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Flight Manual   LS10-s,-st

  

Issued: December 2011  TN LS10-02    

         

7.34 

 

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. 

Canopy:

  

Push off canopy using both red handles 

The gas strut which lifts the instrument panel assists the 
canopy jettison. 

LS-latch (Röger hook)

:  

This device is installed at the upper rear end of the 

canopy and serves as hinge point for the canopy after 
emergency release.. 

 
Checking the emergency release on the ground and removal of canopy: 

One person must sit in the cockpit and one person must hold the canopy at the 
front end. 
1.

 

With canopy closed pull on both red handles to bring them to the open 
position. Thereafter pull strongly on the right hand 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 in.). 

3.

 

The person in the cockpit must then lift the canopy at the rear end to 
disengage the LS-latch (Röger hook). 

4.

 

Open the canopy simultaneously with the movement of the instrument 
panel. 

5.

 

If you want to remove the canopy from the glider disconnect cables, if 
equipment like a GPS antenna is installed on the glare shield. 

Reinstalling the canopy:

 

Two people are required to operate and hold the canopy 
1.

 

Connect all cables, if equipment like a GPS antenna is installed on the 
glareshield 

2.

 

Bring the locking lever at the canopy into the open position (rotate 
clockwise)  

3.

 

Place the canopy on the instrument panel support. Move the locking pin 
with the knurled knob (at the instrument panel support) upwards and move 
the locking pin through the release cut-out in the canopy. Rotate the 
locking lever at the canopy  counter-clockwise until the canopy is locked. 
Both elements are accessible from the fuselage nose with an open canopy. 

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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