EasyManua.ls Logo

Cessna 208B - Page 308

Cessna 208B
488 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
CESSNA SECTION 6
MODEL
2088 (675 SHP) WEIGHT
&
BALANCEIEQUIPMENT LIST
NOTE
CREW
WEIGHT
(POUNDS,
1
2
3
4
5
6
7
8
9
10
20
30
40
50
60
70
80
90
100
200
300
1
The airplane may be configured with left-hand single
=,
commuter seats installed on the right side, and right-hand
single commuter seats installed on the left side. Actual
sea? location should be noted when computing airplane
weight and balance.
To obtain moment for a 170
lb. pilot, add moments shown for
100 lbs. (13.6) and 70 lbs. (9.4) for a total moment
of
23.0.
AND
PILOT/
FRONT
PASS'
SEATS
AND
ARM=135.5
0.1
0.3
0.4
0.5
0.7
0.8
0.9
1.1
1.2
1.4
2.7
4.1
5.4
6.8
8.1
9.4
10.8
12.2
13.6
27.1
40.6
-,
10-PLACE COMMUTER SEATING
F~gure 6-15' We~ght and Moment Tables (Sheet 4 of 10)
-,
1
Revision 23 U.S. 6-47
PASSENGERS (INDIVIDUAL COMMUTER SEATING)
3AND4
ARM=173.9
0.2
0.3
0.5
0.7
0.9
1
.O
1.2
1.4
1.6
1.7
3.5
5.2
7.0
8.7
10.4
12.2
13.9
15.7
17.4
34.8
52.2
EXAMPLE:
AFT PASSENGER
5AND6
ARM=209.9
MOMENT/1000
0.2
0.4
0.6
0.8
1
.O
1.3
1.5
1.7
1.9
2.1
4.2
6.3
8.4
10.5
12.6
14.7
16.8
18.9
21.0
42.0
63.0
SEATS
7AND8
ARM=245.9
0.2
0.5
0.7
1
.O
1.2
1.5
1.7
2.0
2.2
2.5
4.9
7.4
9.8
12.3
14.8
17.2
19.7
22.1
24.6
49.2
73.8
SAND10
ARM=281.9
0.3
0.6
0.6
1.1
1.4
1.7
2.0
2.3
2.5
2.8
5.6
8.5
11.3
14.1
16.9
19.7
22.6
25.4
28.2
56.4
84.6

Table of Contents

Related product manuals