N4884G

Substantial
None

CESSNA 172N S/N: 17273431

Accident Details

Date
Sunday, July 25, 1993
NTSB Number
FTW93LA216
Location
PURCELL, OK
Event ID
20001211X12922
Coordinates
35.010593, -97.370498
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE LACK OF SUITABLE TERRAIN ONTO WHICH TO EXECUTE THE FORCED LANDING WHICH WAS NECCESITATED BY THE PARTIAL POWER LOSS. THE POWER LOSS WAS A RESULT OF THE FATIGUE FAILURE OF THE EXHAUST VALVE ROCKER ARM ATTACHMENT STUD. A FACTOR WAS THE NIGHT CONDITIONS.

Aircraft Information

Registration
N4884G
Make
CESSNA
Serial Number
17273431
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
172N C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LILLY LARRY L
Address
1948 GODDARD
Status
Deregistered
City
NORMAN
State / Zip Code
OK 73069
Country
United States

Analysis

On July 24, 1993, at approximately 2220 central daylight time, a Cessna 172N, N4884G, was substantially damaged when it collided with rough terrain during a forced landing near Purcell, Oklahoma. The forced landing was executed following a partial loss of engine power. The airplane was on a night cross country dual instructional flight. A VFR flight plan was filed and visual meteorological conditions prevailed throughout the area. Neither the instructor pilot nor the rated student pilot were injured.

According to the instructor, the engine lost power down to 1,500 RPM while in cruise flight, about twenty minutes after takeoff from the Westheimer Airport in Norman, Oklahoma. The instructor stated that his efforts to regain power were unsuccessful and the airplane would not sustain level flight at the reduced power. He subsequently executed a forced landing to what appeared to be an open field. The airplane impacted rough terrain during the landing roll.

The number 3 cylinder exhaust rocker arm attachment stud had separated at the face of the cylinder head. The separated stud was found lodged under the number 3 intake valve mechanism. The number 3 intake valve push rod was bent. The operator stated that the stud was examined by a metallurgy lab at the University of Oklahoma and the failure mechanism was determined to be fatigue. The engine and subject parts had accumulated a total of 2,903.5 hours.

Neither the instructor nor the student submitted a pilot/operator accident report. Both subsequently left the country.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW93LA216