DG Flugzeugbau LS8-st Руководство по техническому обслуживанию - Страница 11
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Печатать страницу5.2 Calculation of Loading Limits (continued)
Example for entry in Flight Manual section 6.2:
The discrepancy between Maximum Cockpit Load of 110 kg <242 lbs> and
Minimum Cockpit Load of 130 kg <286 lbs> 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-st
Wing span
Empty Mass
C.G. position
Fuel tank full
Fuel tank partly filled
Tail tank
with tail-
full
battery
Tail tank
empty (+)
Tail tank
without tail-
full (+)
battery
Tail tank
empty (+)
front
Perm.
fixed Trim
rear
mass
Seat
Batteries
Baggage comp.
installed
Vert. tail fin
Engine (
INstalled / REmoved
Date / Inspector
Rev. 6 TN 8024
Weight and Balance
[m]
15
[kg] /
316
[lbs]
[mm] /
649
[in]
[kg] /
110
[lbs]
[kg] /
110
[lbs]
[kg] /
130
[lbs]
[kg] /
90
[lbs]
[kg] /
120
[lbs]
[kg] /
80
[lbs]
[kg] /
---
[lbs]
[kg] /
---
[lbs]
[No.]
2
[No.]
0
[No.]
1
)
IN
18.08.2005
GS
18
325
5-6