ACR G406-4 handleiding
Handleiding
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
G406-4 (453-5012)
570-5012 Rev. P Company Confidential 25-62-21 Page 55 of 70
NOTE: The pin with the airframe ground wire terminated in it, MUST be inserted in Pin 11.
c) Insert the buzzer power and ground wires in Pin 2 (+) and Pin 4 (–) of the receptacle,
respectively.
SUBTASK 25-62-21-450-003
D. Cockpit Remote Switch 9-Pin Plug Installation
1) Inert the wiring pins in the 151-5009 Molex 9-pin cockpit remote switch plug. See Figure 19 Remote
Switch Harness Wiring Diagram on page 53.
a) Insert each harness female pin into the plug.
NOTE: Refer to the wire identification and pin relationships recorded in Step C.(4)(b).
NOTE: Terminal pins may be removed from the plug using Molex extraction tool 11030002,
or equivalent.
b) Insert the remote switch power wire female pin into Pin 1 or Pin 3 of the plug, as appropriate for
the selected 14V or 28V power source.
c) Insert the remote switch ground wire into Pin 9 of the plug.
SUBTASK 25-62-21-450-004
E. Wiring Installation
1) Route the remote switch harness wire bundle and breakout wiring through the airframe.
2) Route the two antenna coax cables through the airframe.
NOTE: Longer coax cables, up to 20 feet (6.1 m), may be fabricated if the cables provided
are too short. Use RG-142 or RG-400 coax cable.
3) Support the wiring and coax cables by clamping or other suitable means, such that the wiring and
cables are properly supported and protected from chaffing and strain. Refer to the aircraft
manufacturer’s written instructions or as described in AC 43.13-1, Chapter 11, § 9 through 12, as
applicable.
SUBTASK 25-62-21-450-005
F. Antenna Connections
1) Connect the two coax cables to the antenna, making sure the cables are routed and supported such
that there is no tensile load (i.e., strain) on the connections.
SUBTASK 25-62-21-450-006
G. Cockpit Remote Switch Power Connection
1) Connect the remote switch power wire. If the wire is spliced, fabricate the splice in a manner
acceptable to the aircraft manufacturer or as described in AC 43.13-1, § 13.
NOTE: The power source provides energy for the remote switch assembly LED, but has no
effect on switch functions, as the switch will control the ELT with or without power.
NOTE: Power should be connected directly to the battery using a 1-amp in-line fuse or
circuit breaker; or an alternate un-switched source, such as the aircraft clock
circuitry.
SUBTASK 25-62-21-450-007
H. Remote Switch Alternate Power Source
1) If the aircraft does not have an electrical system (i.e., no battery), it is permissible to fabricate a
substitute power source for the LED, as follows:
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Productinformatie
| Merk | ACR |
| Model | G406-4 |
| Categorie | Niet gecategoriseerd |
| Taal | Nederlands |
| Grootte | 8218 MB |
