Casualties unknown

Engine Failure Forces Emergency Landing on Sandbar After Oil Pressure Drop (N1673U)

Holy Cross, AK, US

On June 20, 1998, a Cessna 207 (registration N1673U) operated by Inland Aviation Services Inc. was involved in an aviation accident near Holy Cross, AK. Investigators recorded the probable cause as: The improper installation/undertorquing of the engine crankcase bolts by company maintenance personnel, and a subsequent fracture of the engine crankshaft. A factor in the accident was unsuitable terrain for a forced landing. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 2 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
Aircraft registered N1673U
Aircraft registered N1673U. Photo: NTSBgov / Public domain, via Wikimedia Commons

During an air taxi flight over remote terrain, the engine oil pressure dropped and temperature rose, leading to engine failure. The pilot executed an emergency landing on a sandbar, resulting in wing and fuselage damage.

Accident Overview

A pilot and three passengers were on an air taxi flight over remote terrain. While cruising at about 2,200 feet, the engine oil pressure began to drop and the oil temperature began to rise. The pilot decided to divert to the nearest airport, but the engine subsequently quit running. The pilot selected an emergency landing area on a sand bar along a river, which contained several willow trees. During the landing, the airplane sustained damage to the wings and fuselage.

Engine History and Examination

The engine had accrued 1,491 hours since its last overhaul. During that period, company maintenance personnel performed seven cylinder changes. An examination of the engine revealed that the crankshaft was broken along the aft, lower edge of the number two cheek journal, at the forward radius of the number two main bearing journal. The fracture line was straight and flat, running through the full dimension of the number two cheek journal, and was oriented perpendicular to the longitudinal axis of the crankshaft. The number two main bearing was broken and flattened, and the number two main bearing saddle was also flattened and distorted. Additionally, the left and right engine case halves mating surface exhibited galling and fretting at the number two main journal bolt holes.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X10216. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.