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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 7, 1999 · Enstrom F-28C · N51770

Pendleton, OR

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 7, 1999
Injury Outcomes
No injuries (1 uninjured)
Location
Pendleton, OR
Aircraft
Enstrom F-28C
Tail Number
N51770
Operator
General Aircraft Services
Injuries
None
Aircraft Damage
Substantial
NTSB Number
SEA99LA048

During takeoff from the refueling pad, the helicopter's engine lost power and the pilot attempted an autorotation. Because the aircraft did not yet have sufficient airspeed or altitude to complete a successful autorotation, it landed hard and the main rotor blades flexed downward and impacted the tail boom. It was later determined that water contamination had accidentally been transferred from a portable refueling barrel to the aircraft's fuel system during hot refueling (with engine still running). It could not be determined how water was introduced into the refueling barrel.

NTSB Probable Cause

A loss of power due to water contamination of the fuel. Factors include the inability of the helicopter to perform a successful autorotation immediately after takeoff.

Full Narrative

On April 6, 1999, approximately 1730 Pacific daylight time, a main rotor blade of an Enstrom F-28C helicopter, N51770, impacted the aircraft's tail boom during an emergency landing near Pendleton, Oregon. The aircraft, which was owned and operated by General Aircraft Services, sustained substantial damage, but the commercial pilot reported that he was not injured. No flight plan had been filed for the VFR 14 CFR Part 137 aerial application flight, and there was no report of an ELT activation. According to the pilot, he had just taken off from the refueling site and was beginning to initiate a climb when the engine lost power. He attempted to autorotate to a landing, but since the aircraft had not attained sufficient airspeed or altitude to perform a successful autorotation, it hit hard and the main rotor blades flexed downward and impacted the tail boom. It was later determined that the fuel in the portable refueling barrel was contaminated with water. While the pilot kept the aircraft running during the refueling operation (hot refueling), water-contaminated fuel was transferred from the barrel to the helicopter's fuel system and remained undetected. It could not be determined how water was introduced into the barrel itself.

Flight

Event TypeAccident
Event Time17:30 PDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftEnstrom F-28C
Tail NumberN51770
Aircraft CategoryHeli
DamageSubstantial
OperatorGeneral Aircraft Services
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-F1AD · Reciprocating · 225
Seats3

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 43 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility20 sm
CeilingNone
Temperature / Dew Point61 F / 0 C
Altimeter0
Weather SourceWIT

Appendix: Source Data