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Aviation safety reports, made easier to study

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NTSB Report

January 31, 2003 · Bell 206L-1 · N27AE

West Plains, MO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 31, 2003
Injury Outcomes
No injuries (2 uninjured)
Location
West Plains, MO
Aircraft
Bell 206L-1
Tail Number
N27AE
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI03LA062

At the completion of a simulated autorotation maneuver the main rotor severed the tailboom. The check airman reported that at approximately 20 feet above ground level he "determined the sink rate was excessive" and he decided to perform a "power recovery." The check airman stated, "I repositioned my hand, started opening the throttle while leveling the aircraft and applying a cushioning pitch pull." The helicopter impacted off the left side of the runway with "the skids aligned with the direction of travel slightly aft skid low." The check airman reported, "The aircraft rocked up onto the toes of the skids and I increased collective pitch and applied aft cyclic, when I did the main rotor impacted the tailboom severing it."

NTSB Probable Cause

The excessive descent rate that required an abrupt flare, resulting in the main rotor severing the tailboom.

Full Narrative

On January 31, 2003, at 1230 central standard time, a Bell 206L-1 helicopter, N27AE, piloted by a commercial pilot, sustained substantial damage when the main rotor severed the tailboom during an intentional autorotation at the West Plains Municipal Airport (UNO), West Plains, Missouri. Visual meteorological conditions prevailed at the time of the accident. The instructional flight was conducted under the provisions of 14 CFR Part 91 on a company flight plan. The check airman and dual student reported no injuries. The flight departed UNO at 1215 for the local area flight. The helicopter operator was Air Evac EMS Inc., an on-demand air ambulance service. According to a written statement provided by the company check airman, he was demonstrating an autorotation maneuver to the dual student when the accident occurred. The check airman stated: "Entered the autorotation, slowed to 60 [knots], rotor was in the green, gas producer stable and aircraft in trim." The check airman reported that at approximately 20 feet agl he "determined the sink rate was excessive" and he decided to perform a "power recovery." The check airman reported that his grip on the throttle did not allow an adjustment of the throttle. The check airman reported, "I repositioned my hand, started opening the throttle while leveling the aircraft and applying a cushioning pitch pull." The helicopter impacted off the left side of the runway with "the skids aligned with the direction of travel slightly aft skid low." The check airman stated, "The aircraft rocked up onto the toes of the skids and I increased collective pitch and applied aft cyclic, when I did the main rotor impacted the tailboom severing it."

Flight

Event TypeAccident
Event Time12:30 CST
Nearest AirportWest Plains Municipal Airport (0nm)
Runway180
Runway Length5102 ft
Runway Width75 ft
Flight Plan FiledCvfr
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206L-1
Tail NumberN27AE
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsRolls-Royce · 250-C28B · Turboshaft · 550
Seats3

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 43 · Second Class · None
Crew 2Age 41 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind270° @ 10 kt, gusting 19 kt
Visibility6 sm
CeilingOvercast 1900 ft
Temperature / Dew Point46 / 39 C
Altimeter29.95 inHg
Observation Time18:53
Weather SourceWFAC

Appendix: Source Data