Curtiss JN4 accident near Williamson, GA

On November 17, 2016, a Curtiss JN4 (airplane) was involved in an accident near Williamson, GA. 2 people died. Damage to the aircraft: destroyed.

Date
November 17, 2016
Place
Williamson, GA
Aircraft
Curtiss JN4 · Airplane
Injuries
2 fatal, 0 serious, 0 minor
Damage
Destroyed
Position
33.184°N, 84.385°W
NTSB ID
20161117X33619

Official records · ERA17FA050

NTSB summary

HISTORY OF FLIGHTOn November 17, 2016, at 1740 eastern standard time, an experimental, amateur-built Curtiss JN4D, N1662, collided with terrain shortly after takeoff from Peach State Airport (GA2), Williamson, Georgia. The airline transport pilot and pilot-rated passenger were fatally injured. The airplane was destroyed by impact forces and fire. The airplane was registered to and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91. Dusk, visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight, which was originating at the time of the accident. According to a witness, the airplane departed runway 31, appeared to enter a normal climb, and the engine sounded "as it always did." As the airplane passed the runway end markers, about 110-120 ft above the ground, he heard a loud backfire followed by two "pops" that were not as loud. The airplane seemed to hesitate for an instant, then there was silence. He observed the airplane in a left turn. After about 90º of turn, he saw a flicker of flame appear from the forward, left side of the fuselage that progressed into a "raging fire," with an audible "whoomp" sound. The fire streamed back over the top and left side of the fuselage and extended about 1/2 the length of the airplane. The fire persisted and the airplane disappeared behind a tree line and crashed. The witness immediately called the authorities. Another witness provided a cell phone photo of the airplane on the takeoff leg, which showed a fire near the forward section of the airplane. The

Probable cause

The in-flight failure of the propeller due to excessive engine vibration loads and the use of an incorrectly-sized propeller, which resulted in a fatigue crack of the leading edge strip. Contributing to the accident was the inadequate repair of the propeller following a previous crack.

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