N3983H

Substantial
None

Mooney M20K S/N: 25-0387

Accident Details

Date
Friday, October 13, 1995
NTSB Number
ATL96LA005
Location
DALTON, GA
Event ID
20001207X04634
Coordinates
34.760490, -84.970214
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Oil starvation for an unknown reason, which resulted in progressive connecting rod failure and subsequent loss of engine power. Factors relating to the accident were: the unfavoable weather and light conditions (low ceiling and fog at dusk), which hampered the pilot in seeing the runway during the forced landing.

Aircraft Information

Registration
N3983H
Make
MOONEY
Serial Number
25-0387
Engine Type
Reciprocating
Year Built
1980
Model / ICAO
M20K M20T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MIDWEST MOONEY LLC
Address
2 AIRPORT RD
Status
Deregistered
City
FLORA
State / Zip Code
IL 62839-3450
Country
United States

Analysis

On October 13, 1995, at 1932 eastern daylight time, a Mooney M20K, N3983H was substantially damaged following a collision with terrain during a forced landing attempt near Dalton, Georgia. The commercial pilot was not injured in the accident. The aircraft was being operated under the provisions of 14 CFR Part 91 by the pilot. Instrument meteorological conditions existed at the time, and an instrument flight rules flight plan was in effect at the time of the accident. The flight departed Marietta, Georgia at approximately 1900, and was destined for Rockford, Illinois.

The pilot reported that during the climb, at about 7,000 feet above mean sea level, the engine manifold pressure dropped to about 22 inches, and the engine oil pressure dropped to zero, and he advised air traffic control that he would need to execute an emergency landing at the Dalton, Georgia Airport. During the emergency instrument landing procedure, he overshot the intended runway, and impacted the terrain.

Examination of the aircraft revealed old oil stains on the underside of the aircraft, from the engine cowling trailing to the tail. Examination of the engine revealed that the number one and two connecting rods had failed as a result of thermal stretching and breaking of the rod bolts. No oil leakage path was observed during the examination to indicate that the engine was leaking oil at the time of the accident.(See Analytical Inspection Report Attached to This Report.)

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL96LA005