N3JK

Substantial
None

Bellanca 7GCBCS/N: 941-76

Accident Details

Date
Monday, May 13, 2002
NTSB Number
ANC02LA033
Location
Yakutat, AK
Event ID
20020529X00753
Coordinates
59.248054, -138.503616
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The collapse of the left main landing gear during the landing roll due to a fractured main gear leg strut.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
941-76
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
7GCBCB407
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
7GCBC

Registered Owner (Current)

Name
PAGENKOPF JOSEPH C
Address
4631 RIVER RD
City
JUNEAU
State / Zip Code
AK 99801-8715
Country
United States

Analysis

On May 13, 2002, about 1030 Alaska daylight time, a tundra tire-equipped Bellanca 7GCBC airplane, N3JK, sustained substantial damage when the left main landing gear collapsed while landing at the Tanis Mesa airstrip, located about 42 miles southeast of Yakutat, Alaska. The commercial pilot and the one passenger were not injured. The 14 CFR Part 91 business (hunt/guide) flight operated in visual meteorological conditions without a flight plan. The flight departed Yakutat about 1010. The intermediate destination was the Tanis Mesa airstrip, with a return to Yakutat.

The pilot/owner of the airplane contacted the NTSB investigator-in-charge (IIC) by telephone on May 13 at 1240 to report the accident. During the ensuing conversation, he said he was an owner of a guide business, and was landing his tailwheel airplane at the Tanis Mesa turf airstrip for a routine check on a hunting guide and clients. He said that soon after a normal touchdown, the left main landing gear collapsed, and the left wing struck the ground, damaging the outboard two feet of the wing and the left wing lift strut. The pilot said he was unaware of any pre-existing mechanical problems with the airplane, and that the airplane was equipped with 24-inch tundra tires.

Postaccident discussion between the NTSB IIC and an aviation mechanic who repaired the airplane, disclosed that the mechanic discovered what he believed to be a pre-existing crack in the left main landing gear strut at the point the gear leg fractured.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC02LA033