LAX90FA268

NTSB accident investigation · Bell 206B · Quincy, CA · July 25, 1990

Accident · No injuriesField investigationFinal report
Date
July 25, 1990, 14:10 local (21:10 UTC)
Place
Quincy, CA
Injuries
4 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N2292WBell 206B
Weather
Visual (VMC) · Day
Status
Completed · report December 30, 1992
Report
Approved by Office Director
FAA report
19900725028459A
Case key
26648

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

An unidentified contaminate lodged in the fuel governor.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - nonmechanicalCruise
Turboshaft engine,free turbine governor - contaminationCause
Forced landingDescent - emergency
Hard landingDescent - emergency

Analysis

The pilot was conducting a helicopter aerial survey and was cruising at 400 ft AGL in mountainous terrain when the engine, without any warning, sustained a flame out. The pilot immediately executed an autorotation and was able to find a suitable landing area. On final approach he observed a steel cable traversing the landing site directly in the helicopter's flight path. He was able to fly over the cable but in doing so the main rotor RPM decayed and the helicopter sustained a hard landing. The post accident investigation disclosed that the engine would not operate at governor power level angles of less than 50 deg. After bench testing the power turbine governor it operated normally when placed on the engine. Test engineers reported that this conditions, in all probability, indicates a contaminate lodged in the power turbine governor. It was disclodged during the bench test.

Aircraft

Registration
N2292W
Reported as
Bell 206B
Category
Helicopter
Serial number
505
Airframe hours
8,234
Engine
Allison 250-C20B, 317 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 135
Registered owner
Rogers Helicopters, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 3, 1990 · 70 hours before
Departed
Storrie, CA

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
47
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
12,000 total · 12,000 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
50 statute miles
Lowest ceiling
None
Temperature
-0 °F, dew point -0 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.