No fatalities

Propeller Beta Mode During Landing Results in Collision with Snow Bank (N149JA)

Hayden-Yampa Valley, United States of AmericaLanding (descent or approach)

On February 3, 1982, a Mitsubishi MU-2 Marquise (registration N149JA) operated by J. A. Baldwin Manufacturing Company was involved in an aviation accident near Hayden-Yampa Valley, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Occurrence #1: airframe/component/system failure/malfunction (propeller pitch change mechanism, reversing system, prop control unit – undetermined). This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

During landing at 20 feet AGL, the crew heard a propeller go into beta mode, causing a right yaw. The pilot lost control, and the aircraft struck a snow bank, separating the wings from the fuselage. The cause of the propeller anomaly could not be determined due to impact damage.

Incident Overview

While landing at approximately 20 feet above ground level, the flight crew heard a propeller transition into beta mode. This event caused the aircraft to yaw to the right. The pilot lost control of the aircraft, which subsequently collided with a snow bank. The impact resulted in the separation of the wings from the fuselage. Investigators were unable to determine why the propeller entered beta mode because of damage sustained during the collision.

Probable Cause Findings

The official investigation identified three occurrences and related findings:

Occurrence #1: Airframe/Component/System Failure or Malfunction

  • Phase of operation: Landing – flare/touchdown
  • Findings:

1. Propeller system/accessories, pitch change mechanism – undetermined 2. Propeller system/accessories, reversing system – undetermined 3. Propeller system/accessories, prop control unit – undetermined

Occurrence #2: Loss of Control – On Ground/Water

  • Phase of operation: Landing – flare/touchdown
  • Findings:

4. Directional control – not maintained – pilot in command 5. Remedial action – not used – pilot in command 6. Ground loop/swerve – uncontrolled – pilot in command

Occurrence #3: In-Flight Collision with Terrain/Water

  • Phase of operation: Landing – roll
  • Findings:

7. Terrain condition – snowbank