N620Y

Substantial
None

CUB CRAFTERS INC CC11-100S/N: CC11-00005

Accident Details

Date
Wednesday, June 19, 2013
NTSB Number
ANC13CA056
Location
Dillingham, AK
Event ID
20130619X94050
Coordinates
59.071666, -158.039443
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A loss of engine power due to carburetor icing.

Aircraft Information

Registration
Make
CUB CRAFTERS INC
Serial Number
CC11-00005
Engine Type
4-cycle
Year Built
2006
Model / ICAO
CC11-100
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
CC11-100

Registered Owner (Current)

Name
O'CONNOR LLOYD T
Address
PO BOX 546
City
DILLINGHAM
State / Zip Code
AK 99576-0546
Country
United States

Analysis

The airplane departed with 24 gallons of usable fuel, which normally allows for 4.5 hours of flight. Two and half hours into the flight, the engine started running rough. The pilot confirmed the mixture was rich and the carburetor heat was on. About 5 minutes later the engine quit and the pilot executed a forced landing to an area of tundra-covered terrain, substantially damaging the undercarriage, fuselage, and left wing strut. A postaccident examination by a Federal Aviation Administration Inspector revealed that the carburetor had separated from the engine during the forced landing, and the gascolator drain had tundra embedded in it. The pilot stated that he had turned the fuel selector to the OFF position about 30 minutes after the landing.

The carburetor icing chart indicated the possibility of serious carburetor icing at the reported atmospheric conditions. The Pilot's Handbook of Aeronautical Knowledge (FAA-H-8083-25A) states that first indication of carburetor ice in an airplane with a fixed-pitch propeller is a decrease in engine rpm. Additionally, it states that when conditions are conductive to carburetor icing that carburetor heat should be applied immediately and should be left ON until the pilot is certain all the ice has been removed. If ice is present applying partial heat or leaving heat on for an insufficient time might aggravate the situation.

Postaccident examination of the airframe and engine revealed no preimpact mechanical malfunctions or failure that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC13CA056