N6497P

Substantial
Minor

Piper PA24S/N: 24-1617

Accident Details

Date
Friday, January 18, 2019
NTSB Number
CEN19LA071
Location
Beechwood, WI
Event ID
20190119X05628
Coordinates
45.606388, -88.109169
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A partial loss of engine power for reasons that could not be determined based on the available information.

Aircraft Information

Registration
N6497P
Make
PIPER
Serial Number
24-1617
Engine Type
Reciprocating
Year Built
1959
Model / ICAO
PA24PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
KRUSWICK MICHAEL W
Address
7610 COUNTY RD Y
Status
Deregistered
City
OCONTO
State / Zip Code
WI 54153-9318
Country
United States

Analysis

On January 18, 2019, about 1530 central standard time, a Piper PA24, N6497P, sustained substantial damage when it was involved in an accident near Beechwood, Wisconsin. The private pilot sustained minor injuries. The airplane was operated as a Title 14 Federal Code of Regulations Part 91 personal flight.

After 25 minutes of uneventful cross-country flight, the pilot noticed that the carburetor temperature gauge was in the “yellow” range. The gauge continued to move into the “red” range, which would indicate freezing. The engine began to lose power and the pilot pulled the carburetor heat knob to the full “ON’ position, set the fuel mixture to full, and turned on the electric fuel pump. There was no change in engine power, so the pilot checked the magnetos and switched fuel tanks from left to right. After pushing the carburetor heat knob in, the engine seemed to run smoother, but there was no increase in power. He pulled the carburetor heat “ON’ again, but the engine still ran poorly.

By this time, the airplane had descended to 2,000 ft. The pilot trimmed the airplane for 100 mph. The engine remained running, but there was still no increase in power. The pilot pulled the carburetor heat “ON’ again, with no increase in engine power. The airplane was descending about 700 ft per minute and passing through 1,200 ft. The pilot made a distress call and announced that he was making an emergency landing. He configured the airplane for a gear-up landing in a field, during which the airplane sustained substantial damage to the fuselage.

According to the carburetor icing probability chart, given a temperature of -7°C and a dew point of -14°C, it could not be determined if the airplane’s carburetor could have been susceptible to icing, because the dew point depression was not within the chart’s matrix.

Damage to the carburetor assembly precluded determination of proper rigging; however, examination of the engine and fuel system revealed no anomalies. The carburetor heat control was found in the forward, “OFF” position.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN19LA071