DG Flugzeugbau LS8 Series Руководство по техническому обслуживанию - Страница 4

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7 Placards and markings

Numbers refer to placards, for positions of placards see drawings

7.1 LS8

LS 8 Checklist

This sailplane must be operated

in compliance with operating

limitations stated in the form

of markings, placards and Flight

Manual.

1. Main pins secured ?

2. Horizontal tail secured ?

3. Winglets secured ?

4. Test controls ?

5. Tail fin valve operating checked ?

6. When water ballast, then always

in wings and tail tank !

7. Check loading conditions

8. Check tail dolly removed

9. Fasten seat belt harness

10. Connect parachute static line

11. Lock air brakes

12. Check trim position

13. Check release system

14. Lock canopy

>1< at under side of instrument panel

Tyre Pressure

For 4" wheel, on right

3 - 3.5 bar

landing gear door

43.5 to 50.8 psi

Tyre Pressure

For 5" wheel, on right

3.5 bar

landing gear door

50.8 psi

Tyre Pressure

Above tail wheel,

2.5 - 3.5 bar

when fitted

36.3 to 50.8 psi

Tyre Pressure

above tailwheel

6,2 bar/90 psi

small tailwheel according to TN 8021, if installed

Maximum Baggage mass 5 kg / 11 lbs

(Soft items only)

DG Flugzeugbau GmbH

TYPE

LS 8

TCDS

A.047

Serial No.

8xxx

Registration

D-xxxx

>4< Type placard at main bulkhead

Issued: January 2015

Manual valid with the up-to-date cover page only

Maintenance Manual LS8

at main bulkhead

Made in

Germany

TN8021

MINIMUM COCKPIT LOAD :________kg / lbs

Minimum Cockpit Load with empty tail tank:___kg/lbs

>2< under instrument panel cover

DG Flugzeugbau GmbH

Type: LS 8 Serial Number: 8_____

Data Placard

Airspeed Limits (IAS)

Winch Launch / Auto-Tow

Aerotow

In Rough Air

Never exceed (VNE)

Maximum Take-off Mass 525 kg (1157 lbs) including

Water Ballast

Aerobatic manoeuvres not approved

mass Limitations

Maximum Cockpit Load

Minimum Cockpit Load

Minimum Cockpit Load with

tail fin tank empty

and without tail battery ______kg ______lbs

Minimum Cockpit Loads for all combinations of tail

tank and tail battery see Flight Manual pages 6-1/2.

Lighter pilots must compensate lack of mass

as suggested in Flight Manual

Ball of bearing

at forward horizontal tail

Must be fixed

attachment on vertical tail fin

Batt. I

Batt. II positions

OFF

km/h mph Kt.

140

190 118 103

280 174 151

______kg ______lbs

>3< at right cockpit side

Electrical switch

7-1