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Aircraft

Aircraft Specification : TYPE 4 : VULCANAIR

           
General Characteristics
Maximum Ramp Weight	:  2100 kg 4630 lbs
Maximum Take-Off Weight		:  2084 kg 4594 lbs
Maximum Landing Weight :	:  1980 kg 4365 lbs
Typical Max Useful Load:  680 kg 1499 lbs
Maximum Fuel Load (usable): 670 Lt  177 US Gal with long range tanks option
Power plant	:  Textron Lycoming
Engine Designation		:  IO-360-A1B6 (normally Aspirated) installed on P68C
Engine Type	:  4-cylinder, 361 inch, 3 horizontal, direct drive, air    
                                                  cooled, fuel injected.
Power:  200 shp (Aspirated)

Performance
Max Range Cruise Speed	:  301 km/h 160Ktas 
Rate of Climb (2 Engines MTOW)	:  6 m/s 1100 fpm 
Single Engine Rate of Climb (MTOW s.l.)	:  1 m/s 200 fpm 
Stall Speed, 35 deg Flaps, MTOW	:  106 km/h 57Ktas 
Max Altitude	:  5.490 m 18.000ft 
Range, FL 100, 55% Pwr. (incl. 45’ Res.)	:  2960 km 1598 nm 

View PDF file:
VulcanAir Complete Specifications