Honeywell BENDIX/KING KLN 94, Руководство пилота

Страница: 171 / 284

5.13.4. THE AUXILARY (AUX 18) FUEL MANAGEMENT PAGE
The AUX 18 page displays rate of
fuel flow. It has two formats depend-
ing on whether the aircraft is a twin
engine (figure 5-98) or a single
engine (figure 5-99).
5.13.5. THE AUXILARY (AUX 19) FUEL MANAGEMENT PAGE
The AUX 19 page displays the
amount of fuel used. If interfaced
with the ARNAV fuel management
computer, this page displays dashes
since the ARNAV system does not
output fuel used. There are two for-
mats depending on whether the
aircraft is a twin engine (figure 5-100)
or a single engine (figure 5-101).
5.14. THE AIR DATA (AUX 20 – AUX 21) PAGES
Specific models of Shadin Company air data systems may be interfaced
to the KLN 94. When interfaced with one of these systems, the KLN 94
will display real time air data parameters such as true airspeed (TAS), sta-
tic air temperature (SAT), total air temperature (TAT), Mach number,
density altitude, and pressure altitude. With a TAS input from an air data
computer and a compatible heading input, the KLN 94 will calculate and
display real time wind data (magnitude and direction).
NOTE : Heading information inputs to the KLN 94 must be in a format
which is different than available from most mechanical compass systems,
including the Bendix/King KCS 55A (KI 525A HSI with bootstrap heading
synchro) and KCS 305 compass systems. However, the compatible
Shadin air data system will convert three wire analog heading information
from these mechanical systems into the proper format.
KLN 94 Pilot’s Guide Chapter 5 Intermediate Operation
5-37
Figure 5-98
Figure 5-99
Figure 5-100
Figure 5-101