N91335

Substantial
Minor

Bell OH-58CS/N: 70-15345

Accident Details

Date
Friday, April 13, 2001
NTSB Number
MIA01TA121
Location
Panama City, FL
Event ID
20010417X00767
Coordinates
30.204721, -85.823890
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The poor in-flight planning by the pilot for failure to maintain adequate airspeed while maneuvering to begin spray operations resulting in the loss of tail rotor effectiveness, subsequent in flight loss of control, and in flight collision with terrain.

Aircraft Information

Registration
N91335
Make
BELL
Serial Number
70-15345
Model / ICAO
OH-58C

Registered Owner (Historical)

Name
BEACH MOSQUITO CONTROL DISTRICT
Address
1016 COX GRADE RD
Status
Deregistered
City
PANAMA CITY BEACH
State / Zip Code
FL 32407-2722
Country
United States

Analysis

On April 12, 2001, about 2010 central daylight time, a Bell OH-58C, N91335, registered to and operated by Beach Mosquito Control District, crashed shortly after takeoff from the Beach Mosquito Control District Heliport, Panama City, Florida. Visual meteorological conditions (VMC) prevailed at the time and no flight plan was filed for the public-use flight. The helicopter was substantially damaged and the commercial-rated pilot, the sole occupant, sustained minor injuries. The flight originated about 5 minutes earlier.

The pilot stated that the first flight departed at 1915, to spray chemical for mosquitoes but returned due to plugged spray nozzles that he noted midpoint of the second spray pass. Without securing the engine, the plugged nozzles were replaced and the flight departed to again spray chemical. After takeoff while flying about 200-250 feet above ground level (agl) at an indicated airspeed of 30-40 knots, with a 10-15 knot wind from the southeast, he began a left turn to line up for his spray swath. The helicopter yawed 20-30 degrees to the right which could not be corrected with full left anti-torque pedal input. He lowered the collective in an attempt to recover but with insufficient altitude, the helicopter collided with trees then the ground. He further stated that there was no engine or flight control malfunction and the right yaw is a characteristic of "loss of tail rotor effectiveness."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA01TA121