Cessna 206H - Page 134

SOLOY TURBINE PAC SECTION 6
POHS CESSNA T206H/206H WEIGHT & BALANCE/
EQUIPMENT LIST
6-4
F.A.A. Approved May 23, 2003
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)
2019
76.4
2. Usable fuel (at 6.7
lbs./gal.) (88/87 gal. max)
(Sta. 48.0)
589.6
28.3
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
170
17.0
157.4
15.4
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
3616
173.5
7. Fuel allowance for engine
start, taxi and run-up
-16
-0.8
8. TAKEOFF WEIGHT &
MOMENT
3600
172.7
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
UNCONTROLLED
COPY