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26 Cards in this Set

  • Front
  • Back
purpose of the ADI
primary attitude reference in all phases of flight
purpose of the standy attitude indicator
back up to ADIs
prupose of CAINS
provides primary long-range navigation data
purpose of AHRS
provide pitch, roll and heading information for display and the ADIs, BDHIs, and CIs
purpose of TACAN
provide navigation information by determining slant range and relative bearing to a selected tacan station
purpose of GPS
provides users with accurate position, velocity, and time data from satellites
purpose of ICS
provides voice communication among 4 primary stations
purpose of UHF radio
frequency range of 225.000- 399.975 MHz
purpose of HF radio
frequency range of 2.0000- 29.9999 MHz
purpose of VHF radio
frequency range of 116.000- 151.975
purpose of PA
permits crew to passenger voice communication
purpose of IFF
provideds coded ID and altitude signals in response to interrogations
purpose of Weather Radar
provides weather avoidance info out to a range of approximately 240 miles
purpose of radalt
measures height of the aircraft over the surface ranging from 0-5000 feet
purpose of CFIRS
aquires selected flight data and records a minnimum of 2 hours of flight information and 30 min of ICS communication
purpose of ACLS
automated carrier landing
purpose of AACS
backup to ACLS
purpose, location and color of wing and tail position lights
provides visual indication of aircraft attitude-one on each wing tip and aftmost fuselage station- left wing tip is red, right wing tip is green, tail light is white
purpose, location and color of anit-collision lights
anitcollision-right outboard vertical stabilizer and lower fuselage aft of nose wheel well- white or red (white disabled on deck)
purpose, location and color of Approach
indicates aircraft AOA- nose gear fairing- red, green and amber to indicate low, high, or optimum
purpose, location and color of landing/ taxi light
illuminate area in front of aircraft- forward nosewheel door- white
purpose of the advisory lights
provide information on system operation or malfunction
purpose of the caution lights
provides an indication of malfunction or system condition
purpose of the pitot static system
provides pitot (impact) and static (ambient) pressure
purpose of AOA
angle between the longitudal axis of the aircraft and the relative wind
purpose of the AFCS
provides directional stability augmentation, three axis attitude control, and automatic flightpath control of the aircraft