N61865

Substantial
None

HUGHES OH-6A S/N: 69-15987

Accident Details

Date
Friday, October 20, 1995
NTSB Number
LAX96TA016
Location
IMPERIAL, CA
Event ID
20001207X04745
Coordinates
32.859157, -115.649909
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's improper planning/decision and failure to ensure there was an adequate supply of fuel, which led to fuel exhaustion and a forced (autorotative) landing.

Aircraft Information

Registration
N61865
Make
HUGHES
Serial Number
69-15987
Model / ICAO
OH-6A

Registered Owner (Historical)

Name
UNITED STATES BORDER PATROL I&NS
Address
PO BOX 10078
Status
Deregistered
City
EL PASO
State / Zip Code
TX 79995-0078
Country
United States

Analysis

On October 20, 1995, at 1230 hours Pacific daylight time, a Hughes OH-6A helicopter, N61865, sustained substantial damage during a hard landing from an autorotation near Imperial, California. The autorotation was precipitated by a loss of power as the aircraft was returning from an observation mission. The aircraft was owned and operated by the U.S. Border Patrol as a public-use aircraft. Visual meteorological conditions prevailed at the time and an internal agency flight plan was filed. The commercial pilot, the sole occupant, was not injured. The flight originated from Imperial County Airport at 0700 on the day of the accident.

The pilot reported in verbal and written statements that he was airborne continuously from departure on an observation mission. He was returning to the airport and was about 3 miles from landing when the engine flamed out. The pilot initiated an autorotation and landed hard, severing the tail boom. A U.S. Border Patrol officer who examined the helicopter reported that the fuel tank was empty.

The aircraft operator conducted a post-accident examination of the aircraft. The fuel system was pressurized and found to be intact. The remaining fuel was drained and found to be about 1 1/2 pints in quantity. No contaminates were found in the drained fuel, the fuel lines, or filter. No other malfunctions or anomalies were reported with the fuel indicating systems, including the low fuel warning panel light.

The accident aircraft was equipped with an Allison 250-C20B turboshaft engine. The pilot operating manual states that the fuel burn at sea level and 90 knots is about 175 pounds per hour; the burn rate at 60 knots at sea level is about 160 pounds per hour. The pilot stated that he departed on the accident flight with about 104 U.S. gallons (676 pounds) onboard.

The pilot operators manual also states that "fuel low" warning light will illuminate with about 70 pounds of fuel remaining. Using the above data, the low fuel warning light would have illuminated about 24 minutes before the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX96TA016