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Brand: Honeywell Bendix/King

he Mark VII enhanced ground proximity warning system provides protection against controlled flight into terrain (CFIT) as well as windshear. CFIT warnings include excessive rate of descent, terrain closure rate, excessive altitude loss after takeoff or missed approach procedure, insufficient terrain clearance, descent below glideslope, and excessive bank angle.

EGPWS incorporates many features not found in some competing systems such as pin-selectable altitude callouts, envelope modulation, geometric altitude algorithm, turn extrapolation, auto display pop-up, auto tilt of weather radar, and the ability to host Honeywell's Runway Awareness and Advisory System.

Visual and aural warnings of impending windshear are provided via Honeywell's unique computer algorithms that can detect an increase in aircraft performance (a precursor to windshear) and a decrease in aircraft performance (indicative of entry into windshear). The system includes a program module and biaxial accelerometer.

Realizing the advantages of the world's best terrain database, the MK-VII EGPWS is the standard for TAWS. Once in use, customers receive free database updates, as they become available.

Features

  • Basic Ground Proximity Warning.
  • Altitude awareness callouts.
  • Excessive bank angle alerting.
  • Windshear detection and alerting.
  • Terrain and Obstacle Awareness Alerting as well as optional display of this information, and Terrain Clearance Floor.
  • Runway Awareness and Advisory System (optional).
  • Input signal processing (including filtering and signal monitoring).
  • Alert output processing (including alert prioritization, voice message synthesis, audio output and display and warning lamp drivers).
  • Built-in test and monitoring including cockpit-activated self test.
  • Interface with CMC/CFDS/CAIMS maintenance systems with interactive protocols when the aircraft is on the ground.
  • Front panel PCMCIA interface for uploading software and databases.
  • Front panel maintenance test connector, test button, and headset jack for system checkout and troubleshooting.
  • System status LEDs located on the LRU front panel to indicate External Fault, Computer OK and Computer Fail conditions.
  • Provisional cockpit and portable data loader interfaces for software and database uploading.

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