PA-25-260 PUELCHE III
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).
Emergency assistance to isolated people.
PERFORMANCES (with maximum weight 2900 lbs) Spray
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)