N57669

Substantial
None

BELLANCA 8GCBC S/N: 2-74

Accident Details

Date
Saturday, July 8, 1995
NTSB Number
FTW95LA279
Location
WELLINGTON, CO
Event ID
20001207X03941
Coordinates
40.699756, -105.000328
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

FATIGUE FAILURE OF THE LEFT MAIN LANDING GEAR (SPRING STRUT), DUE TO THE IMPROPER MAINTENANCE (GRINDING) BY UNKNOWN MAINTENANCE PERSONNEL.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
2-74
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
8GCBC BL8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
8GCBC

Registered Owner (Current)

Name
ORWICK LOUREN CHRIS
Address
11544 32ND ST NE
City
MICHIGAN
State / Zip Code
ND 58259-9415
Country
United States

Analysis

On July 8, 1995, at 1330 mountain daylight time, a Bellanca 8GCBC, N57669, sustained substantial damage when the left main landing gear failed during landing roll at Owl Canyon Glider Park, Wellington, Colorado. The commercial pilot was not injured. Visual meteorological conditions prevailed for this local area glider tow flight operating under Title 14 CFR Part 91. The flight originated at 1320 and a flight plan was not filed.

According to the pilot, his landing sequence following the glider release contained "a mild bounce." The pilot said he added power for the second touch down and when touch down occurred the left main landing gear separated from the aircraft.

Examination of the aircraft by the investigator-in-charge provided evidence that the landing gear was of the spring steel type. Separation occurred just outboard of the fuselage attach point and during the ground excursion following the separation, the left wing, wing strut, left elevator, wind screen, left side window and propeller sustained damage.

Examination of the fracture surface by the NTSB Metallurgical Laboratory provided evidence of a fatigue failure and evidence that the landing gear spring steel had been ground at some point in time which caused overheating of the steel and subsequent changes in the microstructure. It was the metallurgist's evaluation, that the grinding initiated the fatigue. The metallurgist's report is attached.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA279