September 29th was the last day of certification test flights of 20 m Perkoz, equipped with long wing extensions. The purpose of the tests was to confirm the compliance with requirements of CS-22 regulations for this modified version of SZD-54-2. 21 take-offs and nearly 15 FH have been flown. The tests went smoothly and confirmed all the calculation assumptions made by SZD designers and aerodynamicist.
The glider will get into service in the same manner as the 17.5 m version. The basic flight parameters are as follows:
- VNE - never exceed speed: 240 km/h;
- VRA - rough air speed: 160 km/h;
- VA - manoeuvring speed: 160 km/h;
- VT - max. aerotow speed: 150 km/h;
- VW – max. winch launching speed: 110 km/h;
- manoeuvring load factors: +5,3 / -2.65 g;
- approval for basic aerobatic manoeuvres including half of flick roll & half loop;
- cloud flying.
The test flights have covered the following elements:
- flight on tow as well as winch launching,
- longitudinal, lateral and directional manoeuvreability,
- longitudinal, lateral, directional and dynamic stability,
- stalls and spins in many different configurations of CG location as well as glider loading,
- high speed diving & flutter tests,
- airbrakes tests,
- basic aerobatic.
Our test pilot
stated the glider has passed the exams perfectly. In addition to the
already emphasized advantages (including canopy ergonomy, light and
effective controls, manoeuverability and stability), flutter tests were
finished safely (damping arises immediately, the glider is free of
flutter, aerofoil divergence and control are reversal in each
configuration). Also the results of tests with extended airbrakes while
flying with max. permitted speed were positive. The efficient airbrakes
allow to fly the glider with VNE in a dive at an angle of 50° to the
horizon (the regulations say min. 45°). This is a very good result.
The
spin seems to be abrupt with a relatively significant altitude lost,
however it is possible to stop spinning immediately. Recovery is safe
and easy. The glider does not have the tendency to uncontrollable spin,
stalling behaviour is not unduly sensitive to sideslip, there is also no
tendency to sideslip while turning or changing the spin into a spiral
dive. 20 m Perkoz is highly manoeuverable and easy to control, even
while flying with a minium speed.
The 20 m version is
one of a few configurations of SZD-54-2 Perkoz. In opposite to
relatively heavy and less monouverable foreign designs, our doubleseater
may be used by the pilots on each level of their gliding experience.
Perkoz will meet the expectations of the most demanding and ambitious
aviators.
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Acceleration & control areas deflection sensors |
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Airbrake test at VNE |
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Flutter test hardware (flight data recorder marked as red) |
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Comparison tests with the second 17,5 m Perkoz |
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Comparison tests with the second 17,5 m Perkoz |
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Comparison tests with the second 17,5 m Perkoz |
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Comparison tests with the second 17,5 m Perkoz |
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Comparison tests with the second 17,5 m Perkoz |
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Tests with rear location of CG |
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Zlin 526ML as a towing plane. The cable visible onto glider's fuselage releases immediately the tail ballast |
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Zlin 526ML - the best towing plane in Poland |
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Jak 12M towing Perkoz |
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Zlin 526ML towing Perkoz |
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Winch launch |