User Manual

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
AIR DATA |
TAS 229kt|
MACH .34|
|
|
|
OTH 9
AIR DATA |
TAS 229kt|
MACH .34|
HDWND 30kt|
WIND 078^%|
32kt|
OTH 9
Figure 5-133
AIR DATA |
|
SAT 20^C|
TAT 26^C|
PRS 6500ft|
DEN 9100ft|
OTH10