N56464

Substantial
None

MAULE M-6-235S/N: 7416C

Accident Details

Date
Sunday, May 19, 2013
NTSB Number
ANC13LA049
Location
Big Lake, AK
Event ID
20130521X80914
Coordinates
61.389999, -149.838882
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 execution of a hard landing, which resulted in the overstress fracture of the right main axle housing and the subsequent nosedown.

Aircraft Information

Registration
N56464
Make
MAULE
Serial Number
7416C
Year Built
1982
Model / ICAO
M-6-235

Registered Owner (Historical)

Name
REGISTRATION PENDING
Address
14711 W LAKE RIDGE DR
Status
Deregistered
City
EAGLE RIVER
State / Zip Code
AK 99577-9258
Country
United States

Analysis

On May 19, 2013, about 1130 Alaska daylight time, a tundra-tire and tailwheel-equipped Maule M-6-235 airplane, N56464, sustained substantial damage while landing at the Goose Bay Airport, about 9 miles south of Big Lake, Alaska. The airplane was being operated by the pilot as a visual flight rules (VFR) personal flight under the provisions of Title 14, CFR Part 91, when the accident occurred. The airline transport pilot was not injured. Visual meteorological conditions prevailed and a VFR military flight plan had been filed. The flight departed Elmendorf Air Force Base about 0830.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge (NTSB) on May 19, the pilot stated that he was practicing stop-and-go landings on the gravel covered runway at the Goose Bay Airport. Upon touchdown, the right main gear separated at the axle housing, which pivoted the airplane to the right as the main landing gear leg dug into the gravel covered runway. The airplane subsequently nosed down, coming to rest on the propeller spinner and left wing. The airplane sustained substantial damage to the left wing and lift struts. The pilot noted that the airplane was equipped with 35-inch tundra tires.

A postaccident examination, by the pilot, revealed the right main landing gear axle separated at the axle housing to main landing gear leg attach point.

A Senior Safety Board Metallurgist reported that visual and magnified optical examination of the fractured surfaces revealed features consistent with a bending overstress fracture. (A synopsis of the NTSB Metallurgist's case review is included in the public docket for this 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# ANC13LA049