2467.
WT
76.7
ARM
(FLASHING) MOM
189218.
76.7
(FLASHING) CG
R F
1.
2467.
(FLASHING) GW
After keying in the airplane's empty weight and arm, the
next step is to calculate the weight and balance for the
aircraft at takeoff. For this example, we'll assume the
following load:
Item
Weight
Arm
Fuel
72.5 gal (6 lbs./gal.)
75
Front passengers
340
75
Rear passengers
340
115
Baggage
18
164
With above display showing, press
ENTER
32
Key in
7 2 . 5
X
6
=
;
W T
will display
4 3 5
Press
ENTER
; Key in
A R M
of
7 5 ;
Press
ENTER
New totals will appear for MOM, CG and GW. The
passengers can be added onto the total in the same
manner the fuel was added above. RF will remain the
same throughout the problem; therefore, you will only be
prompted once for the RF. The final calculations can be
used to confirm that the weight and CG are within the
airplane's operating limitations.
WEIGHT AND ARM (cont.)
(WT/ARM)
