We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type data
Airframe
Manufacturer
Cessna
Model
U206G
Year
1977
Serial number
U20604074
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
A4CE
Mode S code
AA30EF
Engine
Make and model
Cont Motor Io 520 Series
Type
Turbo-shaft
Power
285 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
1986 – nowIndividual ownerConcord, NC · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · substantial damage
Feb 3, 1982 · Moses Lake, WA
THE PILOT STATED THAT HE ENCOUNTERED A FREAK GUST OF WIND DURING THE LANDING. THE PLANE TOUCHED DOWN ON THE RIGHT SIDE OF THE RUNWAY IN AN AREA OF SOFT TERRAIN. THE AIRCRAFT VEERED FARTHER TO THE RIGHT AND CONTINUED INTO AN EARTHEN DRAINAGE DITCH. THE DITCH WAS 12 TO 15 FEET DEEP AND RAN PARALLEL TO THE RUNWAY.
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…
Sep 9, 2009
Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
Fuselage · skin · corrodedJul 21, 1998
CORROSION UNDER THE VIBRATION ABSORBING PADS DUE TO WATER BEING TRAPPED WHERE THE BONDING OF THE PAD TO THE SKIN HAS FAILED. SUBMITTER STATES THIS IS A COMMON PROBLEM WITH CESSNA AIRCRAFT.
From FAA Service Difficulty Reports; matched by N-number and serial number.