DeCrane Aerospace Audio International
DVD-9101-201-x Installation & Operation Manual
Document # 540339, Rev B, 06/2009
Page 8 of 25
3.3.9
DO NOT
expose unit to sun or bright light.
3.3.10 The chassis material and structural design of this unit is such that
the unit is not capable of containing fire within the unit. This unit
does not provide for waterproof operation.
3.3.11 Operating temperature should not exceed:
+5
°°°°
to +131
°°°°
F
–15
°°°°
to +55
°°°°
C
3.3.12
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.
The length and routing of external cables shall be carefully studied
and planned before attempting installation of the equipment. Allow
adequate space for installation of cable and connectors.
3.4.2 Power Wires
Power and Ground wires shall be in accordance with
M22759
or
equivalent.
3.4.3 Bonding
The grounding lug shall be electrically bonded to the aircraft
structure using a braided copper bonding strap with <0.01
resistance from the DVD to the aircraft frame.
3.4.4 Video Lines
All serial digital video wiring connections are recommended to use
PIC V76261
shielded coax. Serial digital video provided in SMPTE
259M format.
All connector types shall be compatible with above-
listed wiring requirements.
It is recommended to terminate any unused video outputs with a
75-ohm load inside the aircraft side mating connector.
