Audio International, Inc. CL12/16 Watt Series Cabin Light
Installation & Operations
Document #540037, Rev. B, 4/2000
Page 6 of 11
3.3
Cautions and Warnings
3.3.1 It is important to do a pin-to-pin power and ground check on all
connectors. Ensure that power and ground are applied only where
specified. Damage to the unit may result if power or ground is
applied to the wrong points.
3.3.2 DO NOT connect or disconnect the module while power is applied.
3.3.3 DO NOT remove any factory-installed screws. Damage to the units
may result and void any warranties.
3.3.4 ESD (Electro Static Discharge) guidelines shall be followed.
3.4
Wiring
Requirements
3.4.1 Introduction
The installing agency shall supply and fabricate all external cables
and mating connectors. The length and routing of external cables
must be carefully studied and planned before attempting installation
of the units. Allow adequate space for installation of cable and
connectors. Avoid sharp bends and placing cables near aircraft
control cables. Maintain a minimum clearance of three (3) inches
from any control cable. If wiring is run parallel to combustible fluid
or oxygen lines, maintain a separation of six (6) inches between the
lines.
3.4.2 Power
Wires
All power and ground wires shall be 22 AWG, minimum. Power
ground wires shall be grounded within twelve (12) inches of the
unit. All wires shall be in accordance with MIL-W-22759 or
equivalent. Twisted, shielded cable shall be in accordance with
MIL-W-27500 or equivalent. Protect power wires with circuit
breakers or fuses located close to the electrical power source bus.
3.5
Physical Characteristics
3.5.1 Refer to Section 6.0 for unit dimensions.
3.5.2 When mounting the unit, allow sufficient space for mating
connectors.
3.6 Electrical Characteristics
3.6.1 The lights may be ordered with or without connectors. Refer to
section 1.2 to determine the connector supplied with the unit.
3.6.2 Refer to section 3.7 to determine pin connections as well as the
lighting options supplied with the unit.
