Sample Loading Problem - Cessna TR182 1979 Pilot Operating Handbook

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SAMPLE
SAMPLE AIRPLANE YOUR AIRPLAN E
Moment
Moment
LOADING
PROBLEM
Weight (lb.-ins. Weight
(lb.-ins.
(lbs.)
flOOO) (lbs.) /1000)
1.
Basic Empty Weight (Use the date pertaining
to your airplane as it is presently equipped.
It?Z8.S"
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Includes unusable fuel and full oi I) 1850 62.0
2.
Usable Fuel (At 6 Lbs./Gal.)
Standard Tanks (88 Gal. Maximum)
..
Reduced Fuel (65 Gal.) .
.
.
.
. .
.
390 18.1.
szs
?4$
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3. Pilot and Front Passenger(Sta. 32 to 50) . 340
12.6
2ao 7,S
4. Second Row Passengers . 340
25.2
5. 8aggage (Area "A") or Passengeron Child's
Seat (Station 82 to 110) 120 l.bs. Maximum
120 11.6
6. Baggage- Aft (Area "8")
(Station 110 to 134) 80 Lbs. Max:i mum 72 8.7
7.
RAMP WEIGHT AND MOMENT 3112
138.2
2
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8.
Fuel allowance for engine start, ta xi and runup -12 - .6
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9. TAKEOFF WEIGHT AND MOMENT
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(Subtract step 8 from step 7) 3100 137.6
10.
Locate this point (3100 at 137.6) on the Center of Gravity Moment Envelope,
and since this point falls within the envelope, the loading is acceptable.
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Figure 6-5. Sample Loading Problem
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