LS10-s / LS10-st - DG Flugzeugbau
LS10-s / LS10-st - DG Flugzeugbau
LS10-s / LS10-st - DG Flugzeugbau
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2.18 Limitations placards<br />
Preflight inspection<br />
1. Lead balla<strong>st</strong> (for under weight pilot)?<br />
2. Fin balla<strong>st</strong> tanks emptied or correct<br />
amount filled in?<br />
3. Battery in the fin? Loading chart<br />
regarded?<br />
4. Parachute worn properly?<br />
5. Safety harness buckled?<br />
6. Seat back and pedals adju<strong>st</strong>ed?<br />
7. All controls and knobs in reach?<br />
8. Altimeter?<br />
9. Dive brakes cycled and locked?<br />
10. Wing flaps in initial take-off position?<br />
11. Positive control check? (One person at<br />
the control surfaces).<br />
12. Trim?<br />
13. Canopy locked?<br />
14. Tail dolly removed?<br />
Additional checks for <<strong>st</strong>rong>LS10</<strong>st</strong>rong>-<strong>st</strong>:<br />
15. Engine retracted?<br />
16. Fuel shut off valve in open position?<br />
17. Fuel Pump switch in “Auto” position?<br />
18. Check amount of fuel (DEI-NT<br />
Rated load max. 8250 N<br />
max. 1820 lbs.<br />
Tyre pressure<br />
3.5 bar<br />
(51 psi)<br />
Tyre pressure<br />
2.0 bar<br />
(29 psi)<br />
left landing gear door<br />
Main wheel<br />
Tailwheel<br />
Maximum baggage weight 5 kg (11 lbs)<br />
(soft items only)<br />
Flight manual <<strong>st</strong>rong>LS10</<strong>st</strong>rong>-s,-<strong>st</strong><br />
<strong>DG</strong> <strong>Flugzeugbau</strong> GmbH<br />
type: <<strong>st</strong>rong>LS10</<strong>st</strong>rong>-s serial no: L10-<br />
year of con<strong>st</strong>ruction:<br />
Maximum airspeeds km/h kts.<br />
Winch launch 150 81<br />
Aero-tow 200 108<br />
Manoeuvering VA 200 108<br />
Rough air 200 108<br />
Max. flap extended speed +2, +1 200 108<br />
Landing gear operating 280 151<br />
Maximum speed VNE 280 151<br />
Max. flap extended speed L 150 81<br />
Powerplant extended 200 108<br />
Powerplant extension-retraction 110 59<br />
Approved aerobatic manoeuvres ( only without<br />
waterballa<strong>st</strong> and with engine retracted)<br />
pos. Loop, Stall Turn, Lazy Eight, Chandelle, Spin<br />
Maximum mass:<br />
18m wingspan 600 kg ( 1223 lb.)<br />
15m wingspan 540 kg ( 1190 lb.)<br />
Loading chart<br />
Cockpit load ( parachute included )<br />
maximum 110 kg 242 lbs<br />
minimum with fin battery (2,6kg) kg lbs<br />
minimum without fin battery kg lbs<br />
With lower pilot weight necessary balla<strong>st</strong> mu<strong>st</strong> be<br />
added<br />
Operating limitations for using waterballa<strong>st</strong><br />
min. ground temp °C 13,5 17 24 31 38<br />
°F 56 63 75 88 100<br />
max. flight altitude m 1500 2000 3000 4000 5000<br />
above GND ft 5000 6000 10000 12000 16500<br />
Fill up wing balla<strong>st</strong> tanks<br />
beginning with the outer tank.<br />
between waterballa<strong>st</strong> dump handles<br />
Canopy Emergency Release: open left side normally<br />
pull right side with approx. 15 kg / 33 lbs force to <strong>st</strong>op<br />
Altitude related<br />
never exceed<br />
speed:<br />
m km/h<br />
0-4500 280<br />
5000 270<br />
6000 256<br />
7000 242<br />
8000 228<br />
9000 215<br />
10000 202<br />
Altitude related<br />
never exceed<br />
speed:<br />
ft km/h<br />
0-14800 280<br />
16405 270<br />
19685 256<br />
22966 242<br />
26247 228<br />
29528 215<br />
32809 202<br />
Altitude related<br />
never exceed<br />
speed:<br />
ft kts<br />
0-14800 151<br />
16405 146<br />
19685 138<br />
22966 130<br />
26247 123<br />
29528 116<br />
32809 109<br />
Issued: October 2009 EASA app. 2.13
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