ANC83FA144

NTSB accident investigation · Bell 206L-1 · Bettles, AK · August 13, 1983

Accident · No injuriesField investigationFinal report
Date
August 13, 1983, 10:35 local (18:35 UTC)
Place
Bettles, AK
Injuries
6 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N1081KBell 206L-1
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19830813075829A
Case key
4050

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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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) - mech failure/malfHover
Fluid,fuel - contaminationFactor
Fuel system,screen - inadequateCause
Acft/equip,inadequate designManufacturerCause
Electrical system,electric switch - inoperative
Fuel system - failure,partial
Fluid,fuel - low levelFactor
Precautionary landing - not performedPilot in command
Fluid,fuel - starvationCause
Forced landingLanding - flare/touchdown
Autorotation - not identifiedPilot in command
Hard landingLanding - flare/touchdown

Analysis

According to the plt, the low fuel warning light illuminated when the fuel gage was indicating 200 lbs. He reported he could see the arpt lights & elected to continue the flt. After arriving, he terminated his apch to a 30 to 50 ft hover with no forward speed. As he applied forward cyclic to hover to the refueling area, the eng flamed out. Subsequently, the helicopter landed hard & the main rotor blades struck the tail boom. An exam reveal there was enough fuel remaining in the main cell for aprx 20 min of flt. Disassembly of the sys revealed that debris (dirt & zinc chromate paint chips) was in the filters. The filter screen had openings of .020 inch. Particles were found in the flow switches. However, the clearance between the flow switch plunger & the wall of the casing was only .012 inch. Evidence was found to indicate this rendered a flow swich inoperative so that fuel would not transfer from the main cell to the rear cell where it could be used by the eng.

Aircraft

Registration
N1081K
Reported as
Bell 206L-1
Category
Helicopter
Serial number
45407
Airframe hours
2,499
Engine
Allison 250-C28B, 435 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 135
Registered owner
Offshore Logistic Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · August 13, 1983 · 2 hours before
Departed
MTF · Fairbanks, AK
Destination
BTT · Bettles, AK
Flight plan
VFR
Airport
BTT · Bettles, runway 1, 5,200 × 160 ft, gravel

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
Multi-engine land, Single-engine land
Instrument ratings
Helicopter
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
5,789 total · 40 in this make and model · 4,827 as pilot in command · 41 in the last 90 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
20° at 7 knots
Visibility
15 statute miles
Lowest ceiling
5,000 ft broken
Temperature
45 °F, dew point 39 °F
Altimeter
29.00 inHg
Observed at
BTT

FAA reports on this event · 1

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