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Atlas / NTSB / ERA11CA280

NTSB CAROL · Event

Event ERA11CA280

2011-04-21 Teterboro, New Jersey, United States Airport · TEB None 1 aircraft Status: Completed

Registry · N113CS

FAA Aircraft Registry record.

Make / Model

GULFSTREAM AEROSPACE GVI (G650ER)

Year of manufacture

2014

TCDS

T00015AT · GULFSTREAM AEROSPACE CORP

Engine

ROLLS DEUT BR700-725A112

Seats / Engines

22 seats · 2 engines

Last airworthiness date

20150205

ADS-B equipped

Yes — Mode-S A0379B

Registrant of record

113CS LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's loss of aircraft control during landing in gusty wind conditions.

Factual narrative

According to the pilot flying, the airplane was vectored onto the final approach course and the pilot not flying had configured the airplane to land. The pilot not flying reported that during the approach the airspeed was fluctuating by 20 knots. As the pilot flying initiated a flare to land, the airplane encountered a gust of wind, the airplane rolled left, and full opposite aileron was applied; however, the left wing impacted the runway. The airplane landed, slowed to taxi speed, and exited the runway. Examination of the airplane revealed substantial damage to the left outboard forward wing spar. The wind, approximately 5 minutes prior to the accident, was recorded as 310 degrees at 20 knots, gusting to 33 knots. A peak wind was recorded about the time of the accident as 300 degrees at 33 knots. According to the pilot flying, the airplane was vectored onto the final approach course and the pilot not flying had configured the airplane to land. The pilot not flying reported that during the approach the airspeed was fluctuating by 20 knots. As the pilot flying flared, the airplane encountered a gust of wind, rolled left, and full opposite aileron was applied; however, the left wing impacted the runway. The pilot landed, slowed to taxi speed, and exited the runway. Postaccident examination of the airplane revealed substantial damage to the left outboard forward wing spar. The wind, approximately 5 minutes prior to the accident, was recorded as 310 degrees at 20 knots, gusting to 33 knots. A peak wind was recorded about the time of the accident as 300 degrees at 33 knots. 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 Personnel issues-Action/decision-Action-Delayed action-Pilot - C
  • Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2011_ERA11CA280.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.