DG Flugzeugbau LS10-s Caractéristiques techniques

Flight manual LS10-s,-st

Issued: December 2011 TN LS10-02 0.1

0Revisions

0.1 Record of revisions

Any revision of the present manual, except actual weighing data, must be

recorded in the following table and in case of approved sections endorsed by 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 on the bottom left hand of the page.

Rev.

No.

Affected

Pages/

section

Description Issue

Date

EASA

Approval

Date

Inserted

Date

Signature

0.1, 0.3 ÷

0.6, 2.4, 2.6,

4.2, 4.3,

6.13, 6.14,

7.2,

7.33 ÷ 7.35

Manual revision

TN LS10-02

December

2011

February

17. 2012

Flight manual LS10-s,-st

Issued: December 2011 TN LS10-02 0.3

0.2 List of effective pages

Section page issued replaced/ replaced/

0 0.0 October 2009

0.1 see manual amendments

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0.7 October 2009

1 1.1 October 2009

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2 App. 2.1 October 2009

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" 2.4 " December 11

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" 2.6 " December 11

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3 " 3.1 October 2009

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Flight manual LS10-s,-st

Issued: December 2011 TN LS10-02 0.4

0.2 List of effective pages (cont.)

Section Page issued replaced/ replaced/

4 App. 4.1 October 2009

" 4.2 " December 11

" 4.3 " December 11

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5 " 5.1 October 2009

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App. 5.4 "

5.5 "

5.6 "

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5.10 "

5.11 "

5.12 "

Flight manual LS10-s,-st

Issued: December 2011 TN LS10-02 0.5

0.2 List of effective pages (cont.)

Section Page issued replaced/ replaced/

6 6.1 October 2009

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6.13 " December 11

6.14 " December 11

7 7.1 October 2009

7.2 " December 11

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Flight manual LS10-s,-st

Issued: December 2011 TN 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

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9 9.1 October 2009

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Flight manual LS10-s,-st

Issued: December 2011 TN LS10-02 2.4

EASA app.

2.3 Airspeed Indicator Markings

Airspeed indicator markings and their colour code significance are shown below.

Marking

(IAS) value or

range

km/h (kts)

Significance

White Arc

88 - 200

(47,5 - 108)

Positive Flap Operating

Range

(lower limit is maximum weight

1.1 VSO in landing configuration.

Upper limit 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 limit is rough air speed.)

Yellow Arc

200 - 280

(108 - 151)

Manoeuvres must be conducted

with caution and only in smooth

air.

Red Line

280

(151)

Maximum speed for all

operations.

150

( 81)

Max. speed for landing

configuration L

Yellow

Triangle

100

(54)

Approach speed at maximum

weight without water ballast

only LS10-st

Blue line

( 51)

Speed of best climb Vy, (only for

LS10-st)

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 l (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.

Flight manual LS10-s,-st

Issued: December 2011 TN LS10-02 4.2

EASA app.

4.1 Introduction

Section 4 provides checklists and amplified procedures for the conduct of normal

operation. Normal procedures associated with optional systems can be found in

section 9.

4.2 Rigging and derigging, filling the watertanks, refuelling

4.2.1 Rigging

1. Execute the inspection prior to rigging according to section 4.3 A.

2. Clean and grease all pins and bushes and all 4 automatic control system

connectors.

3. Open the canopy.

4. Set the airbrake handle to the forward stop and control stick and wingflap

handle to neutral.

Always rig inner wings without 15 m or 18 m tips.

With a helper on the wingtip, push the left wing into place, then the right

wing.

Check for correct dihedral. The flaperons should be held at neutral for

rigging, airbrakes locked. All controls will hook up automatically.

Caution: Make sure that the wing trailing 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 fuselage-side control and will be damaged.

Sight through the wing main pin bushings to determine alignment. Push the

main pins in as far as possible. Turn one handle after the other up to the

fuselage wall, while pulling out the white securing knob, then release the

knob back to its locked position. Check the securing.

5. Insert the wing tip extensions (18 m) into the wing.

Press in the locking pin with your finger.

Insert the wing tip until the flaperon connecting pins start to slide into the

centre-flaperon bushes.

Strike firmly with the palm of your hand on to the wing tip to lock the wing

tip extension.

The rigging of the 15 m wingtips (Option) has to be done in the same

manner as the wing tip extensions.

6. Check if you are safe to fly with the fin battery (see Data Placard in cockpit

or entries in section 6). Insert the battery into place. Connect battery to the

aircraft electric system and check operation.

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.

Flight Manual LS10-s,-st

Issued: December 2011 TN LS10-02 6.13

Table of C.G. positions for various items of equipment:

Item mass C.G. behind

datum

kg lbs m ft

1 Battery in front of control stick

2,5 5,5 -1,05 -3,44

Battery in baggage compartment

4BR-255/2

2,5 5,5 0,185 0,61

Battery in the fin 3BR-199 2,6 5,7 4,308 14,13

Water in LH (System No.1)-

(forward) fin tank - up to

3,9 8,6 4 13,12

Water in RH (System No. 2)-

(rear) fin tank - up to

4,6 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

110,0 242,5 0,196 0,64

Powerplant 26,5 58,4 1,05 3,44

Empty fuel tank 1,5 3,3 0,38 1,25

Fuel in main tank max. 7,0 15,4 0,38 1,25

Trim weight rear fuselage 4R8-

109

2,5 5,5 4,383 14,38

Trim weight in front support

4R8-108

2,45 5,4 -1,69 -5,54

Heavy tail wheel (P/N.: S27) **) 3,4 6,6 4,314 14,15

*) usually 2 batteries are installed

**) 3.0kg (6.6 lbs) more than standard tail wheel with plastic hub S23

(mass of plastic hub S23 with tyre= 0,9 kg (1.98 lbs.))

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