N4380B

Substantial
None

CESSNA 170BS/N: 26724

Accident Details

Date
Wednesday, September 23, 2020
NTSB Number
ANC20LA099
Location
Big Lake, AK
Event ID
20200930102060
Coordinates
61.587423, -150.398400
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot’s failure to utilize carburetor heat while flying in conditions conducive to carburetor icing, which resulted in a total loss of engine power.

Aircraft Information

Registration
Make
CESSNA
Serial Number
26724
Engine Type
Reciprocating
Model / ICAO
170BC170
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
170B

Registered Owner (Current)

Name
THORALL KENNETH L
Address
PO BOX 670364
City
CHUGIAK
State / Zip Code
AK 99567-0364
Country
United States

Analysis

On September 22, 2020, about 1900 Alaska daylight time, a Cessna 170B, N4380B, was substantially damaged when it was involved in an accident near Big Lake, Alaska. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 flight.

According to the pilot, he was landing on a remote off-airport gravel bar located along a river. During short final, at about 20 ft above ground level, the airplane’s engine sputtered followed by a partial loss of power. The engine then surged briefly followed by a total loss of engine power as the propeller continued to windmill. Subsequently, the airplane touched down in the river short of the gravel bar and nosed over, coming to rest inverted in the river. The airplane sustained substantial damage to the left wing and empennage.

The pilot reported that he had flown for about 1.5 hours prior to the accident and had about 1.7 hours of fuel remaining in the airplane’s fuel tanks at the time of the accident. He reported that he had been applying carburetor heat during his previous landings at the gravel bar and the fuel tank selector was set to BOTH during the approach.

A Federal Aviation Administration (FAA) aviation safety inspector examined the airplane after recovery and did not observe any abnormalities. He stated that he drained the fuel from the gascolator and the fuel looked normal with no contamination present.

A postaccident engine run was successfully performed. A non-aviation fuel tank was installed on the top of the fuselage to provide a fuel source. Air was applied to the fuel lines to provide pressure to ensure proper fuel flow, no contaminates were noted in the fuel lines.

The weather observation station located about 25 nautical miles away from the accident site reported that, about the time of the accident, the temperature was 55.4° F and dew point 37.4° F. According to the carburetor icing-probability chart located in FAA Special Airworthiness Information Bulletin CE-09-35, the accident flight would have been operating in “serious icing in glide power”.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC20LA099