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August 8, 2005 · Hughes 369D · N58431

North Las Vegas, NV

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 8, 2005
Injury Outcomes
No injuries (2 uninjured)
Location
North Las Vegas, NV
Aircraft
Hughes 369D
Tail Number
N58431
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX05CA263

The tail rotor and stinger were damaged during a full touchdown practice autorotation. During a 120-day recurrent training, the instructor pilot and commercial pilot were performing their fifth full-down autorotation. Both pilots were on the controls during the maneuver and the instructor pilot advised the commercial pilot to push the cyclic forward during the deceleration flare; however, the commercial pilot did not move it far enough and stinger impacted the ground, followed by the tail rotor. The tail rotor was substantially damaged and had to be replaced. No mechanical problems were reported with the helicopter prior to the accident.

NTSB Probable Cause

the pilot's improper use of the cyclic flight control and the flight instructor's inadequate supervision of the flight.

Full Narrative

On August 8, 2005, at 1115 Pacific daylight time, a Hughes 369D, N58431, collided with the ground during a practice autorotation at the North Las Vegas Airport, Las Vegas, Nevada. Las Vegas Metropolitan Police Department, also the registered owner of the helicopter, was operating it under the provisions of 14 CFR Part 91. The instructor pilot and commercial pilot undergoing recurrency training were not injured; the helicopter sustained substantial damage. The helicopter departed from North Las Vegas at 1030 that morning for the local area instructional flight. Visual meteorological conditions prevailed and no flight plan had been filed. The instructor pilot reported that he was conducting a 120-day recurrent training for the commercial pilot. While performing their fifth full-down autorotation with both pilots on the controls, the stinger impacted the ground, followed by the tail rotor. Just prior to the ground contact in the flare, the instructor pilot advised the commercial pilot to push forward; however, the tail rotor impacted the ground. The tail rotor was substantially damaged and had to be replaced. The instructor pilot did not report any mechanical problems with the helicopter prior to the accident. According to the Rotorcraft Flying Handbook (FAA-H-8083-21), "Care must be taken in the execution of the flare so that the cyclic control is not moved rearward so abruptly as to cause the helicopter to climb, nor should it be moved so slowly as to not arrest the descent, which may allow the helicopter to settle so rapidly that the tail rotor strikes the ground."

Flight

Event TypeAccident
Event Time11:15 PDT
Nearest AirportNorth Las Vegas (0nm)
Flight Plan FiledNone
Aircraft FireNo

Aircraft

AircraftHughes 369D
Tail NumberN58431
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsRolls Royce · 250-C20B · Turboshaft

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 57 · Second Class
Crew 2Age 52 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind150°, gusting 14 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point59
Altimeter29.95 inHg
Observation Time17:53
Weather SourceWFAC

Appendix: Source Data