N4085L

Substantial
Minor

Bell UH-1H S/N: 68-15655

Accident Details

Date
Monday, September 6, 1999
NTSB Number
DEN99LA160
Location
SILVERTON, CO
Event ID
20001212X19738
Coordinates
37.819759, -107.640167
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The total loss of engine power for undetermined reasons. A factor was the lack of suitable terrain for a forced landing.

Aircraft Information

Registration
N4085L
Make
BELL
Serial Number
68-15655
Engine Type
Turbo-shaft
Year Built
1968
Model / ICAO
UH-1H UH1
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
BILLINGS FLYING SERVICE
Address
3655 AJ WAY
Status
Deregistered
City
BILLINGS
State / Zip Code
MT 59106-9745
Country
United States

Analysis

On September 6, 1999, at 0830 mountain daylight time, a Bell UH-1H helicopter, N4085L, was substantially damaged during impact with terrain following an autorotation near Silverton, Colorado. The commercial pilot, the sole occupant on board, received minor injuries. The helicopter was being operated by High Country Helicopters, Inc., of Montrose, Colorado, under Title 14 CFR Part 133. Visual meteorological conditions prevailed for the local long-line cargo flight which originated from a staging area approximately 20 minutes before the accident. No flight plan had been filed.

The pilot reported that this was his first trip of the morning, and he was transporting approximately 300 pounds of construction materials which were to be used to close a mine entrance. He said that the load was on the ground and he was hovering while ground personnel were disconnecting the cargo net. He said that one of the ground team radioed him and reported that "fire and smoke was coming from your tail pipe." The pilot said that he noticed that the rotor rpm warning light was on, and the engine out lights and horns had been activated. He lowered the collective and autorotated to the ground, but the main rotors impacted terrain. The tail rotor and its associated gear boxe separated from the aircraft. The tail boom was bent and pushed forward into the transmission.

Aircraft records indicated that the engine was overhauled by the U.S. Army 791 hours before the accident. The maintenance records further indicated that the engine came from a civilian overhaul facility and was installed in N4085L approximately 21 hours prior to the accident.

The Colorado Department of Minerals and Mines reported the mine entrance elevation was 11,500 feet. The density altitude was calculated to be 13,000 feet.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN99LA160