N2330F

Substantial
None

Robinson R22 BETA S/N: 2153

Accident Details

Date
Thursday, January 27, 2000
NTSB Number
FTW00LA077
Location
SARITA, TX
Event ID
20001212X20371
Coordinates
27.210227, -97.800201
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the pilot to maintain main rotor rpm, which resulted in a hard landing.

Aircraft Information

Registration
N2330F
Make
ROBINSON
Serial Number
2153
Engine Type
Reciprocating
Year Built
1992
Model / ICAO
R22 BETA R22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
BURRIS TRAVIS H
Address
801 N TEXAS BLVD
Status
Deregistered
City
ALICE
State / Zip Code
TX 78332
Country
United States

Analysis

On January 27, 2000, at 0845 central standard time, a Robinson R22 Beta helicopter, N2330F, was substantially damaged during a hard landing following a loss of main rotor rpm near Sarita, Texas. The aircraft was registered to a private individual and operated by Mesquite Helicopter Services, Inc., of Alice, Texas. The commercial pilot and the passenger were not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 antelope hunting flight. The local flight originated from the Kennedy Ranch at 0820.

The helicopter's mission was to harvest Nilgai antelope. After the passenger shot a second Nilgai antelope, the pilot maneuvered the helicopter downwind at 50 knots and 70 feet agl, to lead the animal recovery vehicle to where the first antelope had fallen. The pilot executed a right turn to come to a hover over the antelope. As he started a "quick-stop, the engine began to lug down." He "rolled on the throttle, overriding the governor, and nosed [the helicopter] over while lowering the collective." The main rotor low rpm warning sounded about the time he applied forward cyclic. The helicopter was "gaining airspeed but the rpm kept declining." The pilot "milked" the collective; however, he was unable to regain rotor rpm. At about 3-5 feet agl, the rotor rpm was at 80 percent. The pilot leveled the helicopter and attempted a run-on landing. "As [the helicopter] hit the ground," a main rotor blade struck the tail boom, separating it at mid-length. The aircraft turned 90 degrees to the left and rolled over onto its left side.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW00LA077