N369BD

Substantial
None

AEROSPATIALE AS350S/N: 1675

Accident Details

Date
Friday, October 28, 2016
NTSB Number
WPR17LA014
Location
Starbuck, WA
Event ID
20161031X33238
Coordinates
46.588333, -118.123054
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power due to fuel exhaustion, which resulted from the pilot’s reliance on the fuel gauge that was displaying an incorrect fuel amount due to the separation of the fuel transmitter float pin guide from the float.

Aircraft Information

Registration
N369BD
Make
AEROSPATIALE
Serial Number
1675
Engine Type
Turbo-shaft
Year Built
1983
Model / ICAO
AS350AS50
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
POPE JIM D
Address
5305 B RIVER RD NORTH
Status
Deregistered
City
KEIZER
State / Zip Code
OR 97303
Country
United States

Analysis

On October 28, 2016, about 1240 Pacific daylight time (PDT), a Eurocopter S.N.I.A.S. AS350B helicopter, N369BD, sustained substantial damage during a forced landing following a loss of engine power near Starbuck, Washington. The commercial pilot was not injured. The helicopter was registered to a private individual and operated by Leading Edge Aviation LLC under the provisions of Title 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed, and no flight plan was filed for the local flight. The flight originated from a nearby staging area at 1137.

The pilot reported that during the flight as he was making his 6th pass, on the 5th application load, and traveling upslope from the west to the east, the fuel pressure warning light illuminated. The pilot scanned the instruments and noticed the fuel pressure was low, and the fuel quantity was indicating between 40-50%. About 3-4 seconds later the engine started to lose power. The pilot entered an autorotation and set up for a landing in the flattest area he could find in the canyon. During the approach the pilot extended the landing to make it to a more suitable site. The helicopter subsequently landed hard.

The helicopter sustained substantial damage to the tailboom and to the main rotor assembly. During the recovery it was noted that the helicopter fuel tank was intact, undamaged and void of fuel, but the fuel quantity gauge still indicated 42% fuel remaining, which converts to about 60-gallons.The helicopter was recovered from the accident site for further examination.

Examination of the fuel transmitter revealed that the float guide pin was separated from the float assembly at the tack weld. According to the manufacturer, the separation of the float guide pin would allow the float to slide down the center torque shaft and not allow the potentiometer drive plate at the bottom to rotate with changing fuel quantity. Maintenance records for the overhauled fuel transmitter stated that the float guide was replaced at the time of overhaul on November 23, 2015.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR17LA014