9 instructions for continued airworthiness, 3 approved airplane flight manual supplement, 4 pilot’s guide – Honeywell BENDIX/KING KLN 94 User Manual
Page 24
B
KLN 94
Rev. 4, Jan/2003 10599I04.CDL
Page 1-14
1.8.2.4 Switch/Annunciators
1.8.2.4.1 NAV/GPS (Switch/Annunciator)
If the navigation information is displayed on a shared primary indicator a switch/annunciator will
be required to select and annunciate the source.
1.8.2.4.2 WPT/MSG (Annunciator)
The KLN 94 has internal annunciators. The “WPT” and “MSG” external annunciators may be
required in some installations.
1.8.2.4.3 GPS APR, ARM/ACT (Switch/Annunciator)
A switch/annunciator can be used for arming, disarming, or deactivating the approach mode. It
will provide remote annunciation of ARM and ACTV and provide a momentary switch function to
arm and activate the Approach Mode and change the CDI scale factors. The KLN 94 may require
an annunciator to display when approach is armed or active. Refer to
for additional
switch/annunciator information.
1.8.2.4.4 Altitude Source
An altitude source is required for IFR certification. The altitude may be derived from a compatible
encoding altimeter and some RS 232 air data systems.
1.8.3 Approved Airplane Flight Manual Supplement
A flight manual supplement will need to be prepared and approved. The supplement may be
prepared based on the sample, P/N 006-00839-0000. Refer to the
for information on preparing a flight manual supplement and a copy of the
STC approval.
1.8.4 Pilots Guide
The KLN 94 pilots guide must be placed in the aircraft in a location that is accessible to the pilot.
The pilots guide is P/N 006-18207-0000.
1.9 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
The instructions for continued airworthiness given in the TC or STC approvals for this product
supplements or supersedes the instructions for continued airworthiness in this manual.
Most Honeywell products are designed and manufactured to allow "on condition maintenance".
On condition maintenance is described as follows; There are no periodic service requirements
necessary to maintain continued airworthiness. No maintenance is required until the equipment
does not properly perform it’s intended function. When service is required, a complete
performance test should be accomplished following any repair action. Consult the appropriate
unit Maintenance/Overhaul Manual for complete performance test information.