- •12.7. Vhf omnidirectional range (vor);
- •12.1. Особенности радиосистем ближней навигации и посадки
- •12.2. Канал дальности рсбн
- •12.3. Канал азимута рсбн
- •12.4. Принцип работы аппаратуры "vor".
- •12.5. Принцип действия канала азимута с фазовым методом измерения.
- •12.6. Принцип действия фазового канала азимута с доплеровским арм.
- •12.7. Vhf omnidirectional range (vor).
- •Indicator indicator pointer
- •12.8. Радиосистемы посадки.
- •12.9. Instrument Landing System (ils).
- •12.10. Маркерный канал.
- •12.11. Marker Beacon System.
- •12.12. Навигационно-посадочная аппаратура "курс мп-70".
- •12.13.Vhf omnidirectional range (vor) в737.
- •Purpose
- •Abbreviations and Acronyms
- •General description General
- •Description
- •Vor system - flight compartment component location General
- •Vor/ils Antenna
- •Vor system - functional description General
- •Operation
- •Vor system - controls fis Controls
- •Dfcs Controls
- •Audio Control Panel Controls
- •Vor system - radio magnetic indicator displays General
- •Vor system - efis normal displays General
- •Bearing Pointers
- •Deviation Bar and Scale
- •Selected Course Pointer
- •To/from Pointer and Indicator
- •Nav Data Source
- •Vor Frequency
- •12.14. Instrument Landing System (ils) в737.
- •Purpose
- •Abbreviations and Acronyms
- •General
- •Description
- •General
- •Digital Inputs
- •Digital Outputs
- •General
- •Frequency Transfer Switch
- •Navigation/Displays Source Select Panel
- •General
- •General
- •Power Interface
- •Arinc 429 Interfaces
- •Discrete Interfaces
- •Rf Interfaces
- •Receiver Functional Description
- •Efis Controls
- •Dfcs Controls
- •Audio Control Panel Controls
- •General
- •Indications
- •General
- •Normal Display
- •Rising Runway
- •Ncd Display
- •Fail Display
- •90 Degrees of the airplane heading
- •12.15. Marker Beacon System в737.
- •General
- •Abbreviations and Acronyms
- •General description General
- •Operation
- •Monitor and Test
- •Test – 1 General
- •Operation
- •General
- •Operation
Rising Runway
The rising runway shows when there is a LOC signal capture and the radio altitude is below 2500 feet. The symbol goes out of view above 2500 feet. The rising runway symbol is green with a magenta stem.
The rising runway symbol represents the radio altitude above the runway. It moves laterally with the localizer deviation pointer to show localizer deviation. The symbol starts to move when the radio altitude is 200 feet. It touches the airplane symbol when the radio altitude is 0 or at touchdown.
NCD Display
When the ILS data goes to an NCD condition, the CDS shows the localizer and glideslope scales and removes the pointers.
Fail Display
The amber LOC flag replaces the localizer deviation pointer
and scale when the localizer receiver function has a failure. The
amber G/S flag replaces the glideslope deviation pointer and
scale
when the glideslope receiver function has a failure.
ILS - EXPANDED ILS DISPLAY
General
To show ILS displays on the CDS, set the EFIS control panel mode selector to the APP position. You must also tune a valid ILS frequency on the NAV control panel.
Normal Display
The glideslope deviation pointer and scale show at the right of the NAV display. The glideslope deviation pointer is magenta and the scale is white.
The glideslope scale is the standard four dot scale where each dot equals 0.35 degrees of deviation. The glideslope deviation pointer gives fly-to signals to intercept the glideslope beam. The course pointer points to the number that you set on the DFCS MCP. For ILS, you use the DFCS MCP course selector to enter the ILS course (airport runway heading).
The localizer deviation indicator and scale shows at the bottom of the NAV display. The localizer scale is white and the localizer deviation indicator is magenta.
The deviation scale is the standard four dot scale. One dot is equal to 1 degree of deviation. The localizer deviation indicator shows the deviation to the left or right of the runway centerline.
The NAV data source shows in white at the upper right corner of the display. It shows the source of the data for the ILS displays. To the right of the NAV data source is the active ILS frequency display.
The ILS frequency display shows the active ILS frequency and the selected course. If the ILS ground station transmits a morse coded station identifier, the letter identifier replaces the numeric frequency when the receiver captures the ground station signal.
NCD Display
When the ILS data goes to an NCD condition, the CDS shows the localizer and glideslope scales and removes the pointers.
Fail Display
For invalid ILS data, the CDS replaces the localizer deviation
scale and indicator with the amber LOC flag when the localizer
receiver fails. The amber G/S flag replaces the glideslope
deviation
scale and pointer when the glideslope receiver fails.
ILS - CENTERED ILS DISPLAY
General
To show the centered ILS NAV display, push the CTR switch on the EFIS control panel mode selector switch.
Normal Displays
The glideslope deviation pointer and scale show to the right of the HSI display. The glideslope pointer is magenta and the scale is white.
The glideslope scale is the standard four dot scale. Each dot equals 0.35 degrees of deviation. The pointer gives fly-to commands to intercept the glideslope beam.
The course pointer points to the number that you set on the DFCS MCP. For ILS, you use the DFCS MCP course selector to enter the ILS course (airport runway heading).
The localizer deviation indicator and scale show in the center of the HSI compass card. The localizer deviation indicator is magenta and the scale is white.
The localizer scale is the standard four dot scale. Each dot is equal to 1 degree of deviation. The deviation indicator shows the deviation to the left or the right of the runway centerline.
The NAV data source shows in white in the upper right corner of the display. It shows the source of data for the ILS display. The active ILS frequency shows to the right of the NAV data source. The ILS frequency display shows the active ILS frequency and the selected course. If the ILS ground station transmits a morse coded station identifier, then the letter identifier replaces the numeric frequency when the receiver captures the ground station signal.
