No fatalities

Dual Engine Power Loss Due to Ice Accumulation Leads to Gear Collapse in Open Field (N23AZ)

Washington-Dulles, United States of AmericaLanding (descent or approach)

On December 18, 1987, a Swearingen SA226 Metro II (registration N23AZ) operated by AVAir - Air Virginia was involved in an aviation accident near Washington-Dulles, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The pilot in command's improper in-flight planning/decision and failure to use anti-ice/deice system, combined with inadequate initial training by the check pilot and inadequate certification/approval by the company/operator management, led to total loss of… 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

While descending through a cloud layer for landing at Dulles International Airport, an aircraft accumulated trace rime ice. The captain opted not to use engine inlet anti-ice, leading to both engines losing power. The aircraft landed in an open field where the landing gear collapsed.

Event Summary

During a scheduled landing approach to Washington Dulles International Airport (IAD), the aircraft descended through a cloud layer. The crew reported that trace rime ice accumulated on the wing surfaces. Although pitot and stall avoidance system (SAS) heat were used, the captain elected not to activate engine inlet anti-ice.

Shortly after passing the outer marker, the left engine lost power, followed by the right engine. The captain managed to set the aircraft down in an open field. During the landing roll, the landing gear collapsed.

Post-Accident Inspection

Following the event, the engines were successfully run up at a Garrett facility. Ice was found beneath the right wing that matched the curvature of the wing's leading edge. Additionally, a round conical piece of ice was discovered along the wreckage path, matching the nose of the propeller spinner.

Flight Manual Guidance

The flight manual contained a warning and a note stating that engine heat and continuous ignition must be used after leaving icing conditions until the pilot is confident that any significant residual ice will not be ingested into the engines.

Probable Cause

The official probable cause findings identified: (1) loss of engine power (total) due to weather conditions (icing), the pilot in command's improper in-flight planning/decision and failure to use anti-ice/deice system, inadequate initial training by the check pilot, and inadequate certification/approval by the company/operator management; (2) gear collapsed due to terrain conditions (open field, downhill) and dark night lighting.