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The antenna sweep is the same for takeoff and approach PWS modes. The PWS changes the sweep when PWS is active. Both WXR and PWS sweeps decrease to -60 to +60 degrees.
PWS and WXR Sweep Pattern
Position | Dir | Radar Sweep | Paint Sweep | Angle (Degrees) | Time |
Sweep 1 | L-R | Capt WXR data updated | Capt WXR +icon painted | -60 to +60 | |
Sweep 2 | R-L | Both PWS data updated | None | +60 to -60 |
PWS and WXR Sweep Pattern
Sweep 3 | L-R | F/O WXR data updated | F/O WXR +icon painted | -60 to +60 | |
Sweep 4 | R-L | Both PWS data updated | None | +60 to -60 |
The sweep pattern may go to a PWS only mode during takeoff and approach when WXR is not selected and PWS is automatically activated. The scan is -60 to +60 degrees.
PWS Sweep Pattern
Position | Dir | Radar Sweep | Paint Sweep | Angle (Degrees) | Time |
Sweep 1 | L-R | None | None | N/A | |
Sweep 2 | R-L | Both PWS data updated | None | +60 to -60 | |
Sweep 3 | L-R | None | None | N/A | |
Sweep 4 | R-L | Both PWS data updated | None | +60 to -60 |
WXR SYSTEM - OPERATION - FAILURE DISPLAYS
WXR System Alert Messages and Display
Alert messages show on the ND when the R/T processes data that is not satisfactory. The WXR display will continue to show with an alert message.
Only one alert message shows on the ND. When the R/T processes unsatisfactory data from more than one source only the highest priority message shows. These are the alert messages and priority from highest to lowest:
· WXR WEAK shows for an R/T gain calibration failure
· WXR ATT shows when the selected attitude input fails
· WXR STAB shows when stabilization is off.
The alert messages show on these alert lines:
· Line 1 shows WXR in amber
· Line 2 shows WEAK, ATT, or STAB in amber.
WXR System Fail Messages and Display
A failure of these components causes a WXR failure:
· R/T
· WXR control panel
· WXR antenna.
A WXR failure causes these conditions:
· WXR FAIL message shows on ND
· Mode, tilt, and gain messages go out of view
· WXR display goes out of view.
The fail message shows on these alert lines:
· Line 1 shows WXR in amber
· Line 2 shows FAIL in amber.
A failure of these components will cause a PWS failure:
· Loss of any RA
· Loss of ADR data
· Loss of IR data
· Scan and tilt antenna faults
· Internal WXR system faults
· Loss of CAS and TAS.
A failure of the predictive windshear causes an amber PWS FAIL message on the ND.
WXR SYSTEM - ND RANGE DISAGREEMENT
General
The DEUs compare the ND ranges from these components:
· EFIS CP
· WXR R/T
· Flight management computer (FMC).
A difference between any of these ranges causes an amber range disagreement message on alert line 3.
These WXR range disagreement messages are possible:
· WXR RANGE DISAGREE; shows when there is a difference between the EFIS CP range and the WXR R/T range
· MAP/WXR RANGE DISAGREE; shows when there is a difference between the EFIS CP range, the WXR R/T range, and the FMC range.
WXR RANGE DISAGREE will show in these modes:
· Expanded approach
· Expanded VOR
· Expanded map
· Centered map.
MAP/WXR RANGE DISAGREE will show in these modes:
· Expanded map
· Centered map.
This happens during a range disagreement:
· WXR display goes out of view
· mode, tilt, and gain messages show
· FMC range shows.
WXR SYSTEM - WXR R/T FUNCTIONAL DESCRIPTION
General
The WXR R/T makes RF pulses and sends them to the antenna. The antenna transmits pulses and receives the return signals and sends them to the WXR R/T. The R/T processes the return signals to make display data that shows on the NDs. The WXR data on the ND shows the weather patterns in front of the airplane.
The WXR R/T also comes on automatically during take off and approach to detect windshear events in front of the airplane. If a windshear event is detected, the WXR sends cautions or warnings to the flight compartment.
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