Pilot’s Operating Handbook Section 6
EXTRA 500 Weight and Balance and Equipment List
4 Determine weight(s) and moment(s) of passenger(s) and
baggage from the applicable columns of Figure 6-5
(130 kg/510.9 kgm; 50 kg/252.5 kgm; 12 kg/69 kgm).
5 Total items 1 and 2 thru 6 to determine appropriate entries for
item 7 (zero fuel weight) (1783 kg/6407.64 kgm).
6 Determine the values for item 8a (fuel loading main
compartment) from the applicable columns of Figure 6-6a
(293 kg/1104 kgm).
7 Determine the values for item 8b (fuel loading auxiliary
compartment) if applicable from columns of Figure 6-6b
(0 kg/0 kgm).
8 Total items 7 and 8 to determine item 9 (ramp weight)
(2076 kg/7511.64 kgm). Refer to the weight and moment limits
form (Figure 6-7) to ensure values are not out of limits.
9 Determine the values for item 10 (less fuel for taxiing) from the
applicable columns of Figure 6-6 (7 kg/26.4 kgm).
10 Subtract item 10 from item 9 to determine item 11 (takeoff
weight) (2069 kg/7485.24 kgm). Enter item 11 in the weight
and moment limits from (Figure 6-7) to determine if the loading
is within allowable limits. If the determined point falls outside
of the envelope, it will be necessary to reduce the load or
change location of load.
11 Refer to Section 5 to determine the fuel quantity required for the
flight. After determining the fuel used, obtain the appropriate
weight and moment from Figure 6-6. Enter this weight and
moment in item 12a and b (less fuel to destination)
(195.4 kg/736 kgm).
12 Subtract item 12 from item 11 to determine item 13 (landing
weight) (1873.6 kg/6749.24 kgm). Refer to landing weight and
moment limits form (Figure 6-7) to ensure values are not out of
limits.
26. January 2011 6-7
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