ANC90LA135

NTSB accident investigation · Aerospatiale SA-315B · Tok, AK · August 7, 1990

Accident · Serious injuriesLimited investigationFinal report
Date
August 7, 1990, 12:30 local (20:30 UTC)
Place
Tok, AK
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N58000Aerospatiale SA-315B
Weather
Visual (VMC) · Day
Status
Completed · report June 19, 1992
Report
Approved by Office Director
NTSB office
Alaska Regional Office
Safety recommendations
Yes
FAA report
19900807031499A
Case key
5420

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

Improper installation of the fuel filter element in the aircraft by company/maintenance personnel, and subsequent contamination of the fuel system by unfiltered fuel. Factors related to the accident were: inadequate design of the fuel filter assembly, which allowed the improper installation of the filter element, the mechanics lack of familiarity with the aircraft, and failure of ground personnel to insure that fuel from the fuel tanker was free of contamination.

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) - nonmechanicalHover
Fuel system,filter - otherCause
Acft/equip,inadequate designManufacturerFactor
Maintenance,installation - improperCompany maintenance personnelCause
Lack of familiarity with aircraftCompany maintenance personnelFactor
Fluid,fuel - contaminationCause
Forced landingDescent - emergency
Autorotation - performedPilot in command
Hard landingLanding

Analysis

The helicopter was being used in an external load opn to carry cargo with a 100 ft cable. While hovering out of ground effect, the eng lost pwr. A subsequent hovering autorotation resulted in a hard landing. An exam revealed the loss of power was due to fuel contamination although an airframe fuel filter was installed in the main fuel supply line. An exam revealed the filter element had been installed backward in the filter canister. This allowed contaminated fuel to bypass the filter element & enter the eng fuel ctl unit. The reverse instln also resulted in an inop 'fuel filter clogged' warning lgt & prevented the pressure differential button on the filter housing fm extdg. The filter had been inspected & reinstld drg a 100 hr inspn, 17 flt hrs bfr the acdnt. This work was done by a plt under supervision of a mechanic. The mechanic had no prev experience with this make & model of helicopter. 'Top' & 'bottom' were stenciled on the filter element in french. Contaminated fuel was also fnd in the fuel truck.

Aircraft

Registration
N58000
Reported as
Aerospatiale SA-315B
Category
Helicopter
Serial number
2639
Airframe hours
3,607
Engine
Turbomeca ARTOUSTE IIIB, 878 horsepower, turbo shaft
Damage
Substantial damage
Flight
Other work use · Part 133
Registered owner
Pegasus Helicopters, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · August 4, 1990 · 17 hours before
Departed
TKJ · Tok, AK
Flight plan
Company VFR
Airport
NONE

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
43
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
13,000 total · 5,000 in this make and model · 13,000 as pilot in command · 265 in the last 90 days · 98 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 10 knots, gusting 12
Visibility
50 statute miles
Lowest ceiling
5,000 ft broken
Temperature
63 °F, dew point -0 °F
Altimeter
29.00 inHg

FAA reports on this event · 1

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