What happened
On 14 August 2012, a RAF 2000 GTX-SE gyroplane, registration G-ONON, was performing a private flight near Canterbury, Kent. The flight began with a takeoff attempt in a south-easterly direction on a 460 m grass airstrip. During this initial attempt, the pilot noticed a perceived engine hesitation and decided to abort the takeoff. After allowing the engine to reach operating temperature, a second takeoff was initiated in a north-westerly direction.
While the aircraft was at an altitude of approximately 40 to 50 ft, the engine lost power. The pilot confirmed the throttle position remained unchanged and immediately prepared for an emergency landing on the remaining portion of the runway. To reach the end of the strip, the pilot had to halt all forward momentum before descending vertically. This maneuver resulted in a hard landing at the runway's end, causing damage to the propeller and landing gear. There were no injuries to the pilot.
The investigation
The investigation focused on the sudden loss of power and the condition of the engine components. It was noted that a new electronic throttle position sensor had recently been installed on the aircraft. While ground runs following the accident showed normal engine indications, the engine subsequently idled at a significantly higher RPM than specified. The recently installed throttle position sensor was found to have failed, though investigators could not determine if this failure was caused by the accident itself. The pilot's checks confirmed that fuel pumps were functioning correctly and producing appropriate pressure, and no electronic fault codes were present. However, the possibility of fuel vapour lock due to the aircraft being parked in direct sunlight was not ruled out.
Findings
- The engine lost power at an altitude of 40 to 50 ft during the second takeoff attempt.
- The pilot performed a controlled but hard landing to avoid leaving the runway.
- The failure of the recently fitted electronic throttle position sensor was identified, though its direct role in the power loss remained unconfirmed.
- Fuel vapour lock remained a potential contributing factor due to high ambient temperatures and recent sun exposure.