N6174D

Substantial
None

Piper PA-22S/N: 22-4821

Accident Details

Date
Sunday, February 27, 2005
NTSB Number
ANC05LA044
Location
Anchorage, AK
Event ID
20050404X00399
Coordinates
61.180000, -149.971939
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's excessive taxi speed during a turn while taxiing from landing, which resulted in the collapse of the left main landing gear, and structural damage to the fuselage.

Aircraft Information

Registration
Make
PIPER
Serial Number
22-4821
Engine Type
Reciprocating
Year Built
1957
Model / ICAO
PA-22PA22
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-22-150

Registered Owner (Current)

Name
OTOOLE MAKENA
Address
PO BOX 1986
City
CORDOVA
State / Zip Code
AK 99574-1986
Country
United States

Analysis

On February 27, 2005, about 1543 Alaska standard time, N6174D, a ski-equipped Piper PA-22 airplane, converted from a nose wheel to a tailwheel configuration, sustained substantial damage when the left main landing gear collapsed while landing on the frozen Lake Hood Seaplane Base airstrip, Anchorage, Alaska. The private pilot/airplane owner and the sole passenger were not injured. The 14 CFR Part 91 local personal flight operated in visual meteorological conditions without a flight plan. The operator of the airplane was the pilot/owner.

During a telephone conversation with the NTSB investigator-in-charge on March 1, the pilot related he had landed on the ice to the east, and was turning the airplane to the right to taxi to his parking spot, when the left ski dug in and the right wing came up. The left main landing gear subsequently collapsed, and the left wing struck the ice. The pilot related that there were no preaccident mechanical problems with the airplane.

The extent of the damage to the airplane could not be determined until April 1, when the airplane was partially disassembled for repairs. Two NTSB investigators examined the airplane, and discovered substantial damage to the fuselage crossover tube near the left main landing gear attachment cluster. The aviation mechanic repairing the airplane noted that he had to cut a portion of the steel tubing from the crossover tube, and make repairs by welding a thicker tube piece into the void. Other portions of the gear attachment cluster had strengthening steel splices added by welding. The mechanic noted that an FAA Form 337, Major Repair or Alteration, would be completed for the repair work.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC05LA044