N65645

Substantial
None

Cessna 172S/N: 17275797

Accident Details

Date
Thursday, August 27, 2020
NTSB Number
ERA20LA299
Location
Weston, FL
Event ID
20200827X25843
Coordinates
26.018333, -80.760276
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A total loss of engine power due to the failure of the Nos. 1 and 3 connecting rods from lack of lubrication.

Aircraft Information

Registration
Make
CESSNA
Serial Number
17275797
Engine Type
Reciprocating
Year Built
1982
Model / ICAO
172C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
172P

Registered Owner (Current)

Name
PEA-WAYMAN FLIGHT LLC
Address
561 PEARL HARBOR DR
City
DAYTONA BEACH
State / Zip Code
FL 32114-3845
Country
United States

Analysis

On August 27, 2020, about 1225 eastern daylight time, a Cessna 172P airplane, N65645, was substantially damaged when it was involved in an accident near Weston, Florida. The flight instructor and pilot receiving instruction were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

According to the flight instructor, after practicing holding maneuvers over the Everglades, he noticed that the engine oil pressure was "remarkably low,” and the engine oil temperature was "a bit high." He took control of the airplane and flew east toward roadways in case a forced landing became necessary. The engine then began to run rough, vibrate, and lost partial power. He determined the airplane would likely not reach the roadways and he turned toward Dade Collier Airport (TNT), Ochopee, Florida, which was about 12 miles away. The engine then vibrated "incredibly" and lost all power. The flight instructor was unable to restart the engine and performed a forced landing into vegetation. During landing, the airplane flipped over and sustained substantial damage to the wings and forward lower fuselage.

Examination of the airplane by a Federal Aviation Administration inspector revealed that a coating of oil was present on most of the underside of the fuselage, and a hole was found in the engine crankcase near the base of one of the cylinders.

Examination of the engine revealed that the Nos. 1 and 3 cylinder connecting rods were fractured near their crankshaft end. The remnants and fracture surfaces of the rods, as well as their respective journals on the crankshaft were discolored (blackened and bluish surfaces) and smeared, consistent with thermal stress/damage. The No.4 cylinder connecting rod remained attached to the crankshaft but would not rotate. The crankshaft end of the rod was discolored (black and rust colored), consistent with thermal stress. Bearing material was extruded between the rod and the crankshaft lobe. Holes were found in the crankcase near the base of the No.4 cylinder and on the bottom of each crankcase half. There were no obstructions found in any the visible oil passages in the crankshaft. The engine oil pump was undamaged, contained no debris, and operated smoothly.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA20LA299