US Army Intelligence and Security Command Aircraft Crash in Chesapeake Bay

5 fatalities • Patuxent River NAS, United States of America • Landing (descent or approach)

A US Army INSCOM aircraft crashed into the Chesapeake Bay during its approach to Patuxent River NAS, resulting in the loss of all five crew members.

What happened

On a flight originating from Davison AAF (Fort Belvoir), an 88-0321 (N296CA) aircraft was performing its approach to Patuxent River NAS. While flying at an altitude of approximately 800 feet, the aircraft transitioned into an uncontrolled descent and impacted the waters of the Chesapeake Bay. The wreckage was located less than 100 yards from the shoreline, where it settled at a depth of 45 feet.

The incident resulted in five fatalities among the crew members on board. The aircraft was being operated by the US Army Intelligence and Security Command (INSCOM).

Findings

Investigations into the crash determined that the primary factor was a pilot error during the final approach phase. Specifically, the crew incorrectly engaged the beta range on the propellers while at an altitude of 800 feet, which triggered the subsequent uncontrolled descent and impact.

Probable cause

The crew mistakenly selected the propeller beta range during the final approach, leading to an uncontrolled descent.

Frequently asked questions

What happened in the 1989-12-01 Casa 212 Aviocar accident near Patuxent River NAS, United States of America?

A US Army INSCOM aircraft crashed into the Chesapeake Bay during its approach to Patuxent River NAS, resulting in the loss of all five crew members.

Were there any fatalities in the 1989-12-01 Casa 212 Aviocar accident?

The accident was fatal, resulting in 5 fatalities.

What aircraft was involved and where did it happen?

The accident on 1989-12-01 involved a Casa 212 Aviocar, registration N296CA, operated by United States Army, at Patuxent River NAS, United States of America.

What was the probable cause of the accident?

The crew mistakenly selected the propeller beta range during the final approach, leading to an uncontrolled descent.

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