N5038F

Substantial
None

FAIRCHILD HILLER FH-1100S/N: 186

Accident Details

Date
Tuesday, July 31, 2012
NTSB Number
WPR12LA341
Location
Cody, WY
Event ID
20120802X80851
Coordinates
44.417221, -109.138053
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The failure of a tail rotor driveshaft coupling due to fatigue.

Aircraft Information

Registration
N5038F
Make
FAIRCHILD HILLER
Serial Number
186
Engine Type
Turbo-shaft
Year Built
1969
Model / ICAO
FH-1100FH11
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
HARRISON TIMOTHY BRUCE
Address
13 ROLLING HILLS DR
Status
Deregistered
City
CODY
State / Zip Code
WY 82414-8325
Country
United States

Analysis

On July 31, 2012, about 0920 mountain daylight time, a Fairchild Hiller FH-1100 helicopter, N5038F, was substantially damaged following the failure of its tail rotor drive shaft and subsequent autorotation to a hard landing near Cody, Wyoming. The commercial pilot and his three passengers were not injured. The helicopter was being operated by the pilot, doing business as Eclipse Helicopter Services, Cody, under the provisions of 14 Code of Federal Regulations Part 91. No flight plan had been filed for the local personal flight, which had originated about 1 hour before the accident. Visual meteorological conditions prevailed at the time of the accident.

The pilot reported that while in cruise flight, there was a sudden onset of a vibration coming from the rear of the helicopter. He performed an autorotation to a field straight ahead. During the landing sequence, the helicopter spun to the right 180 degrees. The landing skids, tail boom, and main transmission mounts were bent. The pilot reported that a tail rotor driveshaft coupling, identified as a Bendix 19E101-1D coupling, had split in half, which resulted in a loss of tail rotor drive.

Postaccident examination of the tail rotor driveshaft coupling by the National Transportation Safety Board's Materials Laboratory in Washington, D.C., revealed that it failed due to fatigue cracking. A complete history of the part was not available; therefore, the total time in service of the part could not be determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR12LA341