N758CQ

Substantial
None

CESSNA 172 S/N: R172-2992

Accident Details

Date
Sunday, February 18, 1996
NTSB Number
CHI96LA093
Location
WORTHINGTON, MN
Event ID
20001208X05230
Coordinates
43.619873, -95.590690
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

Progressive failure of the engine, beginning with failure of the left magneto, which resulted in preignition or detonation, a burned hole in the #3 piston, subsequent oil exhaustion, and failure of the #1 and #2 connecting rods.

Aircraft Information

Registration
Make
CESSNA
Serial Number
R172-2992
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
172 C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
R172K

Registered Owner (Current)

Name
KISSINGER RICHARD GORDON
Address
200 RAVEN HAVEN LN
City
CENTRE HALL
State / Zip Code
PA 16828-8962
Country
United States

Analysis

On February 18, 1996, at 1310 central standard time, a Cessna 172, N758CQ, sustained substantial damage during a forced landing due to loss of engine power near Worthington, Minnesota. The private pilot and two passengers reported no injuries. The 14 CFR Part 91 flight departed Worthington Municipal Airport, Worthington, Minnesota, at 1255 cst, en route to Buffalo Municipal Airport, Buffalo, Minnesota. Visual meteorological conditions prevailed and no flight plan was filed.

The pilot reported that he departed Worthington, Minnesota, and climbed to 3,500 feet. The first indication that something was wrong was the engine began running rough and there was light smoke in the cockpit. The pilot reported that all the instruments were in the green, the power was set at 2500 RPM with 23 inches of manifold pressure, and the mixture was at full rich. He noticed the oil pressure decreasing and he turned back to land at Worthington Airport. He reported that the engine RPM's began fluctuating, the oil pressure dropped rapidly, and the cockpit began filling with smoke. The pilot decided to secure the engine and execute a forced landing to a gravel road. The airplane touched down on the road, but during landing rollout the right wing hit a yield sign on the side of the road. The airplane swerved into an adjacent field and came to a complete stop.

The oil was checked and there was no indication of oil on the dipstick. A two to three inch hole was discovered in the crankcase of the engine.

An examination of the engine revealed that the number three piston exhibited a hole burned in the bottom side through the crown structure to the piston interior. The number one and number two connecting rods were off the crankshaft. The connecting rod bolts were broken. The bolts were black and necked down at the fractured area. The number one and two crankshaft journals were partially melted. The number three, four, and five connecting rods were burned and discolored. The crankshaft main bearings exhibited normal operational signatures. The fuel system was checked and no defects were discovered.

An examination of the magnetos revealed that the left magneto was contaminated with a blackish debris. The left magneto distributor block interior was coated with the debris. The rear bearing race was found spinning in the left magneto's aluminum housing. Metal particles from the race and housing covered the surface around the magneto distributor block.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI96LA093