PA-25-260 PUELCHE III

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.

JOBS:

  • 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

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)

AIRCRAFT CONFIGURATION

Under development

TECHNICAL DESIGN