Honeywell MK VI - Manual (Page 324)

Honeywell
MK VI MK VIII EGPWS Installation Design Guide
Proprietary notice on title page applies
CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 324
9 DEFINITIONS
The following acronyms are provided for use with this document:
Acronym Interpretation
AAAS Alternate Audio Alert Select
ADC Air Data Computer
ADS Air Data System
AGC Automatic Gain Control
AGL Above Ground Level
AHRS Attitude Heading Reference System
AIC Analog Input Controller
AIMS Airplane Information Management System
ASA AlliedSignal Aerospace
AOA Angle of Attack
ASL Above Sea Level
ATP Acceptance Test Procedure
BCD Binary Coded Decimal
BIST Built in Self Test
BIT Built In Test
BITE Built In Test Equipment
BNR Binary
C/O Callouts
CAA Civil Aviation Authority
CAIMS Central Aircraft Information/Maintenance System
CFDS Centralized Fault Display System
CFIT Controlled Flight Into Terrain
CFM Cubic Feet per Minute
CISRD CFDS Interface System Requirements Document
CMC Central Maintenance Computer
COTS Commercial Off the Shelf
CP Control Panel
CRS Course
CW Clockwise
DAA Digital/Analog Adapter
DADC Digital Air Data Computer
DAU Data Acquisition Unit
DC Digital Command
DDM Difference in Depth of Modulation
DEVN Deviation
DH Decision Height
DITS Digital Information Transfer System
DME Distance Measuring Equipment
DO Discrete Output
DSP Digital Signal Processor
DSU Display Switching Unit
DSWC Digital Stall Warning Computer
EEPROM Electrically Erasable Programmable Read Only Memory
EFCP EFIS Control Panel
EFIS Electronic Flight Instrument System
EGPWC Enhanced Ground Proximity Warning Computer
EGPWD Enhanced Ground Proximity Warning Display
EGPWS Enhanced Ground Proximity Warning System
EICAS Engine Indication and Crew Alert System
EMI Electromagnetic Interference
ENB Enabled
EPROM Erasable Programmable Read Only Memory
F/T Functional test
F/W Fail/Warning