N55259

Substantial
None

Piper PA-28-140 S/N: 28-7325354

Accident Details

Date
Tuesday, December 9, 1997
NTSB Number
CHI98LA062
Location
Dawson, ND
Event ID
20001208X09277
Coordinates
46.866024, -99.753145
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 improper use of carburetor heat. Factors were carburetor icing conditions and a fence.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-7325354
Engine Type
Reciprocating
Year Built
1973
Model / ICAO
PA-28-140 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-140

Registered Owner (Current)

Name
HETH STEVEN L
Address
1701 COUNTY ROAD 6 NW
City
WESTHOPE
State / Zip Code
ND 58793-9779
Country
United States

Analysis

On December 9, 1997, at 1200 central time, a Piper PA-28-140, N55259, sustained substantial damage during a forced landing after departing a private airstrip. The pilot reported no injuries. The pilot said the engine lost power on initial climb and a forced landing resulted in the airplane impacting a fence. The personal 14 CFR Part 91 flight was operating in what the pilot stated was visual meteorological conditions. No flight plan was on file for the local flight. The flight was originating at the time of the accident.

Bismarck Municipal Airport, 40 miles to the west of the accident site was reporting instrument meteorological conditions in the form of a ceiling of 800 feet, five minutes prior to the accident. The temperature was 26 degrees (F),and the dew point was 23 degrees (F). Jamestown Municipal Airport 52 miles to the east of the accident site was reporting instrument meteorological conditions in the form of visibility one and one-half miles in light snow and fog, 12 minutes prior to the accident. The temperature was 28 degrees (F) and the dew point was 23 degrees (F). The pilot reported conditions at the accident site as clear with unrestricted visibility.

The pilot said that after the initial loss of power and he initiated a forced landing, he switched tanks and "tried" the carburetor heat, but engine power was not restored prior to the airplane touching down and impacting a fence..

An Icing Probability chart from a Federal Aviation Administration Advisory Circular is attached to this report. The temperatures and dew points from the above reporting stations indicate conditions favorable to formation of induction system icing.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI98LA062