NTSB PRELIMINARY:
NTSB Identification: ERA15LA315
14 CFR Part 91: General Aviation
Accident occurred Sunday, August 16, 2015 in Bristow, VA
Aircraft: PIPER PA 28-161, registration: N82587
Injuries: 1 Serious.
This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.
On August 16, 2015, at 0906 eastern daylight time, a Piper PA-28-161, N82587, was substantially damaged when it impacted trees and terrain in Bristow, Virginia. The student pilot was seriously injured. Visual meteorological conditions prevailed and no flight plan was filed. The local solo instructional flight was operating in the traffic pattern at Manassas Regional Airport (HEF), Manassas, Virginia and was conducted under the provisions of 14 Code of Federal Regulations Part 91.
A preliminary review of Federal Aviation Administration (FAA) air traffic control communication records indicated that the airplane had been operating in the traffic pattern at HEF for runway 16R. As the airplane made a base leg to final approach leg turn, the pilot advised that she was going to perform a go around. The tower controller acknowledged and provided a clearance to fly right closed traffic. About 4 minutes later, while on the downwind leg, the controller advised the pilot that she appeared to be low, and asked if she required assistance. The pilot indicated that she did, and the controller advised her to climb to 1,000 feet and continue the downwind leg. The pilot's response was unintelligible, and the controller again advised the pilot to climb to 1,000 feet. The pilot responded "I think I'm going too fast, I need [unintelligible]". The controller instructed the pilot to climb again, however there was no response.
The airplane subsequently impacted a wooded area in the backyard of a residence, about 1.5 miles northwest of HEF, and came to rest upright.
An FAA inspector examined the airplane at the accident scene. The fuselage and right wing remained intact; the left wing was separated and remained in the tree canopy about 35 feet above the ground. The fuselage had crush damage on the lower left side along its length, from the nose section to the vertical stabilizer. The right wing leading edge was crushed aft in several places consistent with tree impacts. The horizontal stabilator was partially separated from the fuselage. Flight control continuity was confirmed from the cockpit controls to their respective control surfaces. About 18 gallons of fuel were recovered from the right wing. The engine and airframe were retained for further examination
Records from the pilot's flight school revealed that she had logged about 61 total flight hours, 4.3 solo flight hours, and she had completed 5 solo flights, prior to the accident flight.
The 0955 weather observation at HEF included wind from 180 at 3 knots, 10 statute miles visibility, sky clear, temperature 25 degrees C, dew point 20 degrees C, and an altimeter setting of 30.17 inches of mercury.
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