STEMME S6 User Manual

FLIGHT MANUAL TSA-M, VARIANT S6
Doc.-No.: P400-006.000 E Page: 7-43 Revision: 10
Date of Issue: 07. October 2008 Date of Rev.: 06.07.2020
7.14 Static-Pressure- and Dynamic-Pressure-System ______
A tubular probe measures the total-pressure, static-pressure and total-energy-
compensated-pressure (TEC-pressure). It is located at the left wing-joint
between the inner-wing and outer-wing. The pressure-sensing-lines lead to the
center of the wing. There, they need to be connected to the adapters of the mid-
section of the fuselage. From there, the lines are lead to the rear side of the
instrument-panel.
All tubes of the pressure-system in the forward area of the cockpit are equipped
with filters against moisture and dust.
The assignment of the pressure-ports of different instruments (standard
instruments and optional instruments) to the pressure-system can be taken from
the maintenance manual.

STEMME S6 Specifications

General

Brand	STEMME
Model	S6
Category	Aircrafts
Language	English