CHI98LA062

NTSB accident investigation · Piper PA-28-140 · Dawson, ND · December 9, 1997

Accident · No injuriesLimited investigationFinal report
Date
December 9, 1997, 12:00 local (18:00 UTC)
Place
Dawson, ND
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N55259Piper PA-28-140
Weather
Day
Status
Completed · report July 28, 1999
Report
Approved by Office Director
FAA report
19971209038159A
Case key
10805

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot's improper use of carburetor heat. Factors were carburetor icing conditions and a fence.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine powerTakeoff - initial climb
Weather condition - carburetor icing conditionsFactor
Carburetor heat - improper use ofPilot in commandCause
Forced landingEmergency descent/landing
On ground/water collision with objectLanding - roll
Object - fenceFactor

Analysis

The pilot said that engine power was lost during initial climb. He conducted a forced landing off the airport and the airplane impacted a fence. According to the Icing Probability Chart, the conditions favorable to the formation of induction system icing existed based on the temperature and dew point at the two nearest reporting stations. The pilot said that he 'tried' carburetor heat after the loss of power; however, the airplane touched down prior to engine power being restored.

Factual narrative

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.

Aircraft

Registration
N55259
Reported as
Piper PA-28-140
Category
Airplane
Serial number
28-7325354
Engine
Lycoming O-320-E2A, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Warren S. Devore
Airworthiness certificate
Standard, Normal
Departed
NONE

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
39
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
61 total · 11 in this make and model · 30 as pilot in command · 16 in the last 90 days · 4 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Day
Wind
100° at 5 knots
Visibility
6 statute miles
Lowest ceiling
800 ft broken
Temperature
27 °F, dew point 25 °F
Altimeter
29.00 inHg
Observed at
BIS, 39 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.