N113CSBOMBARDIER BD700 1A102011-04-21 NTSB Accident Report

Substantial
None

BOMBARDIER BD700 1A10S/N: 9354

Summary

On April 21, 2011, a Bombardier BD700 1A10 (N113CS) was involved in an incident near Teterboro, NJ. All 4 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's loss of aircraft control during landing in gusty wind conditions.

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.

This incident is documented in NTSB report ERA11CA280. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N113CS.

Accident Details

Date
Thursday, April 21, 2011
NTSB Number
ERA11CA280
Location
Teterboro, NJ
Event ID
20110504X12246
Coordinates
40.838611, -74.060279
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

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

Aircraft Information

Registration
Make
BOMBARDIER
Serial Number
9354
Model / ICAO
BD700 1A10

Analysis

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA11CA280