Casualties unknown

Engine Failure Forces Emergency Landing, Aircraft Collides with Berm (N9591Y)

Boulder City, NV, US

On May 21, 2000, a Beech 35-B33 (registration N9591Y) operated by Glendale Aviation was involved in an aviation accident near Boulder City, NV. Investigators recorded the probable cause as: catastrophic engine failure resulting in loss of engine power during descent, necessitating a forced landing, during which the airplane collided with a berm. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

During descent, a catastrophic engine failure forced a landing on a model airplane field. The aircraft landed successfully but could not stop before hitting a berm, collapsing the landing gear.

Incident Overview

The aircraft experienced a catastrophic engine failure while descending toward the destination airport, prompting an emergency landing. The pilot reported that the flight was uneventful until preparations began for descent over Lake Mead. Suddenly, a loud 'pop or clunk' emanated from the engine compartment. The engine began to vibrate and run roughly before quitting altogether, accompanied by a large amount of smoke.

Emergency Landing

The pilot selected a paved model airplane field for the forced landing. The landing was successful, but the aircraft could not be stopped before colliding with a berm at the edge of the field. The impact collapsed the landing gear.

Post-Accident Examination

Following recovery, an FAA airworthiness inspector examined the engine. A large hole was discovered in the upper left rear engine case, in the area of the No. 1 and No. 2 connecting rods. The No. 2 connecting rod had separated from the crankshaft, with the journal end severely peened and damaged, protruding from the hole in the case. The No. 2 bearing insert was destroyed, and heat discoloration was noted on the journal saddle. The corresponding portion of the crankshaft also showed heat discoloration and scoring. Additionally, the oil pressure line from the engine to the Hobbs meter pressure switch was found broken at the switch's fitting, with oil covering the engine compartment area around the broken fitting.

Probable cause

catastrophic engine failure resulting in loss of engine power during descent, necessitating a forced landing, during which the airplane collided with a berm

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X21048. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.