Single-engine piston

N1155M

2006 Cessna Turbo 206H Stationair

Registered 1 NTSB/FAA record
Built
2006
Serial
T20608683
Class
Single-engine piston
Engines
Lycoming TIO-540-AJ1A
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Newburyport, MA
Registration record

N1155M on the FAA register

Type
2006 Cessna Turbo 206H Stationair (FAA: Cessna T206H)
Serial
T20608683
Engines
Lycoming TIO-540-AJ1A
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Newburyport, MA
Certificate issued
2023-06-26
Airworthiness date
2006-11-20
Registration expires
2030-06-30
Airworthiness class
Standard · normal
Mode S (hex)
A041D9
Mode S (octal)
50040731
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

  • 2030-06-30
    Registration expires (renewal due).
  • 2023-06-26
    Certificate of registration issued as N1155M to the current registrant.
  • 2006-11-20
    Airworthiness date on the current FAA record (standard category (normal)).
  • 2003-07-23
    N1155M previously assigned to a Cessna Turbo 210M / 210 Centurion / T210M (s/n 21061922); cancelled.
  • 1989-10-19
    Accident at Kernersville, NC; damage: substantial.
Overview

About N1155M

N1155M is a 2006 Cessna Turbo 206H Stationair (FAA model T206H), serial number T20608683. It is registered to an individual in Newburyport, Massachusetts. The current certificate of registration was issued on June 26, 2023 and expires on June 30, 2030.

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 November 20, 2006.

N1155M 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 type. They describe the model, not this airframe's equipment or condition. Cessna Turbo 206H Stationair specs, prices and for-sale inventory →

Safety record

Accident & incident history

1989-10-19 Accident · Kernersville, NC Damage: Substantial NTSB · ATL90LA009
Reported aircraft: Cessna 210
Probable cause: IMPROPER FUEL CONSUMPTION CALCULATIONS BY THE PILOT, WHICH RESULTED IN FUEL EXHAUSTION FROM LACK OF FUEL. ADVERSE WEATHER CONDITIONS WERE RELATED TO THE ACCIDENT.

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 overview· Aircraft registered in Massachusetts· 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.