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
Siai-Marchetti
Model
S.205/22R
Year
1968
Serial number
388
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A9C6F0
Engine
Make and model
Franklin 6v 350 Series
Type
Reciprocating
Power
235 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2011 – 2017Individual ownerPalm Beach Gardens, FL
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · substantial damage
Nov 5, 2011 · Okeechobee, FL
A partial loss of engine power due to a failure of the drive bearings in the alternator drive system. Contributing to the accident was the inadequate maintenance.
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
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.
Wings · bracket · crackedJul 29, 1998
WHILE C/W AD 75-17-32-R2 - LANDING GEAR OPERATING MECHANISM, A CRACK WAS FOUND IN THE RIGHT INTERNAL WING RIB BRACKET. THE CRACK WAS LOCATED AT THE UPPER RADIUS AND WAS APPROXIMATELY .75 INCH IN LENGTH. SUBMITTER STATED THE CRACK WAS MOST LIKELY CAUSED BY IMPROPER INSTALLATION. THE BRACKET IS…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · clevis rod end · failedJul 29, 1998
UPON LANDING, THE LT MLG CONTROL ASSY ROD END SHEARED CAUSING THE LT MAIN LANDING GEAR TO COLLAPSE. THE DIAMETER OF THE THREADED PORTION OF THE ROD END APPEARS TO BE TOO SMALL FOR THE LOADS IMPOSED UPON IT. IT SEEMS A LANDING GEAR CONTROL ASSY INCORPORATING A LARGER DIAMETER ROD END WOULD BE…
From FAA Service Difficulty Reports; matched by N-number and serial number.