N69AG

Substantial
None

Artic Aircraft Corp. S-1B2S/N: 1020

Accident Details

Date
Sunday, May 26, 2002
NTSB Number
SEA02LA089
Location
Tumtum, WA
Event ID
20020531X00795
Coordinates
47.863887, -117.783889
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 improper flare.

Aircraft Information

Registration
Make
ARTIC AIRCRAFT CORP.
Serial Number
1020
Engine Type
Reciprocating
Model / ICAO
S-1B2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
S-1B2

Registered Owner (Current)

Name
CHRISTENSEN PAUL M
Address
14295 277TH AVE NW
City
ZIMMERMAN
State / Zip Code
MN 55398-8634
Country
United States

Analysis

On May 26, 2002, approximately 1350 Pacific daylight time, an Arctic Aircraft S-1B2 "Arctic Tern," N69AG, owned, operated and being flown by a private pilot incurred substantial damage during touchdown in a field approximately five nautical miles southwest of Tumtum, Washington. The pilot and passenger were uninjured. Visual meteorological conditions prevailed and no flight plan had been filed. The flight, which was personal, was operated under 14 CFR 91 and the aircraft departed from a local site approximately 1100.

An inspector assigned to the Federal Aviation Administration's Spokane Flight Standards District Office interviewed the pilot. The pilot reported that upon touchdown the left main landing gear collapsed, the aircraft began skidding and then the right main landing gear collapsed. The aircraft then nosed over and came to a stop.

The pilot reported that he and his passenger departed from a meadow and after some local sightseeing he returned for landing. He further reported that "...just after touching down a noticeable "pop" was heard and the landing gear collapsed..." and that "...the terrain [at the landing site] was a flat dirt field..." (refer to attached NTSB Form 6120-1/2).

The broken landing gear attach fitting was sent to the Safety Board where it underwent a brief metallurgical examination at the Board’s Materials Laboratory. The examination revealed fracture features and deformation typical of an overstress fracture under a combined torsion and bending load. No evidence of pre-existing cracking was noted (refer to attached report).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA02LA089