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Section 6 Pilot’s Operating Handbook
Weight and Balance and Equipment List EXTRA 500
6000
6250
6500
7000
6750
MAC
15% 20% 25% 30% 35% 40%
Weight and Moment Limits (U.S. units)
CG Location is 142.4 in. aft of Reference Datum
Example: At 4578 lbs and a Moment of 6521 in.lbs./100
lbs
in.lbs/100
in. aft of ref. datum
3100
3200
3300
3400
3500
3600
3700
3800
3900
4000
4100
4200
4300
4400
4500
4600
4700
4800
134 136 138 140 142 144 146 148
Maximum
Landing Weight
Maximum Ramp
and Takeoff Weight
4750
5000
5250
5750
5500
4250
4500
Figure 6-7
Weight and Moment Limits (Sheet 2 of 2)
6-22 04. May 2004

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