Agusta A109C rotor blades strike fuel bowser during landing

Casualties unknown • Private helicopter landing site at High Legh, Cheshire, GB

An Agusta A109C sustained extensive rotor damage after its blades struck a fuel bowser during a landing at a private site in Cheshire.

What happened

On 21 June 2006, an Agusta A109C, registration G-HBEK, was performing a private flight from Knutsford to a private landing site at High Legh, Cheshire. The flight was intended to position the aircraft for overnight parking. Due to a high volume of planned movements, the pilot intended to refuel the aircraft using a mobile fuel bowser.

Upon arrival, the pilot noted that another helicopter was parked on the taxiway in an obstructive position. To facilitate refueling with the short hoses available on the bowser and to maintain distance from the other aircraft, the pilot attempted a landing close to the bowser. The landing was complicated by strong, gusty crosswinds, with winds recorded at 25 knots gusting to 32 knots.

Following touchdown and the standard two-minute engine shutdown period, the rotor speed began to decrease. As the RPM dropped below 50%, the main rotor blades began to droop. The blades struck the side of the fuel bowser, and despite the pilot's immediate application of the rotor brake, the blades continued to strike the equipment violently. Eventually, one blade became lodged in the bowser, causing the rotors to stop abruptly.

The investigation

The investigation examined the positioning of the aircraft and the equipment at the landing site. It was established that the pilot sought to land as close to the bowser as possible to ensure the refueling hoses could reach the aircraft's connectors. The investigation also looked into the ground conditions and the placement of the fuel bowser, which had been positioned on the edge of the concrete pad.

Findings

  • The Agusta A109C sustained extensive damage to the main rotor blades and the rotor head assembly, including a sheared rotor damper.
  • Both engines required inspection following the impact.
  • The primary cause of the accident was the rotor blades drooping and striking the fuel bowser as rotor speed decreased during shutdown.
  • The pilot's decision-making was influenced by the need to facilitate refueling and the obstructive position of another aircraft.
  • The fuel bowser sustained only minor damage.

Probable cause

The accident was caused by the main rotor blades drooping and striking the fuel bowser during the engine shutdown sequence, a situation exacerbated by the pilot's decision to land in close proximity to the equipment to accommodate short refueling hoses.

Frequently asked questions

What happened in the 2006-06-21 Agusta A109C accident near Private helicopter landing site at High Legh, Cheshire, GB?

An Agusta A109C sustained extensive rotor damage after its blades struck a fuel bowser during a landing at a private site in Cheshire.

What aircraft was involved and where did it happen?

The accident on 2006-06-21 involved a Agusta A109C, registration G-HBEK, at Private helicopter landing site at High Legh, Cheshire, GB.

What was the probable cause of the accident?

The accident was caused by the main rotor blades drooping and striking the fuel bowser during the engine shutdown sequence, a situation exacerbated by the pilot's decision to land in close proximity to the equipment to accommodate short refueling hoses.

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