Equipment List / Weight And Balance; Weight And Centre Of Gravity Limits Charts - Skyleader 200 Pilot Operating Handbook

6.

EQUIPMENT LIST / WEIGHT AND BALANCE

6.1.

Weight and Centre of Gravity Limits charts

An example of how to use the Weight and Centre of Gravity Limits chart.
C-G position (%MAC)=
W =W +W
M MR ML
EW=W =W +W -F
EPT N M
F=Litr*0,75
• EW=W - Empty weight (kg) = W
EPT
• W - Main undercarriage weight (W
M
• W - Right main undercarriage weight (kg)
MR
• W - Left main undercarriage weight (kg)
ML
• P - Pilots weight (kg)
• F - Fuel weight (Litr * 0,75= kg) (kg)
• B - Baggage weight (kg)
• X - Arm main undercarriage (mm)
M
• X - Arm nose undercarriage (mm)
N
• X - Arm fuel (330 mm )
FUEL
• X - Center of gravity leading edge (mm)
CGLE
• X - Leading enge mean aerodynamic chord (74,7 mm)
LEMAC
• MAC - Mean aerodynamic chord (1274 mm)
• C-G position(%NAC) - Centre of gravity (%)
(
(EW*X + (P*500) + (F*330) + (B*1150)
CGLE)
(EW + P + F + B)
(kg)
(kg)
(kg)
Empty weight
Centre of gravity position(Empty)
Centre of gravity leading edge (X
+W
N M
Max. takeoff weight
=W +W ) (kg)
M MR ML
Max. baggage weight
Min. pilot weight
Max. pilot weight
Front limit of C-G position
Rear limit of C-G position
2 333 371 B
)
-74,7 * 0,0785
305,5 kg
28,1 % MAC
) 432,9 mm
CGLE
472,5 kg
30 kg
60 kg
120 kg
20% MAC
35% MAC
KP 2U POH 05/2022
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