Honeywell MK VII Egpws Line Maintenance Manual, Flap Configuration Monitor Maintenance Messages

EGPWS LINE MAINTENANCE MANUAL

installation does require that the EGPWS has a source of GPS data, software -230-230 or later, Terrain Database version 454 or later, and the Reloadable Customer Definitions (RCD) is loaded. When enabled, Altimeter Monitor operates automatically, without any action required from the flight crew. Altimeter Monitor availability can be verified by performing an EGPWS self test. See Appendix E for Altimeter Monitor Maintenance Messages.

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

The Takeoff Flap Configuration Monitor function offers significant safety enhancements for aircraft equipped with Honeywell’s MK V or MK VII Enhanced Ground Proximity Warning Systems (EGPWS). Honeywell’s Takeoff Flap Configuration Monitor is a software enhancement hosted in the EGPWS Unit. Takeoff Flap Configuration Monitor uses GPS position data, Flap angle inputs, and the Honeywell EGPWS Database to provide aural alerts that supplement flight crew awareness of improper flap setting when the aircraft is aligned on a runway prior to takeoff. EGPWS protection and operation is unaltered by the addition of Takeoff Flap Configuration Monitor. Takeoff Flap Configuration Monitor installation is accomplished via a configuration database upload. The installation does require that the EGPWS has a source of GPS data, flap angle input, software -230-230 or later, Terrain Database version 454 or later, and the Reloadable Customer Definitions (RCD) is loaded. When enabled, Takeoff Flap Configuration Monitor operates automatically, without any action required from the flight crew. Takeoff Flap Configuration Monitor availability can be verified by performing an EGPWS self test. See Appendix F for Takeoff

Flap Configuration Monitor Maintenance Messages.

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

The Long Landing Monitor function offers significant safety enhancements for aircraft equipped with Honeywell’s MK V or MK VII Enhanced Ground Proximity Warning Systems (EGPWS). Honeywell’s Long Landing Monitor is a software enhancement hosted in the EGPWS Unit. Long Landing Monitor uses GPS position data and the Honeywell EGPWS Database to provide aural alerts that supplement flight crew awareness of their position during a landing when the aircraft has not touched down in a nominal amount of time and/or distance. EGPWS protection and operation is unaltered by the addition of Long Landing Monitor. Long Landing Monitor installation is accomplished via a configuration database upload. The installation does require that the EGPWS has a source of GPS data, software -230-230 or later, Terrain Database version 454 or later, and the Reloadable Customer Definitions (RCD) is loaded. When enabled, Long Landing Monitor operates automatically, without any action required from the flight crew. Long Landing Monitor availability can be verified by performing an EGPWS self test.

See Appendix G for Long Landing Monitor Maintenance Messages.

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

The Low Airspeed Monitor function offers significant safety enhancements for Boeing 737NG aircraft equipped with Honeywell’s MK V Enhanced Ground Proximity Warning Systems (EGPWS). Honeywell’s Low Airspeed Monitor is a software enhancement hosted in the EGPWS Unit. Low Airspeed Monitor uses Minimum Operating Speed and Stick Shaker Speed input from the Stall Management and Yaw Damper computers to provide an aural alert that supplements flight crew awareness that their airspeed had passes below 70% of the amber airspeed band. EGPWS protection and operation is unaltered by the addition of Low Airspeed Monitor. Low Airspeed Monitor installation is accomplished via an application software upload. The installation does require that the EGPWS has software -232-232 or later loaded. When installed, Low Airspeed Monitor operates automatically, without any action required from the flight crew. Low Airspeed Monitor availability can be verified by performing an EGPWS self test.

See Appendix H for Low Airspeed Monitor Maintenance Messages.

CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO.: 060-4199-180 REV: G SHEET 18 of 68