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NTSB Report

March 18, 2001 · Enstrom F-28C · N637H

Hollister, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 18, 2001
Injury Outcomes
2 injuries (2 minor injuries)
Location
Hollister, CA
Aircraft
Enstrom F-28C
Tail Number
N637H
Injuries
Minor
Aircraft Damage
Destroyed
NTSB Number
LAX01LA120

The private pilot lost control of the single-engine helicopter after taking off from a field behind his house and it landed hard, then rolled over after he reduced power and lowered the collective. The pilot reported the helicopter was approximately 50-70 feet in the air when the helicopter violently rotated to the left approximately 90 degrees then started to spin to the right 180 degrees. The pilot added there was no normal response to control inputs. The pilot reduced power and lowered the collective. The helicopter impacted the ground tail first, and spun around to the left before coming to rest on its left side. Inspection of the antitorque control system revealed no preimpact anomalies.

NTSB Probable Cause

the pilot's inadequate use of the antitorque controls and subsequent failure to maintain directional control of the helicopter during the takeoff initial climb.

Full Narrative

On March 18, 2001, at 1345 Pacific standard time, an Enstrom F-28C single-engine helicopter, N637H, was destroyed after impacting terrain following a loss of control during takeoff from a field near Hollister, California. The private pilot and passenger received minor injuries. The helicopter was registered to and operated by the pilot under the provisions of CFR 14 Part 91 as a personal flight when the accident occurred. The local flight was originating from Hollister at the time of the accident. Visual meteorological conditions prevailed and no flight plan had been filed. According to the Federal Aviation Administration (FAA) inspector who responded to the accident site, the pilot reported he departed from the field behind his home and was approximately 50-70 feet in the air when the helicopter violently rotated to the left approximately 90 degrees then started to spin to the right 180 degrees. The pilot added there was no normal response to control inputs. The pilot reduced power and lowered the collective. The helicopter impacted the ground tail first, and spun around to the left before coming to rest on its left side. The pilot and passenger exited the helicopter through the left side door, which had been bent open during the impact sequence. Shortly after the pilot and passenger exited the helicopter, it caught fire and was destroyed, with the exception of the tail boom. According to the pilot, the helicopter was fully refueled prior to taking off. According to the FAA inspector, no preimpact anomalies were noted with the antitorque control system. The tail boom was found separated from the helicopter and the tail rotor drive shaft was torn from the gearbox. There were grounds scars found that dimensionally corresponded to the tail rotor blades. Both tail rotor blades had paint rubbed off of the leading edges and were deformed aft.

Flight

Event TypeAccident
Event Time13:45 PST
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftEnstrom F-28C
Tail NumberN637H
Aircraft CategoryHeli
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360 SER · Reciprocating · 190
Seats3

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 45 · Third Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind300° @ 9 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point70 F / 57
Altimeter30.10 inHg
Observation Time21:53
Weather SourceWFAC

Appendix: Source Data