Single-engine piston

N72623

Cessna Turbo 206H Stationair / T206H Stationair / Turbo 206H Amphibian

Registered 1 NTSB/FAA record
Built
—
Serial
T20608162
Class
Single-engine piston
Engines
Lycoming TIO-540 series
Status
Current as of October 2026
Registered owner
Law Office of Vincent G Rieger Pc (Corporation)
Based
Kalispell, MT
Registration record

N72623 on the FAA register

Type
Cessna Turbo 206H Stationair / T206H Stationair / Turbo 206H Amphibian
Serial
T20608162
Engines
Lycoming TIO-540 series
Registered owner
Law Office of Vincent G Rieger Pc
Kalispell, MT
Certificate issued
2019-01-07
Airworthiness date
2000-03-01
Registration expires
2029-01-31
Airworthiness class
Standard · normal
Mode S (hex)
A9BC90
Mode S (octal)
52336220
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).
  • 2019-01-07
    Certificate of registration issued as N72623 to the current registrant.
  • 2000-03-01
    Airworthiness date on the current FAA record (standard category (normal)).
  • 1973-09-24
    N72623 previously assigned to a Cessna 140 (s/n 9799); cancelled.
  • 1971-10-27
    Accident at Denton,Tex, 43; damage: substantial.
Overview

About N72623

N72623 is a Cessna Turbo 206H Stationair / T206H Stationair / Turbo 206H Amphibian, serial number T20608162. The FAA register lists Law Office of Vincent G Rieger Pc as the registrant in Kalispell, Montana. The current certificate of registration was issued on January 7, 2019 and expires on January 31, 2029.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming TIO-540 series 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 March 1, 2000.

N72623 has 1 accident/incident record on file (most serious damage: substantial); 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 / T206H Stationair / Turbo 206H Amphibian type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

1971-10-27 Accident · Denton,Tex, 43 Damage: Substantial NTSB · 3 3895
Reported aircraft: Cessna 140

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.