600840-000031 Stratus ES/ESG Installation Instructions
Rev. 2.2
Last Revised: February 20, 2018
Page 35 of 45
(ii) TCAS
Verify the function of the TCAS while monitoring the effects of Stratus ES/ESG. Self-test and
monitoring targets of opportunity should both be evaluated.
(iii) Weather radar
Verify the function of each weather radar system while monitoring the effects of
Stratus ES/ESG. All displays capable of showing weather radar should be evaluated.
(iv) Radio altimeter
Verify each radio altimeter system functions correctly while monitoring the effects of
Stratus ES/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 EMI tests above, evaluate the necessity of a swing test.
5.7. Weight and balance
Installation of Stratus ES/ESG may have impacted the weight and balance of the aircraft. Refer
to Chapter 7 of FAA-H-8083-1B: Weight and Balance Handbook.
5.8. 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 ES/ESG. A compliance report can be obtained by emailing 9-AWA-AFS-
300-ADSB-AvionicsCheck@faa.gov with the aircraft information. This method is controlled by
the FAA and may be subject to change.
For additional information visit the FAA website: www.faa.gov/nextgen/equipadsb.
6. Using Stratus ES/ESG
See the Stratus ES/ESG Pilot’s Guide (600890-000049) for a full description of
Stratus ES/ESG’s function.
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