N62446

Destroyed
Minor

Bell 47G4S/N: 7655

Accident Details

Date
Sunday, June 23, 2002
NTSB Number
FTW02LA186
Location
Grand Lake, LA
Event ID
20020624X00961
Coordinates
30.033332, -93.269996
Aircraft Damage
Destroyed
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
1
Total Aboard
3

Probable Cause and Findings

the pilot's inability to control the helicopter in a hover due to the restricted movement of the cyclic for undetermined reasons.

Aircraft Information

Registration
N62446
Make
BELL
Serial Number
7655
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
47G4B47G
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
DEEP SOUTH HELICOPTERS INC
Address
7420 ARDOIN RD
Status
Deregistered
City
JENNINGS
State / Zip Code
LA 70546-8343
Country
United States

Analysis

On June 23, 2002, at 1130 central daylight time, a Bell 47G4 helicopter, N62446, was destroyed when it impacted terrain following a loss of control while hovering near Grand Lake, Louisiana. The helicopter was registered to and operated by Deep South Helicopters, Inc., Jennings, Louisiana. The commercial pilot and one passenger received minor injuries, and one passenger was not injured. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 91 observation flight, which was originating from an open field at the time of the accident, and no flight plan was filed.

According to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), and in a telephone interview with the NTSB investigator-in-charge, the pilot reported that he had just finished spray operations. The pilot then repositioned the helicopter to an open field prior to picking up two passengers he would take to survey the area he had just sprayed for them. The pilot occupied the left seat, one passenger occupied the center seat, and the remaining passenger occupied the right seat. As the helicopter was equipped with dual controls, the pilot cautioned both passengers "not to touch anything." The pilot reported that as he brought the helicopter to a hover, approximately 6 to 12 inches off the ground, the helicopter tilted forward "due to the forward center of gravity condition." The pilot added aft cyclic to counter the forward center of gravity condition; however, the helicopter continued to tilt forward. The pilot stated that "as I tried to add more aft cyclic, I felt the cyclic bind up and couldn't move it aft any further." He then lowered collective in an attempt to land, but the helicopter "tilted to the right." The right skid "dug" into the ground, and the helicopter experienced a dynamic rollover, coming to rest on its right side where it caught fire and was destroyed.

An FAA inspector, who traveled to the accident site, reported that control continuity could not be established due to the helicopter being destroyed by thermal and impact damage.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW02LA186