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SECTION 6 CESSNA WEIGHT & BALANCE/EQUIPMENT LIST MODEL 208B G1000 CREW AND PASSENGER LOADING The pilot and front passenger positions in all airplanes have six-way adjustable seats. These seats slide fore and aft on tracks that have adjustment holes for seat position. The Passenger Version has aft passenger seating with two configurations of Commuter Seating. The first Commuter Seating configuration has three individual, fixedposition passenger seats in the left side of the cabin, and three two place fixed-position, bench seats located in the right side of the cabin in a side-by-side arrangement. The second Commuter Seating configuration includes four individual, fixed-position, passenger seats on the left side of the cabin and four individual, fixed-position passenger seats on the right side of the cabin in a side-by-side arrangement. 6-16 U.S. WARNING None of the airplane seats are approved for installation facing aft. 208BPHBUS-00
CESSNA SECTION 6 MODEL 208B G1000 WEIGHT & BALANCE/EQUIPMENT LIST BAGGAGE/CARGO LOADING CABIN CARGO AREA Cargo may be carried in the cabin of either the Cargo Version or the Passenger Version. The cabin interior of the Cargo Version is specifically equipped for the carriage of cargo. However, after seat removal and the installation of miscellaneous equipment, the Passenger Version will also fulfill the requirements of cargo missions. The following paragraphs generally describe the cargo area of both versions. To facilitate the carrying of large or bulky items, all aft seats (Passenger Version Only) and the front passenger seat may be removed from the airplane. If a cargo barrier and its three barrier nets are available for installation, removal of the front passenger seat may not be desired. Mission requirements will dictate whether the barrier is to be used and the number of seats removed. If seats are removed for hauling cargo and the cargo barrier and its nets added, the basic empty weight and C.G. moment of the airplane should be adjusted so that these values accurately represent the weight and moment of the airplane before loading. To calculate the new weight and moment, refer to the airplane equipment list and acquire the weight and C.G. arm of each item of equipment to be removed or added, then record these values on the Sample Weight and Balance Record, to assist in the calculation. For each item of equipment, multiply its weight by its C.G. arm to provide the moment for that item. Subtract weights of removed items (seats) and add weights of installed items (cargo barrier and its nets) to the original basic empty weight to provide a new basic empty weight. Likewise, subtract the moments of removed items and add the moments of installed items to the original moment to provide a new airplane moment. Remember that the moment value is to be divided by 1000 to reduce the number of digits. The new basic empty weight and moment/1000 can be used as illustrated in the Sample Loading Problem when figuring airplane loading with the selected items of equipment removed/installed. 208BPHBUS-00 (Continued Next Page) U.S. 6-17
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CESSNA INTRODUCTION MODEL 208B G100
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CESSNA SECTION 1 MODEL 208B G1000 G
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CESSNA SECTION 2 MODEL 208B G1000 L
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SECTION 3 CESSNA EMERGENCY PROCEDUR
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SECTION 3 CESSNA ABNORMAL PROCEDURE
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CESSNA SECTION 3 MODEL 208B G1000 A
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CESSNA SECTION 4 MODEL 208B G1000 N
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CESSNA SECTION 5 MODEL 208B G1000 P
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SECTION 7 CESSNA AIRPLANE AND SYSTE
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CESSNA SECTION 8 MODEL 208B G1000 H
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