Honeywell MK VI User Manual

Page 105

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Honeywell

MK VI MK VIII EGPWS Installation Design Guide

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105

MK VI EGPWS

COMPUTER

FIXED LANDING GEAR/FLOAT AIRCRAFT

ALTERNATE AIR SWITCH ARRANGEMENT

(Example Shown: Twin Otter)

W*

* KRA 405B Adjustable
Trip pins W,V, & F.

KRA 405B

Adjustable Trip

Landing Flap Discrete (Gnd)

Landing Gear Discrete
(+28)

Power Input: +28VDC

Landing Gear Discrete
On Ground = DC Gnd

16

40
60

35

18

P1 J1

FLAPS UP

APPROACH

FLAPS

APPROACH FLAP

POSITION (5°-7°)

EGPWS

3 AMP

AIRCRAFT +28VDC

Not LANDING

LANDING

FULL LANDING FLAP
POSITION (16°-18°)

The Honeywell KRA 405B provides 3 programmable Adjustable Trip outputs that can be used to supply a
ground to the Landing Gear input discrete when the aircraft is less than 5 to 20 feet Radio Altitude. See the
Honeywell KRA 405B Installation Manual (006-10536-0003) for details of the Adjustable Trip output. Use of
Adjustable Trip outputs of the KRA 405B requires CM2000 Configuration Module along with KPA900
Configuration Module Programmer, PC and software. The Collins ALT-55 (622-2855-001 only) also provides 4
shop adjustable Trip outputs, pins 41,43,46, and 48, contact Collins Avionics for details.

Landing Flap Discrete
(Gnd)

MK VI EGPWS

COMPUTER

FIXED LANDING GEAR/FLOAT AIRCRAFT

ALTERNATE AIR SWITCH ARRANGEMENT

(Example Shown: Twin Otter)

Landing Gear Discrete
(+28)

Power Input: +28VDC

Landing Gear Discrete
On Ground = DC Gnd

16

40
60

35

18

J1

P1

Not LANDING

LANDING

FULL LANDING FLAP
POSITION (16°-18°)

APPROACH FLAP
POSITION (5°-7°)

FLAPS UP

APPROACH

FLAPS

EGPWS

3 AMP

AIRCRAFT +28VDC

NC

NO

AIR SWITCH
RELAY

DIODE

AIR SWITCH
(SHOWN AS A/C ON GROUND)

NO

OPTIONAL EQUIPMENT
EXISTING ON AIRCRAFT

HOUR METER

+28VDC

AIR STREAM

~40 KNOTS

~

Some aircraft (ex: Twin Otter) have an air switch (flapper on the wing) that can be used to provide a Landing
Gear discrete ground when the aircraft is less than approximately 40 knots airspeed (approach airspeed varies
by aircraft). Contact Honeywell EGPWS engineering for assistance in adapting this discrete input design to your
aircraft.

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