Maintenance Manual STEMME S10-VT
Date of Issue: Jan. 01, 1998
Page 6-4
Amendment Nr. 0
Date: --
A4011121_B23.doc
Doc. No. A40-11-121
Foremost and Rearmost CG Empty vs. Empty Weight
foremost CG empty
Rearmost CG empty,
Minimum Cockpit Load:
70 kg / 155 lbs
75 kg / 165 lbs
80 kg / 176 lbs
85 kg / 187 lbs
90 kg / 198 lbs
480
490
500
510
520
530
540
550
560
635
640
645
650
655
660
665
670
675
680
685
690
Empty Weight [kg]
A
llo
w
a
b
le
C
G
e
m
p
ty
a
ft
o
f
D
a
tu
m
[
m
m
]
Nose heavy CG range
tail heavy CG range
allowable CG range
Fig. 6.3.b: Range of Empty Weight CG as a Function of Empty Weight and Minimum Load
WARNING:
The additional battery has a major effect on the aircraft CG. The Equipment List and the Weight
and Balance Report must correspond with the a/c with regard to the additional battery, otherwise
the airworthiness expires due to an undocumented CG. Installation or removal of the additional
battery requires correction of the Equipment List and an update of the Weight and Balance Report
before return to service.
