NTSB Narrative Summary Released at Completion of Accident
On June 30, 2014 about 0849 mountain daylight time (MDT), a Piper PA-28-235, N8814W, owned and operated by a private individual, was destroyed when it impacted mountainous terrain at the Loveland Ski Area near Georgetown, Colorado. A post-impact fire ensued. The pilot and the two passengers on board were fatally injured in the accident. Visual meteorological conditions prevailed for the personal cross-country flight which was being conducted under the provisions of 14 Code of Federal Regulations Part 91 without a flight plan. The flight originated at the Rocky Mountain Metropolitan Airport (KBJC), Broomfield, Colorado, at 0730 MDT, and was en route to Moab, Utah.
A witness who was driving on a switchback road on the Loveland Ski Area saw the airplane flying westbound along the mountains. The airplane was at an altitude of 11,000 to 11,200 feet MSL and in a high nose up pitch attitude. The witness said he saw the airplane "break" into a left turn and enter a spin. The airplane was in a steep left bank and "deep" nose down attitude. He watched the airplane descend rapidly and go out of view behind trees. He rolled down his window to hear if there was a crash. When he didn't hear anything, the witness thought maybe the pilot recovered safely from the rapid descent. However, as he came to a horseshoe bend in the road, he saw the smoke from the post-impact fire. The witness said he did not hear any engine sounds prior to the accident because he had his car windows rolled up.
The accident site was located on the side of a mountain slope at an elevation of 10,960 feet MSL. The airplane wreckage was spread along a 186 foot long path through Subalpine fir trees along a 246-degree magnetic heading. The first point of impact was a Subalpine fir that was broken off approximately 69 feet up from the ground. About 45 feet west-southwest of the first impact point were the airplane's left wing tip, two sections of the left outboard wing, and left aileron. They rested on the ground and were crushed and broken aft. The terrain from the first point of impact to where the airplane's main wreckage came to rest was down-sloping at an angle of approximately 18 degrees. The main wreckage, which consisted of the airplane's engine, propeller, cabin, right wing, left inboard wing, both main landing gear, baggage compartment, aft fuselage, and empennage rested inverted at the base of four Subalpine fir trees. These components were charred, melted, and consumed by fire. A burned area approximately 75 feet long and 54 feet wide surrounded the main wreckage. Several trees knocked down by the airplane were also in the burned area.
Continuity from the control yokes and rudder pedals to the aileron bellcranks, stabilator crosstube, and rudder horns was confirmed at the accident site. The right aileron control surface was charred and melted. The rudder and stabilator surfaces were consumed by fire.
The airplane wreckage was retained for further examination.