Single-engine piston

N501SF

Cessna Turbo 210M / 210 Centurion / T210M

Registered 1 NTSB/FAA record
Built
—
Serial
21061808
Class
Single-engine piston
Engines
Continental TSIO-520 series
Status
Current as of October 2026
Registered owner
Nomarco Inc (Corporation)
Based
Woodburn, OR
Registration record

N501SF on the FAA register

Type
Cessna Turbo 210M / 210 Centurion / T210M
Serial
21061808
Engines
Continental TSIO-520 series
Registered owner
Nomarco Inc
Woodburn, OR
Certificate issued
2023-01-05
Airworthiness date
—
Registration expires
2030-01-31
Airworthiness class
Standard
Mode S (hex)
A63F3D
Mode S (octal)
51437475
Seats (type)
6
Weight class
up to 12,499 lb
Range (type)
732 nm
Cruise (type)
197 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2030-01-31
    Registration expires (renewal due).
  • 2023-01-05
    Certificate of registration issued as N501SF.
  • 2019-08-20
    Accident at Eugene, OR; damage: substantial.
Overview

About N501SF

N501SF is a Cessna Turbo 210M / 210 Centurion / T210M, serial number 21061808. The FAA register lists Nomarco Inc as the registrant in Woodburn, Oregon. The current certificate of registration was issued on January 5, 2023 and expires on January 31, 2030.

The FAA aircraft reference file describes the type as a single-engine piston, one Continental TSIO-520 series engine and 6 seats. Published figures for the type give a cruise speed of about 197 knots and a range of about 732 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category.

N501SF has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
197 kt
Range
732 nm
Fuel burn
17 gph

Published figures for the Cessna Turbo 210M / 210 Centurion / T210M type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2019-08-20 Accident · Eugene, OR Damage: Substantial NTSB · WPR19LA237
Reported aircraft: Cessna T210
Probable cause: The failure of the landing gear electric motor to shut off after landing gear retraction, which resulted in the motor overheating, burning out, and producing smoke in the cockpit. The pilot s decision to land with the landing gear retracted resulted in substantial damage to the airplane.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.