1 fatality

1960-04-27: Ilyushin II-18 (CCCP-75648) — Aeroflot - Russian International Airlines — Sverdlovsk, Russia

Sverdlovsk, RussiaLanding (descent or approach)

On April 27, 1960, an Ilyushin II-18 (registration CCCP-75648) operated by Aeroflot - Russian International Airlines was involved in an aviation accident near Sverdlovsk, Russia during landing or approach. One person was killed. Investigators recorded the probable cause as: Wrong approach configuration on part of the instructor who adopted a too high speed on final (260 km/h) and failed to adopt a correct flare configuration, causing the airplane to adopt a nose down attitude and to struck the runway surface nose first, causing… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781246611Data APIEditorial standards

During a night training approach at Sverdlovsk-Koltsovo Airport, an aircraft struck the runway nose-first, shearing the nose gear, bounced, then veered off runway and caught fire. One crew member was killed, four others injured.

Accident Sequence

The crew was conducting a local training flight at Sverdlovsk-Koltsovo Airport. After completing two landings and two approaches, the crew began a new approach at night. During the final segment, while flying at a speed of 260 km/h, the aircraft pitched nose-down and struck the runway with its nose landing gear. The nose gear was sheared off on impact. The aircraft then bounced and climbed to approximately 10 meters above the runway before contacting the surface again in a nose-down attitude. Following the second impact, the aircraft became uncontrollable and veered off the runway to the right. It came to rest in flames. The flight mechanic was killed, and the four other occupants were injured. The aircraft sustained partial destruction from the fire.

Probable Cause

The official investigation attributed the accident to a wrong approach configuration by the instructor. The instructor adopted an excessively high speed on final approach (260 km/h) and failed to execute a proper flare, leading to the nose-down attitude and nose-first runway contact that caused the nose gear to fail. Additionally, the rear trunk was loaded with 600 kg of ballast instead of the required 1,000 kg. This discrepancy shifted the center of gravity forward, contributing to the nose-down condition. The investigation could not determine whether icing conditions were a contributing factor.