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Aviation safety reports, made easier to study

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July 2, 2003 · Piper PA-24 · N6315P

Winamac, IN

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 2, 2003
Injury Outcomes
No injuries (5 uninjured)
Location
Winamac, IN
Aircraft
Piper PA-24
Tail Number
N6315P
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI03LA187

The airplane was damaged during a forced landing in a rough plowed field following a loss of engine power during cruise flight. Examination of the engine revealed that the crankshaft gear retaining bolt was missing and the gear's anti-rotation pin was sheared. The oil pan of the engine was examined and no bolt was found. The crankshaft gear retaining bolt was not found within the engine. A review of the maintenance records revealed that the engine was last overhauled on April 6, 1986, and had accumulated 522 hours time in service since the overhaul. No subsequent logbook entries were noted that indicated removal of the crankshaft gear or retaining bolt.

NTSB Probable Cause

A loss of engine power due to the improper installation of the crankshaft gear due to the omission of the retaining bolt and subsequent shear failure of the anti-rotation pin. The unsuitable terrain encountered, and the rough field were factors.

Full Narrative

On July 2, 2003, at 1008 central daylight time, a Piper PA-24, N6315P, piloted by an airline transport pilot, sustained substantial damage during a forced landing following an in-flight loss of engine power near Winamac, Indiana. Visual meteorological conditions prevailed at the time of the accident. The pilot and his four passengers reported no injuries. The 14 CFR Part 91 personal flight was operating on an IFR flight plan. The flight departed from Plymouth, Michigan, at 0819, with an intended destination of Perryville, Missouri. The airplane's engine stopped producing power during cruise flight. The pilot was given radar vectors to the Arens Field Airport (RWN), Winamac, Indiana. The pilot was not able to reach RWN and executed a forced landing in a rough plowed field. A postaccident examination was conducted by the Federal Aviation Administration. During the initial examination of the airplane's engine, valve train continuity could not be established. Rotation of the crankshaft produced no movement of the valve train components. A subsequent examination of the accessory section of the engine revealed that the crankshaft gear retaining bolt was missing and the gear's anti-rotation pin was sheared. The oil pan of the engine was examined and no bolt was found. The crankshaft gear retaining bolt was not found within the engine. A review of the maintenance records revealed that the engine was last overhauled on April 6, 1986, and had accumulated 522 hours time in service since the overhaul. No subsequent logbook entries were noted that indicated removal of the crankshaft gear or retaining bolt.

Flight

Event TypeAccident
Event Time11:08 EDT
Nearest Airport0nm
Flight Plan FiledIFR
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-24
Tail NumberN6315P
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360 · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (5 uninjured)
Fatal0
Serious0
Minor0
Uninjured5
Total5
Crew 1Age 30 · First Class · None

Conditions

ConditionsVMC
LightDaylight
Wind20° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point59
Altimeter29.95 inHg
Observation Time13:53
Weather SourceWFAC

Appendix: Source Data