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NYC02LA020

2001-10-20 · Farmville, Virginia, United States · None · 1 aircraft · Status: Completed

Airport FVX

Current FAA registration · N43529

Make / Model
TAYLORCRAFT BC12-D
Year of manufacture
1946 · 55 years old at event
Engine
CONT MOTOR A&C65 SERIES (65 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19700818
ADS-B equipped
Yes — Mode-S A53871

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The CFI's failure to maintain directional control during the takeoff. A factor in the accident was the CFI's decision to conduct the flight from the airplane's right seat, which was not equipped with brakes.

Factual narrative

On October 20, 2001, about 1530 eastern daylight time, a Taylorcraft BC12-D, N43529, was substantially damaged during takeoff from the Farmville Regional Airport, Farmville, Virginia. The certificated flight instructor (CFI) and private pilot were not injured. Visual meteorological conditions prevailed and no flight plan had been filed for the instructional flight conducted under 14 CFR Part 91. The airplane was departing runway 21, a 4,400-foot long, 75-foot wide, asphalt runway. The CFI stated he performed the takeoff, and intended to fly to a local grass strip to provide the private pilot with tail-wheel aircraft instruction. The CFI said he "lost directional control" of the airplane during the takeoff roll, and he elected to allow the airplane to depart the right side of the runway and slow down in the grass. However, the airplane struck a ditch and flipped over, which damaged the vertical stabilizer and rudder. The CFI did not report any mechanical problems with the airplane and he further stated that wind at the time of the accident was light and variable. Additionally, the CFI was seated in the airplane's right front seat, and airplane was equipped with "foot-brakes" at the left front seat pilot station only. The certified flight instructor (CFI) intended to fly to a local grass strip to provide the private pilot with tail-wheel aircraft instruction. During the takeoff roll, the CFI lost directional control of the airplane and elected to allow the airplane to depart the right side of the runway and slow down in the grass. However, the airplane struck a ditch and flipped over, which damaged the vertical stabilizer and rudder. The CFI did not report any mechanical problems with the airplane and he further stated that wind at the time of the accident was light and variable. Additionally, the CFI was seated in the airplane's right front seat, and airplane was equipped with "foot brakes" at the left front seat pilot station only. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2001_NYC02LA020.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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