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24 July 2019
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209-00-24C
M24C PLUS FLIGHT MANUAL
103
8.2 INSTRUMENTS AND CONTROLS
8.2.1 FLIGHT INTRUMENT PANEL
Figure 8.5: Flight instrument panel
1. AIR-SPEED INDICATOR (ASI)
The indicated speed is derived from the difference between total pressure and static pressure.
The pitot tube is located at the front of the fuselage.
The static intake is connected to the two static ports located on the side of the fuselage.
2. ALTIMETER
The indicator is supplied with a barometric scale to adjust for atmospheric pressure.
Pressure is monitored through the static port.
3. VERTICAL SPEED INDICATOR (VSI) (optional)
The vertical speed indicator is an optional instrument. It is positioned next to the altimeter.
It is connected to the static head port.
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