Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 118

SECTION 6
CESSNA
MODELT210M
WEIGHT & BALANCE/
EQUIPMENT LIST
SAMPLE
,<nl
'tM
YOUR
SAMPLE
AIRPLANE
AIRPLANE
LOADING PROBLEM
Moment Moment
Weight
(lb.-ins.
Weight
(lb.-ins.
(lbs.)
/1000)
(lbs.)
/1000)
1. Basic Empty Weight (Use the data pertaining
to your airplane as it is presently equipped.
Includes unusable fuel and full oil)
2342
99.6
::!.4.£1.9
lV!31
2. Usable Fuel (At 6 Lbs./Gal.)
Standard Tanks (89 Gal. Maximum)
Reduced Fuel (64 Gal.)
384 16.5
3. Pilot and Front Passenger (Station 34 to 46)
340 12.6
4. Center Passengers (Station 61 to 77) 340 24.1
5. Aft Passengers .
340 34.3
6. Baggage - Forward of wheel well on folded down
aft seat (Station 89 to 110) (120 lbs. max.)
7. Baggage - On and aft of wheel well
(Station 110 to 152) (120 lbs. max.). 70 9.7
8. RAMP WEIGHT AND MOMENT 3816 196.8
9. Fuel allowance for engine start, taxi and runup
-16 - .7
10. TAKEOFF WEIGHT AND MOMENT
(Subtract step 9 from step 8)
3800
196.1
11. Locate this point (3800 at 196.1) on the Center of Gravity Moment Envelope. Since
this loading falls within the shaded area of the moment envelo[Je, [Jroceed with steps
12, 13 and 14. If the computed loading point falls within the clear area of the moment
envelope, no further steps are required and the loading is assumed satisfactory for take-
off and landing.
12. Estimated Fuel Burn-Off (Climb and Cruise)
(38 gallons at 6 lbs./gal.)
-228 -9.8
13. Subtract step 12 from step 10 for estimated
airplane landing weight 3572 186.3
14. Locate this point (3572 at 186.3) on the Center of Gravity Moment Envelope. Since
this point falls within the overall envelope, the loading may be assumed acceptable
for landing.
Figure 6-5. Sample Loading Problem
6-10