RADAR Flashcards

1
Q

What is RADAR stabilization?

A

The purpose of radar stabilization is to maintain a constant radar scan at
desired tilt angle, level with the Earth’s horizon during normal aircraft operations and maneuvers.
During turns, aircraft bank will roll one wing down. As the radar scans to the wing down side it will paint excessive ground clutter. On the wing high side, the radar will scan above storms and fail to display accurate weather data to the pilot. Stabilization will adjust the tilt angle to maintain a level scan with the horizon.
During climb or decent, stabilization will adjust the tilt angle up or down as appropriate to maintain a level scan with the horizon.
If not for stabilization, the radar would scan above or below possible targets, thus missing potentially dangerous weather.

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2
Q

Describe how to use RADAR tilt

A

Generally focus tilt on FL180-250
At 10 nm, one degree of tilt motion will move the center of the beam up or down 1,000 feet. At 80 nm this one degree of motion will move the center of the beam 8,000 feet. Think about it, five degrees of tilt at 80 nm will move the center of the beam 40,000 feet.

To analyze a convective cell, the flight crew should use the tilt knob to obtain a correct display and point the weather radar beam to the most reflective part of the cell. At high altitude, a thunderstorm may contain ice particles that have low reflectivity. If the tilt setting is not adapted, the ND may display only the upper (less reflective) part of the convective cloud (overscanning). As a result, the flight crew may underestimate or not detect a thunderstorm. In order to get accurate weather detection, the weather radar antenna should also be pointed toward lower levels (i.e. below freezing level), where water can still be found. If a red area is found at a lower level, the antenna tilt should then be used to scan the area vertically. Presence of yellow or green areas at high altitudes, above a red cell, may indicate a very turbulent area.

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3
Q

What is the dead zone?

A

Often when flying in the spring, the pilot will be confronted with
two large level-three returns separated by a narrow band of level three. The temptation will be to rapidly pass through this narrow band of rough weather to the large clear area behind it. Stop, do not fly through, and fly around. This narrow band is so intense that the radar pulses are unable to make it through to the severe storm behind. This is called the dead zone.

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4
Q

How do you use GAIN?

A

When taken out of “auto” and placed in manual gain, all that can be determined from the display is a relative differ- ence between two levels. Level one, two or three displayed in manual gain will not correlate to level one, two or three
weather returns, just a relative difference between the levels. Because mountainous terrain can saturate the radar, it is often useful to use map mode and variable gain to differentiate the different return levels of the terrain. Pilots should never use
variable gain to depict weather.

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5
Q

Effects of Earth’s Curvature

A

The curvature of the Earth limits ground mapping from high alti- tude. Weather radar will not normally paint ground returns from high altitude beyond 90 nautical miles, because the Earth’s horizon at this distance and altitude will be almost parallel to the radar beam. Storms, hills, mountains, large buildings and cities will be painted.

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6
Q

What is GAIN?

A

answer

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7
Q

Reflectivity Limitations

A

The reflectivity of precipitation particles varies considerably depending on the type of precipitation particle. For example, wet hail, rain and wet snow are much more reflective than dry hail, ice crystals or dry snow. Unfortunately, aircraft radars do not see frozen precipitation as well as they see wet precipitation. So thunderstorm tops, which are composed of mostly low-reflectivity precipitation particles, aren’t seen well by aircraft radar. NEXRADs on the other hand, don’t suffer from this limitation, especially at the higher altitudes where most commercial aircraft operate.

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8
Q

What is shadowing/attenuation?

A

the size, shape and intensity of that weather as displayed to the pilot may not be accurate. The more intense the precipitation, the less distance the radar can see into and through a storm. What appears to be a thin, crescent-shaped band of precipitation (Figure 1) could just be the leading edge of a much larger area of heavy to extreme precipitation.
Radar attenuation shows up as black areas on a pilot’s weather radar display (Figure 2). Attenuation can also occur when heavy rain or ice builds up on the radome (Figure 3), when the radome is damaged, or when it isn’t well maintained.
NEXRAD detects weather at much greater distances and is not as prone to attenutation as aircraft radar. Also, if an intervening cell is intense enough, the pilot may not be able to see more distant weather behind it with the aircraft radar regardless of range selected due to attenuation.
This is an example where the ATC controller’s perspective can help keep pilots safe.

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9
Q

Describe the RADAR turbulence feature

A

The RADAR can measure turbulence when accompanied by reflective moisture. based on the Doppler effect and is sensitive to precipitation movement. Like the weather radar, the TURB function needs a minimum amount of precipitation to be effective. An area of light rainfall, depicted in green in normal mode, is shown in magenta when there is high turbulence activity. It is not used to detect CAT

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10
Q

Can RADAR detect the tops of thunderstorms?

