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Flight Manual   LS10-s,-st

  

Issued: December 2011   

TN LS10-02 

 

 

 

          

7.2 

 

7.1

 

Introduction 

Section 7 describes the operation of the sailplane including its systems. 
M.M. = Maintenance manual 
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. 

Construction

 

Wings  

CFRP-foam-sandwich-shell with 
CFRP-roving spar caps 

Flaperons 

CFRP-foam-sandwich-shell 

Rudder

 

GFRP-foam sandwich-shell 

Horizontal stabilizer 

GFRP/ AFRP-foam sandwich-shell  

Elevator 

AFRP -skin 

Fuselage

 

CFRP-GFRP-shell 

Canopy

 

Large single piece canopy, hinged at the front (nose) and supported by a gas 
strut. Canopy is made of Plexiglas GS clear “GS 241“ or optionally green “GS 
green 2942” or optionally blue “GS blue 2928“. 
Canopy glass glued onto a GFRP frame 

Tailplane

 

T-Tail with conventional stabilizer-elevator and spring trim. 

Colours

 

Airframe:  

white 

 

 

registration numbers:  grey RAL 7001 

or

red  RAL 3020 

  blue RAL 5012 

or green  RAL 6001 

Anti collision paint 

Approved colours: red, fluorescent red or orange 
Approved areas: 
1. Rudder: may be painted completely 
2. Horizontal tail: paint only the stabilizer and only up to 200 mm from the 

tips 

3. Wing Sections: the inner wing shall not be painted 
4. 15 m tips: can be painted entirely 
5. 18 m wing tips: paint only the wing and not the ailerons, no more than 400 

mm from the tips 

Note:

 3M mirror foil may be applied to all parts of the airframe 

Summary of Contents for LS10-s

Page 1: ...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...

Page 2: ...issued replaced replaced 0 0 0 October 2009 0 1 see manual amendments 0 2 0 3 0 4 0 5 0 6 0 7 October 2009 1 1 1 October 2009 1 2 1 3 1 4 1 5 1 6 2 App 2 1 October 2009 2 2 2 3 2 4 December 11 2 5 2 6...

Page 3: ...nt Section Page issued replaced replaced 4 App 4 1 October 2009 4 2 December 11 4 3 December 11 4 4 4 5 4 6 4 7 4 8 4 9 4 10 4 11 4 12 4 13 4 14 4 15 4 16 4 17 4 18 4 19 4 20 4 21 4 22 4 23 4 24 4 25...

Page 4: ...ges cont Section Page issued replaced replaced 6 6 1 October 2009 6 2 6 3 6 4 6 5 6 6 6 7 6 8 6 9 6 10 6 11 6 12 6 13 December 11 6 14 December 11 7 7 1 October 2009 7 2 December 11 7 3 7 4 7 5 7 6 7...

Page 5: ...LS10 02 0 6 0 2 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 8 8 1 October 2009 8...

Page 6: ...t is maximum speed permissible with flaps extended positive 2 1 Green Arc 97 200 52 108 Normal Operating Range Lower limit is 1 1 VS1 at maximum weight and most forward c g with flaps neutral Upper li...

Page 7: ...keep blinking When reaching the non usable amount of fuel R is displayed and will keep blinking 2 6 Fuel only LS10 st Fuel capacity Fuselage tank total 12 l 3 20 US gal Non usable amount of fuel 0 3...

Page 8: ...g edge is at the same height as its counterpart at the fuselage before the controls hook up Otherwise a ball bearing of a control hook up bellcrank mounted at the wing root may knock against the fusel...

Page 9: ...ions the wing joints and the horizontal stabilizer 12 Execute a positive control check one helper is needed to hold firmly the control surfaces Only LS10 st 13 Pull off the fuel vent surge bottle from...

Page 10: ...1 4 16 13 65 Water in outer wing tank System No 1 up to 30 0 66 1 0 189 0 62 Water in the centre wing tank System No 1 up to 50 0 110 2 0 189 0 62 Water in the inner wing tank System No 2 up to 110 0...

Page 11: ...2 6 kg 5 7 lbs increases Minimum Cockpit Load by 11 2 kg 24 6 lbs Installation of heavy tailwheel mass difference to standard tail wheel 3 kg 6 6 lbs increases Minimum Cockpit Load by 12 9 kg 28 5 lbs...

Page 12: ...r AFRP skin Fuselage CFRP GFRP shell Canopy Large single piece canopy hinged at the front nose and supported by a gas strut Canopy is made of Plexiglas GS clear GS 241 or optionally green GS green 294...

Page 13: ...iometers B Altimeter G Variometer switch Option C Variometer TE Soaring static Engine operstion D Electrical Variometer switch shown in SOARING position Colours of instrument lines 1 Multi Probe Pitot...

Page 14: ...d handle to jettison the canopy 2 As soon as the canopy is lifted by the instrument panel support the person at the front end must hold the canopy so that it will not be lifted more than approx 3 cm 1...

Page 15: ...ent installation of an oxygen system according to its manufacturer instructions by an adequately licensed maintenance repair shop the sailplane including oxygen system must be inspected Weight and Bal...

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