LAX89LA270

NTSB accident investigation · Bell 206B · Bakersfield, CA · August 9, 1989

Accident · Serious injuriesLimited investigationFinal report
Date
August 9, 1989, 11:15 local (18:15 UTC)
Place
Bakersfield, CA
Injuries
2 serious, 1 uninjured
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N90296Bell 206B
Weather
Visual (VMC) · Day
Status
Completed · report September 9, 1992
Report
Approved by Office Director
FAA report
19890809028339A
Case key
26473

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

The loss of engine power due to the helicopter being flown in exhaust gases emanating from a cogeneration plant chimney stack that exceeded the certification standards of the powerplant. Contributing to the accident was invisible nature of the exhaust gases which made the detection of their presence unlikely.

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) - nonmechanicalManeuvering
Weather condition - temperature extremesFactor
Miscellaneous - starvationCause
Visual lookout - not possiblePilot in commandFactor
Turboshaft engine - failure,totalFactor
Design stress limits of aircraft - exceededPilot in commandFactor
Information unavailablePilot in commandCause
Forced landingDescent - emergency
Autorotation - performedPilot in commandFactor
In flight collision with objectLanding - flare/touchdown
Object - vehicle
Hard landingLanding - flare/touchdown
Proper descent rate - not possiblePilot in commandFactor

Analysis

The helicopter crew was filming a cogeneration plant. The helicopter orbited the plant three times. During the third orbit, the helicopter passed over the exhaust chimney of the plant which was operating at the time. There was no visible indication that exhaust gases were emanating from the chimney. The gases were reported to be 350 degrees fahrenheit with a 3.6 percent oxygen content. The helicopter turboshaft engine lost power over the center of the chimney. The pilot entered autorotation towards an open area of a parking lot. During the flare, the helicopter struck a vehicle, and landed hard, severed the tailboom, and rolled on to its side. The certification standard for the engine was 120 degrees fahrenheit.

Aircraft

Registration
N90296
Reported as
Bell 206B
Category
Helicopter
Serial number
1738
Airframe hours
4,424
Engine
Allison 250-C20, 400 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 91
Registered owner
National Helicopter Service
Airworthiness certificate
Special, Restricted (Special); Standard, Normal
Last inspection
100 hour · June 8, 1989 · 98 hours before
Departed
VNY · Van Nuys, CA
Flight plan
Company VFR

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
51
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
8,000 total · 5,000 in this make and model · 55 in the last 90 days · 20 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
20 statute miles
Lowest ceiling
None
Temperature
84 °F

FAA reports on this event · 1

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