- •20. Weather avoidance radar (wxr).
- •20.1. Назначение, выполняемые функции
- •20.2. Распределение частотного диапазона
- •20.2. Состав типовой мнрлс
- •20.4. Мнрлс «Гроза».
- •20.5. Weather radar.
- •Wxr system - general description Control
- •System Inputs
- •System Outputs
- •Display
- •Antenna
- •Wxr system - system select and system on/off System Select
- •System On
- •Wxr system - pws operation General Description
- •Pws Warning Area
- •Pws Caution Area
- •Pws Display
- •Sweep Patterns
- •Wxr system - operation - failure displays wxr System Alert Messages and Display
- •Wxr System Fail Messages and Display
- •Wxr system - nd range disagreement General
- •Wxr system - wxr r/t functional description General
- •Control Inputs
- •Predictive Windshear Inputs
- •Antenna Control
- •Wxr Central Processor Unit
- •Predictive Windshear Central Processor Unit The pws cpu uses inputs from these systems to turn on the wxr pws function:
- •Oscillator/Transmitter Circuits
- •Rf Transmit
- •Rf Receive
- •Test Start
- •Test Operation
- •Test Pass
- •Test Fail
- •Training Information Point
- •1. Назначение, выполняемые функции.
- •2. Распределение частотного диапазона.
- •3. Состав типовой мнрлс.
Pws Caution Area
PWS gives a caution if it detects a windshear threat in this area:
Within 25 degrees on either side of the airplane projected magnetic heading
More than 0.5 nm but less than 3 nm ahead of the airplane
Not in the PWS warning area.
PWS inhibits new windshear cautions during takeoff and approach if both of these conditions exist:
Airspeed more than 80 knots
Less than 400 feet radio altitude
All PWS alerts are inhibited above 1200 feet radio altitude.
PWS Warning - Flight Deck Effects
A PWS warning has these visual and aural annunciations:
Red WINDSHEAR message on the PFD
Red WINDSHEAR message on the ND
Aural annunciation - WINDSHEAR AHEAD, WINDSHEAR AHEAD (takeoff)
Aural annunciation - GO AROUND, WINDSHEAR AHEAD (approach).
PWS Caution - Flight Deck Effects
A PWS caution has theses visual and aural annunciations:
Amber WINDSHEAR message on the ND
WXR SYSTEM - PWS OPERATION* Windshear symbol on the ND
Aural annunciation - MONITOR RADAR DISPLAY.
WXR SYSTEM - PWS DISPLAYS
General Description
Weather radar with predictive windshear (PWS) detects windshear ahead of the airplane. PWS uses this data to detect windshear:
Doppler radar returns
Inertial data
Air data.
If PWS detects a windshear condition, it alerts the flight crew with visual and aural annunciations.
System On/Off – Takeoff
PWS turns on when the airplane is on the ground and has one of these conditions:
Throttles move through 53 degrees
Flight crew pushes the WXR button on an EFIS control panel.
The WXR button on the EFIS CP does not turn off the PWS if the throttle levers are above 53 degrees. PWS turns off automatically when the airplane climbs above 2300 feet radio altitude.
System On/Off – Approach
PWS turns on automatically when the airplane descends below 2300 feet radio altitude. PWS turns off when one of these conditions occur:
Airplane lands
Airplane climbs above 2300 feet radio altitude.
If PWS is on and WXR is not selected on the EFIS CP, all antenna sweeps search for windshear. If WXR is selected, the antenna uses one sweep to search for windshear and the other sweep to search for normal weather returns. PWS operation does not affect the WXR mode or range selected by the flight crew.
Pws Display
If PWS detects windshear, it makes a windshear symbol on the ND. The symbol is red and black bars. Yellow bars go from the edges of the symbol to the compass rose. The yellow bars help the crew to see the PWS symbol.
The ND mode selector must be in a correct mode for the windshear data to show. These are the ND modes that show windshear data:
Expanded APP
Expanded VOR
Expanded MAP
Centered MAP.
PWS cautions or warnings are inhibited above 1200 feet radio
altitude.
New PWS cautions are inhibited between 80 knots computed airspeed on the ground and 400 feet radio altitude.
New PWS warnings are inhibited between 100 knots computed airspeed and 50 feet radio altitude.
These inhibits apply to both takeoff and approach modes.
NOTE: These inhibits do not remove a PWS caution or warning that already exists.
