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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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April 20, 2002 · Enstrom F-28C · N51769

Hot Springs, MT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 20, 2002
Injury Outcomes
No injuries (3 uninjured)
Location
Hot Springs, MT
Aircraft
Enstrom F-28C
Tail Number
N51769
Injuries
None
Aircraft Damage
Substantial
NTSB Number
SEA02LA075

The pilot was taking off in variable winds in a helicopter that was near its maximum certified gross weight. Just as the aircraft started to move forward out of a hover, the wind shifted from a headwind to a tailwind gust. The pilot was unable to adequately compensate for the unfavorable wind change, and the helicopter impacted the terrain with sufficient force for the main rotor to come in contact with the tail boom.

NTSB Probable Cause

The pilot's failure to adequately compensate for unfavorable wind conditions. Factors include unfavorable/shifting winds, and a tailwind gust.

Full Narrative

On April 20, 2002, approximately 1500 mountain daylight time, an Enstrom F-28C helicopter, N51769, collided with terrain just after liftoff from an off-airport site near Hot Springs, Montana. The commercial pilot and his two passengers were not injured, but the aircraft, which is owned and operated by the pilot, sustained substantial damage. The local 14 CFR, Part 91 pleasure flight was being operated in visual meteorological conditions. No flight plan had been filed. There was no report of an ELT activation. According to the pilot, when he and his passengers boarded the helicopter, the winds were almost nonexistent. But, by the time he was ready to lift off, the winds were variable at about ten knots. In a telephone interview with the Investigator-In-Charge (IIC), the pilot said that right after liftoff, just as the helicopter was starting to move forward, the wind shifted from a headwind to a tailwind gust. Although he attempted to compensate for the change in relative wind, the pilot was unsuccessful, and the helicopter impacted the terrain with sufficient force to result in the main rotor coming in contact with the tail boom. According to the fuel and occupant weights provided by the pilot, the aircraft was being operated within 25 pounds of its certified maximum gross weight.

Flight

Event TypeAccident
Event Time15:00 MDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftEnstrom F-28C
Tail NumberN51769
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-EIAD · Reciprocating · 205
Seats3

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 37 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind10 kt, gusting 15 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point61 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data