N41695

Substantial
None

Bellanca 7GCBCS/N: 593-73

Accident Details

Date
Sunday, September 30, 2007
NTSB Number
LAX07CA288
Location
Laurel, MT
Event ID
20071101X01696
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

Corrosion and fatigue-induced failure of the landing gear structure.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
593-73
Engine Type
Reciprocating
Year Built
1973
Model / ICAO
7GCBCB407
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
7GCBC

Registered Owner (Current)

Name
GUILFOYLE ROBERT J
Address
15632 US HIGHWAY 87
City
SHEPHERD
State / Zip Code
MT 59079-3019
Country
United States

Analysis

On September 30, 2007, about 1505 mountain daylight time, a Bellanca 7GCBC, N41695, experienced the breakage and separation of its left main landing gear during landing rollout at the Laurel Municipal Airport, Laurel, Montana. The airplane was owned and operated by the private pilot, who was receiving flight instruction from his airline transport certificated flight instructor (CFI). The airplane was substantially damaged. Neither pilot was injured. Visual meteorological conditions prevailed at the time, and no flight plan had been filed. The flight was performed under the provisions of 14 CFR Part 91, and it originated from Billings, Montana, about 1400.

The CFI reported to the National Transportation Safety Board investigator that he was providing transition flight training to the student, and they had performed a series of uneventful takeoffs and landings. During the accident landing down the center of runway 22, the left main gear separated at the point where a step had been attached, and as the airplane rolled to a stop, the left wing's lift strut buckled.

The Federal Aviation Administration (FAA) coordinator reported that his examination of the airframe revealed evidence that the step had been spot welded onto the spring steel gear assembly. The assembly fatigued and broke in the vicinity of the spot weld. The FAA coordinator stated that evidence of corrosion was observed in the area where the gear assembly fractured. No evidence of gear maintenance, including the welding of the step to the gear assembly, was documented in the airplane's maintenance records.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX07CA288