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0 Revisions
0.1 Record 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 in the right hand margin, and the Revision No. and the date will be
shown on the bottom left hand of the page.
Rev.
Affected
No.
Pages/
section
1
0.1, 0.3 ÷
0.6, 2.4, 2.6,
4.2, 4.3,
6.13, 6.14,
7.2,
7.33 ÷ 7.35
Issued: December 2011
Flight manual LS10-s,-st
Description
Manual revision
TN LS10-02
TN LS10-02
Issue
EASA
Date
Approval
Date
December
February
2011
17. 2012
Inserted
Date
Signature
0.1
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Summary of Contents for DG Flugzeugbau LS10-s
- Page 1 Flight manual LS10-s,-st 0 Revisions 0.1 Record 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 in the right hand margin, and the Revision No.
- Page 2 Flight manual LS10-s,-st 0.2 List of effective pages Section page issued replaced/ replaced/ October 2009 see manual amendments " " " " " October 2009 October 2009 " " " " " App. October 2009 " " " " "...
- Page 3 Flight manual LS10-s,-st List of effective pages (cont.) Section Page issued replaced/ replaced/ App. October 2009 " " December 11 " " December 11 " " " " " " " " " " " " " 4.10 " "...
- Page 4 Flight manual LS10-s,-st List of effective pages (cont.) Section Page issued replaced/ replaced/ October 2009 " " " " " " " " 6.10 " 6.11 " 6.12 " 6.13 " December 11 6.14 " December 11 October 2009 "...
- Page 5 Flight manual LS10-s,-st List of effective pages (cont.) Section page issued replaced/ replaced/ 7.25 " 7.26 " 7.27 " 7.28 " 7.29 " 7.30 " 7.31 " 7.32 " 7.33 " December 11 7.34 " December 11 7.35 " December 11 7.36...
- Page 6 Flight manual LS10-s,-st 2.3 Airspeed Indicator Markings Airspeed indicator markings and their colour code significance are shown below. Marking (IAS) value or Significance range km/h (kts) White Arc 88 - 200 Positive Flap Operating (47,5 - 108) Range (lower limit is maximum weight 1.1 VSO in landing configuration.
- Page 7 Flight manual LS10-s,-st Fuel quantity indicator: On left hand upper side of the DEI-NT display, digital indication with 2 digits. Limitation data for the non usable amount of fuel printed above the display: Max Fuel capacity 12l 0.3 l When a fuel quantity of approx. 2 Litres is reached a full screen warning “Low Fuel”...
- Page 8 Flight manual LS10-s,-st 4.1 Introduction Section 4 provides checklists and amplified procedures for the conduct of normal operation. Normal procedures associated with optional systems can be found in section 9. Rigging and derigging, filling the watertanks, refuelling 4.2.1 Rigging 1. Execute the inspection prior to rigging according to section 4.3 A.
- Page 9 Flight manual LS10-s,-st 7. Rigging of the horizontal tailplane Check the glued joint of the spherical insert in the eye-bolt in the front horizontal tailplane attachment. Swivel movement is not allowed! Warning: If this insert is loose, flights are strictly prohibited. Contact the aircraft manufacturer.
- Page 10 Flight Manual LS10-s,-st Table of C.G. positions for various items of equipment: Item mass C.G. behind datum 1 Battery in front of control stick -1,05 -3,44 Battery in baggage compartment 0,185 0,61 4BR-255/2 Battery in the fin 3BR-199 4,308 14,13 Water in LH (System No.1)-...
- Page 11 Flight Manual LS10-s,-st Rule of thumb: Installation of 1 trim ballast weight (2.45 kg, 5.4 lbs) in front support........... reduces Minimum Cockpit Load by 5,5 kg / 12 lbs Installation of 1 Battery (2.5 kg, 5.5 lbs) in front of the control stick..
- Page 12 Refer to section 9 "Supplements" for details of optional systems and equipment. 7.2 Airframe The LS10-s is a single-seater high performance glider. The LS10-st is a self-sustainer single-seater high performance motorglider with retractable powerplant. 18 m wingspan with wing parting at y=7 m, wingtips for 15m span optional.
- Page 13 Flight Manual LS10-s,-st 7.15 Pitot-/Static pressure system 1 Multi Probe : Pitot-/Static-/TE pressure port 2 Pitot pressure port at fuselage nose. 3 Static pressure port for airspeed indicator and altimeter – forward fuselage sides. Vacuum Bottles. A ASI E Capacity bottles for variometers...
- Page 14 Flight Manual LS10-s,-st 7.16 Canopy Canopy emergency release Canopy locks : pull both red handles to stops Right handle operates emergency canopy jettison, therefore it has longer travel than left handle. Pull with more than 15kg / 33lbs! Hand force increases for emergency jettison travel to avoid unintentional jettison during normal operation.
- Page 15 Flight Manual LS10-s,-st Caution: If you pulled the emergency release inadvertently while opening the canopy you should hold down the canopy at the emergency release handle. Then lift the canopy at the rear end with your left hand to disengage the Röger hook.
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