Schweizer 2-33 - Page 18

A-CR-CCP-402/MB-001 SCHWEIZER 2-33 AOIs
2-6
Figure 2-6 Sample 2-33 Loading Graph for a 1040 lb gross weight glider
Figure 2-7 Sample Cockpit Placards for a 1040 lbs gross weight glider
0
50
100
150
200
250
300
350
0
50 100 150 200 250 300 350
400
1. Project horizontal line at front seat load.
2. Project vertical line at rear seat load.
3. If intersection of the lines is within the
envelope, the C.G. is within limits.
4. Gross weight must not exceed 1040 lbs.
5. Solo flight from front seat only.
No Ballast
Ballast
Forward C of G Limit
Rear C of G Limit
Max Weight Limit
C-FQON
Lbs.
Rear Seat Load
Front Seat Load
Kg.
Kg.
0
20
40
60
80
100
120
140
160
0 20 40 60
80 100 120 140 160
180
1. Project horizontal line at front seat load.
2. Project vertical line at rear seat load.
3. If intersection of the lines is within the
envelope, the C.G. is within limits.
4. Gross weight must not exceed 1040 lbs.
5. Solo flight from front seat only.