Diamond DA 40, Flight Manual

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DA 40 AFM Mass & Balance
Doc. # 6.01.01-E Rev. 8 01-Dec-2010 Page 6 - 13
1200 kg / 2646 lb
MÄM 40-227 carried out
1150 kg / 2535 lb
Normal
980 kg / 2161 lb
Utility & Normal
780 kg / 1720 lb
Sta
n
da
rd
T
a
nk
O
n
ly
94 96 98 100 102
2700
2500
CG pos. [in]
2300
2100
1900
1700
F
lig
ht Mas
s
[
lb]
1200
1150
1100
1050
1000
950
900
850
800
750
F
light
Ma
s
s
[
k
g]
CG pos. [m]
2.40 2.45 2.50 2.55 2.60
6.4.4 PERMISSIBLE CENTER OF GRAVITY RANGE
%
%
%
%
%
%
%
%
%
%
%
%
%
The CG’s shown in the diagram are those that from the example in Table 6.4.3 -
CALCULATION OF LOADING CONDITION.
Forward Flight CG Limit:
2.40 m (94.5 in) aft of Datum Plane at 780 to 980 kg (1720 to 2161 lb)
2.46 m (96.9 in) aft of Datum Plane at 1150 kg (2535 lb)
linear variation between these values
If MÄM 40-227 is carried out:
%
2.40 m (94.5 in) aft of Datum Plane at 780 kg to 980 kg (1720 lb to 2161 lb)
%
2.48 m (97.6 in) aft of Datum Plane at 1200 kg (2646 lb) %
linear variation between these values %