UAV-1004233-001, AV-30-E Pilot’s Guide
12
Revision A
Aircraft Power
Optional Pitot System
Optional Static System
EL
EC
TR
IC
AL
IN
TE
RF
AC
ES
Digital
Optional OAT Probe
Analog
AIRCRAFT SYSTEMS
Optional GPS Navigator
AV-30-E
PN
EU
M
ATI
C
CO
NN
EC
TO
RS
Figure 3 – AV-30-E Aircraft Systems Interfaces – DG Mode
When installed as a DG, no audio outputs are supported, and air data
related parameters are only available when the optional OAT probe is
equipped.
5.2 Power Input (Required)
Power input is required in both AI and DG configurations and each
unit has a dedicated circuit breaker. The power input is internally
diode OR’ed with the unit’s internal battery via a processor-controlled
switch. This architecture allows the unit to continue operation if
external power fluctuates or is completely lost.
When external power is supplied to the AV-30-E, there is no
mechanism to turn the unit off. When operating on battery, the unit
may be forced off with a user interface action. Reference
Section 10 -
