BENDIXKing AeroNav 910 Pilot's Manual page 16

AeroNav 900/880 Series Pilot's Guide
NOTE
Synthetic Vision is Not for Terrain Avoidance
The synthetic vision display may not be used as the
principal means for terrain avoidance. Synthetic
Vision may not provide the depth/distance cues
necessary for terrain avoidance and should always
be used in conjunction with other flight and
navigation information for terrain avoidance.
AERONAV 905
The BendixKing AeroNav 905 differs from the AeroNav 910 in
that there is no internal VHF nav/com radio. Its primary function
is to conduct GPS-based navigation in an IFR environment,
provided it is connected to an external navigation source
selection annunciator and a CDI/HSI indicator that is installed in
the required field of view. The AeroNav 905 cannot be used to
execute terminal area procedures that rely on radio navigation.
The AeroNav 905 bezel differs physically from the AeroNav 910
in that the radio controls along the left side of the bezel are
absent, the nav source selection knob is replaced by an OBS
button, and the volume knob is replaced by a single-function
on/off button.
Supplemental AeroNav 905 functions include a moving-map,
flight management system (FMS), electronic charts, checklists,
and a number of timer and calculator types of utilities. It also
includes options for control/display of weather radar and display
of external video. The system includes terrain alerting as well as
an option for TAWS.
The AeroNav 905 also provides a synthetic terrain/vision image to
enhance the pilot's awareness of their spatial position relative to
the terrain, obstacles and known traffic. Pitch, roll, and skid/slip
indicators also aid in attitude awareness. If the system is
receiving a heading input, then heading and rate of turn will be
displayed for additional aircraft state awareness. In degraded
conditions, the synthetic vision view will be replaced with a
traditional blue over brown attitude indication. The attitude
sensing and depiction of the AeroNav 905 provides a non-
required secondary indicator in addition to the required attitude
instrument(s) installed in the aircraft.
1-6 System Overview
89000039-010
Rev 1 May 2019