PAUL, ID, USA
N5386
Grumman-Schweizer G-164A
IMMEDIATELY AFTER TAKEOFF AND AT APPROXIMATELY 50 FEET AGL THE AIRCRAFT LOST POWER FOR UNDETERMINED REASONS. THE PILOT EXECUTED A FORCED LANDING DURING WHICH THE LEFT MAIN LANDING GEAR AND WING IMPACTED A HOLE SPINNING THE AIRCRAFT AROUND APPROXIMATELY 160 DEGREES. A POST CRASH FIRE DESTROYED THE AIRCRAFT.
LOSS OF ENGINE POWER FOR UNDETERMINED REASONS AND AIRCRAFT CONTROL NOT POSSIBLE BY THE PILOT IN COMMAND. A FACTOR CONTRIBUTING TO THE ACCIDENT WAS: ROUGH/UNEVEN TERRAIN.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports