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
182M
Year
1969
Serial number
18259793
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
A99D54
Engine
Make and model
Cont Motor O-470 Series
Type
Reciprocating
Power
230 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2004 – 2013Individual ownerBethel, 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
Feb 9, 2004 · Yakutat, AK
The pilot's delayed use of carburetor heat, which resulted in an engine power loss during takeoff-initial climb, a forced landing, and subsequent collision with terrain. A factor contributing to the accident was the presence of carburetor icing conditions.
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 Models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R…
Apr 25, 2007
Airframe (182M)Only with: Air Plains Services Corporation STC SA00152WI installed and a ground power receptacle mounted on the firewall (forward ground power receptacle).
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.
Stabilizers · stop · bentFeb 11, 1999
FOUND RUDDER STOP BENT AND NO LONGER LIMITING RUDDER TRAVEL. FOUND IMPROPER HARDWARE INSTALLED. TRUSS HEAD SCREW INSTEAD OF BOLT DID NOT ALLOW FOR PROPER CONTACT AREA. COULD NOT TELL FROM LOGS WHEN THIS WAS INSTALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number.