600840-000032 Stratus ESG Installation Instructions
Rev. 1.5
Last Revised: September 22, 2016
Page 37 of 47
(iv) Radio altimeter
Verify each radio altimeter system functions correctly while monitoring the effects of
Stratus ESG. Each unit should self-test correctly and be free of continuous variation while
parked on the ramp.
(v) Engine indications & fuel flow (engines operating)
Aircraft must be taken off ground power (if necessary). Start aircraft engines. Check to be
certain that all engine indicators read appropriately.
Check to be certain that all fuel flow indicators read appropriately.
5.6.
Compass swing test
After successful completion of the above EMI tests, evaluate the necessity of a swing test.
5.7.
Flight test
NOTE
: The flight test shall not be performed until after the system functional ground test and
EMI test is complete and passes.
It is recommended that a flight test be conducted after installation to verify proper operation and
installation of Stratus ESG. A compliance report can be obtained by emailing
9-AWA-AFS-300-
with the aircraft information. This method is controlled by the
FAA and may be subject to change.
For additional information visit the FAA website:
http://www.faa.gov/nextgen/equipadsb/
.
6. Using Stratus ESG
See the Stratus ESG Pilot’s Guide (600890-000049) for a full description of Stratus ESG’s
function.
Figure 3: Stratus ESG front panel
