The P92-S ECHO, built out of the experience matured through production and implementation of hundreds of units and the research activities aimed at constant improvement of the machine's characteristics.
The result of this constant effort is summed up as UNMATCHED PERFORMANCE AND OUTSTANDING FLYNG QUALITIES.
Ease of inspection; immediate access for servicing that is efficient and inexpensive at the same time.
The comfort of the controls, the high roll rate and well-matched stick force allow for pleasant flight and easy maneuvering even in demanding situations. A marked longitudinal stability allows for prolonged stick free flying.
All load-bearing structures are light alloy and built to meet International Standards of Airnavigation.
Wing profile and tips feature new design and meet requirements for added speed.
New engine cowling, greater windshield slope and new fairing that joins harmoniously the cabin area with the vertical tail tangibly reduce aerodynamic drag.
Rear visibility is improved with the addition of a third window on the aft fairing.
The cabin features a wide windshield with view unhindered by structural elements. Visibility while turning is also improved by the tapering of the inboard wing roots. Doors feature elbow housings for added comfort and allow for easy access to cabin. Side-by-side seats are adjustable and feature three point attachment safety belts.
Flight controls are traditional type with dual stick, dual rudder pedals and dual throttle knobs on dashboard. Longitudinal trim and electrical flap controls with position indicators are also located on dashboard.
Instrument panel meets General Aviation standards both in size and quality allowing for installation of a wide variety of flight instrumentation inclusive of IFR, engine controls and com/nav apparatus.
Main gear features steel springs while nose gear features a steerable wheel with rubber damper. Specifically designed wheel fairings complete their effeiciency.
Engine cowling is made up two parts and allows for quick and complete opening.
Fuel tanks are integral part of the wing structure and feature 35 liter capacity per each half wing.
Fuel feed is via an engine driven pump.
ENGINE IS FOUR STROKE, FOUR STROKE OPPOSING CYLINDERS
TBO 1200 HR - AUTOMOBILE GRADE FUEL
* ROTAX 912 U DA 59,6 kW (81 hp) REDUCTION GEARBOX 1:2,273
* ROTAX 912 S DA 73,5 kW (100 hp) REDUCTION GEARBOX 1:2,428

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