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
207A
Year
1984
Serial number
20700780
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
8
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A813EE
Engine
Make and model
Cont Motor Io-520-F
Type
Reciprocating
Power
300 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2018 – 2021Sutton Aircraft Salvage LLCPalmer, AK
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · substantial damage
Jul 17, 2015 · Juneau, AK
The pilot's decision to initiate and continue visual flight into instrument meteorological conditions, which resulted in a loss of situational awareness and controlled flight into terrain. Contributing to the accident were the company's failure to follow its operational control and flight release procedures and its inadequate training and oversight of operational control personnel.
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-F)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.
Flight controls · wire · shortedFeb 18, 1998
FLAP UP WIRE CHAFED ON STRINGER IN WING BETWEEN STA 85.62 AND STA 100.00; WIRE SHORTED AND BURNED HOLE IN WING. INSPECTION OF 10-AMP CIRCUIT BREAKER FOUND A FAILURE OF BREAKER TO 'POP'. SUBMITTER RECOMMENDED RUNNING WIRES IN A PLASTIC CONDUIT FROM LEADING EDGE WIRE GROMMETS TO FLAP MOTOR PLUG.
From FAA Service Difficulty Reports; matched by N-number and serial number.