PS Engineering PMA8000G System Installation And Operation Manual - page 21
PS Engineering
PMA8000G IntelliAudio Audio Selector Panel With flightmate®
Installation and Operator’s Manual
200-890-0912
Page 2-14
Rev. 7, July 2017
2.13.3 Marker Checkout
1.
Connect a ramp generator at the antenna end of the marker coax. With the unit under test in HI sensi-
tivity, verify that a 160
V, modulated 95% with 1300 Hz, signal will illuminate the amber (M) marker
light, and that marker audio is present in the headphones when the Marker Audio (MKR) push-button
has been depressed. Select SPR for speaker to verify marker audio availability on the cabin speaker.
Verify that the white (I) and blue (O) lights will illuminate within
3dB of the amber lamp, with 3000
HZ and 400 Hz applied, respectively.
2.
Repeat with the unit in LOW sensitivity, with 430
Volts applied.
3.
Connect the marker antenna and verify proper operation.
2.13.4 Bluetooth Checkout
Verify that the PMA8000G will “pair” with a Bluetooth device, and interface with cellular phone and Mu-
sic source.
2.13.5 Internal Recorder Checkout- PLAYBACK
With headset plugged into pilot’s side jacks, tune COM 1 to local frequency, such as
FSS or ATC ground. Select Com 1 on mic selector switch, and record several incom-
ing radio transmissions.
Momentarily press the PLAY button on the front panel. This action will then automat-
ically play back the last recorded message. Momentarily press the PLAY button again
to stop the play back, and then momentarily press again to play prior messages.
This audio should appear in the pilot and copilot headsets, and only be incoming transmissions from the
transceiver selected in the mic select switch.
Depress the audio panels yoke mounted playback switch (hardwire), and verify that messages play, in the
order received. Repeat for COM 2 The playback will be stopped by audio on the selected com. The mes-
sage can be replayed from the beginning, and audio received during the playback will not be stored.
See
§2.5
for full flightmate information.
2.14 Final Inspection
Verify that the wiring is bundled away from all controls and no part of the installation interferes with air-
craft control operation. Move all controls through their full range while examining the installation to see
that no mechanical interference exists. Verify that the cables are secured to the aircraft structure in accord-
ance with good practices, with adequate strain relief. Ensure that there are no kinks or sharp bends in the
cables and coaxial cables. Verify that the cables are not exposed to any sharp edges or rough surfaces, and
that all contact points are protected from abrasion.
Complete documentation that may be required, such as a logbook entry, weight and balance computation
and FAA Form 337. Sample text for FAA Form 337, and instructions for continuing airworthiness can be
found in Appendix F. Return completed warranty registration application to PS Engineering, or complete
online at www.ps-engineering.com
.
PS Engineering
PMA8000G IntelliAudio Audio Selector Panel With flightmate®
Installation and Operator’s Manual
200-890-0912
Page 2-14
Rev. 7, July 2017
2.13.3 Marker Checkout
1.
Connect a ramp generator at the antenna end of the marker coax. With the unit under test in HI sensi-
tivity, verify that a 160
V, modulated 95% with 1300 Hz, signal will illuminate the amber (M) marker
light, and that marker audio is present in the headphones when the Marker Audio (MKR) push-button
has been depressed. Select SPR for speaker to verify marker audio availability on the cabin speaker.
Verify that the white (I) and blue (O) lights will illuminate within
3dB of the amber lamp, with 3000
HZ and 400 Hz applied, respectively.
2.
Repeat with the unit in LOW sensitivity, with 430
Volts applied.
3.
Connect the marker antenna and verify proper operation.
2.13.4 Bluetooth Checkout
Verify that the PMA8000G will “pair” with a Bluetooth device, and interface with cellular phone and Mu-
sic source.
2.13.5 Internal Recorder Checkout- PLAYBACK
With headset plugged into pilot’s side jacks, tune COM 1 to local frequency, such as
FSS or ATC ground. Select Com 1 on mic selector switch, and record several incom-
ing radio transmissions.
