TM 1-1520-238-23
G-22
Change 6
G.2.
LOADING INFORMATION
G.2.5. Weight And Balance Characteristics
Maximum mission Gross Weight
(without auxiliary fuel tanks)
21,000 lb.
Allowable Extended Range Gross Weight
(with auxiliary fuel tanks)
21,000 lb.
Minimum Flying Weight (typical)
11,500 lb.
Fuel Capacity
Main Tanks
376.0 gal.
(JP4)
2,444.0 lb.
(JP5/JP8)
2,538.0 lb.
unusable fuel
1.9 gal.
(JP4)
12.4 lb.
(JP5/JP8)
12.9 lb.
Auxiliary Tanks
920.0 gal.
(JP4)
5,980.0 lb.
(JP5/JP8)
6,210.0 lb.
unusable fuel
2.7 gal.
(JP4)
17.6 lb.
(JP5/JP8)
18.4 lb.
Longitudinal Reference Datum
35.5 inches forward of the most forward frame assembly (Fig. G-5)
Utility Storage Compartments
L.H. Aft Storage Compartments
Max.
60 lb. @ 15 lb/ft2
Balance Arm Stations (Fuselage Station)
295.0 (Fig. G-5)
L.H. Survival Kit Bay
Max.
100 lb @ 15 lb/ft2
Balance Arm Stations (Fuselage Station)
325.0 (Fig. G-5)
G.2.6. Center of Gravity Limits
WARNING
Aft C.G. Limits can be exceeded when using the aft storage bays.
NOTE
For the AH-64A helicopter, ARM and fuselage station (F.S.) are the same.
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