N67083

Substantial
None

Bell 47G-2 S/N: 2280

Accident Details

Date
Thursday, August 31, 2000
NTSB Number
CHI00LA277
Location
SPRING BROOK, WI
Event ID
20001212X21693
Coordinates
45.940654, -91.679077
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A fatigue failure of the tail rotor drive gear shaft.

Aircraft Information

Registration
N67083
Make
BELL
Serial Number
2280
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
47G-2 B47G
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
CHURCHILL SCOTT
Address
PO BOX 92
Status
Deregistered
City
LE SUEUR
State / Zip Code
MN 56058-0092
Country
United States

Analysis

On August 31, 2000, at 0930 central daylight time, a Bell 47G-2, N67083, collided with the terrain following a loss of control while maneuvering during an aerial application flight in Spring Brook, Wisconsin. The pilot was not injured and the helicopter was substantially damaged. The 14 CFR Part 137 flight was operating in visual meteorological conditions. The flight originated in Spring Brook, Wisconsin, at 0925 central daylight time.

The pilot stated he was going to spray a field and had just made a turn to enter his first swath run when he experienced a loss of tail rotor power. He stated his attempts to return to normal flight were unsuccessful resulting in rotation of the helicopter and airspeed dropping to zero. He reported the helicopter settled into a clearing in a wooded area at the end of the field. The helicopter impacted some small trees and the terrain, which resulted in the separation of the main rotor and substantial damage to the helicopter.

Post accident inspection of the helicopter revealed a failure of the tail rotor drive gear assembly. The assembly was removed from the helicopter and sent to the NTSB Materials Laboratory in Washington, D.C. The metallurgical inspection of the drive gear assembly revealed the drive gear shaft was fractured at the underside of the bevel gear. The examination revealed, "The fracture surface was on a flat transverse plane and contained crack arrest positions over most of the fracture, indicative of fatigue cracking." The metallurgist's report also stated, "The origin area was located on the cylindrical portion of the shaft surface, directly adjacent to the keyway slot. The origin area contained a single ratchet mark, indicating initiation from at least two origin sites in the origin area. Fatigue crack features visible on the scanning electron microscope extended from the origin area through about 90 percent to 95 percent of the shaft cross sectional area." The report defined a ratchet mark as a small step in the fracture surface that separates fatigue origin areas on slightly offset planes.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI00LA277