N943TA

Substantial
None

SIAI-MARCHETTI SF.260B S/N: 11-01

Accident Details

Date
Monday, June 6, 1994
NTSB Number
SEA94LA138
Location
PROSPECT, OR
Event ID
20001206X01614
Coordinates
42.780414, -122.490730
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE FRACTURE OF A CONNECTING ROD. FACTORS INCLUDE NO SUITABLE FORCED LANDING SITE, AND A FENCE AND IRRIGATION SYSTEM IN THE FIELD WHERE THE FORCED LANDING TOOK PLACE.

Aircraft Information

Registration
Make
SIAI-MARCHETTI
Serial Number
11-01
Engine Type
Reciprocating
Year Built
1970
Model / ICAO
SF.260B F260
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
F.260B

Registered Owner (Current)

Name
DE PEYSTER FRANCIS V
Address
24328 S SKYLANE DR
City
CANBY
State / Zip Code
OR 97013-8747
Country
United States

Analysis

On June 5, 1994, approximately 1915 Pacific daylight time (PDT), a Siai-Marchetti SF.260B, N943TA, collided with irrigation equipment and a fence during a forced landing near Prospect, Oregon. Neither the commercial pilot, nor his passenger were injured, but the airplane sustained substantial damage. The personal pleasure flight, which departed Medford, Oregon, about 1830 PDT, was in visual meteorological conditions at the time of the accident. There was no flight plan filed, and no report of an ELT activation.

According to the pilot, about 45 minutes into the flight, there was sudden and violent vibration from the engine. Immediately thereafter, the oil pressure dropped to zero, and the propeller went to maximum rpm, and could not be controlled with the propeller control lever. There were no unobstructed fields available for a forced landing, so he elected to land in a nearby field that was crossed by a fence and an irrigation pipe line. The touchdown was successful, but the aircraft sustained substantial damage when it rolled through the pipe and fence.

This aircraft, which is used extensively for professional air show aerobatics, was powered by a Lycoming IO-540-G engine. The engine was classed as experimental because it contained 10.1 to 1 compression ratio pistons, instead of the standard 8.71 to 1 pistons. The engine was sent to Fort Collins, Colorado, where the FAA supervised an inspection teardown by Demars Aero Limited. The FAA report stated that it appeared the number six connecting rod experienced a fatigue failure, which caused catastrophic damage to the engine crankcase. The fracturing of the case released the engine oil, and the loss of oil pressure resulted in a runaway propeller.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94LA138