Casualties unknown

2000-05-09: Beech B24R (N6951R) — Anchorage, AK

Anchorage, AK, US

On May 9, 2000, a Beech B24R (registration N6951R) was involved in an aviation accident near Anchorage, AK. Investigators recorded the probable cause as: A fatigue failure of the crankcase through bolt, the separation of number 3 cylinder assembly, and the inadequate maintenance/service of the airplane by company maintenance personnel. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During initial descent, an engine ran rough, lost power, then suffered severe vibration and complete power loss. The forced landing resulted in collision with a power line and the street. Investigation revealed a broken cylinder and fatigue cracking in a crankcase thru-bolt.

Event Description

While returning to the airport during initial descent, the engine began to run rough and lose power. The roughness improved momentarily, followed by severe engine vibration, a loud bang, and complete loss of engine power. During a forced landing in a densely populated neighborhood, the airplane struck a power line, veered to the right, collided with the street, and came to rest in the front yard of a daycare center.

Flight Crew

The first pilot, a certificated flight instructor, was providing flight instruction to the second pilot, a certificated private pilot.

Engine Examination

Examination of the engine revealed that the number 3 cylinder was broken free at the crankcase-mounting flange. A metallurgical examination of the number 4 position crankcase thru-bolt showed signs of fatigue cracking that emanated from the thread root. In addition, the cylinder flange mating surface displayed signs of fretting damage consistent with relative movement between the cylinder and the crankcase.

Maintenance History

The operator's director of maintenance stated that about 40 hours before the accident, he repaired a substantial oil leak between the number 3 cylinder and the engine crankcase. He said that during the repair he removed the number 4 position crankcase thru-bolt nut, applied an engine sealant, reinstalled the through bolt nut, and torqued the nut in accordance with the Lycoming overhaul manual. There was no engine log book entry pertaining to the engine total time, aircraft total time, or date when this repair was accomplished.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20931. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.