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SECTION 6 CESSNA<br />

WEIGHT & BALANCE/EQUIPMENT LIST MODEL 208B G1000<br />

CABIN CARGO AREA (Continued)<br />

With all seats except the pilot’s seat removed, a large cabin volume is<br />

available for baggage/cargo. If a cargo barrier is installed, the total<br />

volume available for cargo behind the barrier is 340 cubic feet. Cargo<br />

can be loaded through the large, almost square, two-piece cargo door.<br />

The floor is flat from the firewall at Fuselage Station 100.0, except in the<br />

rudder pedal area, to the aft side of the cargo door (Fuselage Station<br />

332.0), and has a 200 pound per square foot allowable loading.<br />

Strategically located nutplates are provided which will allow the<br />

installation of plywood flooring (standard equipment on Cargo Versions)<br />

for ease of loading and distribution of concentrated loads. Between<br />

Fuselage Stations 332.0 and 356.0, additional cargo space with a<br />

capacity of 320 pounds is provided on a floorboard raised<br />

approximately five inches above the main floorboard.<br />

In the area of the removed front passenger seat, “I” section seat tracks<br />

are installed from Fuselage Station 125.00 to 159.98, and tie-down<br />

block assemblies which clamp to the tracks can be installed to serve as<br />

tie-down attach points. From Fuselage Station 158.00 aft to the raised<br />

baggage/cargo floor, seat tracks are provided and are designed to<br />

receive quick-release tie-down fittings which can be snapped into the<br />

tracks at intervals of 1 inch. The raised baggage/cargo floor contains<br />

eight anchor plates to which quick-release tie-down fittings can be<br />

attached. If rope, cable or other fittings are used for tie-downs, they<br />

should be rated at a minimum of 2100 pounds when used with all<br />

fittings noted in the table on the Cargo Tie-Down Attachments figure,<br />

except the double-stud quick-release tie-downs which require a 3150<br />

pound rating. Maximum allowable cargo loads will be determined by<br />

the individual zone weight limitation and by the airplane weight and<br />

C.G. limitations. The number of tie-downs required is dependent on the<br />

load(s) to be secured. The Cargo Tie-Down Attachments figure, shows<br />

the maximum allowable cargo weight for each type of cargo tie-down<br />

attachment.<br />

On Cargo Versions, the sidewalls in the cargo area are marked with<br />

vertical lines to facilitate the identification of six loading zones.<br />

Markings located on the sidewalls between the lines identify each zone<br />

by number and display the maximum load which can be carried within<br />

the zones. Refer to Cabin Internal Load Markings (Cargo Version)<br />

figure for maximum zone weight limits.<br />

6-18<br />

U.S.<br />

(Continued Next Page)<br />

208BPHBUS-00

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