N76379

Substantial
None

Cessna 140S/N: 10800

Accident Details

Date
Saturday, December 9, 2006
NTSB Number
CHI07LA039
Location
Vienna, MO
Event ID
20061222X01841
Coordinates
38.925834, -91.916114
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 during cruise flight due to fatigued crankshaft cluster gear bolts and the inadequate major overhaul of the engine that was last performed by other maintenance personnel. An additional cause was a subsequent major engine overhaul not performed by the pilot after he purchased the airplane and operated it with an engine that exceeded the engine manufacturer's time between overhaul criteria.

Aircraft Information

Registration
Make
CESSNA
Serial Number
10800
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
140C140
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
140

Registered Owner (Current)

Name
WISETH DEVIN
Address
4391 33RD AVE S APT 107
City
FARGO
State / Zip Code
ND 58104-8645
Country
United States

Analysis

On December 9, 2006, at 1430 central standard time, a Cessna 140, N76379, owned and piloted by a private pilot, received substantial damage on impact with terrain during a forced landing on a farm field near Vienna, Missouri. The pilot stated that the engine lost power after he heard a "bang." Visual meteorological conditions prevailed at the time of the accident. The pilot reported no injuries. The flight last departed from Rolla National Airport (VIH) Rolla/Vichy, Missouri, at 1410.

The pilot purchased the airplane and had taken delivery of it at VIH on the day of the accident. The airplane was powered by a Continental C-85-12F engine, serial number 25578-6-12, which according to logbook entries, was last overhauled on July 25, 1990, and accumulated a total time since overhaul of 257.5 hours.

A disassembly examination of the engine at Teledyne Continental Motors, Mobile, Alabama, revealed three of the crankshaft cluster gear bolts were fractured through. The bolt fracture surface features were consistent with fatigue. Additionally, the crankshaft gear had a hole where a crankshaft dowel was later installed following a design change in 1948 and was reflected in subsequent maintenance manuals. The dowel is used as a reference in machining the crankshaft. During the disassembly, the tappets fell out when the engine was overturned during the disassembly. It was later noted that the tappets did not contain retaining hardware. The interior of the crankcase halves contained a black colored residue when the oil was drained.

Teledyne Continental Service Information Letter, SIL98-9A, Time Between Overhaul Periods, states that engines are to be overhauled at least every twelve years.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI07LA039