Eagle P139-HD, Installation Manual

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GA1-2TP Rev C Page 4 of 7
Items To Evaluate
The following is a list of aircraft systems or components that must be evaluated for
the effects of EMI if they are installed and are to be used at the same time as the
EUT. If the item listed below is not installed or otherwise not applicable, then mark
the N/A __ field.
Engine Temperature Indicator N/A __ Pass __ Fail __
Engine RPM Indicator N/A __ Pass __ Fail __
Engine Torque Indicator N/A __ Pass __ Fail __
Engine Fuel Control N/A __ Pass __ Fail __
Engine Oil Pressure Indicator N/A __ Pass __ Fail __
Engine Oil Temperature Indicator N/A __ Pass __ Fail __
Rotor RPM Indicator N/A __ Pass __ Fail __
Fuel Quantity Indicator N/A __ Pass __ Fail __
Fuel Pressure Indicator N/A __ Pass __ Fail __
Generator Voltage Indicator N/A __ Pass __ Fail __
Battery Voltage Indicator N/A __ Pass __ Fail __
Directional Gyro / Heading Indicator N/A __ Pass __ Fail __
Attitude Indicator N/A __ Pass __ Fail __
Turn and Bank Indicator N/A __ Pass __ Fail __
Annunciator Indicators N/A __ Pass __ Fail __
Flight Time Hour Meter N/A __ Pass __ Fail __
Warning Horn N/A __ Pass __ Fail __
Outside Air Temperature Indicator N/A __ Pass __ Fail __
Transponder N/A __ Pass __ Fail __
Set controls to mode C code 1200, or other code assigned by ATC. Cycle EUT
and confirm proper data transmitted, either by use of transponder ground test
equipment, or by confirmation from ATC of proper reception of correct data.
Check for proper operation of reply light.
VOR N/A __ Pass __ Fail __
Set Voice/Ident to Voice. Check frequencies for audible interference sounds.
Set local VOR frequency for full needle displacement. Adjust course select knob
for gradual reduction of needle displacement to half, fourth, and zero. Note
stability at each displacement and that zero can be achieved without a standoff.
DME N/A __ Pass __ Fail __
Perform self test with EUT cycled. Note that no skips in miles display occurs.
Observe that mile indications do not drift and there is no audible interference in
Ident tone.
Magnetic Compass N/A __ Pass __ Fail __
Swing compass and adjust with EUT operating normally. If EUT causes erratic
operation of magnetic compass, then mark compass as Fail.