Robinson R22 BETA N83509

Summary

On 20 July 2011 at about 15:26 local time, a Robinson R22 BETA registered N83509, operated by Nassau Helicopters Inc, was involved in an accident near Dayton, New Jersey, United States. 2 people were on board and 2 were seriously injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

20 July 2011 at 15:26

Classification

Accident

Location

Dayton, New Jersey, United States

Coordinates

40.3697, -74.5031

Aircraft

Robinson R22 BETA

Registration

N83509

Category

Helicopter

Engines

1

Operator

Nassau Helicopters Inc

Operating rule

Part 91: General Aviation

Purpose of flight

Aerial Observation

Phase of flight

Not recorded

Route

Princeton → Princeton

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

ERA11LA409

2 people were seriously injured.

The pilot's inadequate compensation for wind during an out-of-ground-effect hover, which resulted in a loss of control due to settling with power and loss of tail rotor effectiveness.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot slowed the helicopter to an out-of-ground-effect hover at an altitude of 400 to 500 feet above ground level (agl) while performing a photography mission. The photographer asked for a different vantage point; as the pilot explained that wind and high power demands would prevent him from accommodating the request, the helicopter began to "settle with power." The pilot attempted to arrest the descent with a reduction of power and a forward cyclic input. As the pilot took the corrective action, the helicopter yawed to the right and began to rotate around the main rotor mast. He reduced the throttle to idle to arrest the spin, and the yaw rate slowed. However, the spin continued as the helicopter descended through about 250 feet agl. The pilot stated that the helicopter was still spinning when it struck the ground upright. Review of an audio recording from a video camera aboard the helicopter indicated that the low rotor rpm audio alarm was on during the final 7 seconds of the flight. A witness reported that the engine ran "fine" and "perfectly" all the way to ground contact. Examination of the wreckage revealed no evidence of pre-impact mechanical malfunctions or failures that would have precluded normal operation of the helicopter. The helicopter was operating in a high-power, low-airspeed condition that required the pilot to be especially aware of wind direction in order to avoid tailwinds, which can result in a loss of control due to settling with power and/or a loss of tail rotor effectiveness. Although the pilot’s comment to the photographer indicated that he was concerned about the wind angle, it is likely that he did not maintain a nose-into-the-wind position. When the helicopter began to settle with power, the rotor rpm dropped, and the tail rotor lost effectiveness. There was insufficient altitude for the pilot to affect a recovery before the helicopter impacted the ground.

Quoted verbatim from the NTSB record.