N125FG

Substantial
None

PIPER PA-18-150 S/N: 317482

Accident Details

Date
Saturday, June 3, 1995
NTSB Number
ANC95TA067
Location
SAND POINT, AK
Event ID
20001207X03601
Coordinates
55.260269, -160.659255
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The premature castoring of the tailwheel steering mechanism. A factor associated the accident is the added degree of difficulty in handling airplanes equipped with oversize 'tundra' tires.

Aircraft Information

Registration
Make
PIPER
Serial Number
317482
Engine Type
Reciprocating
Year Built
1951
Model / ICAO
PA-18-150 PA18
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
PA-18-125

Registered Owner (Current)

Name
STATE OF ALASKA
Address
351 RESEARCH CT
City
KODIAK
State / Zip Code
AK 99615-7400
Country
United States

Analysis

On June 2, 1995, about 1940 Alaska daylight time, a Piper PA-18- 150 airplane, N125FG, equipped with 29" tundra tires, received substantial damage while landing on runway 31 at Sand Point Airport, Sand Point, Alaska. Neither the airline transport certificated pilot, or the sole passenger aboard were injured. The 14 CFR Part 91 flight was operated by the State of Alaska's Department of Fish and Game. The purpose of the flight was to return a State of Alaska employee to his work station at Sand Point. The flight operated in visual meteorological conditions, and had departed Port Moller, Alaska, about 1900.

The pilot reported that prior to landing, he noted the wind as approximately 5 to 7 knots, straight down the runway. He said in an interview with the NTSB investigator-in-charge (IIC) on June 8, 1995, that he had considered landing in the gravel alongside of the runway because of the better handling qualities of the tundra tires in gravel as compared to those of a hard surfaced runway, but he elected to land on the runway because of the favorable wind and other factors. During the landing roll, he reported the airplane veered to the right. He said he applied hard left brake, full left rudder, and full power. The airplane began to slowly respond to the left, but prior to becoming straight, the left main gear collapsed.

Postaccident conversations with the Chief Pilot/Mechanic for the Department of Fish and Game disclosed that he had discovered no obvious anomalies with the accident airplane's wheels or brakes. He did discover the anti-castoring break free limits of the steerable tailwheel was set below the limit recommended by the manufacturer. He said that as a result, the tailwheel would freely castor to the right at a lower than normal load force, which would make it very difficult to control the airplane once it started going to the right. The Chief Pilot is a certificated Airframe and Powerplant mechanic with inspection authorization (IA).

The NTSB IIC also spoke with the accident pilot, the Chief Pilot, and other pilots who have extensive experience in landing airplanes equipped with tundra tires. All of the pilots indicated that airplanes equipped with tundra tires are much more difficult to land on hard surfaced runways than gravel or sand. They commented that soft landing surfaces are much more forgiving, and allow the larger tires to move and slide more readily than if they were on a hard surface.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC95TA067