DG Flugzeugbau GmbH
Flight Manual LS 8-18
Weight and Balance
6.2 Cockpit Loading Plan
(Pilot and Parachute) continued
Warning:
New entry with each new weighing or when changing equipment. Entry should be
calculated in accordance with chapter 2 of Maintenance Manual.
State dimensions used
.
State amount of permanently fitted ballast in appropriate position or none.
Serial Number:
.
Minimum Cockpit Load
WITH
WITHOUT
Tail Batterie
and
Tail Batterie
and
Empty
C.G.
Max.
Cockpit
Tail Tank
Tail Tank
Permanently
fixed Ballast
Mass
Tail
Tank
Mass
position Load
full
empty )* full )* empty )*
front
rear
Volume Date / Inspector
[ ]
[ ]
[ ]
[ ]
[ ]
[ ]
[ ]
[ ]
[ ]
[ ]
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
15m
18m
)*
These Minimum Cockpit Load values may only be used, when the pilot can positively exclude unintentional
use of tail fin water and tail fin battery, i.e. he has checked proper valve opening by use of tubing and blowing
through valve and visually checked, that no tail fin battery is installed by removing horizontal tail and re-
installing.
Edition: Dec. 2001
Revision – 1 (TB 8011)
Page 6-2