Table of Contents
Advertisement
User Manual
9. Option -160: RTCA / DO-160 Rev D, E
9.1 General
Option –160 includes a firmware implementation for RTCA/DO160 revision D including change 2,
section 16. For testing to revision E, the GUI ba
software based avionics tests (DO160 Rev E) are
CI P/N 4994-971, which is d
Thi user manual assumes tha
s
sta dard. No attempt is made
n
The RTCA/DO-160D option is c
16, RTCA/DO-160D change No2 and EUROCAE-14D / RT
signal. A selection is made available to specify the typ
available EUT groups.
Throughout this document, RTCA/DO-160D ch
thr ugh 3 will be used to refer to the EUROCAE-14
o
will be used to refer to the RTCA2 standard.
9.2 In
itial Setup
Nominal parameters for the AC Power source are as follows:
Output Voltage
Output Frequ
Nomin
al parameters for the DC Power source are as follows:
Output Voltage
Note: A setting outside these nominal values will disable the test and will prevent access to
the DO160 Menu screens.
The Compact i/iX Series has a maximum voltage range for 300Vrms. Consequently, not all tests for
230VAC nominal input volt
California Instruments
istributed on the same CD as this manual.
t the user is familiar with the text of the relevant DO160, section 16 test
to explain or elaborate on the actual test specification.
apable of performing most sub-sections of RTCA/DO-160D, Section
115V L-N or 230V L-N.
ency
360 Hz to 800 Hz
28V or 14
age EUT's can be performed.
sed software implementation is available. The
covered by a separate Avionics Software Manual,
CA DO160D, Section 16 for the AC Source
e of standard to be applied to the EUT and the
ange No2 will be referred to as RTCA2. Groups 1
D standard. Category A(CF), A(NF) and A(WF)
V L-N
2253i / 2253iX
111
Advertisement
Table of Contents
