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DME SYSTEM - SELF TEST

DME SYSTEM - SELF TEST - раздел Механика, DISTANCE MEASURING EQUIPMENT - INTRODUCTION Self Test Push The Test Switch On The Dme Interrogator To Start A Dm...

Self Test

Push the test switch on the DME interrogator to start a DME selftest.

Front Panel Displays

The LED status indicators go through this sequence:

· The LRU status and control fail LEDs come on red for two seconds.

· The LRU status LED changes to green.

· All LEDs go off for two seconds.

· The applicable LEDs come on to show the LRU status.

The red CONTROL FAIL LED shows when the tuning source is invalid.

The LRU STATUS LED shows interrogator test results. The LRU STATUS LED shows green for a good test or it shows red for a test failure.

 

 

– Конец работы –

Эта тема принадлежит разделу:

DISTANCE MEASURING EQUIPMENT - INTRODUCTION

Purpose... The distance measuring equipment DME system supplies slant range line of... DME SYSTEM COMPONENT LOCATION FLIGHT COMPARTMENT General...

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Abbreviations and Acronyms
· AC - alternating current · ACP - audio control panel · ADF - automatic direction finder · alt - alternate · altn - alternate · app - approach

DME SYSTEM - GENERAL DESCRIPTION
General The DME system has two DME interrogators and two antennas. Description The interrogators get manual tune inputs and flight management computer system (FMCS) autot

General
These are the components in the flight compartment that have an interface with the DME system: · FMC source select switch · Left inboard and outboard display units · Left

DME Outputs
Each DME interrogator has two output buses. One output bus supplies data to the on-side flight control computer (FCC). DME 1 sends data to FCC A and DME 2 sends data to FCC B. the other Output bus

General
The navigation (NAV) control panels supply frequency inputs and test commands to these navigation radios: · DME · ILS · VOR. When you put a paired VOR or ILS fre

Operation
The NAV control panels have an active frequency display window and a standby frequency display window. The frequency that shows in the active frequency display window is the frequency that the navi

Operation
The CPU uses tune inputs to tune the frequency synthesizer. The CPU give a signal to the transmitter to send interrogation pulses. The transmit pulses go through a circulator then to the DME antenn

General
During a ground test or a self test, the display units show these indications: · The DME fail condition for two seconds · The DME NCD condition for the next two seconds ·

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