CESSNA 340 SILVER EAGLE

CESSNA

340 SILVER EAGLE

Used

1972/1984 Cessna O&N Silver Eagle 340 Turbine, Certification was completed on 23 July 2012.............. This aircraft in the photos is the proto type which we consider ship #1, we have delivered ship #2 and is based in South Dakota, ship #3 is a couple of weeks out form deliver and expecting to be delivered by the end of January. #3 will be based in the Salt Lake Utah Area. Ship #1 has been located at PropJet Aviation since the AOPA showing for testing and data collection regarding performance specifications. One of the tests that I was most interested in, was single engine performance...At gross weight, the day was standard and the field elevation at Santa Rosa in 125 ft. At 2000ft above SL we shut down the starboard engine (right hand side), we were at gross weight (6300 lbs), an were able to climb to 17,500ft with speed and rate to spare, in fact our initial climb rate was 900fpm at 130 knots indicated to 10,000ft...from 10,000ft to 14,500ft our climb was 120 knots indicated at 500fpm....on the climb to 17,500 the last 2000ft of the climb as an honest 350 fpm @ 110 IAS...leveling off at 17,500 our indicated air speed on one engine was 137 knots at 176 TAS....yes the plane could have / would have continued the climb but we decided to climb to FL210 on two engines, once there we again shut down the right engine and was able to maintain level flight with a 7 degree up attitude (normal cruise with two engines is 2 degree) with 106 IAS and a 146TAS....very impressive, needless to say there isn't a piston 340 out there that can perform like this (but who would even expect one too...). The best true airspeed with two engine is a constant 235 knots true burning a total for both engines(combined GPH) 44 gallons....there are not many single engine turbines / pressurized certified aircraft... that cruise at this speed can get that burn on one engine... on other tests the SE 340 will climb at gross weight at 160 knots indicated at 2200 fpm up to 12,000ft, then the rate stays at between 800 to 900 fpm up to 17,500....Landing this plane is just fun....with reverse propeller action, the plane can stop in 300ft....take off is 600ft with a rotation at 80 knots indicated....Also on decents from altitude anything from 5000 fpm to what ever you would like, no effect on engines, airframe or propellers....actually I have seen 8,000 fpm and not exceed 180 knots indicated.....

Conversion Package: Two (new) Rolls Royce, 250 B17F/2 engines with power turbine enhancement..two new Hartzell 3 blade full reversible propellers...(5-blade in the works hopefully this year) 252 gallons fuel system, of which the transfer to main tanks is auto transfer, therefore never changing fuel selector to chase fuel from tank to tank...certified known ice (option if not certified donor aircraft)...all new interior...all new paint...(client picks the colors and the leather for the interior...all new LED interior lighting, Boom Beam on the taxi light...O&N Electric Air Conditioner...new Jet-A Heater...Dual 150 amp starter/generator system...New Gill 7638-44, 85lb sealed battery...all new wiring, all new circuit breaker panels...all new Tires, Brakes an upgraded to 414 Cessna 4 puck brake system...Avionics all new...S-TEC 55X auto pilot... Garmin G-600...Garmin GTN-750/650 GPS Nav Com with remote 330 mode ?S? transponder with remote Audio Panel and Intercom...Garmin traffic, Garmin GDL-69 sat weather...WX-500 strike finder...Back up instrument is an Aspen 1000 with self batter powered electrical back up system...Fuselage Strakes (which eliminate the need for Yaw Damper...All AD's complied with, All SB's complied with....New Annual inspection, with 1 year O&N warrantly on conversion....with 3 year warrantly on engines from Rolls Royce...all other items have full factory warranty as per everything is new.... Price - Conversion $1.6M (not including airframe) Taking Orders for 2014 positions