TM 1-1510-223-10
Table 6-1.
Occupants - Useful Loads, Weights, and Moments
WEIGHT
CREW
LAVATORY
F.S. 129
F.S. 292
Moment/100
80
103
234
90
116
263
100
129
292
110
142
321
120
155
350
130
168
380
140
181
409
150
194
438
160
206
467
170
219
496
180
232
526
190
245
555
200
258
584
210
271
613
220
284
642
230
297
672
240
310
701
250
323
730
BT03867
Table 6-2.
Survivability Equipment - Weights and Moments
ITEM
WEIGHT
MOM/100
NACELLE DISPENSER (F.S. 214.7)
Chaff Cartridges (30)
10
21
FUSELAGE DISPENSER (F.S. 288.6)
Chaff Cartridges (30)
10
29
Flare Cartridges (30)
13
37
BT03866
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.
6-10. FUEL AND OIL DATA
a.
Usable Fuel Moment Tables. These tables
(Table 6-3 and 6-4) show usable fuel moment/100 for
US gallons (or pounds) of JP-4, JP-5 and JP-8.
b.
Oil Data. Total oil weight is 52 pounds and is
included in the basic weight of the aircraft
6-3
