Honeywell Home Security System Mk V Users Manual LMM For The EGPWS

2015-01-23

• 0
• 1 INTRODUCTION
  • 1.1 SCOPE
  • 1.2 APPLICABILITY
  • 1.3 REFERENCE DOCUMENTS
• 2 DESCRIPTION AND OPERATION
  • 2.1 GENERAL SYSTEM DESCRIPTION
    • 2.1.1 ENHANCED GROUND PROXIMITY WARNING COMPUTER (EGPWC)
  • 2.2 OPERATION
    • 2.2.1 MODE 1 – EXCESSIVE DESCENT RATE
    • 2.2.2 MODE 2A/2B - TERRAIN CLOSURE RATE
    • 2.2.3 MODE 3 - DESCENT AFTER TAKEOFF
    • 2.2.4 MODE 4A/4B/4C - UNSAFE TERRAIN CLEARANCE
    • 2.2.5 MODE 5 - DESCENT BELOW GLIDESLOPE
    • 2.2.6 MODE 6 - ADVISORY CALLOUTS (OPTIONAL)
      • 2.2.6.1 EXCESSIVE BANK ANGLE CALLOUT
      • 2.2.6.2 TAIL STRIKE CALLOUT
    • 2.2.7 MODE 7 - WINDSHEAR DETECTION (OPTIONAL FOR MK V/VII ONLY)
    • 2.2.8 ENVELOPE MODULATION (NOT AVAILABLE IN MK VI/VIII -001)
    • 2.2.9 TERRAIN CLEARANCE FLOOR AND RUNWAY FIELD CLEARANCE FLOOR
      • 2.2.9.1 RUNWAY DATABASE
    • 2.2.10 TERRAIN ALERTING AND DISPLAY (OPTIONAL)
      • 2.2.10.1 TERRAIN AND OBSTACLE DATABASE
    • 2.2.11 PEAKS DISPLAY MODE (OPTIONAL)
    • 2.2.12 GEOMETRIC ALTITUDE (GPS REQUIRED)
    • 2.2.13 WEATHER RADAR AUTOTILT (MK V AND MK VII ONLY)
    • 2.2.14 SYSTEM DISPLAY AND ANNUNCIATION
    • 2.2.15 RUNWAY AWARENESS AND ADVISORY SYSTEM (OPTION FOR MK V AND MK VII ONLY)
    • 2.2.16 STABILIZED APPROACH MONITOR (OPTION FOR MK V AND MK VII ONLY)
    • 2.2.17 ALTIMETER MONITOR (OPTION FOR MK V AND MK VII ONLY)
    • 2.2.18 TAKEOFF FLAP CONFIGURATION MONITOR (OPTION FOR MK V AND MK VII ONLY)
    • 2.2.19 LONG LANDING MONITOR (OPTION FOR MK V AND MK VII ONLY)
    • 2.2.20 LOW AIRSPEED MONITOR (MK V BOEING 737NG ONLY)
    • 2.2.21 LAMP FORMAT
  • 2.3 SYSTEM MAINTENANCE
    • 2.3.1 MAINTENANCE PHILOSOPHY
    • 2.3.2 SYSTEM OPERATION DURING AN INOP CONDITION
    • 2.3.3 BIT DESCRIPTION
    • 2.3.4 EGPWC FRONT PANEL
      • 2.3.4.1 EGPWS STATUS LED’S
      • 2.3.4.2 FRONT PANEL SELF-TEST INTERFACE (MK V AND MK VII ONLY)
      • 2.3.4.3 AUDIO JACK (MK V AND MK VII ONLY)
      • 2.3.4.4 FRONT PANEL PCMCIA INTERFACE
      • 2.3.4.5 FRONT PANEL TEST CONNECTOR
    • 2.3.5 SELF-TEST FUNCTIONS
• 3 FAULT ISOLATION (TROUBLESHOOTING)
  • 3.1 GENERAL
