N7358G

Substantial
None

Cessna 172K S/N: 17259058

Accident Details

Date
Sunday, February 11, 1996
NTSB Number
FTW96LA116
Location
HEDLEY, TX
Event ID
20001208X05248
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the failure of maintenance personnel to properly torque the connecting rod bolts. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
Make
CESSNA
Serial Number
17259058
Engine Type
4-cycle
Year Built
1970
Model / ICAO
172K C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
172K

Registered Owner (Current)

Name
N7358G INC
Address
356 E DESERT INN RD
City
LAS VEGAS
State / Zip Code
NV 89109-9026
Country
United States

Analysis

On February 11, 1996, at 1730 central standard time, a Cessna 172K, N7358G, was substantially damaged during a forced landing near Hedley, Texas. The instrument rated private pilot and his passenger were not injured. The airplane was being operated by the owner as a personal flight under Title 14 CFR Part 91. The flight departed Memphis, Texas, at 1715. Visual meteorological conditions prevailed for the cross country flight for which a flight plan was not filed.

The pilot reported that he was returning to Amarillo, Texas, from Memphis, Texas. The pilot stated that, "the engine suddenly started making a clanging noise, about five seconds later, a big bang, [and] the propeller stopped, straight up and down." An emergency landing to a hay field was made. During the landing the "front wheel caught" in some sandy soil and the airplane flipped over.

The engine was examined at Horton Aero Services, Lubbock, Texas, on February 15, 1996. The examination revealed that one connecting rod bolt nut from the #4 connecting rod was off the bolt and found loose in the crankcase. The #4 piston pin boss was broken and the piston pin was found loose in the crankcase. The #4 connecting rod bearings were destroyed. The connecting rod bolts on the #1 and #2 connecting rods were not at the prescribed torque. The last major engine overhaul was 35 hours prior to the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA116