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DG Flugzeugbau LS8-s Flight Manual

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Table of Contents

0 M
C
ANUAL
ONTENTS

0.1 Log of Revisions

Any revision of the present manual, except actual weighing data, must be
recorded in the following table and in case of approved Sections endorsed by
the responsible airworthiness authority.
The new or amended text in the revised page will be indicated by a black
vertical line on the right margin, and the revision No. and the date will be
shown on the bottom left hand of the page
Rev.
Pages affected
no.
1
0-1,0-2,0-3, 0-4, 0-5,
4-15, 4-27, 4-28, 4-32,
7-2, 7-3
2
Title page, 0-1 ÷ 0.3, 0-
5, 4-4, 4-9, 7-2, 7-3, 7-
5, 7-13a, 7-14
3
0-1, 0-3, 0-5, 4-8, 7-6
4
0-1, 0-5, 9-5
5
0-1, 0-2, 0-3, 0-5, 1-4,
2-12, 4-24, 7-14
Edition: June 2016 Revision 5
Flight Manual LS8-s and LS8-sb
TN8019, wheel brake
actuated by airbrake handle
ÄM LS8-1, Miscellaneous
improvements from
ser. No. 8527 on
TN8021 small tailwheel
TN DG-G-11 NOAH
Improvements
TN 8024 Manual revision
TN 8024
Description
Contents
Date
EASA
Approval
Feb. 2011 13.10.11
Dezember
14.02.12
2011
January
24.02.
2015
2015
May2015
7.07.
2015
June 2016 5.08.
2016
0-1

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Summary of Contents for DG Flugzeugbau LS8-s

  • Page 1 Flight Manual LS8-s and LS8-sb Contents ANUAL ONTENTS 0.1 Log of Revisions Any revision of the present manual, except actual weighing data, must be recorded in the following table and in case of approved Sections endorsed by the responsible airworthiness authority.
  • Page 2 Flight Manual LS8-s and LS8-sb Contents 0.2 List of Effective Pages Chapter Page Edition Edition Edition Edition Titel page April 2005 Warnings April 2005 See log of revisions See log of revisions See log of revisions See log of revisions...
  • Page 3 Flight Manual LS8-s and LS8-sb Contents 0.2 List of Effective Pages continued Chapter Page Edition Edition Edition Edition April 2005 April 2005 April 2005 April 2005 April 2005 April 2005 April 2005 April 2005 April 2005 3-10 April 2005 3-11...
  • Page 4 Flight Manual LS8-s and LS8-sb Contents 0.2 List of Effective Pages continued Chapter Page Edition Edition Edition Edition April 2005 April 2005 Feb. 2011 Dec. 2011 April 2005 Feb. 2011 Dec. 2011 April 2005 April 2005 Dec. 2011 April 2005 Jan.
  • Page 5 They may be operated in 15m or 18m span and winglets in both versions. The fuselage structure of LS8-s and LS8-sb is different, because the LS8-sb is prepared for later engine installation.
  • Page 6 Flight Manual LS8-s and LS8-sb Limitations 2.12 Further Limitations 2.12.1 O PERATING LACARDS FOR IMITATIONS xx= variant DG Flugzeugbau GmbH -s or –sb Type: LS8-xx Serial No.:_______ Data Placard at right hand cockpit wall Airspeed Limits: km/h Kt MPH. Winch launch/Auto tow...
  • Page 7 Flight Manual LS8-s and LS8-sb Normal Procedures 4.5 N ORMAL ROCEDURES 4.5.1 C OCKPIT HECKLIST LS8-s and -sb Checklist This sailplane must be operated in compliance with operating limitations stated in the form of markings, placards and EASA approved Flight Manual.
  • Page 8 Flight Manual LS8-s and LS8-sb Systems 7.10 V ARIOUS QUIPMENT 7.10.1 E XPENDABLE ALLAST EIGHTS Expendable ballast to compensate pilot weight below Minimum Cockpit Load may be fitted in front of rudder pedals and secured with knurled nut. 7.10.2 A...

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