Manuali utente per Honeywell MK XXII

Sommario

• 1 INTRODUCTION

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  • 1.1 SCOPE

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  • 1.2 APPLICABILITY

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  • 1.3 REFERENCE DOCUMENTS

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• 2 DESCRIPTION AND OPERATION

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  • 2.1 GENERAL SYSTEM DESCRIPTION

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    • 2.1.1 ENHANCED GROUND PROXIMITY WARNING COMPUTER (EGPWC)

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  • 2.2 OPERATION

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    • 2.2.1 MODE 1 – EXCESSIVE DESCENT RATE

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    • 2.2.2 MODE 2A/2B - TERRAIN CLOSURE RATE

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    • 2.2.3 MODE 3 - DESCENT AFTER TAKEOFF

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    • 2.2.4 MODE 4A/4B/4C - UNSAFE TERRAIN CLEARANCE

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    • 2.2.5 MODE 5 - DESCENT BELOW GLIDESLOPE

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    • 2.2.6 MODE 6 - ADVISORY CALLOUTS (OPTIONAL)

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      • 2.2.6.1 EXCESSIVE BANK ANGLE CALLOUT

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      • 2.2.6.2 TAIL STRIKE CALLOUT

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    • 2.2.7 MODE 7 - WINDSHEAR DETECTION (OPTIONAL FOR MK V/VII ONLY)

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    • 2.2.8 ENVELOPE MODULATION (NOT AVAILABLE IN MK VI/VIII -001)

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    • 2.2.9 TERRAIN CLEARANCE FLOOR AND RUNWAY FIELD CLEARANCE FLOOR

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      • 2.2.9.1 RUNWAY DATABASE

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    • 2.2.10 TERRAIN ALERTING AND DISPLAY (OPTIONAL)

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      • 2.2.10.1 TERRAIN AND OBSTACLE DATABASE

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    • 2.2.11 PEAKS DISPLAY MODE (OPTIONAL)

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    • 2.2.12 GEOMETRIC ALTITUDE (GPS REQUIRED)

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    • 2.2.13 WEATHER RADAR AUTOTILT (MK V AND MK VII ONLY)

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    • 2.2.14 SYSTEM DISPLAY AND ANNUNCIATION

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    • 2.2.15 RUNWAY AWARENESS AND ADVISORY SYSTEM (OPTION FOR MK V AND MK VII ONLY)

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    • 2.2.16 STABILIZED APPROACH MONITOR (OPTION FOR MK V AND MK VII ONLY)

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    • 2.2.17 ALTIMETER MONITOR (OPTION FOR MK V AND MK VII ONLY)

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    • 2.2.18 TAKEOFF FLAP CONFIGURATION MONITOR (OPTION FOR MK V AND MK VII ONLY)

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    • 2.2.19 LONG LANDING MONITOR (OPTION FOR MK V AND MK VII ONLY)

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    • 2.2.20 LOW AIRSPEED MONITOR (MK V BOEING 737NG ONLY)

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    • 2.2.21 LAMP FORMAT

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  • 2.3 SYSTEM MAINTENANCE

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    • 2.3.1 MAINTENANCE PHILOSOPHY

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    • 2.3.2 SYSTEM OPERATION DURING AN INOP CONDITION

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    • 2.3.3 BIT DESCRIPTION

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    • 2.3.4 EGPWC FRONT PANEL

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      • 2.3.4.1 EGPWS STATUS LED’S

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      • 2.3.4.2 FRONT PANEL SELF-TEST INTERFACE (MK V AND MK VII ONLY)

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      • 2.3.4.3 AUDIO JACK (MK V AND MK VII ONLY)

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      • 2.3.4.4 FRONT PANEL PCMCIA INTERFACE

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      • 2.3.4.5 FRONT PANEL TEST CONNECTOR

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    • 2.3.5 SELF-TEST FUNCTIONS

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• 3 FAULT ISOLATION (TROUBLESHOOTING)

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  • 3.1 GENERAL

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  • 3.2 TROUBLESHOOTING GUIDE

