N2837R

Substantial
None

PIPER PA 28R-200S/N: 28R-35303

Accident Details

Date
Friday, February 27, 2015
NTSB Number
CEN15LA157
Location
Frankenmuth, MI
Event ID
20150302X02845
Coordinates
43.259998, -83.660003
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the engine due to a lack of oil lubrication for reasons that could not be determined during postaccident examinations.

Aircraft Information

Registration
N2837R
Make
PIPER
Serial Number
28R-35303
Engine Type
Turbo-shaft
Year Built
1969
Model / ICAO
PA 28R-200M600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
NIGHTINGALE CHARLES H
Address
1369 ALLENDALE DR
Status
Deregistered
City
SAGINAW
State / Zip Code
MI 48638-5461
Country
United States

Analysis

On February 27, 2015, about 1419 eastern standard time, a Piper PA-28R-200 airplane, N2837R, was substantially damaged during a forced landing near Frankenmuth, Michigan. The pilot and passenger were not injured. The airplane was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Day visual meteorological conditions prevailed for the flight, with no flight plan filed. The out-and-back flight to Flint, Michigan, originated from the Saginaw County Airport (HYX), Saginaw, Michigan, about 1300.

During departure climb from Bishop International Airport (FNT), Flint, Michigan, the pilot noticed the engine hesitate for one or two seconds and then recover to normal operation. The pilot continued the climb and proceeded towards HYX. Approaching HYX, the engine started to make abnormal noises, followed by a total loss of power. The pilot executed a forced landing into a snow-covered field, during which both wings were damaged.

Federal Aviation Administration (FAA) personnel responded to the accident site and measured engine oil quantity at two quarts on the dipstick. A subsequent FAA teardown examination of the engine revealed a failure of all four piston connecting rods, with heat-related damage to all four cylinders. Engine failure signatures were consistent with a lack of lubrication. No visible oil loss or indication of excess oil consumption was observed at the accident site or during the teardown examination.

The last engine oil change occurred on October 20, 2014. Following this oil change, seven flights totaling 12.8 hours were recorded prior to the accident flight. Records indicated that no oil was added prior to or after these flights.

When interviewed by the FAA, the pilot stated that he noted slightly less than 8 quarts of oil during the preflight for the accident flight. The pilot stated that his habit was to check the engine oil temperature and pressure instruments during warm up and the pre-takeoff run up, but not during flight.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN15LA157