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MK VI MK VIII EGPWS Installation Design Guide
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV:
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SECTION II - INSTALLATION
2.1 Introductio n
This section contains suggestions and factors to consider before installing the Enhanced Ground Proximity
Warning System. Close adherence to these suggestions will assure satisfactory performance from the
equipment.
NOTE
The conditions and tests performed on this article are minimum performance standards. It is
the responsibility of those desiring to install this article either on or within a specific type or
class of aircraft to determine that the aircraft installation conditions are within these
performance standards. The article may be installed only if further evaluation by the
applicant documents an acceptable installation and is approved by the airworthiness
authority.
2.2 Unpacking and Inspecting the Equipment
Exercise extreme caution when unpacking equipment. Perform a visual inspection of the unit for evidence of
damage incurred during shipment. If a damage claim must be filed, save the shipping container and all packing
materials to substantiate your claim. The claim should be filed as soon as possible. The shipping container and
all packing materials should be retained in the event that storage or reshipment of the equipment is necessary.
2.3 Equipment Installation
2.3.1 General
The following paragraphs contain information pertaining to the installation of the MK VI and MK VIII EGPWS,
including instructions concerning the location and mounting of the equipment. The equipment should be
installed in the aircraft in a manner consistent with acceptable workmanship and engineering practices, and in
accordance with the instructions set forth in this publication. To ensure the system has been properly and safely
installed in the aircraft, the installer should make a thorough visual inspection and conduct an overall operational
check of the system, on the ground, prior to flight.
CAUTION
AFTER INSTALLATION OF THE CABLING AND BEFORE INSTALLATION OF THE
EQUIPMENT, A CHECK SHOULD BE MADE WITH THE AIRCRAFT PRIMARY POWER
SUPPLIED TO THE MOUNTING CONNECTOR, TO ENSURE THAT POWER IS APPLIED
ONLY TO THE PINS SPECIFIED IN THE INTERWIRING DIAGRAMS IN SECTION III.
2.3.2 MK VI/MK V III Computer Location
Care should be exercised to avoid mounting components near equipment operating with high pulse current or
high power outputs such as radar and satellite communications equipment. In general, the equipment should be