N8555W

Substantial
None

Piper PA-28-235S/N: 28-10069

Accident Details

Date
Sunday, December 22, 2002
NTSB Number
CHI03LA043
Location
Carleton, MI
Event ID
20021226X05634
Coordinates
42.018054, -83.377220
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The #2 cylinder exhaust valve failed due to undetermined reasons. A factor associated with the accident was the soft terrain encountered during the forced landing.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-10069
Engine Type
Reciprocating
Year Built
1963
Model / ICAO
PA-28-235P28B
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-235

Registered Owner (Current)

Name
SOTTILE ANDRE M
Address
904 HOLLYWOOD DR
City
MONROE
State / Zip Code
MI 48162-3044
Country
United States

Analysis

On December 22, 2002, at 1700 eastern standard time, a Piper PA-28-235, N8555W, operated by a commercial pilot, experienced a nose gear collapse during an off airport forced landing following a loss of engine power. The pilot and passenger were not injured. The airplane received substantial damage. The 14 CFR Part 91 personal flight was operating in visual meteorological conditions without a flight plan. The last leg of the flight originated at Pontiac, Michigan, at 1615.

The pilot reported that while en route to his destination, the engine power dropped to 1,300 rpm. He stated he applied carburetor heat, turned on the auxiliary fuel pump, and switched fuel tanks to no avail. The pilot reported that the passenger checked the engine instruments and all indications were normal. The pilot contacted the Willow Run Air Traffic Control Tower and informed them of the situation, stating that he was going to land at their airport. After turning toward the airport, the pilot determined he was not going be able to reach the airport, so he pilot selected a plowed field in which to land. The nose gear collapsed during the landing and the airplane came to rest on the engine cowling and main landing gear.

The airplane's engine was examined by inspectors from the Federal Aviation Administration Detroit, Michigan, Flight Standards District Office. The inspectors reported that the number 2 cylinder exhaust valve was broken off and a piece of the number 2 cylinder was missing. Portions of the exhaust valve and valve stem were recovered from the engine. Visual examination revealed the fractured surfaces were deformed and obscured by impact damage to such a degree that the failure mode could not be determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI03LA043