N982SH

Substantial
None

Robinson R22 BETA S/N: 2786

Accident Details

Date
Sunday, June 21, 1998
NTSB Number
FTW98LA278
Location
FREER, TX
Event ID
20001211X10321
Coordinates
26.160617, -98.049240
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain tail rotor-ground clearance due to his improper flare while hovering.

Aircraft Information

Registration
N982SH
Make
ROBINSON
Serial Number
2786
Engine Type
Reciprocating
Model / ICAO
R22 BETA R22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SMITH HELICOPTERS INC
Address
PO BOX 3502
Status
Deregistered
City
LAREDO
State / Zip Code
TX 78044-3502
Country
United States

Analysis

On June 21, 1998, at 0850 central daylight time, a Robinson R22 Beta helicopter, N982SH, was substantially damaged following a loss of control while hovering near Freer, Texas. The commercial pilot, sole occupant of the helicopter, was not injured. The helicopter was owned and operated by Smith Helicopters Inc., of Laredo, Texas, under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the cattle herding flight for which a flight plan was not filed. The local flight originated from the operator's trailer 600 yards from the accident site, approximately 15 minutes prior to the accident.

The pilot reported to the FAA inspector that while herding cattle, a bull separated from the herd and the pilot turned the helicopter towards the bull to gather him back into the herd. The pilot added that as he approached the bull, he flared the helicopter in a nose high attitude to stop the forward movement. The pilot further stated that he lost control of the helicopter after the tail rotor impacted the ground.

The right skid broke as the helicopter spun 180 degrees to the right, coming to rest on its right side. There was no fire. The FAA inspector confirmed that the main rotor system was damaged and the airframe sustained structural damage.

The 2,000 hour pilot stated that he did not experience any mechanical problems prior to the tail rotor impacting the ground and the subsequent loss of control. The 1998 model helicopter had accumulated a total of 233 hours since new.

Despite repeated attempts by the NTSB investigator-in-charge, neither the pilot nor the operator returned the completed NTSB Form 6120.1/2 (Pilot/Operator Aircraft Accident Report).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW98LA278