N64292

Substantial
None

Bell 47G-3B-1 S/N: 3730

Accident Details

Date
Sunday, June 13, 1999
NTSB Number
CHI99LA171
Location
AUSTIN, MN
Event ID
20001212X18934
Coordinates
43.669471, -92.970283
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of engine power for an undetermined reason. Factors associated with the accident were the low altitude of the helicopter, which precluded an emergency autorotation, and the crop field.

Aircraft Information

Registration
N64292
Make
BELL
Serial Number
3730
Engine Type
Reciprocating
Year Built
2009
Model / ICAO
47G-3B-1 B47G
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
HAWKER BEECHCRAFT CORP
Address
PO BOX 85
Status
Deregistered
City
WICHITA
State / Zip Code
KS 67201-0085
Country
United States

Analysis

On June 13, 1999, at 1000 central daylight time, a Bell 47G-3B-1, N64292, sustained substantial damage during a forced landing following loss of engine power. The accident occurred in a crop field, near Austin, Minnesota. The commercial pilot reported no injuries. The aerial application 14 CFR Part 137 flight was operating in visual meteorological conditions. No flight plan was on file. The local flight departed about 0945.

The pilot said that the engine "overspeeded" and then quit completely. He said that he was conducting a swath run at the time and the helicopter was flying about 40 MPH at an altitude of 5 to 10 feet above the ground. He said he attempted to make a run-on landing; however, the skids dug into the soft terrain and the helicopter nosed down. He said then the main rotor blades cut through the tail boom. He could not account for the power loss.

The owner had recovered the helicopter to his facility prior to notifying the NTSB of the accident. A post accident examination of the engine, transmission, clutch, and airframe failed to reveal any pre-accident anomalies. There was fuel present in the tank. Fuel filters and strainers were checked and found to be clean. The engine was started and ran. Oil pressure, fuel pressure, and manifold pressure showed indications. A magneto check was conducte4d and both magnetos functioned. The clutch was engaged and found to function. Control continuity was intact except for impact damage and functioned when activated.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI99LA171