Cessna SKYLANE RG R182 Pilot Operating Handbook page 101

SAMPLE
SAMPLE AIRPLANE YOUR AIRPLANE
Moment
Moment
LOADING PROBLEM
Weight (lb.-ins. Weight
(lb.-ins.
(Ibs.)
/1000)
(Ibs.) /1000)
1. Basic Empty Weight (Use the data pertaining
~B
w (z.-Jo:»
to your airplane as it is presently equipped.
1872- .\S
btf,C;~S.1
Includes unusable fuel and full oil) 1808 62.0
2.
Usable Fuel (At 6 Lbs.lGal.)
Standard Tanks (56 Gal. Maximum)
Long Range Tanks (75 Gal. Maximum)
450 21.6
3.
Pilot and Front Passenger (Sta. 32 to 50) 340 12.6
4. Second Row Passengers 340
25.2
5. Baggage (Area "A") or Passenger on Child's
Seat (Station 82 to 110) 120 Lbs. Maximum
120 11.6
6.
Baggage - Aft (Area "B")
(Station 110 to 134) 80 Lbs. Maximum 54
6.5
7.
RAMP WEIGHT AND MOMENT 3112 139.5
8. Fuel allowance for engine start, taxi and runup
- 12 - .6
"_.
~ _ . ~ , -
_._---..
9. TAKEOFF WEIGHT AND MOMENT
(Subtract step 8 from step 7) 3100 138.9
10.
Locate this point (3100 at 138.9) on the Center of Gravity Moment Envelope,
and since this point falls within the envelope, the loading is acceptable.
Figure 6-5. Sample Loading Problem