NTSB CAROL · Event
Event LAX06CA171
Aircraft involved
Probable cause & findings
the pilot's inadequate compensation for the crosswind condition and failure to maintain lateral control of the airplane during takeoff.
Factual narrative
On May 14, 2006, at 1600 Pacific daylight time, a Cessna 320, N5799X, struck a wing tip on the runway during takeoff from runway 25R at Daugherty Field, Long Beach, California. The pilot aborted the takeoff. The pilot was operating the privately owned airplane under the provisions of 14 CFR Part 91. The commercial pilot was not injured; the airplane sustained substantial damage. Visual meteorological conditions prevailed and no flight plan had been filed. The pilot was destined for Southern California Logistics Airport, Victorville, California. In a written statement, the pilot said that the taxi and run-up were uneventful. During takeoff, he noted that the wind was coming from the left (south) and he set the flight controls for a crosswind takeoff. He advanced the throttles to takeoff power and rotated the airplane. As the airplane left the runway surface, the left wing was slightly low and he noticed that the airplane was not climbing. As he turned the airplane into the wind, the right wing dropped and the wing tip fuel tank impacted the runway. He stabilized the airplane and pulled the power to idle. The airplane stopped just beyond the runway. The pilot believed that a gust of wind or small microburst may have kept the airplane from climbing and influenced the right wing tip to impact the ground. The pilot stated that there were no mechanical malfunctions with the airplane. At 1553, the unedited surface weather observation (METAR) at Long Beach reported winds from 180 degrees at 7 knots. Following the accident, the Federal Aviation Administration accident coordinator examined the airplane. The inspector noted that the rear spar at the right wing tip was damaged during its impact with the runway surface. The wing tip impacted the runway surface during takeoff and the pilot aborted the takeoff. The pilot said that the taxi and run-up were uneventful. During takeoff, he noted that the wind was coming from the left (south) and he set the flight controls for a crosswind takeoff. He advanced the throttles to takeoff power and rotated the airplane. As the airplane left the runway surface, the left wing was slightly low and he noticed that the airplane was not climbing. As he turned the airplane into the wind, the right wing dropped and the wing tip fuel tank impacted the runway. He stabilized the airplane and pulled the power to idle. The airplane stopped just beyond the runway. The pilot believed that a gust of wind or small microburst may have kept the airplane from climbing and influenced the right wing tip to impact the ground. The pilot stated that there were no mechanical malfunctions with the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_LAX06CA171.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (microburst). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Experimental investigations on the characteristics of snow accretion using the EMU-320 model train
This paper presents a snow accretion test conducted in a climate wind tunnel to investigate the icing process on a model train.
- Embry-Riddle Scholarly Commons 2017 · Conference paper
Pilot Control Design Influences on Pilot Monitoring Effectiveness of Crew Resource Management in Airbus 320 Landings
The purpose of this paper is to examine the effects of Airbus flight control design on pilot perception of Crew Resource Management (CRM) in the landing phase of flight.
- Embry-Riddle Scholarly Commons 2015 · Journal article (JAAER)
Is “Green Dot” Always the Optimum Engines-Out Glide Speed on the Airbus A320 Aircraft?
The dual-engine failure checklist of the Airbus A320 states that the optimum airspeed at which the aircraft can be flown is the “green dot” speed when an engine restart is considered impossible.
- NASA NTRS 2019 · Conference Paper
Optimal recovery from microburst wind shear
The flight path of a twin-jet transport aircraft is optimized in a microburst encounter during approach to landing. The objective is to execute an escape maneuver that maintains safe ground clearance …
- NASA NTRS 2019 · Conference Paper
Performance limits for optimal microburst encounter
An effort has been made to ascertain the envelope-edges for uneventful aircraft penetrations of microburst windshears on the basis of optimal aircraft control strategies.
- NASA NTRS 2019 · Conference Paper
Aircraft performance in a JAWS microburst
Attention is given to the detailed features of a servere microburst event, the flight behavior of a 727 airliner in such an event as predicted by a numerical simulation, and several low level wind she…
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