  • 3.2 TROUBLESHOOTING GUIDE
  • 3.3 LEVEL 1 SELF-TEST - GO/NO GO TEST
    • 3.3.1 SELF-TEST PREAMBLE
    • 3.3.2 SHORT LEVEL 1 SELF-TEST
    • 3.3.3 LONG LEVEL 1 SELF-TEST
  • 3.4 LEVEL 2 SELF-TEST - CURRENT FAULTS
    • 3.4.1 CURRENT FAULTS - INTERNAL
    • 3.4.2 CURRENT FAULTS - EXTERNAL
  • 3.5 LEVEL 3 SELF-TEST - SYSTEM CONFIGURATION
  • 3.6 LEVEL 4 SELF-TEST - FAULT HISTORY
  • 3.7 LEVEL 5 SELF-TEST - ALERT HISTORY
  • 3.8 LEVEL 6 SELF-TEST - DISCRETE INPUT TEST
    • 3.8.1 ARINC 552 / ALT 55 RADIO ALTITUDE VALIDITY FLAG DISCRETES
    • 3.8.2 GND LANDING GEAR DISCRETE
    • 3.8.3 +28V LANDING GEAR DISCRETE
    • 3.8.4 GND LANDING FLAP DISCRETE OR FLAP OVERRIDE
    • 3.8.5 +28V LANDING FLAP OR FLAP OVERRIDE DISCRETE
    • 3.8.6 FLAP POSITION DISCRETES
    • 3.8.7 SELF-TEST DISCRETE
    • 3.8.8 STEEP APPROACH DISCRETES
      • 3.8.8.1 STEEP APPROACH DISCRETE #1 (MK V AND MK VII ONLY)
      • 3.8.8.2 STEEP APPROACH DISCRETE #2
    • 3.8.9 GND ILS TUNED DISCRETE
    • 3.8.10 +28V ILS TUNED DISCRETE
    • 3.8.11 GLIDESLOPE VALIDITY DISCRETES
    • 3.8.12 GND GLIDESLOPE INHIBIT DISCRETE
    • 3.8.13 +28 V GLIDESLOPE INHIBIT DISCRETE
    • 3.8.14 GND GLIDESLOPE CANCEL DISCRETE
    • 3.8.15 DECISION HEIGHT DISCRETE
    • 3.8.16 MODE 6 VOLUME CONTROL DISCRETE
    • 3.8.17 CALLOUTS ENABLE DISCRETE (MK V AND MK VII ONLY)
    • 3.8.18 GND AUDIO SUPPRESS(INHIBIT)/ALL MODES INHIBIT DISCRETE
    • 3.8.19 +28 V AUDIO SUPPRESS(INHIBIT)/ALL MODES INHIBIT DISCRETE
    • 3.8.20 AOA VALIDITY DISCRETES (MK V AND MK VII ONLY)
    • 3.8.21 DISPLAY SELECT DISCRETES
    • 3.8.22 TERRAIN AWARENESS & TCF INHIBIT
    • 3.8.23 SIMULATOR REPOSITION (MK V AND MK VII ONLY)
    • 3.8.24 WEATHER RADAR ON/OFF
    • 3.8.25 LOCALIZER VALIDITY DISCRETES (MK V AND MK VII ONLY)
    • 3.8.26 ATTITUDE VALIDITY DISCRETES
    • 3.8.27 AIRSPEED VALIDITY DISCRETE
    • 3.8.28 BAROMETRIC ALTITUDE RATE VALIDITY DISCRETES
    • 3.8.29 ACCELERATION SELF-TEST IN PROGRESS DISCRETE
    • 3.8.30 LONGITUDINAL ACCELERATION VALIDITY DISCRETE
    • 3.8.31
    • 3.8.32 NORMAL ACCELERATION VALIDITY DISCRETE
    • 3.8.33 MAGNETIC HEADING VALIDITY DISCRETE
