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SAMPLE PROBLEM
Sample Aircraft
l
Your Aircraft
Weight
Moment
:weight
Moment
(lbs)
(lb-ins)· (lbs)
(lb-ins)
1. Licensed Empty Weight
(Sample Problem)
3471. 5
122.3
2. Oil
*( 24 Qts x
1.
875 lb/qt)
49.0
-0.2
49.0
-0.2
3. Pilot and Passengers
:
Seats 1 and 2
340.0
12.6
Seats 3 and 4 (Standard)
Seats 3 and 4 (Optional)
340.0
23.1
Seats 5 and 6
340.0
33.3
_i
4. Fuel (gals x 6 lbs/gal)
Main Tanks (100 gals)
600.0
21.0
Aux. Tanks (30 gals)
179.5
8.4
Wing Locker Tanks
(0 gals)
5. Baggage
Nose
40.0
-1.2
(Station 96.0)
..
(Station 124.0)
140.0
17.4
(Wing Lockers)
__
;
6. Total Aircraft Weight
(Loaded)
5500.0
236.7
7. Locate this point (5500 at 236.7) on Figure 4-3 and
since this point falls within the envelope, the loading
is acceptable.
*Note: Normally full oil may be assumed for all flights.
Figure 4-1
4-6
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