Hélicoptères Guimbal
CABRI G2
Weight and balance limitations (Imperial units)
Maximum Gross Weight ................................................................... 1543 lb
4
5
75
Fore
Point 1 ...................................................... 1036 lb ................ 83.5 in
Point 2 ...................................................... 1102 lb ................ 83.5 in
Point 3 ...................................................... 1543 lb ................ 79.7 in
Point 4 ...................................................... 1543 lb ................ 75.4 in
Point 5 ...................................................... 1213 lb ................ 75.4 in
75
Note : Rotor axis is .................................. X = 78.7 in
2-10
Longitudinal Weight and Balance diagram
lb
1500
1400
1300
1200
1100
1000
77
79
78.7
Lateral Balance diagram
3,1
0,0
-3,1
77
79
Xcg, in
EASA Approved
3
81
81
SECTION 2
LIMITATIONS
2
1
83
85
in
Aft
83
85
Y = 0 in
Issue 10
Original issue
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