No fatalities

Oil Leak Leads to Single-Engine Go-Around and Crash Near Airport (N9718T)

Shelby, United States of AmericaTakeoff (climb)

On July 9, 1985, a Cessna 303 Crusader (registration N9718T) operated by Eugene F. Young was involved in an aviation accident near Shelby, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: Loss of engine power (partial) due to an oil leak of undetermined origin. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

After takeoff, a pilot noticed oil from the left engine, attempted to land but went around, lost oil pressure, feathered the engine, and crashed 2 miles northeast of the airport; the pilot escaped with minor injuries.

Accident Overview

A pilot, the sole occupant of an aircraft, experienced an oil leak from the left engine shortly after takeoff from runway 23. The pilot initiated a turn to land on runway 05 but could not align with the runway. Choosing to go around, the pilot applied full power, at which point the left engine oil pressure dropped to zero psi. The pilot feathered the left engine and attempted a single-engine go-around. The landing gear and flaps remained extended during the maneuver. The aircraft subsequently crashed approximately 2 miles northeast of the airport and was destroyed by a post-crash fire.

Pilot Injuries and Evacuation

The pilot escaped the wreckage with minor injuries. No other occupants were on board.

Engine and Damage Details

The left engine exhibited an oil leak, the origin of which could not be determined due to the extensive fire damage. The aircraft was destroyed by fire.

Official Findings and Probable Cause

According to the investigation, the accident sequence involved four occurrences:

  • Occurrence #1: Loss of engine power (partial) due to a mechanical failure/malfunction during the takeoff-initial climb phase. The specific reason for the occurrence was undetermined, but a fluid leak (oil) was found.
  • Occurrence #2: Forced landing during the descent-emergency phase.
  • Occurrence #3: In-flight collision with an object (tree(s)) during the landing-flare/touchdown phase.
  • Occurrence #4: In-flight collision with terrain/water during the landing-flare/touchdown phase, with the terrain condition noted as ground.

The probable cause as stated by the investigation is the partial loss of engine power due to an oil leak of undetermined origin.