N47AH

Substantial
None

Bell 47-G3B S/N: 2645

Accident Details

Date
Sunday, October 19, 1997
NTSB Number
SEA98LA006
Location
WINSTON, MT
Event ID
20001208X09121
Coordinates
46.529022, -111.769912
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

Fuel starvation due to fuel flow restriction from a failed carburetor automatic mixture control device. Factors include night light conditions for the forced landing.

Aircraft Information

Registration
Make
BELL
Serial Number
2645
Engine Type
Reciprocating
Year Built
1961
Model / ICAO
47-G3B B47G
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
47G-3B

Registered Owner (Current)

Name
SCOTTS HELICOPTER SERVICES INC
Address
PO BOX 92
City
LE SUEUR
State / Zip Code
MN 56058-0092
Country
United States

Analysis

On October 18, 1997, approximately 2130 mountain daylight time, a Bell 47G-3B, N47AH, being operated and flown by a private pilot, sustained substantial damage during a hard landing following a forced landing near Winston, Montana. The pilot and passenger were uninjured. Visual meteorological bright night conditions existed and no flight plan had been filed. The flight, which was personal, was to have been operated under 14CFR91, and was returning from Townsend, Montana, en route back to Helena.

The pilot reported to an FAA inspector that while climbing through 4,800 feet above ground, the helicopter yawed momentarily and then the engine abruptly ceased developing power. The pilot transitioned into an emergency autorotation and was unable to regain power during the descent. Just prior to landing, the pilot maneuvered to the right to avoid trees and touched down hard on downward sloping terrain. The left skid buckled and the main rotor struck the tail boom, separating the tail rotor and its associated drive and gear box.

Post accident inspection revealed a loose bellows housing on the MA-6AA carburetor's automatic mixture control , marked with P/N 293-549. The bellows housing was found loose on the threaded tube, which was still locked to the seat, allowing the bellows to screw down onto the tube, thereby restricting the fuel delivery orifice. The seat and lock nut remained securely bolted to the float bowl ,however one of the screws was not properly safetied with the tab washer. The last recorded carburetor repair was on 7/22/93, with 817 hours since that repair. Records did not reflect the nature of that repair. According to the carburetor manufacturer's engineering drawings, the bellows is bonded to the threaded tube with a permanent type plastic resin. A check of FAA service difficulty reports found one instance of a failure of the bonding material.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA98LA006