Section 6 Pilot’s Operating Handbook
Weight and Balance and Equipment List EXTRA 500
1400
1500
1550
1600
1650
1700
1750
1800
1850
1900
1950
2000
2050
2100
2150
6000
6250
6500
7000
7
2
5
0
7
5
0
0
7
7
5
0
8
0
0
0
6750
5000
MAC
15% 20% 25% 30% 35% 40%
Weight and Moment Limits (SI units)
CG Location is 3.618 m aft of Reference Datum
Example: At 2076 kg and a Moment of 7511.64 kgm
kg
k
g
m
m aft of ref. datum
3.4 3.45 3.5 3.55 3.6 3.65 3.7 3.75
1450
Maximum
Landing Weight
Maximum Ramp
and Takeoff Weight
5250
5500
5750
Figure 6-7
Weight and Moment Limits (Sheet 1 of 2)
04. May 2004 6-21