N2692D

Substantial
None

Cessna 170B S/N: 20844

Accident Details

Date
Saturday, April 25, 1998
NTSB Number
ANC98LA041
Location
KENAI, AK
Event ID
20001211X09796
Coordinates
60.659255, -150.900909
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A failure of the number six cylinder rod bearing and connecting rod cap for undetermined reasons. Factors in the accident were snow covered terrain that was unsuitable for a forced landing.

Aircraft Information

Registration
Make
CESSNA
Serial Number
20844
Engine Type
Reciprocating
Year Built
1952
Model / ICAO
170B C170
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
170B

Registered Owner (Current)

Name
SUTTON AIRCRAFT SALVAGE LLC
Address
13500 E JENSEN AVE
City
PALMER
State / Zip Code
AK 99645-9430
Country
United States

Analysis

On April 24, 1998, about 2140 Alaska daylight time, a tundra tire equipped Cessna 170B airplane, N2692D, sustained substantial damage during a forced landing, about 44 miles west of Kenai, Alaska. The airplane was being operated as a visual flight rules (VFR) cross-country personal flight when the accident occurred. The airplane was registered to, and operated by the pilot. The certificated private pilot, and the sole passenger, were not injured. Visual meteorological conditions prevailed. The flight originated from a remote airstrip about 2040.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on April 27, 1998, at 0800, the pilot reported he departed Keys Point at Lake Clark, Alaska, and was flying through Lake Clark Pass. While in cruise flight, the oil pressure began to decrease to below the normal operating range. The pilot began a climb to 3,500 feet mean sea level. The engine then began to run rough, and the pilot shut the engine off. He made an emergency landing in a small open area. The airplane touched down in snow covered terrain, and then nosed over. The airplane received damage to the left wing spar, the rudder, and the leading edge of both wings.

A Federal Aviation Administration (FAA) airworthiness inspector, Anchorage Flight Standards District Office (FSDO), Anchorage, Alaska, examined the airplane engine on April 29, 1998. The inspector reported the number six piston connecting rod bearing was destroyed. The connecting rod cap was also destroyed. The number six crankshaft rod bearing journal was blackened and battered.

The pilot reported the engine had accrued a total time of 4,417.28 hours. It had accrued 1,274.18 hours since an engine overhaul. The most recent inspection was an annual inspection conducted on November 28, 1997, 13.65 hours before the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA041