DG Flugzeugbau LS8 - Table of Contents

Maintenance Manual LS8
Issued: December 2009
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Manual valid with the up-to-date cover page only
0-6
0.3 Table of Contents
Section Content page
0
General .....................................................................................................0-1
0.1 Manual amendments ................................................................................0-1
0.2 List of effective pages..............................................................................0-3
0.3 Table of Contents.....................................................................................0-6
0.4 Airworthiness limitations.........................................................................0-9
0.4.1 Repairs................................................................................................0-9
0.4.2 Life time of the airframe ....................................................................0-9
0.4.3 Life time of equipment and components ...........................................0-9
0.4.4 Service time, maintenance documents of equipment and components
............................................................................................................0-9
1 Description of systems.............................................................................1-1
1.1 Overview..................................................................................................1-1
1.2 Aileron control system (Fuselage).........................................................1-5
1.3 Air brake system ......................................................................................1-6
1.4 Elevator control system............................................................................1-7
1.5 Wing control systems and wing waterballast (only LS8)........................1-8
1.6 Aileron control system wings (LS8-a, LS8-b, LS8-18)...........................1-9
1.7 Rudder control system ...........................................................................1-10
1.8 Main landing gear ..................................................................................1-11
1.9 Fuselage waterballastsystem (LS8) .......................................................1-12
1.10 Fuselage water ballast system (LS8-a, LS8-18) ....................................1-13
1.11 Fuselage water ballast system (LS8-b) ..................................................1-14
1.12 Wing water ballast system (LS8-a from ser. no. 8066 on, LS8-b, LS8-18)
................................................................................................................1-15
1.13 Wing water ballast system with winglet ventilation (only LS8-a up to ser.
no. 8065) ................................................................................................1-16
1.14 Pressure ports .........................................................................................1-18
1.15 Drain orifices .........................................................................................1-18
1.15.1 Drain orifices (LS8, LS8-18, LS8-b) ...............................................1-18
1.15.2 Drain orifices (LS8-a) ......................................................................1-19
1.16 Primary and secondary structure............................................................1-19
2 Mass and balance .....................................................................................2-1
2.1 Weighing procedure.................................................................................2-1
2.2 Calculation of loading limits....................................................................2-2
2.3 Calculation of maximum mass of non-lifting parts .................................2-6
2.3.1 MNLP LS8.........................................................................................2-6
2.3.2 MNLP LS8-a......................................................................................2-8
2.3.3 MNLP LS8-b and LS8-18................................................................2-10
2.4 Empty mass C.G. range .........................................................................2-12