A

No. The convective cloud and associated threats may extend significantly above the upper detection limit of the weather radar (called ‘radar top’). This means that reflectivity is not directly proportional to the level of risk that may be encountered: a convective cloud may be dangerous, even if the radar echo is weak.

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11
Q

What can RADAR detect?

A

Rainfall
Wet hail and wet turbulence
Windshear

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12
Q

What can’t RADAR detect?

A
Ice crystals, dry hail* and snow
Clear air turbulence
Sandstorms (solid particles are almost
transparent to the radar beam)
• Lightning
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13
Q

How does RADAR auto tilt/stabilization work?

A

radar uses the EGPWS terrain database and automatically adjusts the antenna tilt based on the aircraft position, altitude, and the selected ND range. Is there a gyro?

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14
Q

PM v PF recommended division of RADAR

A

To maintain a comprehensive situation awareness, the flight crew needs to monitor both the short-distance and long-distance weather. To this end, the crew should select different ranges on the Pilot Monitoring (PM) and Pilot Flying (PF) ND.

In cruise the combination of the
following ranges provides good
weather awareness and allows to
avoid the "blind alley effect"
- 160 NM on the PM ND
- 80 NM on the PF ND

To avoid threatening convective weather, the flight crew should make deviation decisions while still at least 40 NM away; therefore, the following ranges should be selected on the NDs:

Pilot Monitoring (PM) adjusts ranges to plan the long-term weather avoidance strategy (in cruise, typically 160 NM and below).
Pilot Flying (PF) adjusts ranges to monitor the severity of adverse weather, and decide on avoidance tactics (in cruise, typically 80 NM and below as required).
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15
Q

How and when should you adjust gain in manual mode instead of auto?

A

The sensitivity of the receiver may vary from one type of radar system to another. In the CAL (AUTO) position, the gain is in the optimum position to detect standard convective clouds. Manual settings are also available and can be used to analyze weather.

At low altitudes, reducing the gain might be justified for proper weather analysis. Due to increased humidity at lower levels, convective cells are usually more reflective and the weather radar display may have a tendency to show a lot of red areas. This can also be the case at higher altitude with significant positive ISA deviations in a very humid atmosphere (typically the Indian monsoon). In these cases, slowly reducing the gain allows the detection of threatening areas: most red areas slowly turn yellow, the yellow areas turn green and the green areas slowly disappear. The remaining red areas – i.e. the red areas that are the last to turn yellow, - are the most active parts of the cell and must be avoided (fig.17).

At high altitudes, water particles are frozen and clouds are less reflective. In this case, gain should be increased for threat evaluation purposes.

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16
Q

How should weather be avoided vertically?

A

Do not attempt to fly under a convective cloud, even when you can see through to the other side, due to possible severe turbulence, windshear, microbursts and hail. If an aircraft must fly below a convective cloud (e.g. during approach), then the flight crew should take into account all indications (visual judgement, weather radar, weather report, pilot’s report, etc) before they take the final decision.
If overflying a convective cloud cannot be avoided, apply a vertical margin of 5 000 feet

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17
Q

How should you avoid weather laterally?

A

When possible, it is advisable to try to avoid a storm by flying on the upwind side of a cumulonimbus. Usually, there is less turbulence and hail upwind of a convective cloud.
The “area of threat” identified by the flight crew (e.g. a cumulonimbus cloud) should be cleared by a minimum of 20 NM laterally whenever possible (fig.21). An additional margin may be applied in case the convective clouds are very dynamic or have a significant build-up speed.
If the aircraft trajectory goes between several convective clouds, if possible maintain a margin of at least 40 NM with the identified “area of threat”.

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18
Q

What cloud shapes should be avoided?

A

Clouds shapes, in addition to colors, should be observed carefully in order to detect adverse weather conditions. Closely spaced areas of different colors usually indicate highly turbulent zones (fig.19). Some shapes are good indicators of severe hail that also indicate strong vertical drafts (fig.20). Finally, fast changing shapes, whatever the form they take, also indicate high weather activity. finger hook u-shape scalloped edges

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19
Q

What is the preferred method to deviate around a thunderstorm?

A

it is preferable to perform lateral avoidance instead of vertical avoidance. Indeed, vertical avoidance is not always possible (particularly at high altitude) due to the reduction of buffet and performance margins. In addition, some convective clouds may have a significant build-up speed, that extends far above the radar visible top.

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20
Q

What does the E175 SECTOR SCAN on the weather radar do?

A

Reduces the sweep angle to -30deg and increases the sweep rate to 24spm

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21
Q

REACT

A

Rain Echo Attenuation Compensation Technique

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22
Q

What Radar System model is installed?

A

WU-600

23
Q

What are the components of the weather radar system?

