N92RE

Substantial
None

MOONEY, DAN ROTORWAY EXEC 90 S/N: 5144

Accident Details

Date
Friday, September 16, 1994
NTSB Number
FTW94LA304
Location
OWASSO, OK
Event ID
20001206X02255
Coordinates
36.280864, -95.829414
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE FLIGHT INSTRUCTOR'S INADEQUATE SUPERVISION OF THE STUDENT. A FACTOR WAS THE STUDENT'S FAILURE TO MAINTAIN ADEQUATE ROTOR RPM.

Aircraft Information

Registration
N92RE
Make
MOONEY, DAN
Serial Number
5144
Model / ICAO
ROTORWAY EXEC 90

Registered Owner (Historical)

Name
STEWART BRYON R
Address
PO BOX 20103
Status
Deregistered
City
TAMPA
State / Zip Code
FL 33622
Country
United States

Analysis

On September 16, 1994, at 1530 central daylight time, a Rotorway Exec 90 homebuilt helicopter, N92RE, was substantially damaged while landing at Gundy's Airport, Owasso, Oklahoma. The helicopter, flown by a helicopter instructor pilot, was on an instructional flight. There was no flight plan filed and visual meteorological conditions prevailed. The pilot and student were uninjured.

The instructor pilot reported the following information. The student was practicing hovering using the collective, throttle, and anti-torque pedals while the instructor controlled the cyclic. A left yaw developed and the instructor noticed the engine RPM in the lower portion of the green arc. The instructor then added full throttle and right pedal, but the left yaw continued to increase in severity. At this point the collective was lowered until the skids contacted the ground. The right skid contacted first, the helicopter then rolled to the right, severing one main rotor blade and bending the tailboom. The aircraft came to rest on its right side.

The instructor pilot also stated that the hover seemed normal until the left yaw occurred and there were no low RPM indications such as collective position or sound. He believed the yaw was caused by either low main rotor RPM or possibly by low tail rotor RPM resulting from belt slippage or an unknown cause. An examination of the helicopter by a Federal Aviation Administration inspector revealed no mechanical anomalies that could have contributed to the mishap.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW94LA304