What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
N9720P is a Piper PA18 that crashed approximately 30NM sw of Beluga point airport on 27 nov 2014. There were two on board an Alaska west air, 14CFR part 135 flight that originated in the kenai Alaska area. N9720P was the second aircraft in a flight of two flying to the same destination for the purpose of hunting moose. When attempting to land off-airport, the pilot of the first aircraft stated he experienced a temperature inversion approximately 100 ? 200 feet above ground level and experienced carburetor icing. Both aircraft made a straight in approaches to the landing surface which was described as a ?bench?. Due to engine failure/lack of power the accident aircraft impacted the rising terrain just prior to the landing area. Upon engine dissasembly, it was noted that the airbox indicated the carb heat was in the off position at the time of the accident due to slight metal deformation that locked the carb heat box in position. The lack of carb heat application was confirmed by the pilot in command. No internal engine damage aside from slight bearing wear noted at the time of internal inspection.
As the FAA filed it
N9720P IS A PIPER PA18 THAT CRASHED APPROXIMATELY 30NM SW OF BELUGA POINT AIRPORT ON 27 NOV 2014. THERE WERE TWO ON BOARD AN ALASKA WEST AIR, 14CFR PART 135 FLIGHT THAT ORIGINATED IN THE KENAI ALASKA AREA. N9720P WAS THE SECOND AIRCRAFT IN A FLIGHT OF TWO FLYING TO THE SAME DESTINATION FOR THE PURPOSE OF HUNTING MOOSE. WHEN ATTEMPTING TO LAND OFF-AIRPORT, THE PILOT OF THE FIRST AIRCRAFT STATED HE EXPERIENCED A TEMPERATURE INVERSION APPROXIMATELY 100 ? 200 FEET ABOVE GROUND LEVEL AND EXPERIENCED CARBURETOR ICING. BOTH AIRCRAFT MADE A STRAIGHT IN APPROACHES TO THE LANDING SURFACE WHICH WAS DESCRIBED AS A ?BENCH?. DUE TO ENGINE FAILURE/LACK OF POWER THE ACCIDENT AIRCRAFT IMPACTED THE RISING TERRAIN JUST PRIOR TO THE LANDING AREA. UPON ENGINE DISSASEMBLY, IT WAS NOTED THAT THE AIRBOX INDICATED THE CARB HEAT WAS IN THE OFF POSITION AT THE TIME OF THE ACCIDENT DUE TO SLIGHT METAL DEFORMATION THAT LOCKED THE CARB HEAT BOX IN POSITION. THE LACK OF CARB HEAT APPLICATION WAS CONFIRMED BY THE PILOT IN COMMAND. NO INTERNAL ENGINE DAMAGE ASIDE FROM SLIGHT BEARING WEAR NOTED AT THE TIME OF INTERNAL INSPECTION.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N9720P · 1
Matched to the same aircraft by N-number and date.