Hélicoptères Guimbal
SECTION 2
CABRI G2
LIMITATIONS
2-10
Weight and balance limitations (Imperial units)
Maximum Gross Weight ...................................................................
1543 lb
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
Note :
Rotor axis is ..................................
X = 78.7 in
Y = 0 in
Lateral Balance diagram
75
77
79
81
83
85
Xcg, in
Y
cg,
i
n
-3,1
0,0
3,1
Longitudinal Weight and Balance diagram
1
3
4
5
1000
1100
1200
1300
1400
1500
75
77
79
81
83
85
Fore
Aft
in
lb
78.7
2