N6547R

Substantial
None

BEECH C23 S/N: M1588

Accident Details

Date
Saturday, August 21, 1993
NTSB Number
SEA93LA180
Location
LAKEVIEW, OR
Event ID
20001211X13270
Coordinates
42.309665, -120.369926
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A FRACTURED EXHAUST VALVE. THE ROUGH TERRAIN WAS A FACTOR.

Aircraft Information

Registration
N6547R
Make
BEECH
Serial Number
M1588
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
C23 BE23
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AIRCRAFT SALVAGE AND REBUILD INC
Address
100 AIRPORT RD
Status
Deregistered
City
OMAK
State / Zip Code
WA 98841-9351
Country
United States

Analysis

On August 21, 1993, at 0925 hours Pacific daylight time, a Beech C23, N6547R, experienced a partial loss of engine power while in cruise flight. The airplane was unable to maintain altitude and a forced landing was made to an open field, 30 miles west of Lakeview, Oregon. During the landing roll, the airplane collided with the rough terrain. Visual meteorological conditions prevailed at the time and a visual flight rules flight plan was filed. The airplane was substantially damaged and the certificated private pilot and her passenger were not injured. The flight had departed from Klamath Falls, Oregon, on August 21, 1993, at 0840 hours, and was en route to Boise, Idaho.

During a telephone interview, the pilot reported that the flight was cruising at about 4500 feet AGL when the engine rpm dropped 300-400 rpm. Unsuccessful attempts were made to try to regain full power. The airplane was unable to maintain altitude and a forced landing was made to an open field.

During the engine tear down inspection, it was found that the number one exhaust valve head broke away at the neck. There were no remains of the head present. The piston face was severely damaged, along with the bottom spark plug. Compression check of the number one cylinder indicated no compression. The valve stem remained in position in the guide. The broken end of the stem displayed severe heat damage and melting of the metal.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA93LA180