N6624M

Substantial
Minor

Stinson 108-3S/N: 108-4624

Accident Details

Date
Saturday, September 27, 2003
NTSB Number
CHI03LA322
Location
Lincoln, NE
Event ID
20030929X01608
Coordinates
41.449165, -96.520278
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The total loss of engine power due to the fatigue fracture of the engine accessory gear drive. A factor was the concrete marker.

Aircraft Information

Registration
N6624M
Make
STINSON
Serial Number
108-4624
Engine Type
Reciprocating
Year Built
1948
Model / ICAO
108-3S108
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BECKER STEVEN P
Address
3220 N 72ND ST
Status
Deregistered
City
LINCOLN
State / Zip Code
NE 68507-2181
Country
United States

Analysis

On September 27, 2003, at 1530 central daylight time, a Stinson 108-3, N6624M, piloted by a commercial pilot, sustained substantial damage when it lost engine power and nosed over while attempting to land in a field 6 nautical miles north-northeast of Lincoln Municipal Airport (LNK), Lincoln, Nebraska. Visual meteorological conditions prevailed at the time of the accident. The flight was operating under the provisions of 14 CFR Part 91 without a flight plan. The pilot sustained minor injuries. The flight departed the Fremont Municipal Airport (FET), Fremont, Nebraska, at 1510.

The pilot reported that the engine failed while in cruise flight at 3,000 feet mean sea level. The engine could not be restarted, and a forced landing was made to a sod field. During the landing roll, the airplane struck a concrete marker and nosed over.

A Federal Aviation Administration (FAA) airworthiness inspector examined the airplane. The exam revealed that the accessory gear drive was fractured in two pieces, and had become dislodged from the crankshaft. He reported, "a corrosion spot was observed protruding off of the keyway propagating towards the outside of the gear." Metal shavings were found in the accessory area and in the oil reservoir.

The accessory gear drive was inspected by Engineering Systems Inc., (ESI), Aurora, Illinois, on January 13, 2004. The inspection revealed that a fatigue fracture had initiated at the key way that held the gear on the rotating shaft.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI03LA322