BendixKing KLN 900 - Pilots Guide User Manual

Page 152

5-45

5.11.1 The Other 9 Page (OTH 9)
Without a fuel management system this becomes the
OTH 5 page. The following information is displayed
(figure 5-131):

TAS

True airspeed (the true speed of an aircraft
through the surrounding air mass)

MACH Mach number (the ratio of the true airspeed to

the speed of sound at a particular flight
condition).

If a compatible source of heading information is provided
to the KLN 900 and your groundspeed is greater than
30 knots, the following wind data is also displayed (figure
5-132):

TLWND Tailwind component of the wind
HDWND Headwind component of the wind
WIND

The wind “from” direction relative to true North
and the wind speed

5.11.2 The Other 10 Page (OTH 10)
Without a fuel management system this become the
OTH 6 page. The following information is displayed
(figure 5-133):

SAT

Static air temperature (the actual tempera-
ture of the surrounding air mass)

TAT

Total air temperature(the air temperature
including heat rise due to compressibility.
This is the temperature measured directly by
the OAT probe.

PRS

Pressure altitude (to nearest 100 feet or 10
meters)

DEN

Density altitude (to nearest 100 feet or
meters).

Rev 2

Figure 5-131

Figure 5-132

Figure 5-133