No fatalities

17 Aug 2009: CESSNA 140A (N9467A) — ZABER ELI D — White Plains, NY

White Plains, NY, United States

On 17 Aug 2009, a CESSNA 140A (registration N9467A) operated by ZABER ELI D was involved in an aviation accident near White Plains, NY. No fatalities were reported. Investigators recorded the probable cause as: The failure of the right main landing gear due to a preexisting crack adjacent to a weld line. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Cessna 140A experienced a hard landing and veered off the runway at Westchester County Airport on August 17, 2009, resulting in substantial damage to the landing gear structure.

Accident Overview

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

Pilot's Account

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

FAA Inspection

An FAA inspector examined the airplane post-accident and 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 noted that the airplane had recently undergone an annual inspection, and the section where the part failed would not be visible without disassembly.

NTSB Materials Laboratory Findings

The failed landing gear component, a welded "C" channel structure, was sent to the NTSB Materials Laboratory. It had fractures at opposite ends. One fracture was typical of shearing and tensile overstress separation. The other fracture was adjacent to a weld line, with features consistent with overstress separation for most of its length. However, a rusted and discolored region at the center leg of the "C" channel indicated a preexisting crack. Fracture face recontact damage and differential rusting in this region suggested progressive crack extension.

Weather Conditions

At 1356, the weather observation for HPN reported few clouds at 6,000 feet, surface winds variable at 4 knots, visibility 8 statute miles, temperature 31°C, dew point 19°C, and an altimeter setting of 30.16 inches of mercury.

Contributing factors

Main landing gear attach sec — Failure