING WAS NOT OBTAINABLE. TROUBLESHOOTING, IT APPEARS THE RELIEF VALVE IS HUNG UP PUMP WAS REMOVED FROM SERVICE AND SENSDR WVBA2001035Pump · failedPILOT REPORTED RIGHT HYDRAULIC PUMP FAILED CHECK DURING RUN UP. PUMP WAS REMOVED AND IT WAS DISCOVERED THAT THE SHAFT HAD SHEARED. DURING REMOVAL OF THE FITTINGS IT WAS DISCOVERED THAT THE SMALL PRESSED IN NOZZLE, SPRING AND BALL HAD COME LOOSE WITH THE BALLSDR WVBA2001027Igniter · inoperativePILOT REPORTED HEATER WOULD NOT FIRE OFF. IT WAS DETERMINED THAT THE IGNITION UNIT HAD NO OUTPUT. THE UNIT WAS REMOVED AND REPLACED.SDR 20010508CW020Bracket · crackedDURING LANDING GEAR INSPECTION DISCOVERED THE FORWARD BRACKET FOR THE RIGHT INNER GEAR DOOR ACTUATOR WAS CRACKED THROUGH THE BOLT HOLE ON THE BEARING SIDE. NOTE: THIS BRACKET HAS A DOUBLER PIECE BEHIND THE STAMPED PIECE WHICH WAS NOT CRACKED.SDR WVBA2001019Camshaft · damagedDURING INSPECTION, METAL CONTAMINATION WAS DISCOVERED IN THE OIL FILTER. A CHECK OF VALVELIFT WAS DONE AND IT WAS DISCOVERED THAT NR 3 AND NR 4 INTAKE LOBES WERE EXCESSIVE. NR 3 CLYINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TAPPET FOLLOWERS. SDR WVBA2001013Camshaft · damagedDURING INSPECTION METAL CONTAMINATION WAS DISCOVERED IN OIL FILTER. A CHECK OF VALVE LIFT WAS DONE AND IT WAS DISCOVERED THAT NR5 AND NR6 INTAKE LOBES WERE EXCESSIVE. NR6 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TAPPET FOLLOWERS. NOTE: SDR 20001025SH005Hinge · brokenPILOT REPORTED GEAR DOOR BROKEN. DISCOVERED FORWARD HINGE ON LEFT MAIN GEAR DOOR BROKEN IN HALF AND GEAR DOOR BENT FROM CONTACT WITH MAIN GEAR WHEEL. A NEW DOOR INSTALLED AND AIRCRAFT RETURNED TO SERVICE. SUBMITTER RECOMMENDED THESE HINGES BE STRIPPED OF PASDR WVBA01100Camshaft · damagedDURING INSPECTION, METAL CONTAMINATION WAS DISCOVERED IN THE SPIN ON OIL FILTER. FURTHER INVESTIGATION FOUND NR 4 AND NR 6 CYLINDER INTAKE VALVE LIFT IN EXCESS. NR 6 CYLINDER REMOVED AND THE INTAKE LOBE OF NR 4/NR 6 CYLINDERS ON THE CAMSHAFT TO HAVE SEVERE SDR 98ZZZX4517Engine · malfunctionedIN PREPARATION FOR LANDING, PILOT NOTICED LEFT ENGINE'S RPMS LAGGING THE RIGHT ENGINE. WITH ANY POWER REDUCTIONS, THE LEFT ENGINE'S RPMS LAGGED EVEN FURTHER. THERE WAS NO RESPONSE WHEN THE PROPELLER CONTROL LEVER WAS MOVED TO THE FULL FORWARD POSITION (INCRESDR 98ZZZX2170Connect Rod · failedON CLIMB-OUT FROM FAI, RIGHT ENGINE FAILED. NR 5 CYLINDER SEPARATED FROM ENGINE, NR 5 CONNECTING ROD BROKEN AT PISTON PIN. CASE RECEIVED MASSIVE DAMAGE.SDR 97ZZZX5169Solenoid · leakingDURING WORK ON REAR HEATER, HAD COVER OFF OF FUEL SHUT OFF SOLENOID. NOTICED FUEL LEAKING FROM GROMMET ON BODY OF SOLENOID. REMOVED PART FROM SERVICE AS IT PRESENTED A FIRE HAZARD.SDR 97ZZZX2874Fuel Pump · leakingUPON PULLING AIRCRAFT IN HANGAR FOR A SCHEDULED INSPECTION, FOUND THE ENGINE DRIVEN FUEL PUMP LEAKING FUEL FROM THE VALVE BODY PARTING FLANGES. PUMP WAS REMOVED FROM SERVICE. SUSPECT CAUSE, THE PARTING HALF FLANGE SCREWS FOR THE VALVE BODY MAY BE IMPROPERLY
Other aircraft with N300ED · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N300ED is registered now to the first aircraft listed.