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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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.