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  • 3.3 LEVEL 1 SELF-TEST - GO/NO GO TEST

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    • 3.3.1 SELF-TEST PREAMBLE

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    • 3.3.2 SHORT LEVEL 1 SELF-TEST

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    • 3.3.3 LONG LEVEL 1 SELF-TEST

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  • 3.4 LEVEL 2 SELF-TEST - CURRENT FAULTS

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    • 3.4.1 CURRENT FAULTS - INTERNAL

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    • 3.4.2 CURRENT FAULTS - EXTERNAL

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  • 3.5 LEVEL 3 SELF-TEST - SYSTEM CONFIGURATION

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  • 3.6 LEVEL 4 SELF-TEST - FAULT HISTORY

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  • 3.7 LEVEL 5 SELF-TEST - ALERT HISTORY

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  • 3.8 LEVEL 6 SELF-TEST - DISCRETE INPUT TEST

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    • 3.8.1 ARINC 552 / ALT 55 RADIO ALTITUDE VALIDITY FLAG DISCRETES

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    • 3.8.2 GND LANDING GEAR DISCRETE

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    • 3.8.3 +28V LANDING GEAR DISCRETE

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    • 3.8.4 GND LANDING FLAP DISCRETE OR FLAP OVERRIDE

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    • 3.8.5 +28V LANDING FLAP OR FLAP OVERRIDE DISCRETE

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    • 3.8.6 FLAP POSITION DISCRETES

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    • 3.8.7 SELF-TEST DISCRETE

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    • 3.8.8 STEEP APPROACH DISCRETES

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      • 3.8.8.1 STEEP APPROACH DISCRETE #1 (MK V AND MK VII ONLY)

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      • 3.8.8.2 STEEP APPROACH DISCRETE #2

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    • 3.8.9 GND ILS TUNED DISCRETE

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    • 3.8.10 +28V ILS TUNED DISCRETE

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    • 3.8.11 GLIDESLOPE VALIDITY DISCRETES

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    • 3.8.12 GND GLIDESLOPE INHIBIT DISCRETE

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    • 3.8.13 +28 V GLIDESLOPE INHIBIT DISCRETE

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    • 3.8.14 GND GLIDESLOPE CANCEL DISCRETE

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    • 3.8.15 DECISION HEIGHT DISCRETE

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    • 3.8.16 MODE 6 VOLUME CONTROL DISCRETE

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    • 3.8.17 CALLOUTS ENABLE DISCRETE (MK V AND MK VII ONLY)

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    • 3.8.18 GND AUDIO SUPPRESS(INHIBIT)/ALL MODES INHIBIT DISCRETE

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    • 3.8.19 +28 V AUDIO SUPPRESS(INHIBIT)/ALL MODES INHIBIT DISCRETE

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    • 3.8.20 AOA VALIDITY DISCRETES (MK V AND MK VII ONLY)

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    • 3.8.21 DISPLAY SELECT DISCRETES

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    • 3.8.22 TERRAIN AWARENESS & TCF INHIBIT

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    • 3.8.23 SIMULATOR REPOSITION (MK V AND MK VII ONLY)

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    • 3.8.24 WEATHER RADAR ON/OFF

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    • 3.8.25 LOCALIZER VALIDITY DISCRETES (MK V AND MK VII ONLY)

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    • 3.8.26 ATTITUDE VALIDITY DISCRETES

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    • 3.8.27 AIRSPEED VALIDITY DISCRETE

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    • 3.8.28 BAROMETRIC ALTITUDE RATE VALIDITY DISCRETES

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    • 3.8.29 ACCELERATION SELF-TEST IN PROGRESS DISCRETE

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    • 3.8.30 LONGITUDINAL ACCELERATION VALIDITY DISCRETE

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    • 3.8.31

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    • 3.8.32 NORMAL ACCELERATION VALIDITY DISCRETE

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    • 3.8.33 MAGNETIC HEADING VALIDITY DISCRETE

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    • 3.8.34 AOA VANE HEATER DISCRETE

