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Flight Manual   LS10-s,-st

  

Issued: December 2011  TN LS10-02    

         

7.35 

 

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. Then open the canopy simultaneously with the movement of the 
instrument panel and take off the canopy. If you don’t follow this procedure 
the canopy might be damaged by the instrument panel. 

 

7.17

 

Miscellaneous equipment (Options) 

7.17.1

 

Removable Ballast 

The installation of one trim ballast weight 4R8-108 2.45 kg (5.4 lbs) at the 
holder in front of the rudder pedal assy decreases the necessary pilot mass by 
approximately 5,5 kg (12 lbs). (max. 3 front trim weights can be 
installed).Further data regarding Cockpit Load see section 6. 

7.17.2

 

Oxygen system  

A fiberglas receptacle is installed in the left hand side of the main bulkhead for 
3 or 4 Litre oxygen bottles of 100 mm (3.94 in) in diameter. Bottles must be 
fixed with the designated clamp (P/N.: 4R8-41c) 
After permanent 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 Balance, 
Loading Instructions). 
When using a removable oxygen unit, its weight must be counted as cockpit 
load. 

7.17.3

 

 Emergency Locator Transmitter (ELT)  

ELT:

 The ELT may be installed on the holder 9R96 according to installation 

plan 9EP24 attached to the Maintenance Manual and according to the ELT 
manufacturer’s instructions.  
The designated place is the moulding on the RH side of the landing gear box 
below the baggage compartment. As the ELT is not accessible in flight an 
ELT remote control must be installed.  
The gain access to the on-off switch of the ELT e.g. for switching off the 
ELT for ground transport, the radio speaker plate must be mounted on an 
access door according to drawing 4R07-091. 

Caution:

 Antenna installation is only certified according to installation plan 

9EP22 attached to the MM.  
After installation, a functional test and inspection must be performed by a 
licensed inspector.  
The ELT must be switched off during road transport.  
With ELT installed onto holder 9R96, the installation of an additional battery see 
AFM sect. 7.17.4 is not possible. 
 

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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