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NTSB Report

June 7, 2016 · Robinson Helicopter R44 II · N41407

Chireno, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 7, 2016
Injury Outcomes
No injuries (1 uninjured)
Location
Chireno, TX
Aircraft
Robinson Helicopter R44 II (2008)
Tail Number
N41407
Injuries
None
Aircraft Damage
Substantial
NTSB Number
GAA16CA297

The student helicopter pilot reported that during a local flight he diverted his attention to the navigational equipment and removed his hand from the cyclic. He reported that he lost control of the helicopter and believed the helicopter became inverted. He further reported that he presumed that he had damaged the rotor system and elected to make a precautionary landing by entering an autorotation. During the landing, the left helicopter skid touched down on uneven terrain and the helicopter rolled over, which resulted in substantial damage to the tail boom. The pilot reported there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The manufacturer provided a test flight video that showed what will occur when the Helicopter's cyclic is released in forward flight. Per the video, in forward flight, should the pilot release the cyclic, the helicopter will pitch up and roll left.

NTSB Probable Cause

The student pilot's selection of unsuitable terrain for landing, which resulted in the helicopter rolling over during landing, and substantial damage to the tail boom.

Full Narrative

The student helicopter pilot reported that during a local flight he diverted his attention to the navigational equipment and removed his hand from the cyclic. He reported that he lost control of the helicopter and believed the helicopter became inverted. He further reported that he presumed that he had damaged the rotor system and elected to make a precautionary landing by entering an autorotation. During the landing, the left helicopter skid touched down on uneven terrain and the helicopter rolled over, which resulted in substantial damage to the tail boom. The pilot reported there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The manufacturer provided a test flight video that showed what will occur when the Helicopter's cyclic is released in forward flight. Per the video, in forward flight, should the pilot release the cyclic, the helicopter will pitch up and roll left.

Flight

Event TypeAccident
Event Time14:00 CDT
Nearest Airport0nm
Flight Plan FiledVFR
Flight Plan ActivatedUnknown
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRobinson Helicopter R44 II
Tail NumberN41407
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540-AE145 · Reciprocating · 260
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 52 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point63 F
Altimeter29.88 inHg
Observation Time19:55
Weather SourceWFAC

Appendix: Source Data