19.01.2013 Views

LS10-s / LS10-st - DG Flugzeugbau

LS10-s / LS10-st - DG Flugzeugbau

LS10-s / LS10-st - DG Flugzeugbau

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Flight manual <<strong>st</strong>rong>LS10</<strong>st</strong>rong>-s,-<strong>st</strong><br />

Powerplant and powerplant controls (<<strong>st</strong>rong>LS10</<strong>st</strong>rong>-<strong>st</strong> only)<br />

Retractable powerplant with an air cooled two <strong>st</strong>roke engine and GFRP-<br />

Composite propeller.<br />

• Electrical engine extension-retraction, operated automatically with the<br />

ignition switch or manually as back-up, electronic safety devices to avoid<br />

misoperation.<br />

• Engine control in<strong>st</strong>ruments with digital LCD indication (Microprocessor<br />

technology) DEI-NT including outside air thermometer.<br />

Technical data<br />

Wingspan m (feet) 15 (49.2) 18 (59.1)<br />

Wing surface m² (ft²) 10.272 (110.6) 11,454 (123.3)<br />

Aspect ratio / 21.9 28,30<br />

Mean aerodynamic chord MAC m (ft) 0.706 (2.31) 0.674 (2.21)<br />

Length m (ft) 6.763 (22.19)<br />

Fuselage width m (ft) 0.64 (2.09)<br />

Fuselage height incl. tail m (ft) 1.374 (4.51)<br />

Horizontal tail span m (ft) 2.50 (8.20)<br />

Wings outboard and centre (sy<strong>st</strong>em 1) kg (lbs) approx. 83 (183<br />

Wings inboard (sy<strong>st</strong>em 2) kg (lbs) approx. 106 (234)<br />

Wings total kg (lbs) approx. 189 (417)<br />

Fin tank (sy<strong>st</strong>em 1) kg (lbs) 3.9 (8.6)<br />

Fin tank (sy<strong>st</strong>em 2) kg (lbs) 4.6 (10.1)<br />

Waterballa<strong>st</strong> total kg (lbs) approx. 197 (434)<br />

<<strong>st</strong>rong>LS10</<strong>st</strong>rong>-s empty weight approx. *) kg (lbs.) 282 (622) 293 (646)<br />

<<strong>st</strong>rong>LS10</<strong>st</strong>rong>-s wing loading with payload 80 kg/m²<br />

kg (176 lbs.) approx.<br />

(lbs./ft²) 35.2 (7.22) 32.57 (6.67)<br />

<<strong>st</strong>rong>LS10</<strong>st</strong>rong>-<strong>st</strong> empty weight approx. *) kg (lbs.) 322 (710) 333 (734)<br />

<<strong>st</strong>rong>LS10</<strong>st</strong>rong>-<strong>st</strong> wing loading with payload 80 kg/m²<br />

kg (176 lbs.) approx.<br />

(lbs./ft²) 39.1 (8.01) 36.05 (7.38)<br />

Max. weight kg (lbs.) 540 (1190) 600 (1323)<br />

Max. wing loading<br />

Powerplant (only <<strong>st</strong>rong>LS10</<strong>st</strong>rong>-<strong>st</strong>)<br />

kg/m²<br />

(lbs./ft²)<br />

52,6 (10.76) 52.4 (10.73)<br />

engine air cooled Solo 2350 two <strong>st</strong>roke engine<br />

power 15,4 kW (21 hp)<br />

Propeller Technoflug KS-1-G-079-L-050-W GFRP-Composite<br />

Propeller diameter 0.79 m (2.59 ft).<br />

Fuel tank capacity fuselage tank<br />

Empty masses are with common in<strong>st</strong>rumentation.<br />

*Options will increase the empty mass accordingly!<br />

12 Liter (3,2U.S.gal.)<br />

Note: Up to ser. no. L10-015 only approx. 3,6 kg (7.9 lbs.) can be filled into the<br />

fin tank of sy<strong>st</strong>em 1.<br />

Issued: October 2009 1.5

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!