Aircraft stall and crash during landing approach

No fatalities • Kathmandu-Tribhuvan, Nepal • Landing (descent or approach)

A private aircraft experienced a stall and crashed near the runway threshold during a landing approach in heavy crosswinds, resulting in no fatalities.

What happened

During the final stages of an approach to land, a HB-FAX aircraft encountered significant crosswinds. While on short final, the plane entered a stall and impacted the ground within the runway threshold area. Although the impact caused the aircraft to be damaged beyond repair, there were no fatalities or injuries reported among those on board.

Findings

An investigation into the accident revealed that the fuel selector valve had been set to the lower tank. Due to the specific attitude of the aircraft during its final approach, this configuration prevented sufficient fuel from reaching the engine. This fuel starvation was a critical factor in the loss of power that led to the stall.

Probable cause

The engine failed due to fuel starvation caused by the incorrect positioning of the fuel selector valve during a crosswind approach.

Frequently asked questions

What happened in the 1967-02-08 Pilatus PC-6 (Porter & Turbo Porter) accident near Kathmandu-Tribhuvan, Nepal?

A private aircraft experienced a stall and crashed near the runway threshold during a landing approach in heavy crosswinds, resulting in no fatalities.

Were there any fatalities in the 1967-02-08 Pilatus PC-6 (Porter & Turbo Porter) accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1967-02-08 involved a Pilatus PC-6 (Porter & Turbo Porter), registration HB-FAX, operated by Swiss Government, at Kathmandu-Tribhuvan, Nepal.

What was the probable cause of the accident?

The engine failed due to fuel starvation caused by the incorrect positioning of the fuel selector valve during a crosswind approach.

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