N4412X

Substantial
None

SEGO TOOL HAWK H2X S/N: 201X

Accident Details

Date
Wednesday, October 15, 1997
NTSB Number
FTW98LA015
Location
TOOELE, UT
Event ID
20001208X09010
Coordinates
40.569519, -112.330101
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain aircraft control. Contributing was the inadequate design of the flight control systems, resulting in slow response to pilot input.

Aircraft Information

Registration
N4412X
Make
SEGO TOOL
Serial Number
201X
Year Built
1996
Model / ICAO
HAWK H2X

Registered Owner (Historical)

Name
GENERAL AERONAUTICS CORP
Address
2640 W CALIFORNIA AVE STE A
Status
Deregistered
City
SALT LAKE CITY
State / Zip Code
UT 84104-4563
Country
United States

Analysis

On October 15, 1997, approximately 1416 mountain daylight time, a Sego Tool Hawk H2X gyroplane, N4412X, was substantially damaged when it impacted the ground during initial climb following takeoff near Tooele, Utah. The airline transport rated pilot, the sole occupant in the gyroplane, was not injured. The gyroplane was being operated by Geoen Brothers Aviation, Inc., under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the local test flight that was originating at the time of the accident. No flight plan had been filed.

According to the pilot, he was taking off for one of a series of flight tests. He reported that shortly after liftoff, the gyroplane made an uncommanded roll to the right. The pilot said that he applied full left cyclic and full left rudder, but the main rotor system struck the ground. The main rotor blades separated from the gyroplane and the aircraft came to rest with the fuselage twisted.

Postcrash examination of the gyroplane by the design/manufacturing team revealed that the control system design of this aircraft had an inherent lag in time between control input and aircraft response. They found the runway that the gyroplane was taking off from slopped 1.7 to 1.8 degrees to the left. They said that "the moment the aircraft left the ground, gravity moved the fuselage to the left and the rotor disk to the right." Subsequently, a right turn was initiated and ground contact was made by the main rotor disk before the pilot's correction inputs could take effect.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW98LA015