N4373X

Substantial
None

PIPER PA-28-140 S/N: 28-7625023

Accident Details

Date
Sunday, March 20, 1994
NTSB Number
CHI94LA117
Location
ROMEO, MI
Event ID
20001206X00878
Coordinates
42.849334, -83.039466
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. A factor in the accident is weather conducive to the formation of carburetor ice.

Aircraft Information

Registration
N4373X
Make
PIPER
Serial Number
28-7625023
Engine Type
Reciprocating
Model / ICAO
PA-28-140 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HODGSON EDWARD
Address
42132 LOCHMOOR DRIVE
Status
Deregistered
City
MT CLEMENTS
State / Zip Code
MI 48044
Country
United States

Analysis

On March 20, 1994, at 1000 central standard time, a Piper PA-28- 140 airplane, N4373X, sustained substantial damage during a forced landing near Romeo, Michigan. The private pilot sustained no injuries. The personal flight departed the Romeo Airport at 0945 and was conducted under CFR Part 91 in visual meteorological conditions. No flight plan was filed for the local flight.

During a telephone interview, the pilot reported he had experienced a rough engine and a loss of engine power shortly after his third touch-and-go landing on runway 36. He said he rapidly cycled the carburetor heat on then off and tried different throttle positions but the engine did not recover to full power. He initiated a slight left turn to "possibly land on runway 27, or turn around 180 degrees". Realizing he had insufficient altitude, he pulled the throttle to idle and made a slight right turn to perform an emergency landing in an open grassy area on the northern edge of the airport boundary.

Examination of the aircraft by an FAA Airworthiness Inspector revealed upward crushing on the lower nose section and on the right wing. The propeller, nose gear, and right main landing gear were bent aft. The left fuel tank contained approximately five gallons of fuel and the right tank contained about 12 gallons. The fuel strainer was below the fuselage crush line and was dislodged. Clear, red fuel was leaking from the fuel lines. Further inspection of the aircraft and engine revealed no anomalies. The position of the carburetor heat valve was indeterminate due to crushing.

The engine and exhaust system were partially disassembled and inspected by a local aircraft inspector. No discrepancies were noted.

According to the icing probability curves published in DOT/FAA/CT-82/44, potential for carburetor icing existed at glide and cruise power settings. A local flight instructor, who was flying in the traffic pattern 30 minutes prior to the accident, reported a loss of engine power which was corrected with the application of carburetor heat.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI94LA117