Table of contents (cont) – BendixKing KFD 840 User Manual

Page 13

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Honeywell Bendix/King KFD 840 Primary Flight Display


KFD 840 PG PN 7450-0840-01 Table of Contents
Rev E Oct 15, 2010 TC-3

©

Honeywell International Inc. Do not copy without express permission of Honeywell

Table of Contents (cont)

Section

8.

CHECKLIST AREA ................................................................ 8-1

Page

CHECK LIST FUNCTION ....................................................... 8-1

9.

WEIGHT AND BALANCE AREA .......................................... 9-1

PC UTILITY PROGRAM ......................................................... 9-1

File Load Page .................................................................. 9-4

WEIGHT AND BALANCE PAGE ............................................ 9-6

10.

MISCELLANEOUS DATA AREA ........................................ 10-1

WIND, GROUND SPEED, TRUE AIRSPEED, AND OUTSIDE
AIR TEMPERATURE ........................................................... 10-1

Wind ................................................................................ 10-1

Ground Speed ................................................................. 10-2

True Airspeed .................................................................. 10-2

Outside Air Temperature ................................................. 10-2

11.

EMERGENCY OPERATIONS ............................................. 11-1

ADC (AIR DATA COMPUTER) FAILURE ............................ 11-1

ATTITUDE FAILURE, AHRS FAILURE ............................... 11-2

HDG (HEADING) FAIL, CRM FAILURE (COMPASS REMOTE
MAGNETOMETER) .............................................................. 11-3

IN-FLIGHT RESTART .......................................................... 11-4

CONFIGURATION MODULE ERRORS .............................. 11-5

MINOR FAILURE INDICATIONS ......................................... 11-6

12.

APPENDIX . ......................................................................... 12-1

ACRONYMS AND ABBREVIATIONS .................................. 12-1

AIRCRAFT CONFIGURATION ............................................ 12-3





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