Appareo Systems LLC 1505005 Benutzerhandbuch
600840-000031 Stratus ESG Installation Instructions
Rev. 1.1
Last Revised: January 6, 2016
Page 30 of 42
9
Suppression
Check correctness of suppression input
polarity
polarity
10
FPGA Checksum
Contact Appareo
11
EEPROM Checksum
Re-configure Stratus ESG. Verify that
the GPS Week Number Rollover is set
to the correct value.
the GPS Week Number Rollover is set
to the correct value.
12
Squitter Rate
Contact Appareo
13
Mode S Address
Contact Appareo
14
GPS Failure
Contact Appareo
15
1030 MHz RX VCO Lock
Contact Appareo
16
DSC RAM
Contact Appareo
17
FPGA RAM
Contact Appareo
18
GPS Failure
Contact Appareo
19
GPS Failure
Contact Appareo
Table 24: BIT diagnostic codes
5. Functional tests
Final installation checks for Stratus ESG are the responsibility of the installer. The installer must
ensure that Stratus ESG is installed on an aircraft that coincides with the approval given within
the testing performed for the TSOs held by this device (TSO-C112e, TSO-C145d, and TSO-
C166b).
ensure that Stratus ESG is installed on an aircraft that coincides with the approval given within
the testing performed for the TSOs held by this device (TSO-C112e, TSO-C145d, and TSO-
C166b).
After installation is complete, verify function as identified in 14 CFR Part 43, Appendix F. The
IFR6000 with OPT3 (manufactured by Cobham AvComm
IFR6000 with OPT3 (manufactured by Cobham AvComm
– formerly Aeroflex Test Solutions) or
equivalent test set can be used to determine compliance.
Additional testing requirements can be found in Chapter 4 of Advisory Circular (AC) 20-165B.
Additional functional tests may be required.
Additional functional tests may be required.
Aircraft using Stratus ESG must be compliant with 14 CFR Part 91, Sections 91.215 and
91.225. While in airspace specified in 14 CFR Part 91.215, Stratus ESG must be maintained to
14 CFR Part 91.413. When installed correctly, Stratus ESG complies with 14 CFR Part 91.225.
91.225. While in airspace specified in 14 CFR Part 91.215, Stratus ESG must be maintained to
14 CFR Part 91.413. When installed correctly, Stratus ESG complies with 14 CFR Part 91.225.
In addition to maintaining compliance to the regulations above, perform the following functional
tests after configuration.
tests after configuration.
NOTE: Functional tests should be executed in an area where the aircraft has an unimpeded
view of the sky, such that a proper GPS fix can be established.
view of the sky, such that a proper GPS fix can be established.
5.1.
Power bus
Turn on power to the aircraft. Verify that the unit powers on.
5.2.
Discrete inputs
NOTE: Depending on the installation, the functional tests for the following discrete inputs
are optional.
are optional.