N10273

Destroyed
None

Grumman G-164 S/N: 073

Accident Details

Date
Wednesday, July 2, 1997
NTSB Number
MIA97LA201
Location
ALTHA, FL
Event ID
20001208X08458
Coordinates
30.569517, -85.119079
Aircraft Damage
Destroyed
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the left main landing gear spring due to a preexisting fatigue crack resulting in the separation of the left main landing gear, and subsequent nose down during taxi.

Aircraft Information

Registration
N10273
Make
GRUMMAN
Serial Number
073
Engine Type
Turbo-shaft
Year Built
2005
Model / ICAO
G-164 G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TAYLOR CECIL L
Address
17181 E IL HWY 15
Status
Deregistered
City
MT VERNON
State / Zip Code
IL 62864
Country
United States

Analysis

On July 2, 1997, about 0830 central daylight time, a Grumman G-164, N10273, registered to a private owner, operating as a 14 CFR Part 91 positioning flight, experienced a failure of the left main landing gear on taxi and nosed down on the ground. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was consumed by a postcrash fire. The commercial pilot reported no injuries. The flight was originating at the time of the accident.

The pilot stated he was taxing out to conduct an engine run-up before departing on a positioning flight to pick up a load of chemical before departing on an aerial application flight. As he started to turn around the left main gear separated. The airplane came to rest on the nose and left wing. Fuel started leaking out of the fuel tank and the airplane was consumed by fire.

A portion of the left main landing gear spring was forwarded to the NTSB Materials Laboratory for analysis. A fracture was located about 2 to 3 inches inboard of the fuselage skin. A visual magnified examination of the fracture revealed a small preexisting fatigue crack emanating from the lower surface of the spring about 3.5 inches from the leading edge. Closer examination established that the fatigue area was made up of four fatigue cracks, two of the larger had joined to form a single front. See Metallurgist's Factual Report No. 97-134.

The left main landing gear spring was released to Mr. Donald T. Johnson, on August 18 , 1997, and signed for by A. Golden, on August 20, 1997.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA97LA201