1983 CESSNA 206 TURBINE

1983

CESSNA

206 TURBINE

U20606768

Used

1606.0

SOLOY CONVERSION, 1,606 TT, Fresh Annual, Sierra LR Tanks, factory float kit Wipaire 4000 Amphibs, G-500 glass panel

1452 HOURS SNEW/ 287 Hours since HOT SECTION @ PREMIER TURBINES TO ACCOMPLISH FACTORY ISSUED AD. EARLY HOT SECTION DUE TO CALENDAR LIMIT FOR AD COMPLIANCE. ALLISON C-20S ENGINE UPGRADE SOLOY CONVERSION DONE @ TOTAL TIME (TACH) 154 HOURS. ENGINE TOTAL TIME 63 HOURS SINCE NEW. RTS 1/23/85

Overhauled July 2014

SOLOY CONVERSION 420 HP ALLISON C-20S ENGINE IN 1984 WIPLINE RIGHT HAND PASSENGER DOOR SIERRA LONG RANGE TANKS (144 GALLON FUEL CAPACITY) ROSEN SUN VISORS RMD LIGHTING WING TIP PULSE LIGHTS FACTORY FLOAT KIT Wipaire 4000 Amphib Floats AVIONICS PANEL REDONE BY AUTOPILOT CENTRAL, TULSA, OK., NEW 2" ENGINE GUAGES INSTALLED 1986 @ 366 TT.

GARMIN G-500 GLASS PANEL PFD/MFD DUAL GARMIN 530 GPS/NAVCOMS WAAS ENABLED SYNTHETIC VISION GARMIN GRS-77 AHRS GARMIN GMA-340 AUDIO PANEL ACK E-04 ELT WX-1000 STORMSCOPE BF GOODRICH SKYWATCH SKY497 TRAFFIC ADVISORY SYSTEM GLD 69 XM WEATHER GARMIN GTX 330ES DIGITAL MODE S TXPR KING KFC-200 AUTOPILOT/FLIGHT DIRECTOR PS ENGINEERING 6 PLACE INTERCOM SYSTEM SHADIN FUEL FLOW RESERVE INDICATOR SANDIA AEROSPACE ALTITUDE ENCODER STANDBY GYRO

OVERALL WHITE WITH BURGANDY AND GREY STRIPES. 9/10

ALL SEATS COVERED IN GARRETT LEATHER SHEEPSKIN WOOL /FLINT GREY WOOL CARPET. FIREBLOCKED. DUNCAN AVIATION, 11/2000@ 1062.5 TT. 8.5/10

Majority of Pre 2013 ANNUALS/MAINTENANCE HAS BEEN PERFORMED BY DUNCAN AVIATION/LINCOLN WITH THE EXCEPTION OF 3-4 ANNUALS. Recent Annual Complied March 2017 Aerotec Uhl, Oslo Norway (Soloy's Europe rep) SID Inspection July 2014 FOD DAMAGE AT 384.6 (475.6 AF) HOURS ON THE ENGINE, THE ALTERNATE AIR DOOR SPRING CAME LOOSE AND WENT THRU THE ENGINE. IT WAS REMOVED AND OVERHAULED BY AVIALL. REMOVED 10/19/87. REPLACED 12/11/87. IN 1998, THE AIRCRAFT WAS BEING TOWED TO THE MAINTENANCE SHOP AT DUNCAN AVIATION. THE TUG OPERATOR TURNED TOO SHARP AND SNAPPED THE NOSE GEAR. THE NOSE FELL ONTO THE LOWER COWLING AND THE PROP ALSO CONTACTED THE GROUND. THE COWLING WAS REPLACED AND THE PROP WAS PULLED AND REPAIRED. THE ENGINE GEAR BOX WAS DISASSEMBLED FOR INSPECTION. THE ENGINE WAS NOT UNDER POWER AND THERE WAS NO DAMAGE TO THE GEARBOX.