A

Receiver Transmitter Antenna Unit

24
Q

How is the antenna stabilized in pitch and roll?

A

Uses attitude information from the IRU

25
Q

What are the weather radar modes of operation?

A

WX
GMAP
STBY
OFF

26
Q

What is GMAP mode? Can one MFD be in WX mode and the other in GMAP Mode?

A

Ground Mapping Mode, to alert the flight crew in high terrain areas.

The preset GAIN will generally provide the desired display, however, the PM may desire to manually decrease the GAIN.

Yes.

27
Q

What is slave mode?

A

One MFD CCD controls both MFD WX radar screens

28
Q

What does WX do on the display control panel?

A

Toggles weather on and off on the MFD HSI

29
Q

What is the purpose of the TURB mode?

A

Turbulence Detection. The radar processes return signals in order to determine if a turbulence signature is present. Turbulence may only be engaged in the WX mode and at selected ranges of 50NM or less.

30
Q

What is the purpose of the RANGE mode?

A

See weather at 10, 25, 50, 100, 200, 300NM

31
Q

What is the purpose of the GAIN mode? What are the 2 submodes?

A

Varies the RTA receiver GAIN.
Variable and calibrated.

Calibrated is the preset mode used for weather avoidance. The system will be forced into calibrated gain when TGT or RCT (Rain Echo Attenuation Compensation Technique) are selected.

The variable gain mode is useful for additional weather analysis and for ground mapping. Variable gain can increase receiver sensitivity over the calibrated level to show weak targets or it can be reduced below the calibrated level to eliminate weak returns.

32
Q

What is the TGT mode?

A

Target alert mode monitors for red or magenta weather beyond the selected range and 7.5deg on each side of the aircraft heading. If such weather is detected within the monitored heading, outside the selected range, the target alert annunciation changes from a green armed condition to an amber alert condition on the MFD. When this warning is received, the flight crew should select longer ranges to view the questionable target. When TGT is selected, variable gain mode is disabled.

33
Q

What is the normal radar sweep and rate?

A

+-60deg from the aircraft nose at a rate of 12 sweeps per minute

34
Q

What is the SECT mode?

A

Sector scan mode. Selecting the pushbutton reduces the normal sweep angle and rate to +-30deg and 24 sweeps per minute.

35
Q

What provides the weather radar tilt control?

A

The inner knob on the CCD provides tilt control (without variable gain active). Tilt can be varied between 15deg up and down by turning the knob.

36
Q

What is the ACT Mode?

A

Controlled by the inner tilt knob on the CCD
Altitude compensated tilt ACT
Ability to place elevation control under ACT which adjusts the antenna tilt in relation to the altitude and selected range.
The tilt knob can be used for fixed offset corrections of up to 2deg

37
Q

What is the RCT mode?

A

RCT Rain Echo Attenuation Compensation Technique

The RCT function permits the weather radar receiver to automatically adjust sensitivity to compensate for attenuation losses as the radar pulse passes through weather targets on its way to illuminate other targets. Functions in all modes except GMAP.

Cyan fields indicate areas (behind cells) where further compensation is not possible.

38
Q

What is the TEST function?

A

Selected on the MCDU for maintenance

39
Q

What does the weather radar system consist of?

A

The weather radar system consists of an integrated Receiver Transmitter Antenna unit (RTA) and two virtual weather radar controllers.

The RTA is mounted in the nose of the airplane, whereas the virtual controllers consist of the CCDs and the weather mode information displayed on the MFDs below the weather information.

40
Q

How many modes and functions are available when using the radar?

A

Five modes and ten functions are available.

41
Q

What is the Radar Weather Detection Mode (WX)?

A

The WX mode is used to detect areas of severe weather. This will allow the pilots to avoid areas of dangerous weather conditions and possible turbulence. If WX is selected before the initial RTA warm-up period is over (approximately 90s), WAIT is displayed in the mode field. In the wait mode, the transmitter and antenna scan are inhibited.

42
Q

What is the Ground Mapping Mode (GMAP)?

A

A. This mode is used to alert the flight crew about hazards caused by ground targets. This is especially useful in areas of rapidly changing terrain, such as hilly mountainous areas.

B. The selection of preset gain will generally provide the desired mapping display, however the gain can also be manually operated. It is possible to have one pilot working the GMAP while the other is using the WX mode.

C. It is not intended to be used or relied for ground proximity warning.

43
Q

What is the Standby (STBY)/Forced Standby (FSBY) Mode?

A

A. The weather radar remains in a ready state, with the antenna scan motionless and stowed in a tilt-up position. In addition, the transmitter is inhibited and the display memory is erased.

44
Q

What is the OFF Mode?

A

Turns the radar off, provided OFF is selected on both virtual controllers. The system is no longer radiating power and the antenna is stowed.

