N7192G

Substantial
None

Cessna 172KS/N: 17258892

Accident Details

Date
Saturday, November 23, 2002
NTSB Number
NYC03LA023
Location
Prestonsburg, KY
Event ID
20021126X05530
Coordinates
37.650554, -82.786666
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The loss of oil pressure for undetermined reasons, which resulted in a failure of connecting rod end bolts, due to an over temperature condition.

Aircraft Information

Registration
N7192G
Make
CESSNA
Serial Number
17258892
Engine Type
Reciprocating
Year Built
1969
Model / ICAO
172KC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HADDIX STANLEY D
Address
8315 S KY ROUTE 321
Status
Deregistered
City
HAGERHILL
State / Zip Code
KY 41222-8631
Country
United States

Analysis

On November 23, 2002, about 1630 eastern standard time, a Cessna 172K, N7192G, was substantially damaged during a forced landing after experiencing a total loss of engine power near Prestonsburg, Kentucky. The certificated flight instructor and student pilot were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the local instructional flight conducted under 14 CFR Part 91.

According to the pilot, the flight had departed the Paintsville-Prestonsburg-Combs Airport, Paintsville, Kentucky, about 1600. While in cruise flight, at 3,000 feet, the engine began to run rough. The pilot cycled the magneto switch and noted no changes in the engine performance. He then observed the oil pressure gauge in the "zero" position. The engine then lost total power, and a forced landing was performed to a field.

A Federal Aviation Administration inspector examined the airplane after the accident, and observed substantial damage to the engine firewall, and the fuselage. The inspector also noted a 2-inch hole in top of the engine crankcase.

Further examination of the engine revealed that the connecting rod and camshaft area of the number 4 cylinder had sustained extreme heating. The bottom half of the connecting rod was bent out of shape, with one of the rod end bolts remaining wedged in the rod end. The other rod end bolt was missing. The oil screen was removed, and small amounts of metal were observed trapped in the screen. Metal parts were also observed in the oil pan. There was no evidence of oil leakage.

The engine had accumulated about 2,400 hours of operation since it's last overhaul conducted in 1986. An annual inspection of the airframe and engine was performed on August 23, 2002. A 50-hour inspection, which included servicing the engine with 7 quarts of oil, was conducted on November 21, 2002.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC03LA023