N7059

Substantial
None

PIPER PA-18-150S/N: 18-8043

Accident Details

Date
Saturday, April 28, 2012
NTSB Number
ANC12TA035
Location
Paxon, AK
Event ID
20120430X35846
Coordinates
61.210491, -149.890518
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A separation of the right main landing gear suspension strut assembly due to overstress, which resulted in the collapse of the main landing gear while landing.

Aircraft Information

Registration
Make
PIPER
Serial Number
18-8043
Engine Type
Reciprocating
Year Built
1963
Model / ICAO
PA-18-150PA18
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
PA-18-150

Registered Owner (Current)

Name
STATE OF ALASKA DEPARTMENT OF PUBLIC SAFETY
Address
4827 AIRCRAFT DR
City
ANCHORAGE
State / Zip Code
AK 99502-1071
Country
United States

Analysis

On April 27, 2012, about 1620 Alaska daylight time, a ski-equipped Piper PA-18-150 airplane, N7059, sustained substantial damage when the right main landing gear collapsed while landing on a frozen, snow-covered lake, about 28 miles west of Paxon, Alaska. The airplane was operated by the State of Alaska Department of Public Safety, Alaska State Troopers, Anchorage, Alaska, as a visual flight rules (VFR) public use flight under the provisions of Title 14 Code of Federal Regulations Part 91, when the accident occurred. The solo pilot was not injured, and company flight following procedures were in effect, for the flight that departed Anchorage about 1400.

In a written statement to the National Transportation Safety Board investigator-in-charge dated April 30, the pilot reported that while on a routine law enforcement flight he landed on a remote, frozen and snow-covered lake. He said that as the skis contacted the flat and smooth snow-covered ice, the airplane pitched forward violently, then to the right, and then back to the left. The pilot’s postaccident examination revealed that the right main landing gear had collapsed, and subsequently folded under the airplane. The airplane sustained substantial damage to the wings and the fuselage.

The airplane was equipped with a Burl’s Aircraft LLC, Alpha Omega Suspension System (AOSS), which was installed in accordance with supplemental type certificate (STC) SA02214AK.

A postaccident examination of the right main landing gear revealed a fractured suspension strut that had fractured laterally across a bored and threaded suspension tube. The tube had a slight bend with tearing along the fracture line on the inside of the bend.

The pilot reported that other than the fractured main landing suspension strut, there were no preaccident mechanical anomalies with the airplane.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC12TA035