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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 15, 1994 · Bell 206L-3 · N937S

Englewood, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 15, 1994
Injury Outcomes
No injuries (2 uninjured)
Location
Englewood, CO
Aircraft
Bell 206L-3
Tail Number
N937S
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW94LA124

WHILE CONDUCTING A TEST FLIGHT FOLLOWING INSTALLATION OF A FUEL CONTROL/GOVERNOR, THE ENGINE ACCELERATED TO MAXIMUM POWER AND COULD NOT BE CONTROLLED BY THE PILOT. THE PILOT SECURED THE ENGINE AND CONDUCTED AN AUTOROTATION. DURING TOUCHDOWN, THE MAIN ROTOR BLADES CONTACTED THE TAIL BOOM AND SEVERED THE TAIL ROTOR DRIVE SHAFT. EXAMINATION OF THE FUEL CONTROL/GOVERNOR REVEALED A PIECE OF ABRASIVE PAPER IN THE RESET SHAFT HOUSING. ACCORDING TO THE EXAMINATION REPORT, THIS WOULD CAUSE LOSS OF GOVERNOR CONTROL TO THE HIGH SIDE.

NTSB Probable Cause

THE PILOT'S FAILURE TO MAINTAIN ROTOR RPM, HIS DELAYED FLARE, AND IMPROPER TOUCHDOWN. A FACTOR WAS A FAILURE OF THE FUEL CONTROL/GOVERNOR TO THE HIGH SIDE WHICH REQUIRED THE PILOT TO PERFORM A FULL AUTOROTATION.

Full Narrative

On April 15, 1994, at 1610 mountain daylight time, a Bell 206L-3 helicopter, N937S, sustained substantial damage while executing an autorotation following an engine malfunction. The pilot and passenger were not injured. Visual meteorological conditions prevailed and no flight plan was filed for this local test flight. According to the pilot, control of the engine was lost during a test flight and the engine accelerated to maximum power. The pilot secured the engine and performed an autorotative landing. During the landing sequence, the main rotor came in contact with the tail pylon severing the tail rotor drive shaft. The test flight was being conducted due to installation of a fuel control/governor and the passenger (additional crew) was the mechanic who performed the work. The engine, fuel control, and engine governor were removed and sent to the manufacturer, Allied Signal, for further examination. Under direction from local FAA personnel, a functional test and visual examination was conducted. The examination and testing revealed no discrepancies. (The narrative portion of the Allied Signal report is attached. For the full report, contact Allied Signal for report number ECD422-AR64.) Following return of the parts to U. S. West, the aircraft owner, the fuel control and governor were sent to an independent testing laboratory. The results of their examination are attached and provide information that a foreign substance, described as a piece of abrasive paper, was found in the reset shaft housing of the governor. According to the report, under the operating conditions present at the time of the occurrence, if the reset rod sticks, fuel flow will increase.

Flight

Event TypeAccident
Event Time16:10 MDT
Nearest AirportCentennial (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206L-3
Tail NumberN937S
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C30P · Turboshaft · 650
Seats7

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 44 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind330° @ 8 kt
Visibility50 sm
CeilingNone
Temperature / Dew Point66 F / 34 C
Altimeter30.00 inHg
Observation Time22:50
Weather SourceWFAC

Appendix: Source Data