N71212LUSCOMBE 8A2011-09-10 NTSB Accident Report

Substantial
None

LUSCOMBE 8AS/N: 2639

Summary

On September 10, 2011, a Luscombe 8A (N71212) was involved in an incident near Huntington, IN. 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 failure of the right main landing gear strut due to internal corrosion.

The pilot reported that he heard a "pop noise" during his three-point landing. The airplane's nose veered right and the right wing dropped. The right main landing gear collapsed. The right wing sustained substantial damage when it contacted the runway. A post accident examination of the separated landing gear strut revealed that the interior of the strut exhibited a rust color consistent with oxidation. The separation was consistent with overload.

This incident is documented in NTSB report CEN11CA661. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N71212.

Accident Details

Date
Saturday, September 10, 2011
NTSB Number
CEN11CA661
Location
Huntington, IN
Event ID
20110921X15106
Coordinates
40.852779, -85.456947
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the right main landing gear strut due to internal corrosion.

Aircraft Information

Registration
Make
LUSCOMBE
Serial Number
2639
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
8AL8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
8A

Registered Owner (Current)

Name
SMITH BRIAN D
Address
5159 ROUTE 60
City
SINCLAIRVILLE
State / Zip Code
NY 14782-9732
Country
United States

Analysis

The pilot reported that he heard a "pop noise" during his three-point landing. The airplane's nose veered right and the right wing dropped. The right main landing gear collapsed. The right wing sustained substantial damage when it contacted the runway. A post accident examination of the separated landing gear strut revealed that the interior of the strut exhibited a rust color consistent with oxidation. The separation was consistent with overload.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11CA661