Momentarily press the PLAY button on the front panel. This action will then automat-
ically play back the last recorded message. Momentarily press the PLAY button again
to stop the play back, and then momentarily press again to play prior messages.
This audio should appear in the pilot and copilot headsets, and only be incoming transmissions from the
transceiver selected in the mic select switch.
Depress the audio panels yoke mounted playback switch (hardwire), and verify that messages play, in the
order received. Repeat for COM 2 The playback will be stopped by audio on the selected com. The mes-
sage can be replayed from the beginning, and audio received during the playback will not be stored.
See
§2.5
for full flightmate information.
2.14 Final Inspection
Verify that the wiring is bundled away from all controls and no part of the installation interferes with air-
craft control operation. Move all controls through their full range while examining the installation to see
that no mechanical interference exists. Verify that the cables are secured to the aircraft structure in accord-
ance with good practices, with adequate strain relief. Ensure that there are no kinks or sharp bends in the
cables and coaxial cables. Verify that the cables are not exposed to any sharp edges or rough surfaces, and
that all contact points are protected from abrasion.
Complete documentation that may be required, such as a logbook entry, weight and balance computation
and FAA Form 337. Sample text for FAA Form 337, and instructions for continuing airworthiness can be
found in Appendix F. Return completed warranty registration application to PS Engineering, or complete
online at www.ps-engineering.com
.
PS Engineering
PMA8000G IntelliAudio Audio Selector Panel With flightmate®
Installation and Operator’s Manual
200-890-0912
Page 2-14
Rev. 7, July 2017
2.13.3 Marker Checkout
1.
Connect a ramp generator at the antenna end of the marker coax. With the unit under test in HI sensi-
tivity, verify that a 160
V, modulated 95% with 1300 Hz, signal will illuminate the amber (M) marker
light, and that marker audio is present in the headphones when the Marker Audio (MKR) push-button
has been depressed. Select SPR for speaker to verify marker audio availability on the cabin speaker.
Verify that the white (I) and blue (O) lights will illuminate within
3dB of the amber lamp, with 3000
HZ and 400 Hz applied, respectively.
2.
Repeat with the unit in LOW sensitivity, with 430
Volts applied.
3.
Connect the marker antenna and verify proper operation.
2.13.4 Bluetooth Checkout
Verify that the PMA8000G will “pair” with a Bluetooth device, and interface with cellular phone and Mu-
sic source.
2.13.5 Internal Recorder Checkout- PLAYBACK
With headset plugged into pilot’s side jacks, tune COM 1 to local frequency, such as
FSS or ATC ground. Select Com 1 on mic selector switch, and record several incom-
ing radio transmissions.
Momentarily press the PLAY button on the front panel. This action will then automat-
ically play back the last recorded message. Momentarily press the PLAY button again
to stop the play back, and then momentarily press again to play prior messages.
This audio should appear in the pilot and copilot headsets, and only be incoming transmissions from the
transceiver selected in the mic select switch.
Depress the audio panels yoke mounted playback switch (hardwire), and verify that messages play, in the
order received. Repeat for COM 2 The playback will be stopped by audio on the selected com. The mes-
sage can be replayed from the beginning, and audio received during the playback will not be stored.
See
§2.5
for full flightmate information.
2.14 Final Inspection
Verify that the wiring is bundled away from all controls and no part of the installation interferes with air-
craft control operation. Move all controls through their full range while examining the installation to see
that no mechanical interference exists. Verify that the cables are secured to the aircraft structure in accord-
ance with good practices, with adequate strain relief. Ensure that there are no kinks or sharp bends in the
cables and coaxial cables. Verify that the cables are not exposed to any sharp edges or rough surfaces, and
that all contact points are protected from abrasion.
Complete documentation that may be required, such as a logbook entry, weight and balance computation
and FAA Form 337. Sample text for FAA Form 337, and instructions for continuing airworthiness can be
found in Appendix F. Return completed warranty registration application to PS Engineering, or complete
online at www.ps-engineering.com
.