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Aviation safety reports, made easier to study

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April 17, 1994 · Bell 47G-3B-1 · N304JP

Yuma, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 17, 1994
Injury Outcomes
No injuries (1 uninjured)
Location
Yuma, AZ
Aircraft
Bell 47G-3B-1
Tail Number
N304JP
Operator
Sundown Helicopters
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX94LA200

The pilot reported that the helicopter had completed a swath run and was pulling up to clear a line of trees when the engine decelerated to idle. The pilot entered an autorotation and landed hard, damaging the skids and the fuselage. Postaccident inspection of the engine revealed that the throttle arm had come off the carburetor throttle body shaft. The operator stated that the arm and shaft were new components, installed on February 24, 1994, by a contract mechanic. The operator also stated that an 'excessive amount (about 2 inches) of safety wire was on the arm, which allowed the arm to slip off the shaft.'

NTSB Probable Cause

an uncommanded engine deceleration to idle due to the improper installation of the throttle arm on the carburetor shaft.

Full Narrative

On April 16, 1994, at 2000 mountain standard time, a Bell 47G-3B- 1 helicopter, N304JP, landed hard following a loss of engine power while engaged in aerial application operations near Yuma, Arizona. The helicopter was owned and operated by Sundown Helicopters, Inc., of Yuma, Arizona, under the provisions of 14 CFR Part 137 of the Federal Aviation Regulations. Visual meteorological conditions prevailed at the time and no flight plan was filed for the operation. The aircraft incurred substantial damage. The certificated commercial pilot, the sole occupant, was not injured. The flight originated from the field to be sprayed about 1915 hours on the day of the accident. The operator and pilot reported that the helicopter had completed a swath run and was pulling up to clear a line of trees when the engine decelerated to idle. The pilot entered an autorotation and landed hard, damaging the skids and the fuselage. Postaccident inspection of the engine revealed that the throttle arm had come off the carburetor throttle body shaft. The operator stated that the arm and shaft were new components, installed on February 24, 1994, by a contract mechanic. The operator also stated that an "excessive amount (about 2 inches) of safety wire was on the arm, which allowed the arm to slip off the shaft."

Flight

Event TypeAccident
Event Time20:00 MST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 47G-3B-1
Tail NumberN304JP
Aircraft CategoryHeli
DamageSubstantial
OperatorSundown Helicopters
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · V0-435-AIF · Reciprocating · 260
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 47 · Second Class

Conditions

ConditionsVMC
LightDusk
Wind320° @ 2 kt
Visibility40 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data