No fatalities

Left Engine Power Loss Leads to Forced Landing and Injuries (N36CA)

Riviera, United States of AmericaFlight

On February 8, 1984, a Piper PA-31 Cheyenne (registration N36CA) operated by Nevada National Leasing Corporation was involved in an aviation accident near Riviera, United States of America in flight. No fatalities were reported. Investigators recorded the probable cause as: Occurrence #1: loss of engine power (total) - mech failure/malfunc; findings: 1. turbine assembly,turbine blade - fatigue; 2. wrong engine shutdown - performed - pilot in command; 3. inadequate training(emergency procedure(s)) - pilot in command; 4. 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

Aircraft N36CA lost left engine power during climb; pilot shut down right engine, resulting in total power loss. Forced landing in brush with 22° flaps; three occupants injured. Turbine blade fatigue and pilot error cited.

Incident Summary

Aircraft N36CA experienced a left engine power loss approximately eight minutes after takeoff, during the climb to cruise. The pilot transmitted on unicom that an engine was lost and the aircraft was returning. A warning horn was audible in the background. The aircraft did not return, prompting the airport manager to alert the sheriff and initiate a search. The aircraft was located about one hour after departure.

Sequence of Events

The forced landing was conducted in a flat, wings-level attitude with 22° of flaps extended. Initial impact occurred in an area of approximately 8-foot-high brush. The aircraft traveled 595 feet on a heading of 140° from the initial impact point to its final resting position. The pilot's son later reported that the pilot shut down the right engine in flight, resulting in a total loss of power on both engines.

Injuries and Damage

All three occupants were injured. The pilot was restrained by a lap belt and harness but struck his head on the copilot's control yoke during the accident. The left engine turbine blade had failed due to fatigue.

Probable Cause

The official probable cause findings include: loss of engine power (total) due to mechanical failure/malfunction during climb to cruise. Specific findings were: fatigue failure of a turbine blade in the left engine; the pilot performed a wrong engine shutdown; the pilot had inadequate training in emergency procedures; the turbine blade failed totally; propeller feathering was not achieved; and the pilot's emergency procedure performance was poor. The forced landing occurred during descent/emergency, and the aircraft collided with terrain during landing flare/touchdown, with high vegetation as a contributing condition.

Frequently asked questions

What happened in the 8 Feb 1984 Piper PA-31 Cheyenne accident near Riviera, United States of America?

Aircraft N36CA lost left engine power during climb; pilot shut down right engine, resulting in total power loss. Forced landing in brush with 22° flaps; three occupants injured. Turbine blade fatigue and pilot error cited.

Were there any fatalities in the 8 Feb 1984 Piper PA-31 Cheyenne accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 8 Feb 1984 involved a Piper PA-31 Cheyenne, registration N36CA, operated by Nevada National Leasing Corporation, at Riviera, United States of America.

What was the probable cause of the accident?

Occurrence #1: loss of engine power (total) - mech failure/malfunc; findings: 1. turbine assembly,turbine blade - fatigue; 2. wrong engine shutdown - performed - pilot in command; 3. inadequate training(emergency procedure(s)) - pilot in command; 4. turbine assembly,turbine blade - failure,total; 5. propeller…