Taurus ELECTRO manual 472 ENG.pdf - Pipistrel
Taurus ELECTRO manual 472 ENG.pdf - Pipistrel
Taurus ELECTRO manual 472 ENG.pdf - Pipistrel
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66 TAURUS <strong>ELECTRO</strong> www.pipistrel.si<br />
Aircraft and systems on board<br />
REV. 0<br />
Seats and safety belts<br />
Seats have no stiff internal structure and do not offer different settings. All <strong>Taurus</strong> ultralight<br />
motorgliders ship with H type safety belt attached to the fuselage at three mounting points.<br />
Pitot-Static lines<br />
The pitot tube is inside the nose-tip. Pitot lines made of plastic materials lead from there to the instrument<br />
panel and are secured from non-intentional damage. Static ports are located on both sides<br />
of the nose below the middle line and are marked with red circles. Static lines are led from the static<br />
ports to the instrument panel, are of composite materials and secured.<br />
Air brakes (spoilers)<br />
Spoilers are most commonly used to increase drag and steepen the final approach.<br />
During takeoff, climb and cruise spoilers MUST be retracted and locked (handle in cockpit in full<br />
forward position). To unlock and extend spoilers, pull the handle upwards.<br />
Flap settings<br />
<strong>Taurus</strong> Electro is equipped with flaperons which offer five (5) different flap settings. Apart from the<br />
limitations for extesion of +9° and +18° flaps, there are recommendations for the use of flaps with<br />
different speed-ranges and types of flight operation.<br />
Recommended speed ranges for certain flap settings in when gliding:<br />
flaps in negative position; -5° (up):<br />
flaps in neutral position; 0° (neutral):<br />
flaps in 1 st position; +5° (down):<br />
flaps in T position; +9° (down):<br />
flaps in L position: +18° (down):<br />
faster than 150 km/h km/h (80 kts)<br />
120 - 150 km/h (65 - 80 kts)<br />
90 - 120 km/h (50 - 65 kts)<br />
80 - 90 km/h (43 - 50 kts)<br />
FINAL APPROACH - LANDING<br />
Water ballast reservoir<br />
<strong>Taurus</strong> Electro is equipped with a water ballast reservoir to provide for better control over the aircraft’s<br />
centre of gravity. The reservoir is placed in front-cabin and secured with two (2) fastening<br />
butterfly screws with as the retaining mechanism. The quantity of the reservoir is 9 litres (9 kg). Lever<br />
arm for centre of gravity calculations is -1800 mm. There are placards on the instrument panel indicating<br />
minimum and maximum allowable crew weight with and without (9 kg) water ballast. The<br />
mentioned figures are to be respected at all times!<br />
WARNING! Check the water balance reservoir in front-cabin and verify<br />
crew’s weight before every flight as it may influence the centre of gravity of<br />
aircraft to the point where it is no longer controlLable!