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(Figures 19-18 and 19-21).
2. Determine the moment index for each
passenger using the Crew and Passenger
Weight and Moment Table (see Figures
19-6 and 19-13). Enter the weight and
moment index for each passenger on the
PAYLOAD COMPUTATIONS side of the
Weight and Balance Computation Form
(Figures 19-18 and 19-21).
3. Determine the moment index for any cabinet
contents using the Baggage and
Cabinet Compartments Standard Weight
and Moment Table (see Figures 19-7 and
19-14). Enter the weight and moment
index on the PAYLOAD COMPUTATIONS
side of the Weight and Balance
Computation Form.
4. Determine the moment index for baggage
loading in the nose, toilet seat, and
tail cone compartments using the
Baggage and Cabinet Compartments
Standard Weight and Moment Table (see
Figures 19-7 and 19-14). Enter the weight
and moment index on the PAYLOAD
COMPUTATIONS side of the Weight
and Balance Computation Form.
5. Total the weights and moment indices of
the payload items at the bottom of the
PAYLOAD COMPUTATIONS side of the
Weight and Balance Computation Form
and enter these values on line 2 PAYLOAD
of the Weight and Balance
Computation Form.
6. Enter the sums of the values on lines 1
and 2 onto line 3 ZERO FUEL WEIGHT
of the Weight and Balance Computation
Form.
7. Divide the zero fuel moment index by
the zero fuel weight and multiply by 100
(1,000) to determine the zero fuel weight
center of gravity.
8. Check the zero fuel weight and center of
gravity by locating the weight and center
of gravity on the Example Center-of
Gravity Limits Envelope Graph (Figures
19-19 and 19-22).
510OM-00 19-21
CITATION MUSTANG OPERATING MANUAL
NOTE
Approved points are located below
the maximum zero fuel weight line.
9. Look up the weight of fuel to be used for
the flight and the corresponding moment
index in the Fuel Loading Table (Figures
19-8 and 19-15). Enter the weight and
moment index on line 4 FUEL LOADING
of the Weight and Balance Computation
Form.
10. Enter the sums of the values on lines 3
and 4 onto line 5 RAMP WEIGHT of the
Weight and Balance Computation Form.
11. Divide the ramp moment index by the ramp
weight and multiply by 100 (1,000) to determine
the ramp weight center of gravity.
12. Check the ramp weight by locating the
weight and center of gravity on the
Example Center of Gravity Limits
Envelope Graph (see Figures 19-19 and
19-22).
NOTE
Approved points are located below
the maximum ramp weight line.
13. Enter the taxi fuel weight and moment
index on line 6 LESS FUEL FOR TAXIING
of the Weight and Balance
Computation Form. A standard 85-pound
(38.56-kilogram) burn-off is assumed.
The moment index for taxi is the difference
between the moment index of the
fuel loaded and the moment index of the
fuel remaining on-board after taxi.
14. Enter the differences between the values
on lines 5 and 6 onto line 7 TAKEOFF
WEIGHT of the Weight and Balance
Computation Form.
15. Divide the takeoff moment index by the
Takeoff Weight and multiply by 100
(1,000) to determine the takeoff center of
gravity. Enter the takeoff center of gravity
on line 7 of the Weight and Balance
Computation Form.
16. Check the takeoff weight by locating the
weight and center of gravity on the
Example Center-of-Gravity Limits
Envelope Graph (see Figures 19-19 and
19-22).
NOTE
Approved points are located inside
the envelope below the maximum
takeoff weight line.
17. Determine the estimated weight of the
fuel to be used in flight. The moment
index of the fuel used in flight is the difference
between the moment index of
the fuel remaining after taxi and the moment
index of the fuel remaining after
reaching the destination.
18. Enter the weight and moment index of the
fuel used in flight on line 8 LESS FUEL
TO DESTINATION of the Weight and
Balance Computation Form.
19. Enter the differences between the values
on lines 7 and 8 onto line 9 LANDING
WEIGHT of the Weight and Balance
Computation Form.
20. Divide the landing moment index by the
landing weight and multiply by 100
(1,000) to determine the landing centerof-
gravity. Enter the landing center-ofgravity
on line 9 of the Weight and
Balance Computation Form.
21. Check the landing weight by locating the
weight and center of gravity on the
Example Center of Gravity Limits
Envelope Graph (see Figures 19-19 and
　
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