Investigation number
200502078
Occurrence date
Location
Shannons Flat
State
New South Wales
Report release date
Report status
Final
Investigation type
Occurrence Investigation
Investigation status
Completed
Aviation occurrence category
Engine failure or malfunction
Occurrence class
Accident
Highest injury level
Minor

At 1110 Eastern Standard Time on 12 May 2005, a Eurocopter EC120B helicopter, registered VH-ADC, departed Canberra enroute to Jindabyne, NSW, with the pilot and two passengers on board. The pilot reported that at about 30 minutes after departure, while in cruise flight at 5,000 ft above ground level in smooth flying conditions, the main rotor speed (NR) RPM audio warning sounded.

The pilot reported that a scan of the instrument panel revealed that the NR was exceeding 450 RPM and that he then used the collective pitch lever to reduce the NR. The pilot noted that it took approximately 5 to 7 seconds to arrest the high NR rate, which then silenced the audio warning. The helicopter was flared for landing as it lost altitude and impacted the undulating ground It then bounced back into the air momentarily, before it impacted the ground once more and slid to a halt. The pilot then applied the rotor brake to stop main rotor rotation and assisted the passengers to exit the helicopter. There were no injuries to the passengers and minor injuries to the pilot.

The helicopter was determined to be within weight and balance limitations and carried sufficient fuel for the flight. Testing of the engine could not duplicate the in-flight engine shutdown as reported.

Aircraft Details
Manufacturer
Eurocopter
Model
EC120
Registration
VH-ADC
Operation type
Private
Sector
Helicopter
Departure point
Canberra, ACT
Destination
Jindabyne, NSW