Establish A Plan To Route The Sense Lines; Establish A Plan For The Electrical Power; Optional Probe Heat Installation - Honeywell BendixKing KLR 10 Installation Manual

Lift reserve indicator
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KLR 10 Installation Manual
2.5

ESTABLISH A PLAN TO ROUTE THE SENSE LINES

The sense lines must be installed through the aircraft structure with the following limitations:
 Do not remove hose end caps until final connector installation. This keeps contamination from
entering the sense lines during installation.
 A minimum bend radius of 4" for the lines must be observed.
 Attach the sense lines at regular intervals by means of suitable clamps.
 Do not clamp sense lines at the end fittings.
 Use AN931 Grommets (preferred) or bulkhead fittings where the sense lines pass thru bulkheads.
 Engineering data may be required if installing on a pressurized aircraft.
 Keep the sense lines well clear of any moving controls or cables.
Refer to AC43.13-1B chapter 12 section 4 for instructions on replacing/installing new pitot static lines.
2.6

ESTABLISH A PLAN FOR THE ELECTRICAL POWER:

The KLR 10 requires less than ¼ amp (250 mA) of electrical power within its acceptable voltage range of
10-28 VDC. Our recommendations would be to have the KLR 10 get power from the avionics bus through
an on/off switch in series with the positive lead for the control module (this would offer some protection
from surges during starts and the on/off switch would enhance operational flexibility).
For additional information please refer to AC43.13-1B Chapter 11, which has a wealth of information on
wire, switches, loads, etc., also AC43.13-2B Chapter 2 paragraph 207 is useful.
2.7

OPTIONAL PROBE HEAT INSTALLATION:

The optional heated probe requires 7.8 amps of electrical power at 12 or 24VDC.
Determine the size of wire required from AC43.13-1B Chapter 11 Section 5, (12VDC in free air #14 wire
will be adequate for runs up to 20' & for 24VDC in free air #16 wire will be adequate for runs up to 25').
As an added precaution to prevent interference with other aircraft systems use MIL Spec. shielded wire.
Electrical cable/wire must be installed such that the risk of mechanical damage and/or damage caused by
fluids, vapors, or sources of heat, is minimized. Route as far away as possible from any instrument,
system or wiring that may be effected (i.e. compass/flux gate, antenna or antenna coax).
We recommend that you use a Mil. Spec. DC switch with silver contacts rated for twice the required
amperage (i.e. Eaton 8500K9, MS24523-22 SPST switch).
AC43.13-1B Chapter 11 has a wealth of information on wire, switches, loads, etc. also AC43.13-2B
Chapter 2 paragraph 207 is useful.
Planning
Page 2-4
P/N D201305000058
Rev 1 Jul 2013

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