25
Seat 3
170
37.7
Seat 4
160
35.5
Seat 5
190
50.5
Seat 6
110
29.3
Baggage
Nose 60
4.4
Tail cone
110
50.8
Zero fuel weight
9716
3017.2
+ Fuel
5424
1644.1
= Ramp weight
15,140
4661.3
— Taxi fuel
-200
-61.8
= Takeoff gross weight
14,940
4599.5
— En Route fuel
-2000
-612.9
= Landing weight
12940
3986.6
C G = 3 0 8 . 0 8
I N P U T
O U T P U T
% M A C (use CG from WT/MOM problem)
L E M A C 2 8 5 . 6
C G 3 0 8 . 0 8
% M A C
2 7 . 8
M A C 8 1 . 0
APPENDIX A (cont.)
SAMPLE PROBLEMS
I N P U T
O U T P U T
P - D / A L T
I A L T 1 0 0 0 0
P A L T 9 9 2 0
B A R O
3 0 . 0 0
D A L T 1 1 0 2 0
T ° C 5
P L A N T A S
P A L T 1 2 0 0 0
T A S 2 3 7 . 7
T ° C 2
M A C H #
0 . 3 7
C A S 1 9 5
D A L T
1 3 2 2 6
H D G / G S
W D I R
2 7 0
W S P D
2 0
G S
1 9 2 . 2
C R S
3 5 5
H D G
3 4 9 . 1
T A S 1 9 5
L E G T I M E
D I S T
2 5
T I M E
0 0 : 0 7 : 4 2
G S 1 9 5
F U E L R E Q
T I M E 0 2 : 4 5 : 0 0
F U E L
3 8 . 5
F P H 1 4
X / H - W I N D
W D I R
2 7 0
X - W I N D
1 0 -
W S P D
2 0
H - W I N D
1 7 . 3 -
R W Y 3 0