V A L A V I O N I C S L T D
C O M 2 0 0 0 – V H F T R A N S C E I V E R
I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L
Revision 3
Page 8 of 31
March 2013
2
SECTION II -
INSTALLATION
2.1
GENERAL INFORMATION
2.1.1
Scope
This section of the manual will provide the needed information to successfully complete the installation of your new
COM 2000 –
VHF Transceiver
. Please read this section completely before proceeding with the installation process.
Although the COM 2000 installation procedures are designed with the do-it-yourselfer in mind, we at Val Avionics
Ltd. strongly suggest that you seek the advice of a qualified avionics installation facility before beginning this or any
other installation project. Qualified avionics installation technicians can offer good advice as to time-tested
installation practices and techniques that can save you many hours of time and frustration.
2.2
UNPACKING AND INSPECTION
Use care when unpacking the equipment. Inspect the unit and supplied parts for visual signs of damage during
shipment. Examine the unit for loose screws, dents, broken buttons and other signs of damage that may have
occurred during shipment. Verify the contents of the container with the list in section 1.5. If any damaged or missing
parts are discovered during the inspection save the shipping material and contact the freight carrier to file a claim. If
it is suspected that parts were omitted from the container please feel free to contact Val Avionics Ltd., to acquire the
missing items.
2.3
EQUIPMENT INSTALLATION PROCEDURES
2.3.1
Cooling
Requirements
Forced air-cooling is not required for the COM 2000 –
VHF Transceiver
. However, when planning the location for
mounting, ensure adequate spacing from heat producing sources such as heating or defrosting ducts.
2.3.2
Mounting Requirements
The COM 2000 mounting tray should be rigidly mounted in the avionics stack using the hardware provided in the
installation kit. Ensure that the mounting location will provide easy access and a clear view of the equipment’s front
panel from the pilot’s position. Ensure that the mounting position will provide adequate clearance between the unit
and the associated wire harness and the aircraft controls. Bracing at the rear of the unit should be installed to ensure
rigidity in the panel. Consult FAA Advisory Circular AC 43.13-2A for acceptable practices and techniques.
