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NTSB Report

September 6, 1999 · Bell UH-1H · N4085L

Silverton, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 6, 1999
Injury Outcomes
1 injury (1 minor injury)
Location
Silverton, CO
Aircraft
Bell UH-1H
Tail Number
N4085L
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
DEN99LA160

The pilot said this was his first trip of the morning, and he was transporting approximately 300 pounds of construction materials. He said that the load was on the ground and he was hovering while ground personnel disconnected 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 aircraft records indicate 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.

NTSB Probable Cause

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

Full Narrative

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.

Flight

Event TypeAccident
Event Time08:30 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell UH-1H
Tail NumberN4085L
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsLycoming · T53-L-13 · Turboshaft

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 44 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind130° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point61 F / 45 C
Altimeter30.00 inHg
Observation Time14:53
Weather SourceWFAC

Appendix: Source Data