    • 3.8.34 AOA VANE HEATER DISCRETE
    • 3.8.35 PLI DESELECT SWITCH DISCRETES (MK V AND MK VII ONLY)
    • 3.8.36 AUTOPILOT DISCONNECT DISCRETES
    • 3.8.37 TACTICAL SELECT DISCRETE
    • 3.8.38 ALTITUDE ALERT DISCRETE
    • 3.8.39 CORRECTED BAROMETRIC ALTITUDE VALIDITY DISCRETE
    • 3.8.40 MOMENTARY FLAP OVERRIDE DISCRETE
    • 3.8.41 WEIGHT ON WHEELS DISCRETE
    • 3.8.42 GPWS INHIBIT DISCRETE
    • 3.8.43 RAAS ENABLE DISCRETE (MK V AND MK VII ONLY)
    • 3.8.44 RAAS INHIBIT DISCRETE (MK V AND MK VII ONLY)
    • 3.8.45 STABILIZED APPROACH MONITOR ENABLE DISCRETE (MK V AND MK VII ONLY)
    • 3.8.46 STABILIZED APPROACH MONITOR INHIBIT DISCRETE (MK V AND MK VII ONLY)
    • 3.8.47 LOW AIRSPEED MONITOR INHIBIT DISCRETE (MK V – 737NG ONLY)
• 4 MAINTENANCE PRACTICES
  • 4.1 GENERAL
  • 4.2 DATABASE UPDATE
    • 4.2.1 DATABASE UPDATE FREQUENCY
    • 4.2.2 LOADING A DATABASE
  • 4.3 FLIGHT HISTORY DOWNLOADING
    • 4.3.1 OBTAINING AN EGPWS FLIGHT HISTORY DOWNLOAD CARD
    • 4.3.2 DOWNLOAD PROCEDURE
    • 4.3.3 TRANSCRIPTION OF THE PCMCIA CARD
  • 4.4 PROGRAMMING THE CONFIGURATION MODULE (MK VI, MK VIII, MK XXII ONLY)
    • 4.4.1 CONFIGURATION MODULE REPROGRAMMING (MK VI, MK VIII, MK XXII ONLY)
• 4
• 5 SERVICING
  • 5.1 GENERAL
• 6 REMOVAL/INSTALLATION
  • 6.1 EGPWC
    • 6.1.1 REMOVAL
    • 6.1.2 INSTALLATION
  • 6.2 CONFIGURATION MODULE (MK VI, MK VIII, AND MK XXII ONLY)
    • 6.2.1 REMOVAL
    • 6.2.2 INSTALLATION
  • 6.3 DISPLAY SWITCHING RELAYS (IF INSTALLED)
    • 6.3.1 REMOVAL
    • 6.3.2 INSTALLATION
• 7 ADJUSTMENT/TEST
  • 7.1 ADJUSTMENT
  • 7.2 TEST
    • 7.2.1 EGPWS GROUND TESTS
• 8 INSPECTION/CHECK
  • 8.1 GENERAL
• 9 CLEANING/PAINTING
  • 9.1 GENERAL
• 10 REPAIRS
  • 10.1 GENERAL
• 10
• 11 APPENDIX A: WINVIEWS
• 12 APPENDIX B: TROUBLESHOOTING DO’S AND DO NOT’S
• 13 APPENDIX C: RAAS MAINTENANCE MESSAGES (AURAL & DISPLAYED)
• 14 APPENDIX D: STABILIZED APPROACH MONITOR MAINTENANCE MESSAGES
• 15 APPENDIX E: ALTIMETER MONITOR MAINTENANCE MESSAGES
• 16 APPENDIX F: TAKEOFF FLAP CONFIGURATION MONITOR MAINTENANCE MESSAGES
• 17 APPENDIX G: LONG LANDING MONITOR MAINTENANCE MESSAGES
• 18 APPENDIX H: LOW AIRSPEED MONITOR MAINTENANCE MESSAGES