Aviation Accident Summaries

Aviation Accident Summary SEA04CA107

Hood River, OR, USA

Aircraft #1

N717CS

Steward Rocky 162F

Analysis

During cruise at 2,200 feet mean sea level, the helicopter lost engine power, necessitating the pilot to make an autorotation. Having departed earlier in the morning with full fuel and making two previous flights, the pilot felt he had sufficient fuel for a third flight. On the return leg of the third flight the pilot noticed the engine LOW RPM light illuminate, a low RPM needle indication, a high manifold pressure gage indication, but no LOW FUEL warning light. Assuming he had lost engine power, the pilot made an autorotation to an open hay field. During the landing sequence into the high vegetation, the aircraft initially went up on its nose before rolling over on its left side. A post accident examination revealed no fuel was present when the right tank was dipped, and that 4 to 6 ounces of fuel was present when the helicopter's common drain was opened. The pilot indicated that during the course of the day he was using higher takeoff power settings due to the warmer weather, and that his miscalculations had caused him to run out of fuel.

Factual Information

On June 16, 2004, about 1130 Pacific daylight time, a Stewart Rocky 162F helicopter, N717CS, lost engine power and was substantially damaged during a forced landing near Hood River, Oregon. The helicopter is owned by the pilot and was being operated as a visual flight rules (VFR) flight under the provisions of Title 14, CFR Part 91, when the accident occurred. The airline transport pilot, the sole occupant of the helicopter, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the flight that originated from the Ken Jernstedt Airfield (4S2), Hood River, Oregon, at 0945. In a written statement dated June 16, 2004, the pilot reported that while flying at 2,200 feet mean sea level he noticed a low RPM needle and warning light, a high manifold gage indication, but no LOW FUEL warning light, which would indicate approximately 3 gallons of fuel remaining. The pilot further reported that he tried adding throttle and reducing collective, but when this did not correct the problem he assumed he had lost engine power. The pilot stated that he then made an immediate 180 degree turn and performed an autorotation to a large hay field, "...which was about 4 feet high and thick." The pilot further stated that the landing went well until the helicopter slowly rotated towards the nose and the main rotor blade made ground contact. The helicopter subsequently rolled over on its left side. The pilot related that during a post accident examination he dipped the right tank and found no fuel present. At the request of the NTSB investigator-in-charge the pilot also drained what fuel remained from a common drain into a jar which measured approximately 3 inches in diameter. The total amount of fuel drained into the jar measured about 1 inch, equating to approximately 4 to 6 ounces according to the pilot. The pilot reported that during the day it was taking higher power settings to lift off and hover due to the warmer weather. The pilot further reported, "I just miscalculated my fuel. I think I ran out of fuel."

Probable Cause and Findings

The pilot's miscalculation of fuel consumption and his inadequate in-flight planning/decision, which resulted in fuel exhaustion and loss of engine power. A factor was the high vegetation.

 

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