N3560B

Substantial
None

PIPER PA-28-161S/N: 28-8016182

Accident Details

Date
Thursday, September 9, 2010
NTSB Number
CEN10LA531
Location
Buchanan, MI
Event ID
20100909X65425
Coordinates
41.867221, -86.296943
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A failure of the engine's No. 3 and No. 4 cylinder valve lifters for undetermined reasons, which resulted in a total loss of engine power.

Aircraft Information

Registration
N3560B
Make
PIPER
Serial Number
28-8016182
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
PA-28-161P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DVS CORP
Address
198 RIVERSIDE DR
Status
Deregistered
City
CHESTERTON
State / Zip Code
IN 46304-1537
Country
United States

Analysis

On September 9, 2010, at 1251 eastern daylight time, a Piper PA-28-161, N3560B, collided with the terrain during an off airport forced landing following a loss of engine power near Buchanan, Michigan. The pilot was not injured. The airplane was substantially damaged. The airplane was operated by Donnair Aviation. The 14 Code of Federal Regulations Part 91 flight was operating in visual meteorological conditions prevailed and no flight plan was filed. The last leg of the flight originated from the Dowagiac Municipal Airport (C91), Dowagiac, Michigan, at 1242.

The pilot reported he departed Valparaiso, Indiana, and flew to C91 where he made a touch and go landing. He then climbed to an altitude of 3,000 feet above mean sea level (msl) for the flight back to Valparaiso. The pilot stated he turned the fuel pump on, switched fuel tanks, and turned the fuel pump back off. About 11 minutes later, the engine lost all power and the propeller stopped rotating. The pilot made an off airport forced landing in a corn field. The nose gear was pushed back into the firewall and the right wing was pulled away from the fuselage during the landing.

The airplane was equipped with a Lycoming O-320-D3G engine, serial number L-8748-39A. The engine was overhauled in September 2005, and it had accumulated 1,637 hours since the overhaul. The total time on the engine was 6,987.9 hours. Reconditioned lifters were installed on the airplane during the engine overhaul.

A postaccident inspection of the engine revealed the head of the #4 cylinder exhaust valve lifter was separated from the lifter body. The fractured surface of lifter body was completely smeared from impact damage. The heads on the #3 cylinder intake valve lifter, the #4 cylinder intake valve lifter, and the #4 cylinder exhaust valve lifter were all fractured with a portion of the head separated. Six pieces of the separated sections from the valve lifter heads were found inside the crankcase. The fractured surfaces, when examined by the investigator in charge under a 10X magnifier, did not show any indications of fatigue.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10LA531