Owner type Co-owned
Year built 1973
Type Fixed wing single engine
Engine Reciprocating
Airworthiness Standard, normal
Airworthiness date December 18, 1973
Certificate issued September 19, 2013
Expires September 30, 2029 From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-520 model are included below.
On this page Registration Potential ADs 90 Information bulletins 16 NTSB investigations 0 FAA incident reports 1 Difficulty reports 4 Potential STCs 518 Related links Airworthiness directives that may apply · 90 Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
1969 In force Superseded2026 ADs by the year they took effect: 92 ADs 1969 1 1970 1 1971 1 1972 1 1974 2 1975 2 1976 2 1977 3 1978 1 1979 5 1980 4 1981 2 1982 1 1985 3 1986 2 1987 3 1988 7 1989 1 1990 3 1991 1 1993 3 1995 1 1996 1 1997 1 1998 2 1999 1 2000 3 2002 1 2003 1 2004 1 2005 1 2006 1 2007 2 2008 2 2009 3 2010 2 2011 3 2012 3 2014 1 2016 1 2020 2 2022 3 2023 6 2024 1
See all 101 ADs
NTSB investigations No NTSB investigations matched to N7485Q Matched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna TU206F aircraft FAA incident reports · 1 FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 4 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 97ZZZX1871 Axle · corroded AIRCRAFT TOTAL TIME 3,075.0 HOURS. AIRCRAFT HAD BEEN CONVERTED TO SEAPLANE BY STC 1483GL IN 1991 AND OPERATED IN SALT WATER FOR 3 YEARS PRIOR TO ANNUAL INSPECTION IN 1997. ON DISASSEMBLY FOR MAINTENANCE AND INSPECTION, THE MLG AXLES WERE REMOVED FROM THE GEA Mar 17, 1997 · N7485Q · Cessna TU206F · Main Landing Gear Strut/Axle/Truck SDR 97ZZZX1638 Structure · corroded AIRCRAFT TOTAL TIME 3,075 HRS. AIRCRAFT BUILT AS LAND PLANE AND MODIFIED FOR FLOATS INSTALLATION IAW WIPAIRE STL SA1483GL. POH SUPPLEMENT REQUIRES 'OPERATION IN FRESH WATER ONLY' PLACARD DUE TO NO STAINLES STEEL CONTROL CABLES OR FUSELAGE INTERIOR PRIMER. C Mar 17, 1997 · N7485Q · Cessna TU206F · Fuselage Miscellaneous Structure SDR 97ZZZX1637 Control Cable · corroded AIRCRAFT TOTAL TIME 3,075 HRS. AIRCRAFT BUILT AS LAND PLANE AND MODIFIED FOR FLOATS INSTALLATION IAW WIPAIRE STL SA1483GL. POH SUPPLEMENT REQUIRES 'OPERATION IN FRESH WATER ONLY' PLACARD DUE TO NO STAINLES STEEL CONTROL CABLES OR FUSELAGE INTERIOR PRIMER. C Mar 17, 1997 · N7485Q · Cessna TU206F · Flight Control System SDR 96ZZZX3890 Cylinder · cracked HYDRAULIC LEAK. CRACK INSIDE OF HYDRAULIC CYLINDER. REPLACED PART WITH NEW. INSPECTED, FOUND CORROSION, POSSIBLY CAUSED BY GEAR INDICATOR LIGHT WIRES AND HYDRAULIC LINE BEING CLAMPED TO CYLINDER. A RUBBER/PLASTIC PAD HAD BEEN GLUED TO CYLINDER TO PREVENT C Jul 1, 1996 · N7485Q · Cessna TU206F · Landing Gear Retraction/Extension System STCs that may be installed · 518 Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 518 STCs