Garmin 011-01257-20 Installationshandbuch - Seite 32
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4.3
J3472 Connector Pin Assignments
This section covers the pin connections of J3472 only.
4.3.1 Aircraft Power and Lighting
Power Input requirements and Lighting Bus inputs are listed in the following tables. The power-input
pins accept 11-33 Vdc. AIRCRAFT POWER 2 is for connecting to an alternate power source, such as on
aircraft with two electrical buses. Refer to Figure B-1 for power and lighting interconnections.
Table 4-3. Aircraft Power Pin Assignments, J3472
Pin
Pin Name
53
AIRCRAFT POWER 1
55
AIRCRAFT POWER 1
30
AIRCRAFT POWER 2
32
AIRCRAFT POWER 2
69
POWER GROUND
71
POWER GROUND
14
POWER GROUND
16
POWER GROUND
27
GMA REMOTE POWER OFF
Pins 53 and 55 of J3472 are internally connected to form AIRCRAFT POWER 1. Pins 30 and 32 of
J3472 are internally connected to form AIRCRAFT POWER 2. AIRCRAFT POWER 1 and AIRCRAFT
POWER 2 are "diode ORed" to provide power redundancy.
4.3.2 Lighting Bus
The GMA 1347D can be configured to track a 28 Vdc or 14 Vdc lighting bus using these inputs. The
GMA 1347D can also automatically adjust for ambient lighting conditions based on photocell input on
the PFD/MFD by digital means.
Table 4-4. Aircraft Lighting Pin Assignments, J3472
Pin
Pin Name
51
14 V LIGHTING HI
52
28 V LIGHTING HI
Page 4-6
Revision C
Description
Unit power
Unit power
Unit power
Unit power
Aircraft ground
Aircraft ground
Aircraft ground
Aircraft ground
ARINC active high signal turns unit off
Description
14V Backlighting input, 0 to 14 Vdc
28V Backlighting input, 0 to 28 Vdc
GMA 1347D Installation Manual
190-00303-21
I/O
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