N1152X

Substantial
None

PIPER PA-28-180 S/N: 287505216

Accident Details

Date
Sunday, March 20, 1994
NTSB Number
NYC94LA069
Location
BATAVIA, OH
Event ID
20001206X00988
Coordinates
39.070983, -84.180236
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

THE LOSS OF ENGINE POWER AS THE RESULT OF A FRACTURED CYLINDER HEAD.

Aircraft Information

Registration
N1152X
Make
PIPER
Serial Number
287505216
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
PA-28-180 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ARNOLD AND SONS INC
Address
220 LARCH LN
Status
Deregistered
City
LEXINGTON
State / Zip Code
KY 40511
Country
United States

Analysis

On March 20, 1994, at 1355 eastern standard time, a Piper PA-28-180, N1152X, piloted by James F. Arnold, III, sustained substantial damage during a forced landing in Batavia, Ohio. The pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight was being conducted under 14 CFR Part 91.

The flight departed Dayton Ohio, destined for Lexington, Kentucky. In his report, the pilot stated:

[I]...climbed to 4500 [feet]...[the] airplane and engine were operating normally....Suddenly ...the engine started vibrating terribly...[it] started losing RPM and oil pressure. All oil pressure was soon lost....I began looking for a suitable off airport place to land....The short field was completely circled by trees and I did not have enough distance to stop before [impacting] ...trees and brush.

Mr. Eric M. Aponte, Aviation Safety Inspector for the Federal Aviation Administration, examined the engine. In his report, Mr. Aponte stated:

This investigation revealed that the malfunction occurred when the engine cylinder head no. 2 split open (head and barrel separation) at the cylinder barrel (between no. 4 and no. 5 cooling fins), probably due to stress corrosion and or metal fatigue of the cylinder barrel wall.

Aircraft maintenance records were reviewed with no indication of previous cylinder repairs other than a complete engine overhaul....Total...time since engine overhaul [was] 261.9 hours.

END OF REPORT

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC94LA069