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The test starts with the aural message DISCRETE TEST. If the
condition of a discrete input changes, you hear the new state of
the discrete.
NOTE: The landing gear handle must be in the Off position to
test the gear inhibit switch on the GPW module.
NOTE: Before moving the landing gear handle install landing
gear locking pins.
You hear the aural message DISCRETE INPUT TEST - PRESS
TO CANCEL every 60 seconds. Push a short or long cancel to
end the self-test.
GPWS - SELF-TEST - LEVEL 6
EFFECTIVITY
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GPWS - SELF-TEST - LEVEL 6
GPWS - SELF-TEST - LEVEL 6
EFFECTIVITY
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Purpose
There are three status LEDs on the front panel of the ground
proximity warning computer (GPWC). The LED indicators show
the status of the GPWC when power is supplied. The LEDs turn
on for these conditions:
* External fault - yellow
* Computer OK - green
* Computer fail - red.
The yellow external fault LED shows that the GPWC has
detected an external interface fault. The green computer OK
LED shows that the GPWC is operating with no internal faults.
The red computer fail LED shows that the GPWC has an internal
fault.
GPWS - STATUS LEDS
EFFECTIVITY
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GPWS - STATUS LEDS
GPWS - STATUS LEDS
EFFECTIVITY
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General
This summary shows this information:
* GPWS modes
* Mode conditions
* Aural messages for each mode
* Annunciators or displays that come on.
GPWS - MODE DESCRIPTION SUMMARY
EFFECTIVITY
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GPWS - MODE DESCRIPTION SUMMARY
GPWS - MODE DESCRIPTION SUMMARY
EFFECTIVITY
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General
This graphic is for reference only.
GPWS - SYSTEM SUMMARY
EFFECTIVITY
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GPWS - SYSTEM SUMMARY
GPWS - SYSTEM SUMMARY
EFFECTIVITY
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Purpose
The VHF omnidirectional ranging (VOR) system is a navigation
aid that gives magnetic bearing data from a VOR ground station
to the airplane.
The VOR ground stations transmit signals that give magnetic
radial information from 000 degrees to 359 degrees. All VOR
stations reference the 000 degree to magnetic north.
Abbreviations and Acronyms
* ACP - audio control panel
* DEU - display electronic unit
* DFCS - digital flight control system
* DME - distance measurement equipment
* EFIS - electronic flight instrument system
* FCC - flight control computer
* FDAU - flight data acquisition unit
* FMC - flight management computer
* HSI - horizontal situation indicator
* ILS - instrument landing system
* LCD - liquid crystal display
* MCP - mode control panel
* NAV - navigation
* NCD - no computed data
* PWR - power
* REU - remote electronic unit
* RF - radio frequency
　
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