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
182P
Year
1973
Serial number
18261995
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
ACA562
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
2008Voigt Aviation INCPark Rapids, MN
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
Aug 13, 1983 · West Milford, NJ
THE ACFT HAD ATTAINED AN ALT OF 300 FT AGL WHEN THE ENGINE LOST POWER. THE PILOT TURNED BACK 180 DEGREES TOWARD A CLEARING NEAR THE ARPT. THE ACFT WENT THROUGH SOME TREES AND MADE A HARD LANDING WHICH COLLAPSED THE NOSE GEAR. AN ANNUAL INSPECTIN HAD JUST BEEN COMPLETED ON THE DAY OF THE ACCIDENT.
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 (182P)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.
Fuel · line · chafedJul 9, 1996
DURING WINDSHIELD REPLACEMENT, FOUND AILERON CONTROL CABLE, WHICH TRAVELS UP THE FORWARD RIGHT DOOR POST, WAS CHAFING ON THE ADJACENT FUEL LINE. ORIGINAL WALL THICKNESS IS .030 INCH AND THE DEPTH OF THE CHAFE WAS .020 INCH.
From FAA Service Difficulty Reports; matched by N-number and serial number.