Hélicoptères Guimbal
SECTION 6
CABRI G2
WEIGHT AND BALANCE
Approved under DOA EASA.21J.211
6-5
In Imperial units :
Item
Weight
(lb)
Arm X
(in)
Arm Y
(in)
Mom X
Mom Y
Equipped aircraft
EW
(
1
)
AX
(
1
)
AY
(
1
)
MX
(
1
)
MY
(
1
)
Right
occupant and seat
51.2
12.6
Left
occupant and seat
(
5
)
51.2
-11
Doors
right
(
4
)
49.2
23.6
left
-23.6
Main luggage
compartment
73
12.7
Front luggage
compartment
12.8
0
Fuel (
2
)
(
2
)
(
3
)
(
3
)
Supplements (
6
)
(
6
)
(
6
)
(
6
)
Total
Sum =
GW
MX / GW MY / GW
Sum =
MX
Sum =
MY
(
1
) Report aircraft equipped weight data
(
2
) Use 6.0 lb/gal for AVGAS density, and 6.3 lb/gal for automotive
gasoline density.
(
3
) For fuel position, use :
Fuel Quantity .................................... X ........... Y
0 to 13 U.S. gal ......... ................... 72.2 in -12.3 in
13 to 40 U.S. gal ......... ................... 74.2 in -13.3 in
40 to 45 U.S. gal ......... ................... 74.9 in -13.5 in
(
4
) Use - 6.8 lb (negative weight) when a door is removed
(
5
) Use - 7.7 lb when left seat is removed
(
6
) Refer to Section 9 for removable supplements
For bear paws, Use 1.5 kg and no impact on CG position.
