N8162C

Substantial
Minor

Piper PA-18 S/N: 18-3618

Accident Details

Date
Saturday, July 18, 1998
NTSB Number
ANC98LA102
Location
KODIAK, AK
Event ID
20001211X10455
Coordinates
57.789752, -152.400314
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

The loss of engine power due to carburetor icing and the pilot's improper use of the carburetor heat control. A factor associated with the accident is the rough and uneven terrain at the forced landing area.

Aircraft Information

Registration
N8162C
Make
PIPER
Serial Number
18-3618
Engine Type
Reciprocating
Year Built
2003
Model / ICAO
PA-18 PA18
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AIRCRAFT GUARANTY TITLE & TRUST LLC TRUSTEE
Address
PO BOX 2549
Status
Deregistered
City
ONALASKA
State / Zip Code
TX 77360-2549
Country
United States

Analysis

On July 18, 1998, at 1554 Alaska daylight time, a float equipped Piper PA-18 airplane, N8162C, sustained substantial damage during a forced landing after takeoff from the Lily Lake Seaplane Base, Kodiak, Alaska. The airline transport pilot was not injured, and the sole passenger sustained minor injuries. The flight was operated under 14 CFR Part 91, as a personal flight. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed.

The pilot told the NTSB investigator-in-charge on July 18, that he taxied with carburetor heat applied, and had a normal run-up and magneto check prior to takeoff. He performed a takeoff with carburetor heat off, and at 300 feet above the surface during the initial climb, the engine "coughed." He said he applied carburetor heat and the engine smoothed out. He stated that he then removed carburetor heat and the engine lost total power. There was not enough room to land on the lake, so he landed straight ahead on a road at the departure end of the lake. During the landing roll, the floats contacted soft gravel, and the float struts and fuselage buckled.

The airplane's engine had been overhauled 167 hours prior to the accident. Inspection of the airplane by an FAA inspector revealed no anomalies. The engine was removed to Anchorage, Alaska, and operated normally on a test stand on August 24. The carburetor was disassembled and inspected on September 11, with no anomalies noted.

The Aviation Safety Bureau of Transport Canada chart "Conditions Known Favorable For Carburetor Icing" shows an outside air temperature of 57 degrees Fahrenheit combined with a dew point of 40. Fahrenheit falls in the "moderate icing - cruise power" range.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA102