Honeywell MKXXII installation manual Category 10 Attitude Input Select, Attitude Signals

Honeywell

MK XXII EGPWS Installation Manual

3.3.10 Category 10 – Attitude Input Select

Category 10 defines the Roll and Pitch Attitude interface.

3.3.10.1 Attitude Signals

Roll Angle is used for Bank Angle callout, Pseudo Altitude Algorithm and Terrain Awareness display.

Pitch Angle is used for the Tail Strike alert.

NOTE: For MD900 series aircraft where no Tail Strike alert is applicable, Pitch is not required, so a roll only configuration may be selected.

Appendix E Table E 3.1.10 defines the Attitude Input Select type and identifies the first MK XXII EGPWS version in which the option was available (see the Effectivity entry).

3.3.10.2 Instructions

1.Using Appendix E Tables E 3 and Table E 3.1.10 ,select the Attitude Input Select type that matches the aircraft configuration, feature preferences, and version (part number) being installed.

2.Record the ID number for the Attitude Input Select from Appendix E Table E 3.1.10 under the Ident No. heading for Step (Category) 10 on Table E 3. This number will be used for programming the configuration module

3.Using the Attitude Input Select ID number from Appendix E Table E 3.1.10 as “x”, go to Appendix E Table E 3.1.10-x.The electrical interfaces (pin-outs) for the Attitude Input Select Type are used to determine the wiring interconnects and record it on Appendix A Fig A1-3.

CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 89