GAA15CA084
2015-05-20 · Morrisville, Vermont, United States · None · 1 aircraft · Status: Completed
Airport MVL
Current FAA registration · N710JF
- Make / Model
- FAUNCE JOHN W PA-11
- Year of manufacture
- 2008 · 7 years old at event
- Engine
- LYCOMING O-290-D2 (140 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 20080604
- ADS-B equipped
- Yes — Mode-S A97CDB
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the landing roll and his deliberate application of excessive braking pressure.
Factual narrative
The pilot of the tailwheel equipped airplane reported a left crosswind during approach to the runway. During touchdown the airplane veered to the left of the runway centerline. The pilot attempted to return the airplane to the runway centerline by applying right rudder control and right brake. The airplane veered right and exited the right side of the runway. Approaching a ditch on the right side of the runway, the pilot applied the brakes and the airplane nosed over and came to rest inverted. The pilot exited the airplane and reported seeing a shift in the windsock on the airfield from a left crosswind to a left quartering tailwind. The airplane sustained substantial damage to the left wing strut. The pilot reported no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot of the tailwheel equipped airplane reported a left crosswind during approach to the runway. During touchdown the airplane veered to the left of the runway centerline. The pilot attempted to return the airplane to the runway centerline by applying right rudder control and right brake. The airplane veered right and exited the right side of the runway. Approaching a ditch on the right side of the runway, the pilot applied the brakes and the airplane nosed over and came to rest inverted. The pilot exited the airplane and reported seeing a shift in the windsock on the airfield from a left crosswind to a left quartering tailwind. The airplane sustained substantial damage to the left wing strut. The pilot reported no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Surface speed/braking-Incorrect use/operation - C
- — Environmental issues-Physical environment-Terrain-Sloped/uneven-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2015_GAA15CA084.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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