DG Flugzeugbau LS10-st Manual de vuelo - Página 13

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7.15 Pitot-/Static pressure system

1 Multi Probe : Pitot-/Static-/TE pressure port

2 Pitot pressure port at fuselage nose.

3 Static pressure port for airspeed indicator and altimeter – forward fuselage

sides.

Vacuum Bottles.

A ASI

Altimeter

C Variometer

D Electrical Variometer

Colours of instrument lines:

1 Multi Probe:

Pitot

Static

2 Front total pressure

3 Static pressure front

4 Variometer capacity bottles

Note: To preserve the sealing-rings inside the holder for the Multi Probe, the end

of the probe should be greased with e.g. Vaseline from time to time.

Issued: December 2011

Flight Manual LS10-s,-st

E Capacity bottles for variometers

G Variometer switch (Option):

TE (Soaring) / static ( Engine operstion)

(switch shown in „SOARING" position

clear

red

green

yellow

blue (for ASI and altimeter only!)

clear Ø8 mm (0,315 in)

TN LS10-02

7.33