The Other 9 Page (Oth 9); The Other 10 Page (Oth 10) - Honeywell KLN 900s Pilot's Manual

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).
AIR DATA
TAS
MACH
OTH 9
AIR DATA
TAS
MACH
HDWND
WIND
OTH 9
AIR DATA
SAT
TAT
PRS
DEN
OTH10
5-45
|
229kt|
.34|
|
|
|
Figure 5-131
|
229kt|
.34|
30kt|
078^%|
32kt|
Figure 5-132
|
|
20^C|
26^C|
6500ft|
9100ft|
Figure 5-133
Rev 2