Two-Seats PUELCHE

MAIN FEATURES

Technical characteristics:

  • Engine: Lycoming O-540-B4B5 (235 HP).
  • Propeller: Hartzell HC-C3YR-1RF / 7693

Constructive details:

  • Main Structure: Fully in 4130 steel tubes.
  • Front and rear panels: last generation instruments.
  • Landing gear: Laminar type (leaf spring).
  • Fuel tank: Central (53 gallons).
  • Wing tips: Type “Laviasa ND”

Jobs:

  • Training (General Piloting and / or Aeroapplicator)
  • Early detection in forest fires.
  • Towing of gliders and advertising posters.
  • Duct inspection (gas and oil).
  • Police patrol.
  • Installation of Flir camera for surveillance and patrol.

PERFORMANCE

Deck race (feet) 740 Deck race over obstacle of 50 feet (feet) 1270 Improvement rate of climb (MPH) 88 Ascent regime (feet x min.) 710 Maximum speed (MPH) 145 Cruise speed (75 % of power) (MPH) 130 Fuel consumption

(75% of the power, optimal mix) (gph) 14

Fuel consumption
(75% of the potency, completely rich mixture) (gph) 16

Scope (75% of the power, optimum mix, 53 gallon tank) (miles) 425 Loss rate with maximum weight, flaps down (MPH) 61 Loss rate with 1700 lbs. of weight (MPH) 52

AIRCRAFT CONFIGURATION

Under development

TECHNICAL DESIGN