N111PM

Substantial
None

Bell 206B S/N: 1770

Accident Details

Date
Friday, April 26, 1996
NTSB Number
IAD96LA067
Location
LOGAN, WV
Event ID
20001208X05592
Coordinates
37.800937, -81.870033
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

the pilot's failure to maintain an adequate fuel supply for the flight which resulted in a loss of engine power due to fuel exhaustion, and the loss of rotor rpm during the autorotation. The downhill sloping terrain was a related factor.

Aircraft Information

Registration
Make
BELL
Serial Number
1770
Engine Type
Turbo-shaft
Year Built
1975
Model / ICAO
206B B06
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
5
FAA Model
206B

Registered Owner (Current)

Name
TRI ROTOR SPRAY AND CHEMICAL
Address
9170 E ROAD 2
City
ULYSSES
State / Zip Code
KS 67880-8151
Country
United States

Analysis

On April 26, 1996, at 0945 eastern daylight time (EDT), a Bell 206B helicopter, N111PM, sustained substantial damage following a forced landing near Logan, West Virginia. The pilot and the two passengers reported no injuries. Visual meteorological conditions prevailed at the time of the accident, no flight plan was filed. The business flight was conducted under 14 CFR 91, and originated in Huntington, West Virginia, at 0815 EDT. The intended destination was Rita, West Virginia.

The pilot told the Federal Aviation Administration (FAA) Inspectors that he was in cruise flight at 600 feet above ground level (AGL), when the helicopter engine lost power. He reported that he initiated an autorotational descent. The pilot stated that, due to rough and sloping terrain, he was forced to extend his glide to landing. The pilot stated: "Due to low rotor rpm, the main rotor flexed on touchdown and severed the rear portion of tailboom."

The FAA Inspector's report stated: "Interview with [the] pilot revealed [that the] engine flameout occurred due to fuel exhaustion. Pilot admitted to having inadequate fuel on board. Aircraft was approximately 2 minutes from intended fuel stop. Pilot stated [that he had] no recollection [of] low fuel warning/alert." Postaccident examination of the helicopter revealed less than 1 quart of fuel in the fuel cell. FAA Inspectors stated that the helicopter's fuel quantity and low fuel warning systems appeared to be capable of normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# IAD96LA067