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CEN13CA412

2013-07-14 · Hector, Minnesota, United States · None · 1 aircraft · Status: Completed

Airport 1D6

Current FAA registration · N855F

Make / Model
UNIVERSAL STINSON 108-1
Year of manufacture
1947 · 66 years old at event
Engine
FRANKLIN 6A4150 SERIES (150 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19551208
ADS-B equipped
Yes — Mode-S ABBA68

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s inadvertent application of the brakes and failure to main directional control of the airplane during the takeoff roll, which resulted in the airplane nosing over.

Factual narrative

During the takeoff roll, at about 50 knots, the airplane began to drift to the left. The pilot stated that as the airplane drifted to the left, she inadvertently tapped on the right brake, and then released the brake while adding right ailerons inputs. Corrections were made to maneuver the airplane back to the runway centerline. The right wingtip was lowered and impacted the ground 2 or 3 times. She continued to apply inputs to the right rudder pedal. The airplane nosed-over and sustained substantial damage to both wing spars and the vertical stabilizer. The second pilot stated that he didn’t know why the airplane responded as it did and was unsure if there were any malfunctions with the airplane prior to the accident. He estimated the wind to be from the left at 5 knots. A postaccident examination of the airplane by a Federal Aviation Administration inspector revealed no evidence of preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. During the takeoff roll, at about 50 knots, the airplane began to drift to the left. The pilot stated that as the airplane drifted to the left, she inadvertently tapped on the right brake, and then released the brake while adding right ailerons inputs. Corrections were made to maneuver the airplane back to the runway centerline. The right wingtip was lowered and impacted the ground 2 or 3 times. She continued to apply inputs to the right rudder pedal. The airplane nosed-over and sustained substantial damage to both wing spars and the vertical stabilizer. The second pilot stated that he didn’t know why the airplane responded as it did and was unsure if there were any malfunctions with the airplane prior to the accident. He estimated the wind to be from the left at 5 knots. A postaccident examination of the airplane by a Federal Aviation Administration inspector revealed no evidence of preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. As the pilot was making continuous rudder pedal inputs, it is likely that she inadvertently applied the brakes. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2013_CEN13CA412.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.