Gnd landing flap discrete, 28v landing flap discrete, Momentary flap override discrete – Honeywell MK VI User Manual

Page 298: Self-test discrete, Gnd ils tuned discrete #1

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Honeywell

MK VI MK VIII EGPWS Installation Design Guide

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6.6.4 GND Landing Flap Discrete

Type:

Supplied by Flap or Flap selector handle switch.

Signal Status:

Landing Flaps or Not Landing Flaps

Fault monitoring: Indication of landing flaps selected for more than 60 seconds at airspeeds above 250 (180 for GA Slow)

knots will result in a flap switch fault which will cause a GPW INOP indication.

Note: This can be caused by either a flap switch fault or by the Flap Override switch being left in the on position.

Level 6 Audio readout

GND Landing Flaps Discrete
or Flap Override

Landing Flaps =>

Not Landing Flaps =>

“Landing Flaps”
“Not Landing Flaps”

6.6.5 +28V Landing Flap Discrete

Type:

Supplied by Flap or Flap selector handle switch.

Signal Status:

Landing Flaps or Not Landing Flaps

Fault monitoring: Indication of landing flaps selected for more than 60 seconds at airspeeds above 250 (180 for GA Slow)

knots will result in a flap switch fault which will cause a GPW INOP indication.

Note: This can be caused by either a flap switch fault or by the Flap Override switch being left in the on position.

Level 6 Audio readout

+28 V Landing Flaps Discrete
or Flap Override

Landing Flaps =>

Not Landing Flaps =>

“Landing Flaps”
“Not Landing Flaps”

6.6.6 Momentary Flap Override Discrete

Type:

Supplied by a momentarily actuated cockpit switch.

Signal Status:

Flap Override activated if not active or Flap Override canceled if currently active.

Fault Monitoring:

Activation of this input continuously for more than 15 seconds will result in the ‘Momentary Flap
Override Invalid” fault which will cause a GPW INOP indication.

Level 6 Audio readout

Momentary Flap Override

Flap Override Selected =>

Flap Override Not Selected =>

“Flap Override”
“Not Flap Override”

6.6.7 Self-Test Discrete

Type: Supplied by a momentarily actuated cockpit self-test switch.

Signal Status:

Self Test or Normal

Fault Monitoring:

Activation of this input continuously for more than 60 seconds will result in the ‘Self Test Invalid”
fault which will cause a GPW INOP indication.

Note: This input is used to start and stop the Level 6 self test, there is no audio output for this discrete in Level 6.

6.6.8 GND ILS Tuned Discrete #1

Type: Supplied by ILS/VOR Mode Selector.

Signal Status:

ILS tuned or VOR tuned

Level 6 Audio readout

GND ILS Tuned Discrete #1

ILS Tuned =>

ILS Not Tuned =>

“ILS 1 Tuned”
“ILS 1 Not Tuned”

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