Cessna TU206G STATIONAIR, Pilot Operating Handbook

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SOLOY TURBINE PAC SECTION 6
POHS CESSNA U/TU 206G WEIGHT & BALANCE/
EQUIPMENT LIST
6
-4
F.A.A. Approved October 4, 2005
SAMPLE
LOADING PROBLEM
SAMPLE AIRPLANE YOUR AIRPLANE
WEIGHT
(LBS.)
MOMENT
(LB.-INS.
/1,000)
WEIGHT
(LBS.) MOMENT
(LB.-INS.
/1,000)
1. Basic empty weight
(includes unusable fuel
and full oil)
2079 73.2
2. Usable fuel (at 6.7
lbs./gal.) (76 gal. max)
(Sta. 46.0)
509 23.4
3. Pilot and co-pilot (Sta. 32
to 43)
340 12.6
4. Center Passengers:
Standard Seating (Sta. 69
to 79)
Club Seating (Sta. 63 to
74)
Aft Passengers
Standard Seating (Sta. 94
to 100)
Club Seating (Sta. 98 to
109)
Baggage IV or V (Sta. 109
to 145)
340 23.8
340 34.0
5. *Cargo “A” (Sta. 10 to 50)
*Cargo “B” (sta. 50 to 84)
*Cargo “C” (Sta. 84 to 109)
*Cargo “D” (Sta. 109 to
145)
6. RAMP WEIGHT AND
MOMENT
3604 167
7. Fuel allowance for engine
start, taxi and run-up
-4 -.2
8. TAKEOFF WEIGHT &
MOMENT
3600 166.8
9. Locate this point on the Center of Gravity Moment Envelope.
*Maximum allowable loads will be determined by the number of tie-downs
used, as well as floor loading limits of 200 lbs. per square foot.
Figure 6-7. Sample Loading Problem (Sheet 1 of 2)
(For Aircraft S/Ns: U20603522 thru U20604649)
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