2 fatalities

1996-06-21: Harbin Yunsunji Y-12 (B-3822) — China Flying Dragon Special Aviation Company — Shanghai-Hongqiao, China

Shanghai-Hongqiao, ChinaLanding (descent or approach)

On June 21, 1996, a Harbin Yunsunji Y-12 (registration B-3822) operated by China Flying Dragon Special Aviation Company was involved in an aviation accident near Shanghai-Hongqiao, China during landing or approach. 2 people were killed. Investigators recorded the probable cause as: The crew initiated the last turn prematurely, causing the aircraft to descend below the minimum descent altitude in limited visibility. The aircraft deviated 3 km to the right of the approach path. Lack of visibility was a contributing factor. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781206930Data APIEditorial standards

A twin-engine aircraft crashed on a hill about 3 km short of Shanghai Hongqiao Airport after the crew made a premature last turn in limited visibility. One pilot and one passenger were killed, and 10 others were injured.

Incident

During a descent to Shanghai-Hongqiao Airport following an uneventful flight from Dalian, the aircraft encountered limited visibility due to marginal weather conditions. While completing a last turn to join the approach path, the twin-engine aircraft crashed on the top of a hill approximately 3 km short of the runway. The accident resulted in the death of one pilot and one passenger, and injuries to 10 other occupants.

Investigation

Investigators examined the circumstances of the crash, focusing on the crew's actions and environmental factors. The aircraft was found to have deviated from the intended approach path, and visibility conditions were noted as limited.

Probable Cause

The official investigation determined that the crew initiated the last turn prematurely. This caused the aircraft to descend below the minimum descent altitude (MDA) in limited visibility. At the time of the accident, the aircraft had deviated 3 km to the right of the approach path. The lack of visibility was identified as a contributing factor.