N97719

Substantial
None

STINSON 108S/N: 108-719

Accident Details

Date
Thursday, July 13, 2023
NTSB Number
ANC23LA051
Location
Ninilchik, AK
Event ID
20230717192643
Coordinates
60.033611, -151.650770
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A partial loss of engine power due to failure of the No. 1 cylinder intake valve head.

Aircraft Information

Registration
Make
STINSON
Serial Number
108-719
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
108S108
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
108

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 July 12, 2023, about 1624 Alaska daylight time, a Stinson 108 airplane, N97719, was substantially damaged when it was involved in an accident near Ninilchik, Alaska. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated he departed Homer Airport (HOM) destined for Anchorage, Alaska. A few miles northwest of the Ninilchik Airport (NIN) he noticed a loss of engine power and the oil pressure decreasing. The pilot determined he was too far from the NIN airport to return so he elected to perform a forced landing to a road. During the landing roll the right wingtip struck a traffic sign, which resulted in substantial damage to the right wing.

Postaccident examination of the engine revealed the No. 1 cylinder was fractured from the engine and remained partially attached by exhaust tubes and the intake manifold. The intake valve head and stem was fractured about an inch from the interior base of the valve. The piston and intake valve were destroyed by the internal forces in the engine and the fragments were not located.

The pilot reported the engine had a total time of 626 hours at the time of the accident. The last annual inspection was completed 12 months before the accident at an engine total time of 556.4 hours. The engine logbook showed the manufacturer’s recommended time between overhaul is 1,200 hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC23LA051