N993KC

Substantial
Serious

ROBINSON HELICOPTER R22 BETAS/N: 2926

Accident Details

Date
Wednesday, September 12, 2007
NTSB Number
DFW07LA197
Location
Fort Stockton, TX
Event ID
20070923X01430
Coordinates
31.363889, -103.019447
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The failure of the v-belt drive system to the main rotor for undetermined reasons. Contributing to the accident was insufficient altitude to perform a successful autorotation.

Aircraft Information

Registration
N993KC
Make
ROBINSON HELICOPTER
Serial Number
2926
Engine Type
Reciprocating
Year Built
1999
Model / ICAO
R22 BETAR22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SMITH HELICOPTERS INC
Address
PO BOX 398
Status
Deregistered
City
COTULLA
State / Zip Code
TX 78014-0398
Country
United States

Analysis

On September 12, 2007 at 1438 central standard time N993KC, a Robinson R22 Beta helicopter, experienced a hard landing after a malfunction of the belt drive system for the main rotor. The pilot received serious injuries and his passenger received minor injuries as a result of a hard landing. The pilot had just taken off from a trailer and had climbed to about 50 feet above ground level to conduct a predator control mission about 10 miles northwest of Fort Stockton, Texas. The flight was conducted in visual meteorological conditions under 14 Code of Federal Regulations, Part 91.

In an interview with the pilot, a Federal Aviation Administration (FAA) inspector stated that the pilot had just transitioned to a low level cruise after takeoff when he heard a loud bang and felt a vibration in the pedals. He observed the engine rpm was excessively high and noticed the rotor RPM was below 80 percent accompanied by the low rotor RPM warning. He then lowered the collective and searched for a location to make an emergency landing. The pilot then initiated an autorotation, was not able to recover the rotor RPM, and landed hard with near zero forward speed. The aircraft bounced backwards after initial impact and came to rest in the upright position.

An FAA inspector conducted an on scene investigation and noted that one of the v-belts to the main rotor drive system had separated which caused the other belt to slip off the upper spindle. The pilot stated the clutch light was operating normally prior to takeoff.

Weather reported at 1411 central daylight time at Fort Stockton (KFST), 10 miles north west of the accident site, was winds 110 degrees at 9 knots, 10 miles visibility, scattered clouds at 2100 feet and 2600 feet, temperature 24 degrees Celsius, dew point 18 degrees Celsius, and an altimeter reading of 30.11 inches of Mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW07LA197