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Flight manual LS10-s,-st

 

Issued: December 2011   

TN LS10-02 

4.3

EASA app.

 
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.  
Install the horizontal tailplane and fix it by turning the slotted nut mounted 
on the rear attachment (using supplied key or suitable coin) until there is no 
more free play and the red marking on the main attachment bracket is no 
longer visible via the hole in the upper shell. 

8.

 

Install total energy tube, secure against rotating using tape. 

9.

 

Mount all necessary equipment in the baggage compartment. Safely secure 
all items. 

10.

 

Connect automatic parachute ripcord at red marked position at main 
bulkhead. Wrap cord around the lift pin tube. 

11.

 

Tape the gaps of the wing-fuselage junctions, 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 the fuel vent line (bottom side of the 
fuselage). 

14.

 

Open fuel shut off valve. 

 

4.2.2

 

De-Rigging:  

Derigging follows the reverse of rigging. 

Waterballast must be dumped first. 
Airbrakes should be locked. 

Note:

 It is also possible to de-rig with the airbrakes not locked. In such case you 

have to make sure that the airbrakes won’t be damaged in the trailer in case they 
extend due to vibrations. It is not necessary to lock the airbrakes for rigging 

 

Disassembling the wing tips: 

Use a 6 mm diameter pin for pressing in the locking pin on the wing’s upper 
surface. Pull out the wing tips. 

 

Only LS10-st 

Push the fuel vent surge bottle onto the fuel vent line (bottom side of the 
fuselage). 
Close fuel shut-off valve. 

Note:

 During road-transport with full fuel tank fuel may spill via the carburettors 

or via the ventilation line. To avoid this the fuel shut-off valve should be 
closed during de-rigging and the fuel vent surge bottle installed. 

 

Содержание LS10-s

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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