No fatalities

17 Jan 2020: Cessna 185 D — Laytonsville, MD

Laytonsville, MD, United States

On 17 Jan 2020, a Cessna 185 D was involved in an aviation accident near Laytonsville, MD. No fatalities were reported. Investigators recorded the probable cause as: The failure of the tailwheel attachment tube during the takeoff roll, which resulted in a loss of directional control, a runway excursion, and the left main landing gear collapsing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

During a practice takeoff, a pilot experienced a veer after applying power. The airplane became momentarily airborne, then veered off the runway, collapsing the left main landing gear and causing substantial damage to the left wing and tail surfaces.

Accident Overview

A pilot was conducting a practice flight focused on takeoffs and landings. After completing two uneventful circuits in the traffic pattern, the pilot aligned the airplane on runway 8 for another takeoff.

Sequence of Events

As the pilot applied engine power, right rudder was used to center the airplane on the runway. Approximately 50 feet into the takeoff roll, the airplane veered to the left. In response, the pilot applied right brake and right rudder, but the airplane became "momentarily airborne." The pilot then reduced engine power, and as the airplane settled back onto the runway, it veered to the right. Despite attempts to stop the airplane with brakes, it continued off the right side of the runway, traveled through mud, and subsequently the left main landing gear collapsed.

Wreckage Examination

An examination by a Federal Aviation Administration (FAA) inspector revealed that the airplane came to rest on the left side of the fuselage. The tailwheel attachment tube was separated from the empennage, but the tailwheel control cables remained attached. Substantial damage was incurred by the left wing, left elevator, and left horizontal stabilizer.

Contributing factors

Nose/tail landing gear — FailureAttain/maintain not possible