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
208B
Year
1996
Serial number
208B0581
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
12
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A32B21
Engine
Make and model
P&W Pt6a Ser
Type
Turbo-prop
Power
750 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2022 – nowState Of AlaskaPalmer, AK · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · substantial damage
Dec 19, 2005 · Brevig Mission, AK
The pilot's inadequate compensation for crosswind conditions, which resulted in the left wing striking the ground while taxiing. A factor in the accident was a crosswind.
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.
Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series…
May 12, 2008
Airframe (208B)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007.
Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 Airplanes
Jan 21, 1998
Airframe (208B)
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 · bulkhead · crackedJan 11, 2012
AFT CANTED BULHEAD AT STA 474.40 HAS TWO CRACKS EACH APPROX. 1.5 INCHES IN LENGTH. DURING REMOVAL OF THIS PART OTHER DAMAGE WAS FOUND. BOTH VERTICAL STAB WEBS (PNS: 2631021-15 AND 2631022-2)WERE REPLACED TO SIGNIFICANT FRETTING. THE AFT BULKHEAD ASSEMBLY WAS ALSO REPLACED DUE TO FRETTING.
From FAA Service Difficulty Reports; matched by N-number and serial number.