Casualties unknown

1998-08-08: Westland-Bell 47 G-3 — in Finow, DE

in Finow, DE

On August 8, 1998, a Westland-Bell 47 G-3 was involved in an aviation accident near in Finow, DE. Investigators recorded the probable cause as: Flight error: the pilot did not sufficiently monitor rotor rpm during climb and failed to notice a drop in rpm, leading to reduced tail rotor effectiveness and a spin. This summary draws on records from the German Federal Bureau of Aircraft Accident Investigation (BFU).

Sourcesthe German Federal Bureau of Aircraft Accident Investigation (BFU)Primary reportUpdated 1785061435Data APIEditorial standards

On 8 August 1998, a Westland-Bell 47 G-3 helicopter was destroyed in Finow after entering an uncontrolled spin during climb. The pilot failed to monitor rotor rpm, causing loss of tail rotor effectiveness.

Accident Details

On 8 August 1998, a Westland-Bell 47 G-3 helicopter was destroyed in an accident at the Finow airfield. The helicopter, operated by its owner-pilot for a private sightseeing flight with two passengers, was taking off from the runway into the wind, climbing in a low-altitude trajectory over the taxiway.

Flight Sequence

After accelerating to 40–60 km/h and initiating a climb, the helicopter passed over a hangar or shelter located directly ahead on the planned takeoff path. At that point, the helicopter began to yaw uncontrollably to the right. After several rotations, it struck the ground. All occupants evacuated before the helicopter caught fire and was completely consumed by the flames.

Investigation Findings

The investigatory body found no evidence of technical defects. All damage was attributed directly to the accident sequence. Based on statements from the pilot and knowledgeable passengers, a technical cause was considered unlikely.

Probable Cause

The investigation concluded that the accident was likely due to a pilot error: during the climb, the pilot did not sufficiently monitor the rotor rpm and failed to notice—or noticed too late—a drop in rpm. This reduction in rotor speed diminished the effectiveness of the tail rotor, causing the helicopter to yaw. Given the low altitude above the shelter, recovery from the emergency was virtually impossible.