N8638V

Substantial
None

Bellanca 8GCBC S/N: 162-75

Accident Details

Date
Wednesday, August 16, 2000
NTSB Number
LAX00LA303
Location
RENO, NV
Event ID
20001212X21775
Coordinates
39.489253, -119.840057
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The fatigue failure and separation of the right main landing gear.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
162-75
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
8GCBC BL8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
8GCBC

Registered Owner (Current)

Name
MONBERG ROBERT M
Address
PO BOX 56681
City
NORTH POLE
State / Zip Code
AK 99705-1681
Country
United States

Analysis

On August 16, 2000, at 0935 hours Pacific daylight time, a Bellanca 8GCBC, N8638V, collapsed the landing gear during landing rollout at a private dirt glider airstrip near Reno, Nevada. The airplane was owned and operated by the Nevada Soaring Association and was engaged in glider towing operations under 14 CFR Part 91 of the Federal Aviation Regulations. The airplane incurred substantial damage. The airline transport pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed and included calm wind conditions. No flight plan was filed for the local area business flight, which originated at the private airstrip about 20 minutes prior to the accident.

The pilot reported to Federal Aviation Administration (FAA) inspectors that he was making a 3-point landing after towing a glider aloft. The airplane bounced slightly on touchdown and, on the second ground contact, the pilot heard a snap sound and the right main landing gear collapsed. The airplane fell down on the right wing and spun around in the dirt.

An FAA airworthiness inspector from the Reno Flight Standards District Office examined the airplane and the runway. The inspector observed the two touchdown markings on the dirt runway and reported that they were about 12-feet apart and not heavy impressions. About 20 feet beyond the second touchdown point, drag markings consistent with a separated main landing gear were found.

The inspector reported that the right main landing gear strut separated near the fuselage with a transverse fracture. A majority of the fracture face appeared dirty and rusty, with the remaining portion exhibiting a pattern of beach markings and a chevron-like pattern.

According to the operator, this airplane has been used exclusively for glider tow operations and has accumulated over 4,000 flight hours. The operator and the FAA inspector estimated the total number of landing cycles somewhere between 15,000 and 16,000 for the life of the part.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX00LA303