N9294F

Substantial
Unknown

HUGHES 269CS/N: 650421

Accident Details

Date
Wednesday, November 2, 1994
NTSB Number
CHI95LA029
Location
GARDEN CITY, KS
Event ID
20001206X02569
Coordinates
37.969089, -100.860038
Aircraft Damage
Substantial
Highest Injury
Unknown
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
0

Probable Cause and Findings

inadvertant engagement of the rotor drive system, while the helicopter had been left unattended by the pilot.

Aircraft Information

Registration
N9294F
Make
HUGHES
Serial Number
650421
Year Built
1975
Model / ICAO
269C

Registered Owner (Historical)

Name
SALE REPORTED
Address
PO BOX 198
Status
Deregistered
City
BATES CITY
State / Zip Code
MO 64011-0198
Country
United States

Analysis

On November 2, 1994, at 1515 hours central standard time (CST), a Hughes 269-C helicopter, N9294F, operated as a business aircraft by Henkle Drilling and Supply, Inc., of Garden City, Kansas, contacted a pole with its rotor blades at the owner's facility one mile west of Garden City, Kansas. The helicopter turned on its side and was substantially damaged. There were no persons on board the helicopter during the accident and no injuries. Visual meteorological conditions existed at the time of the accident and no flight plan was filed.

The flight was operating under 14 CFR Part 91 and had originated from the Garden City Regional Airport at approximately 1445 CST. The airline transport rated pilot had repositioned the helicopter and was awaiting a part to transport to a company site in Sublette, Kansas. After landing at 1450 hours CST, the engine was placed at idle (approximately 1400 RPM), the rotor disengaged, and the pilot exited the helicopter. Winds were 10 knots gusting to 20 knots. The rotors engaged with no persons on board, and the helicopter struck a building.

Post-crash inspection revealed that the belt tensioner was still in the disengaged position, and the collective was in the full up position. Witnesses stated that the gusting winds were causing the static rotor blades to flap vertically. As rotor blade pitch is increased, the engine anticipator tends to increase engine speed. Maintenance and operations personnel stated that as engine speed increases, the drive belts are able to grab the drive pulleys. Witnesses described hearing the engine operating at a high speed during 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# CHI95LA029