Lancair Columbia 400 Information Manual page 229

Columbia 400 (LC41-550FG)
HSI Moving Map Range and View Button (Range/View) – When selected, the
•
Range/View button allows the left knob to control the HSI's moving map range
and view. Pushing the left knob will cycle the HSI through the four HSI views.
Turning the left knob will change the HSI moving map range (when in view).
Only two of the four allowable modes will contain a moving map depiction. The
allowable modes and knob label varies as follows:
360° with moving map
360° with no moving map
120° with moving map
120° with no moving map
Initialization
The Entegra PFD is equipped with a solid state Air Data and Attitude Heading Reference System
(ADAHRS) which requires a 3 to 5 minute alignment time prior to flight.
The Entegra PFD is
designed to operate
during engine start
and shut down
procedures. PFD start-
up is automatic once
power is applied via
the battery switch.
Engine start will not
affect the ADAHRS
alignment. A common
Entegra PFD startup procedure is to turn on the battery and conduct the aircraft preflight during
the ADAHRS alignment process.
The PFD presents the initialization display immediately after power is applied. The software
version number and the aircraft the speeds are configured for are listed in the initialization box.
The PFD presents the Initialization Display immediately after power is applied. Remain
stationary until the warm-up block is removed. Typical alignment time is 3 minutes but may take
longer if the aircraft is subjected to forward motion. Air data (airspeed, altitude, vertical speed)
will become valid prior to attitude data. The warm-up block is automatically removed when
warm-up is complete. The warmup block automatically transitions to the next several boxes and
then is automatically removed when warmup is complete.
For faster alignment (3 minutes or less) it is recommended that the aircraft
not be moved until alignment is complete. The OK TO TAXI screen is
provided for increased flexibility during ground operations, but it may
extend overall alignment time.
Initial Issue of Manual: November 10, 2004
Latest Revision Level/Date: -/11-10-2004
View Selection
NOTE
Description of the Airplane and Systems
Left Knob Label
Section 7
RC050002
7-37