45
Q

What is the Slave Mode?

A

One controller is in OFF position whereas the other controller is in an operating mode. The operating one is in control of both sweeps.

46
Q

What is the Antenna Stabilization Function?

A

The antenna is stabilized in pitch and roll using attitude information from the IRU. Momentarily selecting the STAB OFF checkbox disables antenna stabilization and causes an amber STAB to be displayed.

47
Q

What is the Receiver Gain (GAIN) Function?

A

The GAIN control varies the RTA receiver gain. There are two modes: variable and calibrated. The normal preset is calibrated mode and is used for weather avoidance. The system will be forced into calibrated gain when RCT or TGT are selected. The variable mode is useful for additional weather analysis and for ground mapping. In WX mode, variable gain can increase receiver sensitivity over the calibrated level to show weak targets or it can be reduced below the calibrated level to eliminate weak returns.

48
Q

What is the Range Function?

A

The range can be manually set (CCD) to a desirable value (10 NM, 25 NM, 50 NM, 100 NM, 200 NM, 300 NM). The label OVRG is shown whenever the Map range is greater than 300 NM.

49
Q

What is the Target Alert (TGT) Function?

A

The TGT function monitors for weather beyond the selected range and 7.5° on each side of the airplane heading. If such weather is detected within the monitored heading, outside the selected range until a range of 200 NM, the TGT annunciation changes from a green-armed condition to an amber alert condition on the MFD.

This annunciation advises the flight crew that potentially hazardous weather lies directly in front and outside of the selected range. When this warning is received, the flight crew should select longer ranges to view the questionable target. Note that TGT is inactive when hazards are within the selected range.

Selecting the TGT function forces the system to preset gain and turns off variable gain mode. Selections of ranges of 200 NM or greater automatically turns off TGT function and allows variable gain mode. It can only be selected in the WX mode.
• The TGT annunciation on MFD may occur when the range is increased to 200 NM or greater, even though the function is deactivated.
• In such cases, system logic follows the TGT function annunciation, and gain is automatically preset.
• Selection of 1000 NM range always clears TGT annunciation.

50
Q

What is the Sector Scan (SECT) Function?

A

The normal radar sweep is ± 60 degrees from the airplane nose, at a rate of 12 sweeps per minute. Selecting the SECT pushbutton reduces the angle of sweep to ± 30 degrees and increases the sweep rate to 24 sweeps per minute.

51
Q

What is the TILT Function?

A

The inner knob on the CCD provides tilt control giving the pilot manual control of the antenna tilt angle. The CCD inner knob is a dedicated tilt knob if VAR Gain is not active. Tilt can be varied between 15° up (clockwise rotation) and 15° down (counterclockwise rotation).

Adjusts on tilt minimizes ground clutter when viewing weather targets. To find the ideal tilt angle after the airplane is airborne, adjust the TILT control so that ground clutter does not interfere with viewing of weather targets. Usually, this can be done by tilting the antenna downward in 1° increments until ground targets begin to appear at the display periphery. When ground targets are displayed, move the tilt angle upward in 1° increments until the ground targets begin to disappear.

Ground returns can be distinguished from strong storm cells by watching for closer ground targets with each small downward increment of tilt. The more the downward tilt, the closer the ground targets that are displayed.

Proper tilt adjustment is a pilot judgment, but typically the best tilt angle lies where ground targets are barely visible or just off the radar image.

The following table gives the approximate tilt settings for different altitudes and ranges.

Tilt adjustments is also used for proper tilt management in order to avoid missing or underestimating weather targets. E.g., the upper levels of convective storms are the most dangerous because of the probability of violent Windshears and large hail. But hail and Windshear are not very reflective because they lack reflective liquid water. Convective thunderstorms become much less reflective above the freezing level. This reflectivity decreases gradually over the first 5000 ft to 10000 ft above the freezing level. Proper tilt management demands that tilt be changed continually when approaching hazardous weather so that ground targets are not painted by the radar beam.

52
Q

What is the Rain Echo Attenuation Compensation Technique (REACT) Function?

A

Used in WX mode to compensate for attenuation of the radar signal as it passes through a storm. It does this by increasing the gain of the receiver as weather is detected.

The cyan field indicates areas where further compensation is not possible. This is a warning indicating that attenuation is hiding possible severe weather and should be considered dangerous.

The REACT compensation is active in all modes except GMAP mode.

The REACT compensation can be active in all modes except GMAP mode.

53
Q

What is the TEST function?

A

The test function is selected on MCDU avionics test page. The test is used to select a special test pattern to allow verification of system operation. If fault codes are detected they will be displayed at the same location where tilt angle is displayed in the Weather mode field.

Output power is radiated in test mode, unless the WX radar is in FSBY mode.