TM 1-1520-238-23
Change 8
G-23
G.2.
LOADING INFORMATION
FORWARD – The normal forward C.G. limit is at fuselage station (F.S.) 201.0 inches to 19,400 pounds and a straight
line taper from 201.0 to 202.2 inches from 19,400 to 21,000 pounds.
AFT – The normal aft C.G. limit is at fuselage station (F.S.) 207.0 inches to 14,660 pounds, and a straight line taper
from 207.0 to 203.3 inches from 14,600 to 20,600 pounds.
All flight C.G.’s must remain within these limits. C.G. limit tables are found in table G-10 and a takeoff and landing
longitudinal C.G. limit envelope is found in figure G-8, page G-33.
G.2.7. Weight/Balance and Loading
GENERAL
AH-64A crew member provisions consist of the Pilot and Co-pilot/gunner (CPG) located in the cockpit.
PERSONNEL MOMENTS
Always try to use the exact weight of each crewmember including all equipment and any personal items stored in the
crew station (cockpit). If weighing facilities are not available, then use the best estimate available. Table G-1
presents the crew C.G. with the seat in its nominal location.
Table G-1.
Crew Member Weights
Crew Member
Co-pilot Station
Pilot Station
Weight Including
Equipment (lb)
Nominal
Arm (in)
Moment
(in-lb/100)
Nominal
Arm (in)
Moment
(in-lb/100)
130
82.2
107
143.3
186
140
82.2
115
143.3
201
150
82.2
123
143.3
215
160
82.2
132
143.3
229
170
82.2
140
143.3
244
180
82.2
148
143.3
258
190
82.2
156
143.3
272
200
82.2
164
143.3
287
210
82.2
173
143.3
301
220
82.2
181
143.3
315
230
82.2
189
143.3
330
240
82.2
197
143.3
344
250
82.2
206
143.3
358
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