background image

Flight manual LS10-s,-st

 

Issued: December 2011   

TN LS10-02 

2.6

EASA app. 

 

 

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 
         red                 0.3 l 
When a fuel quantity of approx. 2 Litres is reached a full screen warning 

Low Fuel

” appears, when this warning has been confirmed (by pushing 

the selector knob at the right hand side of the display) the fuel display will 
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 

 (3.20 

US 

gal.) 

Non usable amount of fuel:0.3 l   

(0.08 US gal.) 

Usable amount of fuel: 

 

11,7 l  

(3.09 US gal) 

 
Approved fuel grades: 

 

 

Automobile super gasoline min. 95 octane (ROZ) (RON) leaded or 

unleaded 

or: 

AVGAS 100 LL (only if super gasoline is not available) 

or:  

mix 50% AVGAS 100LL with 50% car gasoline min. 92 octane 

(ROZ) (RON) 
mixed with self-mixing Super quality two stroke oil - specification TSC 3 or  
API TC or JASO FC or higher quality. Mixing ratio 1:40 

Note:

 The SOLO company recommends the following oil types: CASTROL 

Actevo 2T or Castrol Super Two stroke. 

 

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...

Reviews: