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Dynon SkyView HDX - Instructions for Continued Airworthiness

Dynon SkyView HDX
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Appendix A: Maintenance and Troubleshooting
23-10 SkyView HDX System Installation Manual - Revision E
23.8.9 External Light Control Signal Output
SkyView displays are compatible with external light control signals. The state of the
external light control signal is shown here.
23.8.10 Brightness Level Output
SkyView displays can output a brightness level signal to control the brightness of
compatible external equipment screens. The level of the output is shown here.
23.8.11 Contact Input Status
Each SkyView display has four (4) contact inputs. The status of each contact input is
shown here as either HIGH or LOW. CONTACT INPUT 1 is implemented as EXTERNAL
LEVEL button. CONTACT INPUT 2 is implemented as EXTERNAL GO AROUND button.
CONTACT INPUT 3 and CONTACT INPUT 4 have not been implemented.
23.8.12 Serial Port Status and Current Baud Rate
Each SkyView display has five (5) general purpose serial ports. The status of each serial
port is shown with transmit (TX) and receive (RX) character counters and the ports current
baud rate. The character counters show any outgoing or incoming character and roll over
at 9999.
23.8.13 Button and Joystick States
The state of each button is shown on the BUTTON STATE line. You will see 1 2 3 4 5 6
7 8 on the line. When you press a button, its respective number on the button state line
is replaced with an asterisk (*). For example, if you press and hold button 3, you will see
1 2 * 4 5 6 7 8.
The state of each joystick is shown on the JOYSTICK STATE line. Each joystick is
denoted with an L or R (left or right, respectively), a counter to show joystick turns, and
the letters UDLRC to denote moving the joystick Up, Down, Left, Right, and Center (when
pressed like a button).
23.8.14 Operational Hours
This is a running count of the hours a screen has been on since was initially
manufactured.
23.9 Instructions for Continued Airworthiness
Follow these steps for continued airworthiness:
Conduct any periodic checks that are mandated by local regulations (IE, FAA
for US Aircraft), such as (but not limited to):
o Transponder test
o Pitot / Static system test - refer to “Performing Pitot/Static Checks” near the
end of the SV-ADAHRS-200 Installation and Configuration section.
Annually test the SV-BAT-320 Backup Battery.
Annually perform a ZERO PRESSURE IAS/AOA CALIBRATION.

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