NORMAL LONGITUDINAL CENTER OF GRAVITY LIMITS

CHAPTER 7 PERFORMANCE DATA FOR AH-64A HELICOPTERS EQUIPPED WITH T-700-GE-701 ENGINES

TM-1-1520-238-10 Helicopter Attack AH-64A Apache Manual
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TM 1-1520-238-10 6-18 Change 3 G.W. = 15,400 LBS MOMENT/100 = 31,000 M01-208-1A ARM-INCHES NORMAL LONGITUDINAL CENTER OF GRAVITY LIMITS C.G. 201.5 MOVE DOWN READ MOVE RIGHT TO MOMENT (31,000) WEIGHT HERE ENTER GROSS METHOD KNOWN POSITION AND FIND C.G. ARE EXCEEDED LOADING LIMITS DETERMINE IF WANTED EXAMPLE 203.3 READ ARM HERE 24,000 25,000 26,000 27,000 28,000 29,000 30,000 31,000 32,000 33,000 34,000 35,000 36,000 37,000 38,000 39,000 40,000 41,000 41,500 205 204 15,000 16,000 17,000 18,000 19,000 202.2 20,000 21,000 13,000 14,000 203 202 201 12,000 42,500 42,000 206 207 43,000 SHADED AREA REPRESENTS OUT OF CG LIMITS NOTE MAXIMUM GROSS WEIGHT - Figure 6-3. Center of Gravity Limits

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