No fatalities

Pilot Unable to Prevent Propeller Feathering During Night Approach, Forced Landing on Highway (N3588Y)

Hayward, United States of AmericaLanding (descent or approach)

On April 27, 1988, a Piper PA-31-350 Navajo Chieftain (registration N3588Y) operated by Helicopters Unlimited was involved in an aviation accident near Hayward, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Pilot's failure to detect an uncommanded propeller feathering procedures established in the pilot's operating handbook. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary report: the U.S. National Transportation Safety Board (NTSB) historical archiveUpdated 2026-07-04Data APIEditorial standards

During a night visual approach, a pilot heard a flutter from the right engine and lost airspeed despite full throttle. A forced landing on a freeway resulted in a collision with a motor vehicle. Post-crash inspection found the left propeller feathered and engine controls in a high RPM setting.

Incident Summary

The pilot was conducting a visual descent at night to the destination airport. During the approach, the pilot reduced airspeed and deployed flaps. As the aircraft neared the airport, the pilot increased the flap angle and adjusted the propellers to the landing RPM, causing further airspeed decrease. At that moment, the pilot reported hearing a noise resembling flutter, which they believed originated from the right engine. Despite applying full throttle, the airspeed continued to decrease, prompting the pilot to execute a forced landing on a nearby freeway.

Collision and Post-Crash Examination

Upon touchdown, the aircraft collided with a motor vehicle and slid to a stop. A post-crash examination revealed that the RPM control levers and bellcranks were set to the high RPM position. The left propeller was found in the feathered position, indicating an uncommanded feathering event.

Probable Cause

The official probable cause was determined to be the pilot's failure to detect an uncommanded propeller feathering procedures established in the pilot's operating handbook. Contributing findings included a partial loss of engine power due to a failure of the propeller system/accessories feathering system, the pilot's non-compliance with emergency procedures, and impaired visual/aural perception during the approach phase. The forced landing occurred during the approach in VFR pattern conditions, and the collision with a vehicle took place during the landing flare/touchdown on a dark night on a roadway.

Frequently asked questions

What happened in the 27 Apr 1988 Piper PA-31-350 Navajo Chieftain accident near Hayward, United States of America?

During a night visual approach, a pilot heard a flutter from the right engine and lost airspeed despite full throttle. A forced landing on a freeway resulted in a collision with a motor vehicle. Post-crash inspection found the left propeller feathered and engine controls in a high RPM setting.

Were there any fatalities in the 27 Apr 1988 Piper PA-31-350 Navajo Chieftain accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 27 Apr 1988 involved a Piper PA-31-350 Navajo Chieftain, registration N3588Y, operated by Helicopters Unlimited, at Hayward, United States of America.

What was the probable cause of the accident?

Pilot's failure to detect an uncommanded propeller feathering procedures established in the pilot's operating handbook.