| Integrated Standby Flight Display |
Integrated Standby Flight Display (ISFD)
The ISFD displays attitude, airspeed, altitude, ILS, and
magnetic heading information. It is connected directly to the
auxiliary pitot and alternate static sources. Attitude
information is provided by internal inertial sensors. ILS
information is provided by the No. 1 ILS receiver. The
display receives its heading information from the same
source as the captain’s primary flight display. Heading
information is not available in polar regions.
The standby magnetic compass must be used to validate
the heading information provided by the ISFD.
An ambient light sensor automatically adjusts display
intensity for ambient light conditions.
The ISFD displays attitude, airspeed, altitude, ILS, and
magnetic heading information. It is connected directly to the
auxiliary pitot and alternate static sources. Attitude
information is provided by internal inertial sensors. ILS
information is provided by the No. 1 ILS receiver. The
display receives its heading information from the same
source as the captain’s primary flight display. Heading
information is not available in polar regions.
The standby magnetic compass must be used to validate
the heading information provided by the ISFD.
An ambient light sensor automatically adjusts display
intensity for ambient light conditions.
| Tap the control or indication for a description of its function. |
