N224TV

Substantial
Minor

BELL 206B S/N: 2482

Accident Details

Date
Tuesday, February 23, 1993
NTSB Number
FTW93LA090
Location
OKLAHOMA CITY, OK
Event ID
20001211X11831
Coordinates
35.430423, -97.519760
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
2
Total Aboard
3

Probable Cause and Findings

THE PASSENGERS INADVERTENT CONTROL INTERFERENCE. A FACTOR WAS THE PILOT'S INADEQUATE SUPERVISION OF THE PASSENGER

Aircraft Information

Registration
N224TV
Make
BELL
Serial Number
2482
Engine Type
Turbo-shaft
Year Built
1978
Model / ICAO
206B B06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
MORTON MICHAEL J
Address
5542 SHALE DR
Status
Deregistered
City
TROY
State / Zip Code
MI 48098-3936
Country
United States

Analysis

On February 23, 1993, at approximately 1725 central standard time, a Bell 206B helicopter, N224TV, was substantially damaged upon impact with terrain while hovering at the Downtown Airpark in Oklahoma City, Oklahoma. The instructor pilot sustained minor injuries, while his two passengers escaped uninjured. Visual meteorological conditions prevailed for the business flight.

According to the Federal Aviation Administration (FAA) inspector, the helicopter terminated a VFR flight from Shawnee, Oklahoma, and proceeded to a hover area at the airport to demonstrate basic hovering flight maneuvers to the passengers.

According to the pilot, he had the helicopter outfitted with dual controls in order to provide the front seat occupant of the helicopter with the feel of the helicopter. In a level, open area of the airpark, he proceeded to demonstrate the flight characteristics of the helicopter while hovering at 3 feet. The pilot stated that he allowed his friend in the front seat to lightly ride along on the controls. The passenger applied too much pressure to the cyclic causing the helicopter to drift to the left, followed by an overcorrection to the right, which the pilot was unable to override.

The pilot further stated that the rear of the right landing gear skid struck the ground, creating a pivot point for a "dynamic roll." The helicopter came to rest on its right side with its tailboom severed from the fuselage. All occupants exited the helicopter unassisted.

According to witnesses, the helicopter was observed hovering in an erratic fashion, making abrupt attitude and altitude changes. Just prior to the main rotor blades striking the ground, the helicopter was observed hovering backwards until the right rear skid tube impacted the ground.

The wreckage was released to the operator at the accident site.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW93LA090