SPIDER Spider 8, Instruction Manual

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(C)Spider 8 Electromagnetic Compatibility Test
Procedure
(C)1.Test Definition
The purpose of these test procedures is to demonstrate Electromagnetic Compatibility
(EMC) between the aircraft’s electrical or electronic systems, and the Spider 8 being tested.
This test procedure is an aircraft-level test, to determine if there is any electromagnetic or
radio frequency interference (EMI/RFI) to the various critical aircraft systems, radios and
installed equipment.
(C)2.Special Tools and Equipment
The following equipment may be required depending on aircraft installed equipment and
availability of navigation aids and ATC radar in the area where testing is conducted.
a. NAV/COM Ramp Tester (e.g. NAV-402AP, IFR-4000);
b. Transponder/DME Ramp Tester (e.g. ATC-600A, ATC-601, IFR-6000);
c. TCAS Ramp Tester (e.g. TCAS-201, IFR-6000);
d. Headsets; and
e. Other equipment as required to exercise all modes of operation for systems under
test.
(C)3.Test Conditions
All aircraft systems under test must be functional prior to starting the EMC test. Any reduced
functionality of the system(s) should be noted. All testing shall be conducted in day VFR
conditions with a clear view of the sky to ensure that a GPS fix can be obtained for starting
the Iridium transmission.
For the test, the following conditions are required:
a. All engines running with all generators online (for part of the test);
b. All electrical busses powered; and
c. All avionics/electrical systems and installed equipment powered and active.