Magni Gyro M-24C Orion, Flight Manual

Page: 24 / 116

M24C_AUS
M24C FLIGHT MANUAL
.
PAGE ISSUE B
24 December 2011
2.6 INSTRUMENTS AND CONTROLS
2.6.a INSTRUMENTS (Fig.6)
COMPASS (1)
A standard magnetic compass is installed on the upper part of the instrument panel, in the panel’s centre
line.
AIR-SPEED INDICATOR (ASI) (2)
The air-speed indicator has a range between 0 and 120 mph. (20-120 Kn when in Knots) The indicated
speed is derived from the difference between dynamic 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.
ALTIMETER (ALT) (3)
Three-pointer altimeter with 0 - 20.000 ft scale. The indicator is supplied with a barometric scale (in
millibar) to adjust for atmospheric pressure.
Pressure is monitored through the static port.
VERTICAL SPEED INDICATOR (VSI) (4) (Optional)
The vertical speed indicator is an optional instrument. It is positioned next to the altimeter. This instrument
is calibrated in ft/min. It is connected to the static head port.
GPS EQUIPMENT (Optional) (5)
The position and type of GPS equipment (global positioning system) is left to the user’s discretion.
The operator manual of the GPS is supplied together with the equipment.