3 fatalities

Overweight Otter Crash After Beer Bottle Load Shift (C-FJIK)

Leo Creek, CanadaTakeoff (climb)

On November 26, 1979, a De Havilland DHC-3 Otter (registration C-FJIK) operated by Smithers Air Service was involved in an aviation accident near Leo Creek, Canada during takeoff. 3 people were killed. Investigators recorded the probable cause as: It was determined that there were no less than 4,773 bottles on board. A weight and balance calculation on this discovery indicated that the gross weight of the Otter was 637 pounds over the maximum, with the C of G 11.5 inches aft of the rear limit. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

An Otter aircraft crashed after takeoff due to severe overweight and aft center of gravity from 4,773 beer bottles, exceeding elevator control limits. Three passengers died in the post-crash fire; the pilot was thrown clear.

Accident Details

A de Havilland Canada Otter aircraft, chartered to transport three passengers and a stove to a remote hunting and fishing lodge, crashed shortly after takeoff on the return flight to Smithers. Environmentally conscious passengers had chosen to take their empty beer bottles with them—approximately 250 to 300 cases. One passenger occupied the cockpit; the other two sat in the first row of seats. The remainder of the aircraft was filled with empty beer bottles.

Immediately after liftoff, the aircraft pitched to a steep nose-high attitude that the pilot was unable to prevent or correct. The Otter then stalled and fell to the ground. On impact, a severe fuel-fed fire erupted, gutting the aircraft. The pilot was thrown clear, but the three passengers died in the fire.

Pilot Background

The pilot of the Otter was Emil Mesich, owner of Smithers Air Service. Following the accident, the company ceased trading and went into receivership. Mesich later worked for Central Mountain Air Services Ltd., based at Smithers.

Weight and Balance Analysis

An investigation determined there were 4,773 bottles on board. Weight and balance calculations showed the Otter’s gross weight was 637 pounds over the maximum, with the center of gravity (C of G) located 11.5 inches aft of the rear limit. Calculations by de Havilland Canada indicated that an Otter will run out of elevator control when the C of G is four inches aft of the rear limit. The pilot had estimated that a dozen bottles weighed 3 to 4 pounds, but the true weight was 7 pounds.

Probable cause

It was determined that there were no less than 4,773 bottles on board. A weight and balance calculation on this discovery indicated that the gross weight of the Otter was 637 pounds over the maximum, with the C of G 11.5 inches aft of the rear limit. Calculations made by DHC showed that an Otter will run out of elevator control with the C of G four inches aft of the rear limit. The pilot had estimated that a dozen bottles weighed 3 to 4 pounds when the true weight was 7 pounds.