2 fatalities

2024-05-05: Rockwell Grand Commander 690 (N690BM) — Commander 690 BM — Palmyra, United States of America

Palmyra, United States of AmericaFlight

On May 5, 2024, a Rockwell Grand Commander 690 (registration N690BM) operated by Commander 690 BM was involved in an aviation accident near Palmyra, United States of America in flight. 2 people were killed. Investigators recorded the probable cause as: The pilot’s loss of control following an encounter with structural icing, which resulted in an inflight breakup of the airplane. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781188905Data APIEditorial standards

An airplane broke up in flight after the pilot reported losing the autopilot and reversed course. Witness saw fire. Wreckage scattered over 3 miles. Both occupants died.

Flight and Communication

The airplane was cruising at 20,000 feet on an instrument flight rules (IFR) cross-country flight when the pilot reversed course. Upon being queried by an air traffic controller, the pilot stated, “we have lost…we need to climb.” Asked about the issue, the pilot responded, “we have lost autopilot.” No further communications were received, and radar contact was lost shortly thereafter.

Witness Observation and Wreckage

A witness reported seeing the airplane on fire as it descended toward the ground. The wreckage was heavily fragmented and scattered across a wooded area, with a debris path spanning over 3 miles. The left wing, left engine, left propeller, and empennage were heavily burnt and located at the main wreckage site. The right wing had separated at the wing root and was found approximately 1/4 mile north of the main wreckage, showing fire damage; the right engine and right propeller were not located. The vertical and horizontal stabilizers were found about 3/4 mile north of the main wreckage.

Wreckage Examination

All fractures displayed overstress features consistent with an in-flight breakup. Mapping indicated that the tail components likely separated first, followed by the right wing. This structural failure resulted in the horizontal and vertical stabilizers deforming and then separating from the airplane. The lack of heat damage on these components suggested that separation occurred before the fire, and that the inflight fire observed by the witness was likely a result of the breakup. No evidence of any mechanical malfunctions or failures that would have preceded the inflight breakup was found.

Occupants

Both occupants were killed.

Probable cause

The pilot’s loss of control following an encounter with structural icing, which resulted in an inflight breakup of the airplane.