Flight manual LS4-a, LS4-USA edition, LS4-a USA edition
Issued February 2019 TN4049 9-8
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
9.4 Neo-Winglets
Introduction
In the following text the changes to those sections of the flight manual which are
affected by the installation of neo-Winglets will be given. For operation without neo-
Winglets the data of the other LS4 (LS4-a) flight manual sections are applicable.
Section 1 General
Subsection amended
Page 1-6 Descriptive data
Technical details
Option TN4049: Removable wing tips with neo-Winglets
Technical data units LS4-a
ax. mass with neo-Winglets installed kg 505
ax. wing loading with neo-Winglets installed kg/m² 48
Note: max. mass of LS4 unchanged
Note: neo-Winglets raise the empty mass about 2 kg.
Caution: If the sailplane will be operated with neo-winglets the max. mass is reduced,
see above.
Page 1-7 3-side view of the neo-Winglets