18 fatalities

Ryan Flight 103 Accident: Improper Loading and Aft Center of Gravity Cited (N401RA)

Homer, United States of AmericaLanding (descent or approach)

On November 23, 1987, a Beechcraft 1900C (registration N401RA) operated by Ryan Air was involved in an aviation accident near Homer, United States of America during landing or approach. 18 people were killed. Investigators recorded the probable cause as: The failure of the flight crew to properly supervise the loading of the airplane which resulted in the centre of gravity being displaced to such an aft location that the airplane control was lost when the flaps were lowered for landing. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 16 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards
Aircraft registered N401RA
Aircraft registered N401RA. Photo: Jean-Luc ALTHERR / CC0, via Wikimedia Commons

During arrival, Ryan flight 103 crashed short of runway 03 due to an aft center of gravity caused by improper cargo loading, leading to loss of control when flaps were lowered. Ice accumulation on leading edges was also present. 18 occupants were killed, 3 survived.

Impact and Rescue

The aircraft, operating as Ryan flight 103, crashed short of runway 03 during arrival. The fuselage remained intact upon impact, but the belly structure was compressed, and vertical deceleration forces exceeded the design capability of the seats. Rescue personnel experienced difficulty shutting off the aircraft's electrical power, which delayed the removal of the first officer from the aircraft.

Weight and Balance

Investigation revealed that the aircraft was loaded with approximately 600 pounds more cargo than the first officer had requested. The center of gravity was calculated to be 8 to 11 inches behind the allowable aft limit. The flight crew did not comply with company and Federal Aviation Administration procedures in computing the center of gravity.

Ice Accumulation

During the flight, up to 3/8 inches of ice accumulated on the aircraft's leading edges. Flight tests showed that there would be no significant difficulty in controlling the aircraft with up to 1.5 inches of ice on the leading edges, but static stability would deteriorate during flap extension with an aft center of gravity configuration.

Flight Control Evidence

There was evidence that the crew lost control of the aircraft as the flaps were lowered. The right flap actuator was found in the 7 to 12 degree position, and the stabilizer trim was found at the full nose-down position.

Probable Cause

The official probable cause of the accident was the failure of the flight crew to properly supervise the loading of the airplane, which resulted in the centre of gravity being displaced to such an aft location that airplane control was lost when the flaps were lowered for landing.