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NTSB Report

February 4, 2015 · Autogyro Gmbh Calidus · N595X

Crozet, VA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 4, 2015
Injury Outcomes
No injuries (1 uninjured)
Location
Crozet, VA
Aircraft
Autogyro Gmbh Calidus (2014)
Tail Number
N595X
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ERA15CA121

After departing from the airport where the pilot kept the gyroplane, he flew to his family farm and landed without incident on a 1,500-foot-long grass polo field. Later on, during an attempted takeoff from the same field, when the gyroplane was traveling at 25 to 30 knots and was about 150 feet into the takeoff roll, the gyroplane rose to a balanced position on its main wheels, but then began to bounce up and down violently. The pilot then lost control of the gyroplane and it rolled over on its left side about 300 feet into the takeoff roll. The pilot advised that there was nothing mechanically wrong with the gyroplane. He further advised that it was "pilot error" and that he had "over advanced" the blades by pushing the control stick too far forward and that the blades were not yet at speed (too low a rotor rpm) when he did it. The pilot was not injured, but the gyroplane incurred damage to the rotor blades, the pusher propeller, the horizontal stabilizer, the vertical stabilizer, the rudder, the engine cowling, and the wheel pants.

NTSB Probable Cause

The pilot's improper control inputs which resulted in a loss of control and rollover during the takeoff roll.

Full Narrative

After departing from the airport where the pilot kept the gyroplane, he flew to his family farm and landed without incident on a 1,500-foot-long grass polo field. Later on, during an attempted takeoff from the same field, when the gyroplane was traveling at 25 to 30 knots and was about 150 feet into the takeoff roll, the gyroplane rose to a balanced position on its main wheels, but then began to bounce up and down violently. The pilot then lost control of the gyroplane and it rolled over on its' left side about 300 feet into the takeoff roll. The pilot advised that there was nothing mechanically wrong with the gyroplane. He further advised that it was "pilot error" and that he had "over advanced" the blades by pushing the control stick too far forward and that the blades were not yet at speed (too low a rotor rpm) when he did it. The pilot was not injured, but the gyroplane incurred damage to the rotor blades, the pusher propeller, the horizontal stabilizer, the vertical stabilizer, the rudder, the engine cowling, and the wheel pants.

Flight

Event TypeAccident
Event Time14:00 EST
Nearest AirportPolo Field (0nm)
RunwayNone
Runway Length1500 ft
Runway Width450 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftAutogyro Gmbh Calidus
Tail NumberN595X
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotax · 914UL · Reciprocating · 115
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 60 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind6 kt, gusting 18 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point55 / 21 C
Altimeter30.04 inHg
Observation Time18:53
Weather SourceWFAC

Appendix: Source Data