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    • 3.8.35 PLI DESELECT SWITCH DISCRETES (MK V AND MK VII ONLY)

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    • 3.8.36 AUTOPILOT DISCONNECT DISCRETES

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    • 3.8.37 TACTICAL SELECT DISCRETE

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    • 3.8.38 ALTITUDE ALERT DISCRETE

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    • 3.8.39 CORRECTED BAROMETRIC ALTITUDE VALIDITY DISCRETE

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    • 3.8.40 MOMENTARY FLAP OVERRIDE DISCRETE

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    • 3.8.41 WEIGHT ON WHEELS DISCRETE

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    • 3.8.42 GPWS INHIBIT DISCRETE

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    • 3.8.43 RAAS ENABLE DISCRETE (MK V AND MK VII ONLY)

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    • 3.8.44 RAAS INHIBIT DISCRETE (MK V AND MK VII ONLY)

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    • 3.8.45 STABILIZED APPROACH MONITOR ENABLE DISCRETE (MK V AND MK VII ONLY)

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    • 3.8.46 STABILIZED APPROACH MONITOR INHIBIT DISCRETE (MK V AND MK VII ONLY)

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    • 3.8.47 LOW AIRSPEED MONITOR INHIBIT DISCRETE (MK V – 737NG ONLY)

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• 4 MAINTENANCE PRACTICES

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  • 4.1 GENERAL

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  • 4.2 DATABASE UPDATE

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    • 4.2.1 DATABASE UPDATE FREQUENCY

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    • 4.2.2 LOADING A DATABASE

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  • 4.3 FLIGHT HISTORY DOWNLOADING

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    • 4.3.1 OBTAINING AN EGPWS FLIGHT HISTORY DOWNLOAD CARD

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    • 4.3.2 DOWNLOAD PROCEDURE

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    • 4.3.3 TRANSCRIPTION OF THE PCMCIA CARD

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  • 4.4 PROGRAMMING THE CONFIGURATION MODULE (MK VI, MK VIII, MK XXII ONLY)

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    • 4.4.1 CONFIGURATION MODULE REPROGRAMMING (MK VI, MK VIII, MK XXII ONLY)

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• 5 SERVICING

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  • 5.1 GENERAL

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• 6 REMOVAL/INSTALLATION

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  • 6.1 EGPWC

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    • 6.1.1 REMOVAL

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    • 6.1.2 INSTALLATION

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  • 6.2 CONFIGURATION MODULE (MK VI, MK VIII, AND MK XXII ONLY)

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    • 6.2.1 REMOVAL

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    • 6.2.2 INSTALLATION

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  • 6.3 DISPLAY SWITCHING RELAYS (IF INSTALLED)

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    • 6.3.1 REMOVAL

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    • 6.3.2 INSTALLATION

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• 7 ADJUSTMENT/TEST

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  • 7.1 ADJUSTMENT

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  • 7.2 TEST

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    • 7.2.1 EGPWS GROUND TESTS

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• 8 INSPECTION/CHECK

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  • 8.1 GENERAL

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• 9 CLEANING/PAINTING

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  • 9.1 GENERAL

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• 10 REPAIRS

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  • 10.1 GENERAL

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• 11 APPENDIX A: WINVIEWS

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• 12 APPENDIX B: TROUBLESHOOTING DO’S AND DO NOT’S

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• 13 APPENDIX C: RAAS MAINTENANCE MESSAGES (AURAL & DISPLAYED)

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• 14 APPENDIX D: STABILIZED APPROACH MONITOR MAINTENANCE MESSAGES

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• 15 APPENDIX E: ALTIMETER MONITOR MAINTENANCE MESSAGES

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• 16 APPENDIX F: TAKEOFF FLAP CONFIGURATION MONITOR MAINTENANCE MESSAGES

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• 17 APPENDIX G: LONG LANDING MONITOR MAINTENANCE MESSAGES

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• 18 APPENDIX H: LOW AIRSPEED MONITOR MAINTENANCE MESSAGES

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