N9467A

Substantial
None

CESSNA 140AS/N: 15469

Accident Details

Date
Monday, August 17, 2009
NTSB Number
ERA09LA467
Location
White Plains, NY
Event ID
20090818X52121
Coordinates
41.066944, -73.707496
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the right main landing gear due to a preexisting crack adjacent to a weld line.

Aircraft Information

Registration
Make
CESSNA
Serial Number
15469
Engine Type
Reciprocating
Year Built
1950
Model / ICAO
140AC140
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
140A

Registered Owner (Current)

Name
KOURTIS VINTAGE AVIATION LLC
Address
12150 E 96TH ST N STE 200
City
OWASSO
State / Zip Code
OK 74055-5340
Country
United States

Analysis

On August 17, 2009, about 1330 eastern daylight time, a Cessna 140A, N9467A, was substantially damaged during landing at Westchester County Airport (HPN), White Plains, New York. The airplane was operated by a private individual. The commercial pilot was not injured. Visual meteorological conditions prevailed at the time, and no flight plan was filed for the 14 Code of Federal Regulations Part 91 personal flight. The flight originated at East Hampton, New York at 1300.

The pilot reported that his approach to runway 34 was stable and on speed. As he began to flare, he sensed that he was slightly high, so he added power, leveled the nose, and flared again. The airplane touched down initially, bounced, and touched down again. The pilot described the landing as "firm." The airplane then "veered uncontrollably off to the left side of the runway." After exiting the airplane, the pilot noted that the right, main landing gear was separated from its gear box.

An inspector from the Federal Aviation Administration (FAA) inspected the airplane following the accident. He reported that the right side "bulkhead assembly – landing gear failed. Specifically, the structure immediately under the gear that sandwiches the gear in place failed." The inspector reported that the airplane had recently undergone an annual inspection and the section where the part failed would not be visible without disassembly.

The failed landing gear component, which was a welded “C” channel structure, was forwarded to the NTSB Materials Laboratory for inspection. The part had fractures at opposite ends. The fracture at one end of the structure was typical of shearing and tensile overstress separation. The fracture at the other end was adjacent to a weld line. For the majority of this fracture, the features were consistent with an overstress separation. However, a rusted and discolored region at the center leg of the “C” channel was indicative of a preexisting crack. Fracture face recontact damage and differential rusting of the fracture in this region was suggestive of progressive crack extension.

The 1356 weather observation for HPN included the following: few clouds at 6,000 feet, surface winds variable at 4 knots, 8 statute miles visibility, temperature 31 degrees Celsius, dew point 19 degrees Celsius, and an altimeter setting of 30.16 inches of mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA09LA467