1 fatality

1998-10-01: Rockwell Grand Commander 680 (N5YZ) — Desert Aircraft Sales — Palm Springs, United States of America

Palm Springs, United States of AmericaLanding (descent or approach)

On October 1, 1998, a Rockwell Grand Commander 680 (registration N5YZ) operated by Desert Aircraft Sales was involved in an aviation accident near Palm Springs, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: The pilot's failure to properly use the manual turbocharger wastegates and to monitor the manifold pressure during takeoff. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781204870Data APIEditorial standards

During a local checkout flight, the aircraft stayed low and reported a fuel problem. It struck power lines while returning. Postaccident examination found engine detonation and partially closed manual wastegates, which can increase manifold pressure beyond limits.

Accident Overview

During a local area aircraft checkout flight, the aircraft remained low and the pilot informed the tower of a fuel problem. The pilot attempted to return to the airport but collided with power lines approximately 1.5 miles north of the airfield.

Aircraft and Modifications

The aircraft had been modified with higher horsepower engines and turbochargers equipped with manual wastegates. The engines were restricted to a maximum manifold pressure of 29.5 inHg.

Preflight Fueling

In preparation for a trip, the aircraft had been fueled twice the day before with aviation-grade 100LL fuel. A postaccident fuel sample tested negative for jet fuel contamination.

Engine Examination

Examination of the engines revealed evidence of severe detonation. During the postaccident inspection of the aircraft systems, the manual wastegates were found partially closed. In this position, the wastegates can provide additional manifold pressure, potentially exceeding engine limitations.

Probable Cause

The official probable cause was stated as the pilot's failure to properly use the manual turbocharger wastegates and to monitor the manifold pressure during takeoff.