N3248T

Substantial
None

Beech A36S/N: E-2948

Accident Details

Date
Friday, July 2, 2004
NTSB Number
CHI04LA187
Location
Algona, IA
Event ID
20040715X00986
Coordinates
43.070915, -94.229621
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The failure of the connecting rod which resulted in the loss of engine power during cruise flight and subsequent forced landing. A contributing factor was the delayed lowering of the landing gear in order to clear the other vehicle encountered during the forced landing.

Aircraft Information

Registration
Make
BEECH
Serial Number
E-2948
Engine Type
Reciprocating
Year Built
1995
Model / ICAO
A36BE36
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
A36

Registered Owner (Current)

Name
BRYDON ROBERT J
Address
1603 NEWFIELD LN
City
AUSTIN
State / Zip Code
TX 78703-3318
Country
United States

Analysis

On July 2, 2004, about 1715 central daylight time, a Beech model A36, N3248T, piloted by a commercial pilot, was substantially damaged as a result of a forced landing following a loss of engine power and subsequent in-flight fire. The 14 CFR Part 91 business flight was operating in visual meteorological conditions without a flight plan. No injuries were reported. The flight originated from the Mason City Municipal Airport, Mason City, Iowa, at 1630, and was bound for the Joe Foss Field Airport, Sioux Falls, South Dakota.

The pilot reported that about 15 minutes into the flight, while level at 4,500 feet mean sea level, the airplane engine "blew up." The pilot stated that he executed a forced landing on a road. He stated that he kept the landing gear retracted to insure that he could clear a car that was traveling in the opposite direction. The pilot stated that once clear of the car he lowered the landing gear, but due to the low altitude, the landing gear did not fully extend before contact with the road occurred.

Examination of the engine revealed a hole in the top of the crankcase near the number 5 and 6 cylinders. The hole in the crankcase was aligned with the number 6 connecting rod journal. All of the engine accessories remained intact and attached to the engine.

Fractured pieces of the number 6 connecting rod, piston and piston pin were found within the crankcase. The fractured piston exhibited signatures consistent with overload failure. The fracture surfaces of the connecting rod were smeared and no determination could be made concerning the fracture surfaces.

The number 5 piston was lodged within its cylinder. The connecting rod remained attached to the piston. The connecting rod cap was separated from the connecting rod. The fracture surfaces were smeared and no determination could be made concerning the fracture surfaces.

Examination of the main bearings and the connecting rod bearings of the undamaged connecting rods revealed no evidence of oil starvation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI04LA187