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RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
BENDIX/KING
2.1
UNPACKING AND INSPECTING EQUIPMENT
Exercise extreme care when unpacking the equipment. Make a visual inspection of the unit for
evidence of damage incurred during shipment. If a claim for damage is to be made, save the ship-
ping container to substantiate the claim. The claim should be promptly filed with the transportation
company. It would be advisable to retain the container and packaging material after all equipment
has been removed in the event that equipment storage or reshipment should become necessary.
The conditions and tests required for TSO approval of this article are minimum performance stan-
dards. 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 TSO stan-
dards. The article may be installed only if further evaluation by the applicant documents an ac-
ceptable installation and is approved by the Administrator.
THE KG 102/102A CONTAINS A VERY SENSITIVE
GYRO. IN ORDER TO PREVENT DAMAGE DUR-
ING SHIPMENT ALL SHIPMENTS MUST BE MADE
IN THEIR ORIGINAL PACKING CONTAINERS.
2.2
PREINSTALLATION CHECK
The equipment has been completely tested before leaving the factory. To ensure that the equip-
ment has not been damaged in shipment, it is suggested that the preinstallation bench test be per-
formed. The bench test harness or aircraft cables wired per Figures 2-9 and 2-10 are required for
this test. Inputs and performance are indicated in the component technical characteristics speci-
fications, paragraph 1.4.1 through 1.4.6.
IT HAS BEEN DETERMINED THAT THE KCS 55/
KCS 55A PICTORIAL NAVIGATION SYSTEM AND
ITS ASSOCIATED KA 52 AND/OR KA 57 AUTOPI-
LOT ADAPTORS ARE NOT FULLY COMPATIBLE
WITH THE PIPER ALTIMATIC II AUTOPILOT.
HONEYWELL SUGGESTS THAT NO ATTEMPT
BE MADE TO INTERFACE THE KCS 55/55A SYS-
TEM WITH THE ALTIMATIC II OR ANY OTHER "RF
SENSING DESIGN" AUTOPILOT SYSTEM.
EXTREME CAUTION SHOULD BE TAKEN TO EN-
SURE THAT 28 VOLTS DC IS NOT APPLIED TO
UNITS THAT ARE SWITCHED TO THE 14 VOLTS
DC POSITION ON THE KG 102/102A.
FOR THE CENTURY 21/31/41 AUTOPILOT INTER-
FACES, AN IC 930 ADAPTER IS AVAILABLE
FROM CENTURY FLIGHT SYSTEMS. CONTACT
AT TEL: (817) 325-2517.
Rev 11, Apr/2007
©Honeywell International Inc. Do not print without express permission of Honeywell
SECTION II
INSTALLATION
NOTE
WARNING
CAUTION:
NOTE:
KCS 55/55A
Page 2-1
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