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0 Manual Contents
0.1 Log of Revisions
Rev
Pages
no.
1
0-1, 0-3, 0-4, 0-5, 0-6, 0-8, 0-11, 1-
27, 3-4, 4-16, 4-19, 4-21,
10-2, 10-8, 11-2, 11-18, 11-20
2
0-1, 0-3, 0-7, 1-1, 1-7,
1-11, 1-12, 8-3
3 Title page, 0-1, 0-3, 0-4, 0-6 ÷ 0-8,
0-11, 1-3, 1-7 ÷ 1-9, 1-22, 1-29,
1-36, 1-40, 1-48a, 4-1, 4-21, 4-27,
6-4, 10-2a, 11-15, 9E2
4 0-1, 0-3, 0-7, 1-17, 8-1
5 0-1, 0-4 up to 0-8, 1-28, 1-30, 3-7,
4-12, 4-13, 4-23, 4-24, 4-28, 6-1,
6-2, 9-1, 10-2, 10-2a, 10-9
6 0-1, 0-3, 0-6 ÷ 0-8, 0-12, 1-10, 4-11,
5-3, 5-4, 5-6, 6-2, 8-1, 8-2, 9-1, 9-2,
10-2
Edition: June 2016
Maintenance Manual LS8-st
Reference
TN 8017, necessary changes to
the power plant
TN8019, wheel brake actuated
by airbrake handle.
ÄM LS8-1, Miscellaneous
improvements Ser.no. 8474
and from ser. No. 8527 on
TN 8021
Small tailwheel
Mechanical fuel pump
Manual revision
TN 8022
TN 8024
Manual revision, repair manual
Rev. 6 TN 8024
Contents
Rev. date
Nov.
2010
Feb. 2011
December
2011
January
2015
October
2015
June
2016
0-1

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Summary of Contents for DG Flugzeugbau LS8-st

  • Page 1 Maintenance Manual LS8-st Contents 0 Manual Contents 0.1 Log of Revisions Pages Reference Rev. date 0-1, 0-3, 0-4, 0-5, 0-6, 0-8, 0-11, 1- TN 8017, necessary changes to Nov. 27, 3-4, 4-16, 4-19, 4-21, the power plant 2010 10-2, 10-8, 11-2, 11-18, 11-20...
  • Page 2 Maintenance Manual LS8-st Contents 0.2 List of Effective Pages Chapter Page Edition Replaced Replaced Replaced Title page April 2005 Dec. 2011 See log of revisions See log of revisions See log of revisions See log of revisions See log of revisions...
  • Page 3 Maintenance Manual LS8-st Contents 0.2 List of Effective Pages (continued) Chapter Page Edition Replaced Replaced Replaced April 2005 Dec. 2011 April 2005 April 2005 April 2005 April 2005 April 2005 April 2005 April 2005 April 2005 4-10 April 2005 4-11...
  • Page 4 Maintenance Manual LS8-st Contents 0.2 List of Effective Pages (continued) Chapter Page Edition Replaced Replaced Replaced April 2005 April 2005 April 2005 June 2016 April 2005 June 2016 April 2005 June 2016 April 2005 April 2005 April 2005 April 2005...
  • Page 5 Maintenance Manual LS8-st Contents 0.2 List of Effective Pages (continued) Chapter Page Edition Replaced Replaced Replaced 10-1 April 2005 10-2 April 2005 Nov. 2010 Oct. 2015 June 2016 10-2a Dec. 2011 Oct. 2015 10-3 April 2005 10-4 April 2005 10-5...
  • Page 6 Maintenance Manual LS8-st Contents IMITED ARTS AINTENANCE NSTRUCTIONS 0.4.1 Repairs Repair or replace damaged parts prior to next flight. Follow the instructions in the Repair Manual LS8. Major repairs must be accomplished by an approved repair station or by an approved mechanic rated for composite aircraft structure work in accordance with DG repair methods.
  • Page 7 Maintenance Manual LS8-st Systems (continued) 1. S YSTEM ESCRIPTION AND DJUSTMENT 1.4 Elevator Control System (continued) 1.4.2 Deflections and Tolerances Elevator: 28° - 30° down 22° - 26° For easier checking, measured angles may be converted to mm / in deflection values, using the actual local radius of the defined measuring place.
  • Page 8 Maintenance Manual LS8-st Instructions 4.5 Installation of Control Surfaces (continued) Disassembly of Rudder (1) disconnect rudder cables. Attention: Don’t loose spacing casings. Attention: Rudder cables may be drilled. If this is changed unintentionally, neutral positions of rudder and pedals do no longer correspond and must be realigned as detailed below.
  • Page 9 Maintenance Manual LS8-st Weight and Balance 5.2 Calculation of Loading Limits 1. Determine Minimum Cockpit Load for 15 m wingspan and full and empty tail fin tank version following procedure given in section 5.1 from table “Empty Weight C.G. Position”, section 5.4 in <kg/mm> or <in/lbs>.
  • Page 10 Maintenance Manual LS8-st Weight and Balance 5.2 Calculation of Loading Limits (continued) 2. Maximum approved Weight of Non-lifting Parts may vary between 305◦kg and 315 kg <672 to 694 lbs>, depending on empty weight and empty weight C.G. position. In contrast to methods used up to now, maximum weight of non-lifting parts can be determined in relation to empty weight and empty weight C.G.
  • Page 11 Maintenance Manual LS8-st Weight and Balance 5.2 Calculation of Loading Limits (continued) Example for entry in Flight Manual section 6.2: Wing span Empty Mass [kg] / [lbs] C.G. position [mm] / [in] [kg] / Fuel tank full [lbs] [kg] /...
  • Page 12 Maintenance Manual LS8-st Instruments and. Equipment 6.3 Seat Belt Harness (with multiple point buckles) Manufacturer Type TCDS No. Schroth 4-01-0.104 (Lap belt and 40.073/11 shoulder strap) Gadringer Lap belt 5202 40.070/32 Shoulder strap 2700 40.071/05 6.4 Compass Manufacturer Type TCDS No.
  • Page 13 Maintenance Manual LS8-st Placards 8. Markings and Placards MINIMUM COCKPIT LOAD: kg / lbs LS8-st Checklist with tail battery, tail tank full min. ________ with tail battery, tail tank empty min. ________ This powered sailplane must be operated in without tail battery, tail tank full min.
  • Page 14 Maintenance Manual LS8-st Placards 8. Markings and Placards (continued) ▲ Soaring at instrument panel FUEL: Two stroke Mixture 1:40 of Vario ASI Static/pitot switches Unleaded Four Star/Premium min. 95 ROZ ▼ powered (Option) or AVGAS 100 LL with 2-stroke oil Castrol Super TT/TTS...
  • Page 15 Maintenance Manual LS8-st Placards 9. Parts List In this list, the most important parts of propulsion system, electrical system as well as components of control surface sealing and water ballast system are provided. For drawing numbers of control system parts refer to diagrams section 1. For drawing numbers of propulsion system brackets refer to diagrams section 10.
  • Page 16 Maintenance Manual LS8-st Parts List Propeller attachment 45002052 Rubber stop for propeller 9.2 Parts for electrical system 45002070 Battery for power supply 12V/min.7Ah (2 installed) 45002049 DEI-NT for LS8-t 45002050 Control box-NT for LS8-t 60510463 limit switch 164-564 with plug contacts for positions...
  • Page 17 Maintenance Manual LS8-st Diagrams Diagram 2: Fuel system up to serial no. L8528 In Datei br-236 Issued: June 2016 Rev. 6 TN 8024 10-2...