N247CSTINSON 108-22012-06-25 NTSB Accident Report

Substantial
None

STINSON 108-2S/N: 108-3247

Summary

On June 25, 2012, a Stinson 108-2 (N247C) was involved in an incident near Mile Hi Landing Strip, ID. All 2 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's misjudgment of the speed and distance required to land, which resulted in a runway overrun.

The pilot stated that he was landing at a remote grass airstrip. After touchdown, the airplane continued beyond the end of the runway and nosed over, coming to rest inverted. As a result of the accident sequence, the airplane sustained damage to the rudder and vertical stabilizer.

The pilot reported no pre impact mechanical malfunctions or failures with the airplane that would have precluded normal operation. He opined that the accident may have been prevented if he had maintained a slower approach speed and touched down at the runway threshold.

This incident is documented in NTSB report WPR12CA291. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N247C.

Accident Details

Date
Monday, June 25, 2012
NTSB Number
WPR12CA291
Location
Mile Hi Landing Strip, ID
Event ID
20120703X05426
Coordinates
45.151111, -114.997222
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's misjudgment of the speed and distance required to land, which resulted in a runway overrun.

Aircraft Information

Registration
Make
STINSON
Serial Number
108-3247
Engine Type
Reciprocating
Year Built
1947
Model / ICAO
108-2S108
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
108-2

Registered Owner (Current)

Country
United States

Analysis

The pilot stated that he was landing at a remote grass airstrip. After touchdown, the airplane continued beyond the end of the runway and nosed over, coming to rest inverted. As a result of the accident sequence, the airplane sustained damage to the rudder and vertical stabilizer.

The pilot reported no pre impact mechanical malfunctions or failures with the airplane that would have precluded normal operation. He opined that the accident may have been prevented if he had maintained a slower approach speed and touched down at the runway threshold.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR12CA291