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December 13, 2000 · Cartercopter Model 1 · N121CC

Olney, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 13, 2000
Injury Outcomes
No injuries (2 uninjured)
Location
Olney, TX
Aircraft
Cartercopter Model 1
Tail Number
N121CC
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW01LA040

The pilot was performing a short test flight in an experimental prototype gyroplane. After a low level, low airspeed flight down runway centerline, the pilot executed a run-on landing at 30 MPH about 300 feet from the departure end of the runway. The aircraft slowed to about 20 MPH as it rolled off of the runway surface, and onto a muddy field. Subsequently, the nose landing gear collapsed, allowing a 4-foot x 4-foot long section of nose boom to dig into the mud. The aircraft then pitched down about the nose as the main rotor impacted the ground. After the rotor impact, the aircraft rolled to the right, and the right wing impacted the ground. The aircraft sustained structural damage to the right wing, rudder, and main rotor. Skid marks, found about 150 feet forward of the original touch down point, and correlating to the aircraft's landing gear/tires, were observed on the runway. The designer and manufacturer of the prototype monitored the entire flight with on-board parameter recording devices. These data suggested that the pilot did not lower the collective enough for the brakes to be effective.

NTSB Probable Cause

The pilot's delay in lowering the collective during a run-on landing, which resulted in a runway overrun. A factor was the muddy terrain.

Full Narrative

On December 13, 2000, at 1700 central standard time, a Cartercopter Model-1 experimental prototype gyroplane, N121CC, registered to and operated by Cartercopter LLC of Wichita Falls, Texas, was substantially damaged during landing on runway 22 at the Olney Municipal Airport near Olney, Texas. The commercial pilot and his pilot rated passenger were not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 local test flight. The pilot reported that he was performing a short test flight from one end of the runway to the other end. After a low level, low airspeed, flight down the runway centerline, the pilot executed a run-on landing at 30 MPH about 300 feet from the departure end of the runway. The aircraft slowed to about 20 MPH as it rolled off of the runway surface, and onto a muddy field. Subsequently, the nose landing gear collapsed, allowing a 4-foot x 4-foot long section of nose boom to dig into the mud. The aircraft then pitched down about the nose as the main rotor impacted the ground. After main rotor impact, the aircraft rolled to the right, and the right wing impacted the ground. Examination of the wreckage revealed structural damage to the right wing, rudder, and main rotor. Skid marks, found about 150 feet forward of the original touch down point, and correlating to the aircraft's landing gear/tires, were observed on the runway. The operator, who is the designer and manufacturer of the prototype, reported that he was monitoring the entire flight with on board parameter recording devices. He stated that the pilot "failed to lower the collective after landing and so there was not enough weight on the wheels for the brakes to be effective."

Flight

Event TypeAccident
Event Time17:00 CST
Nearest AirportOlney Airport (0nm)
Runway22
Runway Length5098 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCartercopter Model 1
Tail NumberN121CC
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsGm · LS 1 CORVETTE · Reciprocating · 350
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 37 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility6 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data