No fatalities

2000-07-20: Mitsubishi MU-2 Marquise (N8484T) — Skyline Aviation (Netherlands) — Den Helder-De Kooy, Netherlands

Den Helder-De Kooy, NetherlandsLanding (descent or approach)

On July 20, 2000, a Mitsubishi MU-2 Marquise (registration N8484T) operated by Skyline Aviation (Netherlands) was involved in an aviation accident near Den Helder-De Kooy, Netherlands during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The problem was the consequence of an expired adjustment screw of the speed controller ('prop governor') on the right engine, so that it did not come into 'reverse pitch' but continued to provide forward thrust, causing an asymmetric aerodynamic braking… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781203382Data APIEditorial standards

An aircraft conducting a radar tracking flight over the North Sea veered off runway 03 at Den Helder-De Kooy Airport after experiencing asymmetric braking due to a propeller governor malfunction. The crew escaped uninjured, but the aircraft was damaged beyond repair.

Incident Overview

An aircraft on a radar tracking mission departed Den Helder-De Kooy Airport and flew over the North Sea. After an uneventful flight, the crew returned to De Kooy Airport for landing. Following touchdown on runway 03, the pilots activated the thrust reverser systems, at which point the aircraft became uncontrollable.

Pilot Actions

The pilot attempted to regain control by moving the left throttle from reverse back to forward thrust to turn the aircraft to the right. He then feathered the right propeller and cut off the fuel supply, causing the right engine to stop. Despite these efforts, the aircraft veered off the left side of the runway and came to rest in a ditch.

Outcome

Both pilots escaped uninjured. The aircraft sustained damage beyond economic repair.

Probable Cause

According to the official investigation, the landing speed, touchdown point, runway length, and runway condition were all considered satisfactory. The problem was attributed to an expired adjustment screw on the speed controller (prop governor) of the right engine. This prevented the propeller from achieving reverse pitch, instead continuing to provide forward thrust, which resulted in an asymmetric aerodynamic braking effect. Additionally, the Beta light indicator had burned out and could not illuminate, depriving the pilot of a potential warning about the reverse thrust system malfunction.