FTW89FA075

NTSB accident investigation · Bell 206B · West Cameron · April 5, 1989

Accident · No injuriesField investigationFinal report
Date
April 5, 1989, 13:27 local (18:27 UTC)
Place
West Cameron
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N5004LBell 206B
Weather
Visual (VMC) · Day
Status
Completed · report February 15, 1991
Report
Approved by Office Director
FAA report
19890405006609A
Case key
22765

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

Inadequate maintenance/inspection of the aircraft fuel system by company maintenance personnel and fuel contamination, which resulted in a partial loss of engine power. Related factors were: a binding (stuck) fuel filter cap bypass valve and partial failure (intermittent operation) of the respective annunciator light system.

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(partial) - nonmechanicalApproach - vfr pattern - final approach
Maintenance,inspection - inadequateCompany maintenance personnelCause
Fuel system - binding(mechanical)Factor
Annunciator panel light(s) - failure,partialFactor
Fluid,fuel - contaminationCause
Forced landingDescent - emergency
Autorotation
In flight collision with objectLanding - flare/touchdown

Analysis

The helicopter had svrl inflt eng decelerations that maintenance efforts did not isolate. After replacing the eng fuel controller, a test flt was made (from an oil drilling platform). Drg the flt, the eng surged, then decelerated. The plt was unable to reach the helipad. He elected to land on the platform, short of the helipad, rather than accept sea conds of 8 ft waves. Drg the landing, the helicopter was damaged. A post-acdnt exam revealed fuel contamination had occurred. Contamination had bypassed filters in the fuel sys & had clogged & collapsed the eng fuel nozzle screen. The airframe fuel filter cap bypass vlv was fnd stuck open in the bypass mode. A pin (connected to the fuel filter cap impending bypass test button) was fnd bent, holding the bypass vlv open. An open bypass vlv should have illuminated a respective annunciator light in the cockpit; however, when checked, the annunciator light operd only intermittently due to a faultycomponent in the sys. Drg tests, the clogged/collapsed fuel screen prevented sufficient fuel flow to sustain eng power.

Aircraft

Registration
N5004L
Reported as
Bell 206B
Category
Helicopter
Serial number
2451
Airframe hours
6,728
Engine
Allison 250-C20B, 235 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 91
Operator
Industrial Helicopters
Registered owner
Notlef, Inc
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · March 17, 1989 · 42 hours before
Airport
WC26 · West Cameron, Blk 266

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
50
Certificate
Commercial
Airplane ratings
Multi-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Right
Toxicology
Performed
Flight hours
7,008 total · 4,540 in this make and model · 6,740 as pilot in command · 117 in the last 90 days · 39 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 25 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
64 °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.