ACR&Artex G406-4 ELT - Manual (Page 67)

25-62-21
Page 67 of 86
JUL 31/12
ACR ELECTRONICS, INC / ARTEX PRODUCTS
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
G406-4 (453-5012)
(6) Crimp appropriately sized ring terminals on the buzzer ends of the buzzer power and ground
wires.
(7) Crimp an appropriately sized ring terminal on the airframe end of the Pin 11 ground wire.
(8) Crimp an appropriately sized ring terminal on the remote switch power source wire end.
NOTE: If desired, the power wire may be spliced to a power source in a manner acceptable
to the aircraft manufacturer, or as described in AC 43.13-1, Paragraph 11-167.
(9) Crimp female terminal pins (151-6628) to the cockpit remote switch end, as follows:
NOTE: Use Molex crimp tool 63811-3300, or an equivalent tool for 0.062 in. terminal pins.
(a) Each harness wire.
(b) Remote switch ground wire.
(c) Remote switch power wire.
(10) Bundle the wiring into a complete harness, with breakouts as appropriate, such that the wiring
can be properly supported and attached to the airframe. Refer to the aircraft manufacturer’s
written instructions or AC 43.13-1, Chapter 11, § 9 through 12, as applicable.
SUBTASK 25-62-21-450-002
C. ELT 12-Pin Receptacle Installation
(1) Feed the harness wires on the ELT end through the mounting frame cap assembly (452-
0228). See "Figure 20. Remote Harness Wiring at ELT End".
Figure 20. Remote Harness Wiring at ELT End
12-PIN MOLEX
RECEPTACLE
PIN 1
NOTE: FEED THE WIRE BUNDLE THROUGH THE MOUNTING
FRAME CAP HOLE PRIOR TO INSERTING THE PINS INTO THE
RECEPTACLE
TO COCKPIT REMOTE
SWITCH AND GROUND