Aviation Accident Summaries

Aviation Accident Summary ATL96LA046

PALM CITY, FL, USA

Aircraft #1

N551MR

North American P-51D

Analysis

On final approach, the pilot advanced the throttle, with no response from the engine. The pilot stated that the engine had quit, and he attempted an unsuccessful restart. To avoid a stand of trees the pilot maneuvered through a yard. The aircraft struck an oak tree, came to rest on the approach end of runway 36, and burned. The engine examination revealed that the carburetor idle setting was improperly adjusted which would have resulted in depleting the fuel in the carburetor, a delayed response to throttle movement from the idle position, and loss of engine power.

Factual Information

On February 12, 1996, approximately 1600 eastern standard time, a North American P-51D, N551MR, collided with a tree and the ground while on final approach to the Naked Lady Ranch Airstrip, Palm City, Florida. The flight operated under the provisions of Title 14 CFR Part 91, and visual flight rules. No flight plan was filed for the personal flight, and visual meteorological conditions prevailed. The private pilot was seriously injured, and the aircraft was destroyed by a post crash fire. The flight departed Leeward Air Ranch Ocala, Florida, about 1510. The pilot had been performing aerial work at Leeward Air Ranch, and was returning home to the Naked Lady Ranch. A prelanding check, which included lowering the landing gear and the flaps, was completed. While on final approach, he attempted to add power, but there was no response. The propeller was windmilling, and the pilot said that the engine had lost all power. The pilot stated that the boost pump was on, he switched the fuel tanks, used the primer, and retracted the flaps. He stated that the airplane could not glide to the airfield, so he tried to maneuver through a yard to avoid a stand of trees. The airplane struck an oak tree and cartwheeled. According to the pilot, the airplane was destroyed by a post crash fire. According to the FAA Aviation Safety Inspector the functional engine examination revealed that the carburetor idle was improperly adjusted which would result in depletion of the fuel in the carburetor with the throttle at idle, and a delayed response of the engine to throttle movement, from the idle position.

Probable Cause and Findings

An improperly adjusted carburetor which resulted in fuel starvation.

 

Source: NTSB Aviation Accident Database

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