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Aviation safety reports, made easier to study

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January 19, 2005 · Bell 206B · N8040T

Pinehurst, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 19, 2005
Injury Outcomes
No injuries (2 uninjured)
Location
Pinehurst, TX
Aircraft
Bell 206B
Tail Number
N8040T
Operator
Helicopter Services
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DFW05LA066

The 3,000-hour flight instructor and a private helicopter pilot were conducting proficiency flight training in a helicopter. At approximately 300-feet (AGL) and during the second autorotation, the helicopter was flared and the rate-of-descent was arrested; however, the low rotor RPM horn sounded and the certified flight instructor (CFI) elected to take the helicopter to the ground. The helicopter landed hard and the main rotor blade severed the tail boom.

NTSB Probable Cause

The flight instructor's delay in taking remedial action, which resulted in a hard landing.

Full Narrative

On January 19, 2005, approximately 0900 central standard time, a Bell 206B helicopter, N8040T, was substantially damaged during a hard landing during a practice autorotation near Pinehurst, Texas. The flight instructor and the private pilot, who was receiving instruction, were not injured. The helicopter was owned by Odengene Air Shuttle, Inc. of Sugarland, Texas, and operated by Helicopter Services, Inc. of Spring, Texas. Visual meteorological conditions prevailed, and a flight plan was not filed for the training flight conducted under the provisions of 14 Code of Federal Regulations Part 91. The local flight departed David Wayne Hooks airport (DWH), near Houston, Texas, at 0800. According to a written statement submitted by the 3,000-hour flight instructor, the private pilot hadn't flown for over a year and proficiency flight training maneuvers were to be conducted. The flight training maneuvers were flown over the private pilot's property. Various training maneuvers were conducted, including pick-up and set-down practice, basic navigation procedures, normal departures and approaches, steep approaches to a hover, quick stops, and steep approaches to the ground. An autorotation was performed without incident. A second autorotation was initiated at 1,000 feet above ground level (AGL); at 300 feet AGL, the instructor started to roll power on, and the engine did not respond immediately. The flight instructor stated that the engine "started to make power" and the rate of decent was arrested in the flare; however, the low RPM horn sounded and he elected to take the helicopter to the ground. During the hard landing, the main rotor blade contacted the tail boom. The flight instructor further reported that the helicopter sustained structural damage during the hard landing when a main rotor blade severed the tail boom, just aft of the horizontal "fin". At 0853, the automated weather observing system at DWH reported wind from 120 degrees at 4 knots, 10 statute miles visibility, sky 4,800 scattered, 8,500 broken, temperature 45 degrees Fahrenheit, dew point 37 degrees Fahrenheit, and an altimeter setting of 30.42 inches of Mercury.

Flight

Event TypeAccident
Event Time09:00 CST
Nearest AirportDavid Wayne Hooks Memorial (15nm ESE)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206B
Tail NumberN8040T
Aircraft CategoryHeli
DamageSubstantial
OperatorHelicopter Services
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 420
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 49 · Second Class · None
Crew 2Age 59 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind120° @ 4 kt
Visibility10 sm
CeilingBroken clouds 8500 ft
Temperature / Dew Point45 C / 37 C
Altimeter30.42 inHg
Observation Time14:53
Weather SourceWFAC

Appendix: Source Data