Casualties unknown

2001-03-06: Agusta A109E, (I-CLRM) — Roma Elicottero Agusta A109E, IT

Roma Elicottero Agusta A109E, IT

On March 6, 2001, an Agusta A109E, (registration I-CLRM) was involved in an aviation accident near Roma Elicottero Agusta A109E, IT. Investigators recorded the probable cause as: Loss of power of engine number 1. This summary draws on records from the Italian National Flight Safety Agency (ANSV).

Sourcesthe Italian National Flight Safety Agency (ANSV)Primary reportUpdated 1785083425Data APIEditorial standards

On 6 March 2001, an Agusta A109E helicopter (I-CLRM) experienced a loss of power from engine number 1 during takeoff from a helipad in Malagrotta, Rome, resulting in a rollover and minor injuries to two passengers.

Flight History

On 6 March 2001, at 14:45 UTC (15:45 local time), an Agusta A109E helicopter, registration I-CLRM, was conducting a takeoff from a helipad in the Malagrotta area of Rome, Italy. After a vertical ascent to approximately one meter, the pilot applied forward cyclic and collective to initiate forward flight. The helicopter did not respond promptly, and the Master Warning light and an audible 'Rotor Low' alarm indicated insufficient power. The helicopter began to lose altitude. The pilot attempted to turn left to return to the helipad, but the aircraft impacted terrain with a slope of about 45 degrees a few meters from the pad. The uneven ground caused the helicopter to roll over. The engines were shut down and electrical systems isolated. All occupants evacuated the aircraft without assistance.

Injuries

The two passengers on board sustained minor injuries. The pilot reported no injuries. No fatalities occurred.

Damage

The helicopter sustained substantial damage. No third-party damage was reported.

Personnel

The pilot, a 54-year-old Italian male, held a valid commercial helicopter pilot license with ratings for AB47, AB206, and A109 types. His total flight experience was 6,054 hours and 10 minutes, including 741 hours and 15 minutes on the Agusta A109E. In the previous 90 days he had logged 10 hours and 10 minutes on type, with 10 minutes in the last 24 hours. Two technicians were aboard as passengers, one specialized in airframe maintenance and the other in avionics.

Aircraft Information

The accident aircraft was an Agusta A109E Power, serial number not specified, built in 1999. It was a twin-engine helicopter with a maximum takeoff weight of 2,850 kg and an empty weight of 1,883 kg. The rotor diameter was 11.00 meters.

Investigation Findings

The investigation determined that the accident was caused by a loss of power from engine number 1. The loss of power during the takeoff phase led to insufficient rotor RPM and lift, resulting in the aircraft descending and impacting the sloped terrain, causing the rollover.

Probable cause

Loss of power of engine number 1.