N4232H

Substantial
None

Mooney M20JS/N: 24-0671

Accident Details

Date
Monday, September 30, 2002
NTSB Number
SEA02LA187
Location
Oakley, ID
Event ID
20021021X05347
Coordinates
42.244998, -113.879447
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

Failure (fracture) of the two number four piston compression rings, leading to the erosion of a section of the piston sidewall, resulting in the exhaustion of the engine's oil supply during cruise flight, followed by a forced landing on a country road. Factors include mail boxes mounted on metal poles immediately adjacent to the side of the road.

Aircraft Information

Registration
Make
MOONEY
Serial Number
24-0671
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
M20JM20P
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
M20J

Registered Owner (Current)

Name
HUPP GARRETT
Address
175 VAN HORN ST
City
SUNBURY
State / Zip Code
PA 17801-2541
Country
United States

Analysis

On September 30, 2002, approximately 1630 mountain daylight time, the wings of a Mooney M20J, N4232H, collided with mail boxes mounted on steel posts during the landing roll after the pilot successfully executed a forced power-off landing on a country road. The private pilot and his passenger were not injured, but the aircraft, which is owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 personal pleasure flight, which departed Walker Field, Grand Junction, Colorado, about two hours earlier, was being operated in visual meteorological conditions. The ELT was not activated.

According to the pilot, while en route, the aircraft began to lose oil pressure and eventually the propeller failed to respond correctly to the movement of the propeller rpm governor control lever. Eventually the oil pressure dropped to zero, and the pilot elected to make an emergency landing on a country road. Although the pilot was able to maneuver the aircraft to a successful touchdown on the road he selected, during the landing roll, the wings of the aircraft collided with mail boxes situated immediately adjacent to the edge of the road.

A post-accident inspection of the engine revealed that both compression rings on the number four piston had fractured, and a 3/8 inch wide section of the piston surface had been eroded away. The eroded area extended from the land of the bottom compression ring, through the land of the top compression ring, to within 1/16 inch of the piston dome. The depth of the erosion was approximately 1/8 inch (level with the bottom surface of the ring land). In addition, according to the FAA inspector who looked at the engine after the number four cylinder was removed, except for a small residual amount, the engine had lost all of its oil supply, and the number three connecting rod bearing was beginning to extrude from between the rod end and the crankshaft journal. The investigation also revealed that the number four cylinder exhaust pipe was contaminated with both oily soot and a coating of unburned oil. In addition, the fuselage skin in the area aft of the exhaust pipe for the number two and number four cylinders was coated with what appeared to be relatively fresh oil.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA02LA187