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Doc. No. 6.01.05-E Revision 2 30-Apr-2003 Page 6 - 10
% 6.4.4 PERMISSIBLE CENTER OF GRAVITY RANGE % a) Standard tank
Center of Gravity Position [in]
94 96 98 100 102
2600
1150
1150 kg / 2535 lb
1100
2400
Normal
1050
Flight Mass [lb]
Flight Mass [kg]
2200
1000
980 kg / 2161 lb
950
2000
900
Utility & Normal
850
CG
1800
800
Envelope
780 kg / 1720 lb
750
2.40 2.45 2.50 2.55 2.60 Center of Gravity Position [m]
% The CG shown in the diagram is that from the example in Table 6.4.3 (a) 'CALCULATION OF LOADING CONDITION', row 7 (pre take-off condition).
The flight CG position must be within the following limits:
Most forward flight CG:
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
Most rearward flight CG:
2.59 m (102.0 in) aft of Datum Plane
%
Doc. No. 6.01.05-E Revision 2 30-Apr-2003 Page 6 - 11
% b) Long Range Tank
% Center of Gravity Position [in]
% 94 96 98 100 101
2600
%
% 1150
2200
1150 kg / 2535 lb
% 1100
2400
1000
Flight Mass [lb]
Flight Mass [kg]
Normal
%
%
%
%
%
%
1050
980 kg / 2161 lb
950
2000
900
Utility & Normal
% 850
CG
% % % 750 800 780 kg / 1720 lb 1800 Envelope
% 2.40 2.45 2.50 2.55
% Center of Gravity Position [m]
%
% The CG shown in the diagram is that from the example in Table 6.4.3 (b) 'CALCULATION
% OF LOADING CONDITION', row 7 (pre take-off condition).
% The flight CG position must be within the following limits:
% Most forward flight CG:
% 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
% Most rearward flight CG:
% 2.55 m (100.4 in) aft of Datum Plane
%
Doc. No. 6.01.05-E Revision 2 30-Apr-2003 Page 6 - 12
" .4"
005m/1
FLIGHT MASS (WEIGHT) [lb]
2550
2500 2400 2300 2200
2100 2000 1900
1800 1700
%
%
%
%
%
%
%
%
%
%
%
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本文链接地址：钻石40飞机飞行手册 DA 40 Airplane Flight Manual(50)
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