TM 1-1510-225-10
6-6
Table 6-3. Useful Load Weights and Moments Cargo
CABIN
F.S. 152-188
F.S. 188-248
F.S. 248-305
F.S. 305-348
CENTROID
F.S. 170
F.S. 218
F.S. 276
F.S. 325
WEIGHT
MOMENT/100NT/100
10
17
22
28
33
20
34
44
55
65
30
51
65
83
98
40
68
87
110
130
50
85
109
138
163
60
102
131
166
195
70
119
153
193
228
80
136
174
221
260
90
153
196
248
293
100
170
218
276
325
200
340
436
552
650
300
510
654
828
975
400
680
872
1104
1300
500
850
1090
1380
1625
510
867
1112
1408
1658
550
935
1199
1518
1788
600
1020
1308
1656
700
1190
1526
1932
800
1360
1744
2208
900
1962
2484
1000
2180
2760
1100
2398
3036
1200
2616
3312
1300
2834
3588
1370
3781
NOTE: All cargo must be supported by the seat tracks in a uniform distribution and tied down to the tracks by an
approved method.
Section III. FUEL/OIL
6-9. FUEL LOAD.
Fuel loading imposes a restriction on the amount
of load which can be carried. The required fuel must
first be determined, then that weight subtracted from
the total weight of crew and fuel. Weight up to and
including the remaining allowable capacity can be
subtracted directly from the weight of crew and fuel.
As the fuel load is increased, the loading capacity is
reduced. Figure 6-2 depicts the density variation of
aviation fuel.