Single-engine piston

N206RA

2021 Cessna Turbo 206H Stationair HD

Registered 1 NTSB/FAA record
Built
2021
Serial
T20609654
Class
Single-engine piston
Engines
Lycoming TIO-540-AJ1A
Status
Current as of October 2026
Registered owner
Acord Transportation Inc (Corporation)
Based
Chandler, OK
Registration record

N206RA on the FAA register

Type
2021 Cessna Turbo 206H Stationair HD (FAA: Textron Aviation T206H)
Serial
T20609654
Engines
Lycoming TIO-540-AJ1A
Registered owner
Acord Transportation Inc
Chandler, OK
Certificate issued
2022-01-15
Airworthiness date
2021-09-28
Registration expires
2029-01-31
Airworthiness class
Standard · normal
Mode S (hex)
A1A9C5
Mode S (octal)
50324705
Seats (type)
6
Weight class
up to 12,499 lb
Range (type)
721 nm
Cruise (type)
128 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2029-01-31
    Registration expires (renewal due).
  • 2022-01-15
    Certificate of registration issued as N206RA to the current registrant.
  • 2021-09-28
    Airworthiness date on the current FAA record (standard category (normal)).
  • 2013-08-16
    N206RA previously assigned to a Cessna U206G Stationair / U206 Amphibian / 206 Turbine (s/n U20605329); cancelled.
  • 2000-07-25
    Accident at Pistol Creek, ID; damage: destroyed.
Overview

About N206RA

N206RA is a 2021 Cessna Turbo 206H Stationair HD (FAA model T206H), serial number T20609654. The FAA register lists Acord Transportation Inc as the registrant in Chandler, Oklahoma. The current certificate of registration was issued on January 15, 2022 and expires on January 31, 2029.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming TIO-540-AJ1A engine and 6 seats. Published figures for the type give a cruise speed of about 128 knots and a range of about 721 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (normal), dated September 28, 2021.

N206RA has 1 accident/incident record on file (most serious damage: destroyed); details are below.

Cruise
128 kt
Range
721 nm
Landing over 50 ft
2,358 ft
Fuel burn
15 gph

Published figures for the Cessna Turbo 206H Stationair HD type. They describe the model, not this airframe's equipment or condition. Cessna Turbo 206H Stationair HD specs, prices and for-sale inventory →

Safety record

Accident & incident history

2000-07-25 Accident · Pistol Creek, ID Damage: Destroyed Fatal injury NTSB · SEA00FA142
Reported aircraft: Cessna TU-206G
Probable cause: A loss of engine power due to the fracture of the #2 cylinder intake valve stem and the puncturing of the #2 piston dome by the intake valve head. Factors include no suitable landing site within the maneuvering abilities of the aircraft, and coniferous trees in the area where the pilot attempted a forced landing.

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

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Browse: Cessna aircraft for sale· Cessna Turbo 206H Stationair HD overview· Aircraft registered in Oklahoma· Registry by state· FAA registry stats

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.