ACR&Artex C406-N - Manual (Page 71)

25-62-13
Page 71 of 109
MAR 1/13
ACR ELECTRONICS, INC / ARTEX PRODUCTS
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-N (453-5060), C406-N HM (453-5061)
(8) Crimp appropriately sized ring terminals on the airframe ends of the following wires:
(a) Harness ELT plug Pin 11 ground wire.
(b) Harness ELT plug strain relief ground wire.
(c) Remote switch plug ground wire.
(9) Crimp appropriately sized ring terminals on the airframe ends of the following wires:
NOTE: If desired, the power wires may be spliced or otherwise connected to their individual
power sources in a manner acceptable to the aircraft manufacturer, or as described
in AC 43.13-1, Paragraph 11-167.
(a) Harness ELT plug +28 VDC switchable power source wire. Use a power source
controlled by the avionics switch or master switch. This circuit draws power at all times
and will drain the battery if not switched off. See SUBTASK 25-62-13-450-006 on
page 74 for circuit protection requirements.
(b) Harness remote switch plug +28 VDC battery power source wire. This power source
must be direct from the battery. Use the clock circuit or a similar source of battery
power. See SUBTASK 25-62-13-450-007 on page 74 for circuit protection requirements.
(10) Provide a means of termination on the airframe end of the ARINC 429 twisted pair of wires
compatible with the aircraft navigation system ARINFC 429 output source.
(11) 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 +28 VDC battery power wire.
(12) 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.