Aviation Accident Summaries

Aviation Accident Summary LAX94LA220

STOCKTON, CA, USA

Aircraft #1

N140PH

ROBINSON R22-B

Aircraft #2

N2314Z

ROBINSON R22-B

Analysis

THE HELICOPTER WAS BEING UTILIZED TO DRY CHERRY TREES IN A LOCAL ORCHARD AND LANDED FOR FUEL AT A PRIVATE AIRSTRIP. THE PILOT HAD REDUCED COLLECTIVE PITCH TO ZERO AND THE ROTOR BLADES WERE STILL TURNING AT FLIGHT IDLE. A SISTER HELICOPTER FROM THE SAME OPERATOR LANDED TO THE RIGHT OF THE IDLING HELICOPTER TO REFUEL. WHEN THE PILOT OF THE SECOND HELICOPTER REDUCED COLLECTIVE PITCH TO ZERO, THE ROTOR BLADES MESHED WITH THOSE OF THE FIRST HELICOPTER.

Factual Information

On May 19, 1994, about 0720 hours Pacific daylight time, a Robinson R22-B helicopter, N140PH, collided with a second Robinson R22-B, N2314Z, while on the ground at a private airstrip, about 10 miles north of Stockton, California. The two helicopters were being operated as a visual flight rules (VFR) flight to dry cherry trees in the local area when the accident occurred. The helicopters, operated by Sunrise Helicopters Inc., Stockton, California, both received substantial damage. The pilot of N140PH, a certificated commercial pilot, received minor injuries. The pilot of N2314Z, also a certificated commercial pilot, was not injured. Visual meteorological conditions prevailed. The flight originated at Stockton Metropolitan Airport, about 0540 hours. The pilots reported that after terminating the tree drying operation over a local orchard, both aircraft proceeded to Wallom Field, a private airstrip, to refuel. The pilot of N140PH landed near the refueling point and had reduced the engine power to idle. The rotor blades were still turning. The pilot of N2314Z landed to the right side of the first aircraft. After the landing gear skids had touched down, the pilot lowered the collective pitch control to full down. As the second helicopter's rotor blades reached flat pitch, they meshed with those of N140PH. Both helicopters pivoted on the ground and both aircraft received damage to the main rotor blades, mast and transmission, and tail boom.

Probable Cause and Findings

THE FAILURE OF THE PILOT-IN-COMMAND OF THE LANDING HELICOPTER TO MAINTAIN SUFFICIENT CLEARANCE FROM A SECOND HELICOPTER.

 

Source: NTSB Aviation Accident Database

Get all the details on your iPhone or iPad with:

Aviation Accidents App

In-Depth Access to Aviation Accident Reports