NTSB CAROL · Event
Event LAX07LA019
Registry · N56MB
FAA Aircraft Registry record.
Make / Model
CESSNA AIRCRAFT CO LC41-550FG
Year of manufacture
2008
Engine
CONT MOTOR TSIO-550-C (310 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20080429
ADS-B equipped
Yes — Mode-S A725A6
Registrant of record
NUTACAIR400 LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to extend the landing gear prior to touchdown.
Factual narrative
On October 27, 2006, about 1345 mountain standard time, a Cessna 310N, N56MB, experienced a propeller strike and collision with the runway during landing at the Lake Havasu City Airport, Lake Havasu City, Arizona. Air Michelle was operating the airplane under the provisions of 14 CFR Part 91. The private pilot and two passengers were not injured; the airplane sustained substantial damage. The personal cross-country flight originated from John Wayne-Orange County Airport, Santa Ana, California, about 1220 Pacific daylight time, with a planned destination of Lake Havasu City. Visual meteorological conditions prevailed, and a flight plan had not been filed. The National Transportation Safety Board investigator-in-charge (IIC) interviewed the pilot immediately following the accident. He stated that he lowered the landing gear to the down and locked position while on the downwind leg of the traffic pattern for runway 32. During the landing flare, the pilot audibly distinguished an abnormal sound. He opted to abort the landing and manipulated the throttle control to the maximum power position. While climbing to the crosswind leg, the pilot noted that the airplane's performance was not sufficient to complete a landing pattern. He maneuvered the airplane in a 180-degree turn back to the runway (heading 140 degrees). As the airplane touched down, the pilot experienced a loss of control. The airplane veered to the left and departed the runway surface, subsequently encountering a dirt area. After egressing the airplane, the pilot noticed that the left main landing gear had collapsed and propeller blades on both engines appeared to have contacted the ground; the nose and right gear were in the down and locked position. During a telephone conversation with the Safety Board IIC, a witness reported that he observed the airplane approaching the runway, with the landing gear in the up position. The airplane continued to the runway in the gear-up configuration, until the left propeller stuck the runway surface. The airplane then became airborne and the landing gear dropped into the down position. The airplane appeared to make a left turn and then intercepted the runway in the opposite direction. A Federal Aviation Administration certified aircraft mechanic performed an examination of the airplane shortly after the accident. He stated that he found no mechanical malfunctions or failures that would have precluded the landing gear from operating normally. During landing, the airplane veered off the runway and the left main landing gear collapsed following an aborted gear-up landing during which the propeller contacted to the runway. The pilot said he extended the landing gear on entry to the downwind leg of the traffic pattern; however, ground witnesses saw the landing gear retracted during the entire approach and attempted landing. During the landing flare with the landing gear in the retracted position, the left propeller contacted the runway surface. The pilot aborted the landing. While climbing to the crosswind leg, the pilot noted that the airplane's performance was not sufficient to complete a landing pattern. He then performed a 180-degree return back to the runway and extended the landing gear. As the airplane touched down, the airplane veered off the runway surface, encountered a dirt area, and the left main landing gear collapsed . At the request of Safety Board investigators, an FAA certified aircraft mechanic performed an examination of the airplane shortly after the accident. He stated that he found no mechanical malfunctions or failures that would have precluded the landing gear from operating normally. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_LAX07LA019.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 (loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation)
ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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