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Taurus ELECTRO manual 472 ENG.pdf - Pipistrel

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56 TAURUS <strong>ELECTRO</strong> www.pipistrel.si<br />

Weight and balance<br />

REV. 0<br />

<strong>Pipistrel</strong> d.o.o.<br />

Ajdovščina<br />

Weight and Balance - <strong>Taurus</strong> 503 Electro<br />

Weighing and C.G. calculation - empty mass<br />

Serial Number<br />

1 date of weighing / 1. example 2. example 3. example<br />

2 acomplished by /<br />

3 date of "Equipment list" /<br />

4 main wheel Lh G 1 Lh kg 123,0 123,4 122,0<br />

5 main wheel Rh G 1 Rh kg 124,4 124,8 123,5<br />

6 main wheel total G 1 kg 247,4 248,2 245,5<br />

7 tail wheel G 2 kg 49,6 48,8 47,5<br />

8 distance a mm 22 24 23<br />

9 distance b mm 4402 4406 4400<br />

Registration<br />

10 empty mass =(6+7) G empty kg 297,0 297,0 293,0<br />

11 empty mass C.G. X CG.empty mm 713 700 690<br />

12<br />

max cockpit load without w.ballast<br />

(from "Empty mass c.g. limits" diagram)<br />

kg 180,0 175,5 169,0<br />

a<br />

Xcg<br />

Component<br />

mass<br />

Lh wing<br />

incl.flaperon<br />

Rh wing<br />

incl.flaperon<br />

Fuselage -<br />

complete<br />

kg kg kg kg<br />

Horiz. tail<br />

b<br />

Empty mass<br />

Empty mass is with equipment and accesories per equipment list, and without occupants, fuel, baggage and water ballast.<br />

X CG.empty = (G 2 .b)/G empty - a<br />

Useful load distribution<br />

13 max mass<br />

kg <strong>472</strong>,5 <strong>472</strong>,5 <strong>472</strong>,5 <strong>472</strong>,5 <strong>472</strong>,5 <strong>472</strong>,5 <strong>472</strong>, 5<br />

14 max useful load = (13-10) kg 175,5 175,5 179,5<br />

550 kg 550 kg 550 kg 550 kg 550 kg 550 kg 550 kg<br />

15<br />

max cockpit load without w.ballast<br />

(declared, see Notes)<br />

16<br />

min cockpit load without w.ballast<br />

(from "Empty mass c.g. limits" diagram)<br />

kg<br />

175,5<br />

less fuel<br />

less bagage<br />

175,5<br />

less fuel<br />

less bagage<br />

169,0<br />

kg 86,0 82,0 78,0<br />

17 Inspector signature & stamp /<br />

Notes: ● Declared max cockpit load without water ballast is: 14 - fuel - baggage, if 14 is less than, or equal to, 12.<br />

12, if 14 is more than 12.<br />

● Water ballast is installed for solo flight with lightweight pilot for not to exceed aft c.g. limit.<br />

Min cockpit load may be reduced for 2,3 kg per each litre of water ballast.<br />

● If water ballast is left in the tank for duo flight, max cockpit load must be reduced for 2,3kg per each litre of water ballast.<br />

● Influence of fuel and baggage on aircraft c.g. (and corresponding cockpit load) is neglectable.<br />

● Max mass of single occupant (due to structural load per seat) is 110kg.<br />

● Fuel [kg] = 0,76 kg/litre × litres.

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