Stoots Aviation was established in 1979 in Fairbanks, Alaska. STC's for High Performance Lycoming Engine Conversions,  
              Hartzell Propeller Installations, Tail Wheel Conversions on Cessna Models  170, 172 and 175 Airframes.
                Contact us at stoots@gci.net   or  907-474-4039 Hangar  907-590-5559 Cell
New STC IO-390A1A6 210HP                    Now FAA APPROVED STC SA02343AK FOR CESSNA 175, A, B, C         Later Model Cessna 172 Approval Coming Soon!
The New IO-390 A3A6 210 HP Lycoming Engine has now been installed on my '58 Cessna 175. Installation is the same as the IO-360 200 HP. All PMA/FAA approved parts for the IO-360 will be used for the IO-390.

The IO-390 comes with Roller Tappets and Cam and Counter Weighted Crankshaft. This engine runs really Smooth. With only 2hrs of flight time on the installation it's showing about 5mph faster on about the same fuel burn. I'm using the HC-C2YR-1BF/F8477-4 Hartzell Prop. With more flight time I will get the numbers down to show it's performance. As you can see below at 65% Cruise power fuel comsumption is .4 gph LESS! than the IO-360 200hp.

TC E00006NY  IO-390 A1A6, A3A6 
Rated Maximum Continuous HP @ RPM & BSFC           210 @ 2700 & .50
Performance Cruise (75% Rated)                                      158 @ 2450
Economy Cruise      (65% Rated)                                      137 @ 2350
Fuel Consumption, gph @ 75% Rated                               12.5 (IO-360 = 12.3)
                                         65% Rated                                 9.1 (IO-360 = 9.5)
Bore, Inches                                                                      5.319 (IO-360 = 5.125)
Stroke, Inches                                                                   4.375 (IO-360 = 4.375)
Displacement, Cubic Inches                                               389
Compression Ratio                                                            8.9:1 (IO-360 = 8.7:1)
Weight, Lbs.                                                                      315
Dimensions, Inches : Height                                               19.35 (IO-360 = 19.35)
                                Width                                                34.25 (IO-360 = 34.25)
                                Length                                               30.70 (IO-360 = 31.33)
Oil Sump Capacity, Qts                                                     8
Fuel, Aviation Grade, Octane                                             100 or 100LL
Fuel Injector, Precision Airmotive                                       RSA-5AD1
Fuel Pump, Diaphragm Type                                              Standand


                            STC SA02343AK NOW FAA APPROVED!!

                                   CESSNA MODELS 175, A, B, C

                          CESSNA 172 MODELS B Thru S Coming Soon.

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