No fatalities

29 May 2010: CIRRUS DESIGN CORP SR22 — Ilan Brand — Avalon, CA

Avalon, CA, United States

On 29 May 2010, a CIRRUS DESIGN CORP SR22 operated by Ilan Brand was involved in an aviation accident near Avalon, CA. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to achieve the proper touchdown point, which resulted in a runway overrun. 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 pilot overran the runway after landing with a tailwind, underestimating the required distance. The airplane sustained substantial damage to the right aft main wing spar.

Incident Overview

During a landing at an airport, a pilot experienced a runway overrun after choosing to land with a tailwind. The pilot had listened to the airport weather report prior to landing, which indicated a slight tailwind on runway 22, the runway in use by other traffic. Despite this, the pilot opted to land on runway 22 rather than switching to a runway that would provide a headwind.

Pilot Account

In a phone conversation, the pilot stated that he landed "within the first couple hundred feet" of the runway at approximately 85 knots with full flaps deployed. During the landing roll, the airplane overran the runway, exiting the end and coming to rest on a 45-degree downslope. The pilot acknowledged that he "underestimated" the length of the runway, attributing this to the airplane being near its maximum gross weight and the presence of a slight tailwind.

Weather and Runway Details

According to the Avalon aviation weather report, the wind at the time of the accident was from 020 degrees at 5 knots. The Southwest U.S. Airport/Facility Directory lists runway 04/22 as 3,000 feet long. The first 2,000 feet of runway 22 have an upslope of 1.8%, while the remaining portion is level.

Performance Calculations

At maximum gross weight under the prevailing weather conditions, the airplane had a calculated ground roll of about 1,250 feet and a total landing distance of about 2,500 feet. When accounting for the 5-knot tailwind and the 1.69% upslope (as calculated), the final ground roll was estimated to be approximately 1,300 feet, with a total landing distance of about 2,650 feet.

Damage

The airplane sustained substantial damage to the right aft main wing spar.

Contributing factors

Causes

Landing distance — Not attained/maintainedPilot

Other contributing factors

Response/compensation