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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

March 20, 1994 · Piper PA-28-180 · N1152X

Batavia, OH

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 20, 1994
Injury Outcomes
No injuries (1 uninjured)
Location
Batavia, OH
Aircraft
Piper PA-28-180
Tail Number
N1152X
Injuries
None
Aircraft Damage
Substantial
NTSB Number
NYC94LA069

THE PILOT STATED THAT IN CRUISE FLIGHT, THE ENGINE STARTED TO VIBRATE AND THE OIL PRESSURE AND RPM DECREASED. HE INITIATED A FORCED LANDING TO A FIELD AND DURING THE LANDING ROLL THE AIRPLANE IMPACTED TREES. EXAMINATION OF THE ENGINE REVEALED THAT THE NUMBER 2 CYLINDER HEAD HAD FRACTURED. MAINTENANCE RECORDS INDICATED THAT THE ENGINE HAD ACCUMULATED 262 HOURS SINCE THE LAST OVERHAUL.

NTSB Probable Cause

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

Full Narrative

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

Flight

Event TypeAccident
Event Time13:55 EST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-180
Tail NumberN1152X
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360 · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 35 · Third Class

Conditions

ConditionsUnknown
LightDaylight
Wind90° @ 6 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point48 / 0 C
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data