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Atlas / NTSB / WPR10CA281

NTSB CAROL · Event

Event WPR10CA281

2010-05-29 Avalon, California, United States Airport · KAVX None 1 aircraft Status: Completed

Registry · N314CP

FAA Aircraft Registry record.

Make / Model

CIRRUS DESIGN SR22

Year of manufacture

2008 · 2 years old at event

TCDS

A00009CH · CIRRUS DESIGN CORP

Engine

CONT MOTOR IO-550-N (310 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

20080902

ADS-B equipped

Yes — Mode-S A355ED

Registrant of record

WILBURY LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to achieve the proper touchdown point, which resulted in a runway overrun.

Factual narrative

The pilot stated that he listened to the weather report at the airport prior to landing, which reported a slight tailwind on runway 22 that was in use by other airplanes in the traffic pattern. The pilot chose to land on runway 22 with a tailwind rather than changing runways to favor a headwind. In a phone conversation, the pilot stated that he landed "within the first couple hundred feet" of the runway at about 85 knots, using full flaps. He said that during the landing roll he overran the runway, resulting in the airplane exiting the end of the runway and coming to rest on a 45 degree downslope. The pilot stated that he "underestimated" the length of the runway due to the fact that the airplane was almost at max gross weight and there was a slight tailwind. The airplane sustained substantial damage to the right aft main wing spar. According to the Avalon aviation weather report, at the time of the accident the wind was from 020 degrees at 5 knots. According to the Southwest U.S. Airport/Facility Directory, the accident runway 04/22 is 3,000 feet long. The first 2,000 feet of runway 22 is sloped up 1.8%, and the rest of the runway is level. At maximum gross weight in the weather conditions of the airport at the time of the accident, the airplane had a calculated ground roll of about 1,250 feet, with a total landing distance of about 2,500 feet. Taking into account the 5 knot tailwind and the 1.69% upslope, this airplane's final ground roll was calculated to be about 1,300 feet, and the total landing distance was about 2,650 feet. The pilot stated that he listened to the weather report at the airport prior to landing, which reported a slight tailwind on runway 22 that was in use by other airplanes in the traffic pattern. The pilot chose to land on runway 22 with a tailwind rather than changing runways to favor a headwind. In a phone conversation, the pilot stated that he landed "within the first couple hundred feet" of the runway at about 85 knots, using full flaps. He said that during the landing roll he overran the runway, resulting in the airplane exiting the end of the runway and coming to rest on a 45 degree downslope. The pilot stated that he "underestimated" the length of the runway due to the fact that the airplane was almost at max gross weight and there was a slight tailwind. The airplane sustained substantial damage to the right aft main wing spar. According to the Avalon aviation weather report, at the time of the accident the wind was from 020 degrees at 5 knots. According to the Southwest U.S. Airport/Facility Directory, the accident runway 04/22 is 3,000-feet-long. The first 2,000 feet of runway 22 is sloped up 1.8%, and the rest of the runway is level. At maximum gross weight in the weather conditions of the airport at the time of the accident, the airplane had a calculated ground roll of about 1,250 feet, with a total landing distance of about 2,500 feet. Taking into account the 5 knot tailwind and the 1.69% upslope, this airplane's final ground roll was calculated to be about 1,300 feet, and the total landing distance was about 2,650 feet. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Aircraft-Aircraft oper/perf/capability-Aircraft capability-Landing distance-Not attained/maintained - C
  • Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Response/compensation
  • C Personnel issues-Task performance-Planning/preparation-Performance calculations-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2010_WPR10CA281.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.