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