N121CC

Substantial
None

CarterCopter LLC CarterCopterS/N: 1

Accident Details

Date
Friday, June 17, 2005
NTSB Number
DFW05CA163
Location
Olney, TX
Event ID
20050802X01139
Coordinates
33.350555, -98.751663
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's inability to maintain control of the gyrocraft during a forced landing as a result of a loss of cyclic and collective control. Contributing factors were the sheared propeller drive pulley bolts, broken wire on the co-pilots cyclic boost control solenoid, failure of the ballistic parachute to deploy, and the lack of suitable terrain for forced landing.

Aircraft Information

Registration
N121CC
Make
CARTERCOPTER LLC
Serial Number
1
Engine Type
Reciprocating
Model / ICAO
CarterCopterBPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WAYPOINT AVIATION INC
Address
4778 NW 5TH COURT
Status
Deregistered
City
COCONUT CREEK
State / Zip Code
FL 33063
Country
United States

Analysis

On June 17, 2005, at 0957 central daylight time, a CarterCopter gyrocraft, N121CC, registered and operated by CarterCopters LLC, of Wichita Falls, Texas, was substantially damaged when it impacted trees following a loss of control while maneuvering near Olney, Texas. The private pilot and flight test engineer were not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 research and development flight. The local flight originated from the Olney Municipal Airport (ONY), near Olney, Texas, approximately 0945.

The operator reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that while conducting a test flight, the gyrocraft had been flying at an airspeed of 151 miles per hour (mph) in smooth air conditions. The 2,400-hour pilot "heard a noise from the engine compartment" and reduced throttle. As airspeed decayed, the "spindle tilted to the left" and the gyrocraft started to roll to the left. The pilot pushed the control stick to the right and noted that he lost half of the "rotor control" as the gyrocraft continued turning to the left. As the pilot established a nose down attitude to maintain airspeed, he engaged the ballistic parachute switch; however, the parachute did not deploy. As a high rate of decent increased, the pilot attempted to flare using the control stick only and did not "pull collective." Subsequently, the gyrocraft impacted mesquite trees before hitting the ground. The gyrocraft came to rest on its left side in a level attitude approximately three miles east of ONY.

An examination of the gyrocraft by the operator revealed that the main rotor blades were destroyed. The left and right wing, tail boom and horizontal stabilizer were separated from the fuselage. The bolts holding the propeller drive pulley to the propeller drive shaft were found "sheared." A wire to the co-pilot cyclic boost control solenoid was found separated.

At 1004, the automated surface observing system at the Graham Airport (RPH), located 20 miles southeast from the accident site, reported wind from 130 degrees at 5 knots, visibility 10 statute miles, scattered clouds at 6,000 feet, temperature 30 degrees Celsius, dew point 18 degrees Celsius, and an altimeter setting of 29.83 inches of Mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW05CA163