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Atlas / NTSB / CEN10CA533

NTSB CAROL · Event

Event CEN10CA533

2010-09-12 Farmington, New Mexico, United States Airport · FMN None 1 aircraft Status: Completed

Registry · N24WW

FAA Aircraft Registry record.

Make / Model

CESSNA 210L

Year of manufacture

1975 · 35 years old at event

Engine

CONT MOTOR IO 520 SERIES (285 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

19750619

ADS-B equipped

Yes — Mode-S A22FAF

Registrant of record

PARK AVENUE GROUP INC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s premature retraction of the landing gear and the flaps during landing. Contributing to the accident was the inadvertent dimming of the cockpit lighting, resulting in a perceived unsafe gear configuration.

Factual narrative

The pilot was landing at mid-day in bright sunny conditions after completing a practice instrument landing system (ILS) approach. The pilot reported that he extended the landing gear and flaps when he was about three miles from the airport. The airplane crossed the threshold of the runway and was just about to touchdown when he noticed that the landing gear green indicator lights appeared not to be illuminated. The pilot went to full throttle, and immediately raised the landing gear and flaps. During the go-around attempt the airplane settled and the propeller struck the runway. The pilot held full power and a nose high attitude as the airspeed decreased. The airplane struck obstructions on the side of the runway and came to rest upright approximately 3,000 feet down the 6,704 foot long runway. There was substantial damage to the left wing. The solo pilot was not injured. An inspection of the aircraft systems by a Federal Aviation Administration inspector revealed that the cockpit lighting dimmer switch was set to the “Night Dim” position. The pilot was landing after completing a practice instrument landing system approach in bright day conditions. The pilot reported that he extended the landing gear and flaps when he was about three miles from the airport. The airplane crossed the threshold of the runway and was just about to touch down when the pilot noticed that the landing gear green indicator lights appeared not to be illuminated. The pilot applied full throttle and immediately raised the landing gear and flaps. During the go-around attempt the airplane settled and the propeller struck the runway. The pilot held full power and a nose-high attitude as the airspeed decreased. The airplane struck obstructions on the side of the runway, resulting in substantial damage to the left wing. It then came to rest upright approximately halfway down the length of the runway. An inspection of the aircraft systems by a Federal Aviation Administration inspector revealed that the cockpit lighting dimmer switch, which controlled the illumination intensity of the landing gear lights, was set to the “Night Dim” position. 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 systems-Landing gear system-Gear extension and retract sys-Incorrect use/operation - C
  • C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
  • F Aircraft-Aircraft systems-Indicating/recording systems-Central warning-Incorrect use/operation - F
  • F Environmental issues-Task environment-(general)-(general)-Effect on operation - F

Verbatim from NTSB's published report. Source file NTSB_2010_CEN10CA533.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