1 fatality

8 Apr 2010: SNOW ROCKET F1 (N28VS) — SNOW VAN E — Borrego Springs, CA

Borrego Springs, CA, United States

On 8 Apr 2010, a SNOW ROCKET F1 (registration N28VS) operated by SNOW VAN E was involved in an aviation accident near Borrego Springs, CA. One person was killed. Investigators recorded the probable cause as: The pilot was unable to maintain control of the aircraft due to the in-flight failure and separation of the flight control stick; the specific reason for the failure of the control stick could not be determined. This summary draws on records from NTSB.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A pilot was killed when an experimental amateur-built aircraft suffered a flight control failure while performing maneuvers near Borrego Springs, California.

What happened

On April 8, 2010, an experimental amateur-built Snow Rocket F1, registration N28VS, crashed in the desert near Borrego Springs, California. The aircraft was being operated by the pilot for a practice session in preparation for the annual Borrego Hammerhead Roundup aerobatic competition.

At approximately 12:58 PDT, the pilot entered the designated aerobatic box at an altitude between 2,700 and 3,000 feet above ground level. To gain the energy required for maneuvers, the pilot entered a 30-to-35-degree descent. During this descent, the pilot transmitted via radio that he had "no back stick."

As the aircraft descended through 1,800 to 2,000 feet, ground observers attempted to communicate with the pilot to see if the aircraft was under control; the pilot responded that it was not. When advised to use the aircraft's trim, the pilot stated, "there is no trim." The aircraft was observed descending through 600 feet before the descent angle steepened further, and the airplane impacted terrain behind a sand dune. The pilot, the sole occupant, sustained 1 fatal injury.

The investigation

An examination of the wreckage by the FAA revealed the aircraft was resting inverted. The engine had separated from the fuselage, and the fuselage was crushed aft.

NTSB investigators examined the elevator flight control system and found multiple separations between the rear control stick and the elevator control surface, all showing signs of overload. The front and rear control sticks had separated from their control columns.

Metallurgical analysis of the control components showed that fractures in the interconnected control column, portions of the sticks, the elevator control servo, and the control rod were all caused by overstress. Specifically, the fracture in the front control stick initiated at the edge of a 0.22-inch diameter hole drilled into the tube wall. While the aluminum alloy composition of the sticks was within specification, the hardness and conductivity measurements were consistent with a T4 or lower strength T6 condition.

Probable cause

The pilot was unable to maintain control of the aircraft due to the in-flight failure and separation of the flight control stick; the specific reason for the failure of the control stick could not be determined.

Contributing factors

Control column section — FailureAttain/maintain not possible