N1161DCessna 140A2008-08-16 NTSB Accident Report

Substantial
None

Cessna 140AS/N: 15724

Summary

On August 16, 2008, a Cessna 140A (N1161D) was involved in an incident near Lowman, ID. All 1 person 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 failure to maintain directional control during the landing roll.

After touching down on the grass/turf airstrip in a tail wheel equipped airplane, the pilot failed to maintain directional control. As the pilot was attempting to regain control of the airplane, it ground looped, resulting in the collapse of one of the main landing gear legs. In addition to the collapse of the landing gear leg, the accident sequence resulted in the bending of internal structure of the right wing. According to the pilot, there were no issues with the flight controls or the tail wheel steering system.

This incident is documented in NTSB report SEA08CA186. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N1161D.

Accident Details

Date
Saturday, August 16, 2008
NTSB Number
SEA08CA186
Location
Lowman, ID
Event ID
20080908X01412
Coordinates
44.142223, -115.314445
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain directional control during the landing roll.

Aircraft Information

Registration
Make
CESSNA
Serial Number
15724
Engine Type
Reciprocating
Model / ICAO
140AC140
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
140A

Registered Owner (Current)

Name
JEFFERIES STANLEY J
Address
PO BOX 1573
City
COOS BAY
State / Zip Code
OR 97420-0334
Country
United States

Analysis

After touching down on the grass/turf airstrip in a tail wheel equipped airplane, the pilot failed to maintain directional control. As the pilot was attempting to regain control of the airplane, it ground looped, resulting in the collapse of one of the main landing gear legs. In addition to the collapse of the landing gear leg, the accident sequence resulted in the bending of internal structure of the right wing. According to the pilot, there were no issues with the flight controls or the tail wheel steering system.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08CA186