Aviation Accident Summaries

Aviation Accident Summary LAX97LA178

SANTA MARGARITA, CA, USA

Aircraft #1

N83795

Robinson R-22

Analysis

The density altitude was approximately 4,000 feet when the helicopter took off and departed the area. A witness reported that, moments later, the helicopter made a high speed flyby in the opposite direction at 2 or 3 feet above ground level after which the pilot made a climbing, steep turn at a near vertical bank angle. The helicopter then descended in the banked attitude until it impacted the terrain. The pilot reported that he recalled hearing the low rotor rpm warning horn before impact and that there were no mechanical malfunctions with the aircraft.

Factual Information

On May 11, 1997, at 1830 hours Pacific daylight time, a Robinson R-22 helicopter, N83795, impacted terrain while maneuvering after takeoff at Santa Margarita, California. The aircraft was substantially damaged. The commercial pilot and one passenger received minor injuries. Visual meteorological conditions prevailed for the personal flight. A witness reported that, immediately after liftoff, the aircraft made an abrupt left turn and departed the area at a low altitude in an easterly direction. Shortly thereafter, the helicopter made a low altitude, high speed, flyby in the opposite direction. After the flyby at 2 to 3 feet above the ground, the aircraft climbed to about 40 feet and made a "hard" right turn. It remained in the turning banked attitude until it descended and impacted the ground. In a sketch attached to his statement, the witness indicated that the bank angle was approximately 90 degrees. In his statement the pilot reported that, during the turn, the cyclic pitch control felt "mushy" and slow to respond and he recalled that the low rpm warning horn sounded prior to impact. In his report to the NTSB, the pilot reported that there were no mechanical malfunctions with the aircraft. The density altitude was approximately 4,000 feet.

Probable Cause and Findings

The failure of the pilot to maintain adequate rotor rpm during a low pass maneuvering flight resulting in loss of control. High density altitude was a factor in the accident.

 

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