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NTSB Report

March 28, 1997 · Bellanca 14-13 · N86851

Oroville, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 28, 1997
Injury Outcomes
No injuries (1 uninjured)
Location
Oroville, CA
Aircraft
Bellanca 14-13
Tail Number
N86851
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX97LA134

While cruising at 3,500 feet mean sea level, the engine suddenly began knocking and vibrating. Moments later, all engine power was lost. The pilot initiated a forced landing on a nearby road, but during the approach collided with a tree. An inspection of the engine revealed several holes in the upper portion of the case in the vicinity of the number 6 cylinder. Further examination revealed that both of the number 6 connecting rod bolts were broken and the rod cap was crushed and fragmented. The owner reported that the rod bolts had been in service for about 1,185 hours. The engine's total time was about 2,350 hours.

NTSB Probable Cause

a loss of engine power due to connecting rod bolt failure. The reason for the bolt failure was not determined. A contributing factor was the presence of trees in the emergency landing path.

Full Narrative

On March 27, 1997, at 1825 hours Pacific standard time, a Bellanca 14-13, N86851, owned and operated by the pilot, experienced a loss of engine power while cruising at 3,500 feet mean sea level near Oroville, California. According to the pilot, the sequence of events started when his "perfect running engine" suddenly began knocking and vibrating. Moments later, all engine power was lost. The commercial pilot attempted to land on a nearby road. During the approach the airplane collided with a tree, and the airplane was substantially damaged. The pilot was not injured. Visual meteorological conditions prevailed during the personal flight, and no flight plan was filed. The flight originated from Redding, California, at 1750. The pilot and the Federal Aviation Administration (FAA) coordinator inspected the airplane, manufactured in 1946, and the Franklin engine. The FAA reported observing several holes in the upper portion of the engine case in the vicinity of the number 6 cylinder. The largest hole was about 0.75 inches wide by 2.0 inches long. The FAA reported it appeared as though something was trying to get out from inside the engine. An additional examination of the engine revealed that both of the number 6 connecting rod bolts were broken and the rod cap was crushed and fragmented. According to the owner, the rod bolts had been in service for about 1,185 hours. The engine's total time was about 2,350 hours.

Flight

Event TypeAccident
Event Time18:25 PST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBellanca 14-13
Tail NumberN86851
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · 6A4-150-B3 · Reciprocating · 150
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 50 · Second Class

Conditions

ConditionsVMC
LightDusk
Wind180° @ 6 kt
Visibility50 sm
CeilingNone
Temperature / Dew Point64 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data