Wiring, A. general considerations and recommendations – ACR&Artex B406-4 User Manual

Page 65

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25-62-03

Page 65 of 87

JUN 20/13

ACR ELECTRONICS, INC / ARTEX PRODUCTS

DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL

B406-4 (453-5004)

TASK 25-62-03-450-805

6. Wiring

SUBTASK 25-62-03-990-001

A. General Considerations and Recommendations

CAUTION:

IF GROUND OR OTHER CONNECTIONS ARE BROKEN OR OTHERWISE DAMAGED, THE

ELT IS STILL CAPABLE OF AUTOMATIC ACTIVATION; HOWEVER, THE COCKPIT

REMOTE SWITCH MAY BE INCAPABLE OF RESETTING THE ELT AND OPERATION MAY

NOT BE INDICATED ON THE REMOTE SWITCH LED.

CAUTION:

INCORRECT TERMINATION OF THE WIRING IN THE CONNECTORS MAY DAMAGE THE

ELT, CAUSE TRANSMISSION ISSUES, OR RESULT IN A NON-FUNCTIONING REMOTE

SWITCH. VERIFY THE WIRING AGAINST THE WIRING DIAGRAM AND PERFORM A

CONTINUITY CHECK TO CONFIRM GOOD CONNECTIONS AND PROPER PIN

LOCATIONS.

CAUTION:

TO PREVENT INADVERTENT ELT ACTIVATION OR POSSIBLE COMPONENT DAMAGE,

DO NOT CONNECT THE HARNESS TO THE ELT OR COCKPIT REMOTE SWITCH PANEL

UNTIL ALL POWER AND GROUND WIRING CONNECTIONS ARE COMPLETED.

(1)

The following wiring and grounding considerations and recommendations are applicable:

(a)

Minimum 22 AWG wire size.

(b)

Shielding is recommended to help prevent EMI and RF interference.

(c)

Use high quality conductor meeting MIL-W-16878, M22759, M27500, or a commercial

equivalent acceptable for use in aircraft applications.

(d)

Provide a “Drip Loop” in the remote switch harness connection to the ELT to divert

moisture from the connector. See TASK 25-62-03-990-805 on page 21 for a definition.

(e)

Provide a “Service Loop” in the remote switch harness connection to the remote switch

panel, such that the assembly can be withdrawn from the panel far enough to easily

disconnect the harness plug. See TASK 25-62-03-990-805 on page 21 for a definition.

(f)

ELT and remote switch panel grounds must be common to aircraft ground.

SUBTASK 25-62-03-450-001

B. Remote Switch Panel Harness Fabrication and Installation

(1)

In most cases, the aircraft has been pre-provisioned with wiring for connecting the ELT to the

G737 control panel (remote switch panel assembly). Install a remote switch panel harness in

accordance with the following instructions ONLY if wiring has not been provided and/or spare

wires are not available.

NOTE: If spare wires are used, terminate the wires in accordance with Figure 19. Remote

Switch Panel Harness Wiring Diagram on page 66, and the procedures herein.

NOTE: If an ELT/NAV Interface -B (453-6501) is being installed with the ELT, refer to the

“ELT/NAV Interface -B Description, Operation, Installation and Maintenance Manual”

(570-6501) for additional wiring instructions.

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