DG Flugzeugbau LS8-sb Wartungshandbuch - Seite 10
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Seite drucken5.2 Calculation of Loading Limits (continued)
Example for entry in Flight Manual section 6.2:
Wing span
Empty Mass
C.G. position
Max. Cockpit Load
with tail-
battery
without tail-
battery
Perm.
fixed Trim
mass
Batteries
installed
Date / Inspector
The discrepancy between Maximum Cockpit Load of 110 kg <242 lbs> and
Minimum Cockpit Load of 140 kg <309 lbs> (for LS8-sb) with tail fin tank
full and tail fin battery indicates, that before each take off the installation
position of the tail fin battery must be checked and a functional check for
the tail fin tank valve is required to make sure that no unintended amount
of water remains in the fin tank.
To check the valve place tail tank filling adapter into the tank outlet and
open the cockpit lever. If air cannot be blown into the tank, the valve is not
functioning properly (for instance frozen solid or operating cable
fractured).
Edition: June 2016
Maintenance Manual LS8-s and LS8-sb
Tail tank
full (+)
Tail tank
empty (+)
Tail tank
full (+)
Tail tank
empty (+)
front
rear
Seat
Baggage comp.
Vert. tail fin
Rev. 6 TN 8024
LS8-s
[m]
15
18
[kg] /
273
282
[lbs]
[mm] /
665
[in]
[kg] /
110
[lbs]
[kg] /
120
[lbs]
[kg] /
780
[lbs]
[kg] /
110
[lbs]
[kg] /
70
[lbs]
[kg] /
---
[lbs]
[kg] /
---
[lbs]
[No.]
1
[No.]
0
[No.]
1
18.08.2005
GS
Weight and Balance
LS8-sb
15
18
273
282
665
110
140
80
130
70
---
---
1
0
1
18.08.2005
GS
5-6