MAIN FEATURES

• Engine: Lycoming to injection. Model IO-540-D4A5 (260 HP-24 V)
• Propeller: Hartzell tripala. Model HC-C3YR-1RF / F8468A
• Main Structure: Completely in 4130 steel tubes
• Wing end pieces: Laviasa type ND.
• Fuel tank: Central (53 gallons).
• Product hopper: Capacity (180 gallons).
• Laminar type landing gear (crossbow)
• Headlights on the leading edge semi-left wing.
• New dashboard - optional.
• New spraying system spikes - optional.
• Incorporation of satellite banderillero and complementary - optional.

• Spraying liquids, fungicides and pesticides.
• Spraying fertilizers and sowing seeds.
• Detection and immediate actions in forest fires.
• Towing of gliders and advertising posters.
• Sowing of fingerlings.
• Detection of leaks in pipelines (oil and gas).
• Police patrol.
• Emergency assistance to isolated people.

PERFORMANCE

• Decorating race mts (feet): 207 (680)
• Decorating race on obstacle of 50 feet mts (feet): 372 (1220)
• Speed ​​of best ascent regime (MPH): 83
• Ascent regime (feet x min.): 705
• Maximum speed (MPH): 120
• Cruising speed (75% of power) (MPH): 108
• Fuel consumption (75% of the power, optimal mix) (gph): 11.5
• Fuel consumption (75% of the power, completely rich mixture) (gph): 17.7
• Scope (75% of power, optimum mix) (miles): 479. Scope (75% of power, rich mix) (miles): 311
• Loss speed with maximum weight, flaps down (MPH): 61
• Loss rate with 1700 lbs. of weight (MPH): 46
• Landing run with maximum weight mts (feet): 259 (850)

AIRCRAFT CONFIGURATION

TECHNICAL DESIGN