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Aviation safety reports, made easier to study

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NTSB Report

April 29, 2001 · Cartercopters Cartercopter · N121CC

Olney, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 29, 2001
Injury Outcomes
No injuries (2 uninjured)
Location
Olney, TX
Aircraft
Cartercopters Cartercopter
Tail Number
N121CC
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW01LA108

The pilot was conducting a test flight over the runway. The experimental prototype gyrocraft took off from the runway and flew approximately 2-3 feet above the ground. The pilot applied "right cyclic control" for drift correction while raising the collective approximately "6 degrees for climb." The pilot reported that at the same time the nose pitched up rapidly and rolled to the right. Corrective control inputs were applied to level the gyrocopter; however, it rolled left and over flew the edge of the runway. The pilot reduced the collective, and the aircraft touched down on the ground in a level attitude rolling approximately 25 mph. As the gyrocraft slowed to approximately 5 mph, the nose landing gear collapsed, the gyrocraft nosed down, and the main rotor blades contacted the ground and sustained structural damage. The pilot had accumulated 3,800 flight hours. This was the pilot's first flight in the accident aircraft.

NTSB Probable Cause

the pilot's failure to maintain directional control during the takeoff initial climb. Contributory factors were the pilot's lack of experience with the aircraft and the soft terrain.

Full Narrative

On April 29, 2001, at 1446 central daylight time, a Cartercopters Cartercopter experimental prototype gyrocraft, N121CC, was substantially damaged when it encountered soft terrain and nosed down during landing following an aborted takeoff at the Olney Municipal Airport, Olney, Texas. The aircraft was registered to and operated by CarterCopters LLC, of Wichita Falls, Texas. The commercial pilot and his crewmember were not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 test flight. The local flight was originating at the time of the accident. According to the FAA inspector, who responded to the accident site, the pilot was conducting a test flight over runway 17. The pilot took off from runway 17 and flew approximately 2-3 feet above the ground. According to the pilot, he applied "right cyclic control" for drift correction while raising the collective approximately "6 degrees for climb." The pilot reported that at the same time the nose pitched up rapidly and rolled to the right. Corrective control inputs were applied to level the gyrocopter; however, it rolled left and over flew the edge of the runway. The pilot reduced the collective, and the aircraft touched down on the ground in a level attitude rolling approximately 25 mph. As the gyrocraft slowed to approximately 5 mph, the nose landing gear collapsed, the gyrocraft nosed down, and the main rotor blades contacted the ground and sustained structural damage. The pilot had accumulated 3,800 flight hours. However, this was the pilot's first flight in this aircraft. According to the manufacturer, the flight was conducted in order to understand the prototype's flight characteristics.

Flight

Event TypeAccident
Event Time14:46 CDT
Nearest AirportOlney Municipal (0nm)
Runway17
Runway Length5500 ft
Runway Width150 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCartercopters Cartercopter
Tail NumberN121CC
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsGm · Corvette LS1 · Reciprocating · 350
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 66 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind160° @ 8 kt, gusting 12 kt
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data