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Archive / FAA Aviation Weather Handbook / FAA Aviation Weather Handbook: Chapter 25 — Analysis

Chapter 25 — Analysis, Part 4

Chapter 25 — Analysis — Part 4

FAA-H-8083-28B (2026)

Chapter 25, Analysis 25-20

25.3.1.1 Examples

See Figure 25-21 for an example of a 500 mb chart.

Figure 25-21. Example of a 500 mb Constant-Pressure Chart

Constant pressure level forecasts are used to provide an overview of weather patterns at specified times and

pressure altitudes and are the source for wind and temperature aloft forecasts.

Pressure patterns cause and characterize much of the weather. Typically, lows and troughs are associated

with clouds and precipitation , while highs and ridges are associated with fair weather, except in winter

when valley fog may occur. The location and strength of the jet stream can be viewed at 300 mb, 250 mb,

and 200 mb levels.

25.3.2 Radiosonde Observation (Weather Balloon) Analysis

A common means of analyzing radiosonde observations is the skew-T diagram (see Figure 25-22). Skew-T

diagrams are primarily intended for, and used by, meteorologists as part of their analyses of the atmosphere.

For example, the skew-T diagram can be used to:

• Determine the freezing level (or levels).

• Determine the stability of the atmosphere.

• Determine the potential for severe weather.

• Determine the height and depth of inversions.

Chapter 25, Analysis 25-21

• Infer cloud bases, tops, and layers.

• Determine soaring conditions.

25.3.2.1 Issuance

Skew-T diagrams are primarily intended for, and used by, meteorologists as part of their analyses of the

atmosphere and formulation of various forecasts.

Skew-T diagrams are available from the NWS NCO. Their “Model Analyses and Guidance ” website

contains a user’s guide that provides descriptions, details, and examples of the various products, including

the skew-T.

25.3.2.2 Format

The skew -T diagram provided on the NWS NCO “Model Analyses and Guidance ” website uses the

following format (other weather providers and websites may have different formats, especially colors):

• Horizontal axis is temperature in degrees Celsius, skewed to the right, labeled -20, 0,

and 20 (Celsius).

• Vertical axis is pressure levels in millibars, labeled 1,000 (near sea level) to 100 (approximately

53,000 ft MSL).

• Bold, solid red line represents the temperature profile over the station taken from the radiosonde

observation (weather balloon).

• Bold, solid green line represents the dewpoint profile.

• Wind aloft is shown on the far-right side.

Figure 25-22. Skew-T Diagram Example

Chapter 25, Analysis 25-22

25.3.2.3 Examples

Two examples are provided below: a multiple freezing level example (see Figure 25-23) and a cloud top

example (see Figure 25-24).

25.3.2.3.1 Multiple Freezing Level Example

Note how the temperature profile (bold red line) crosses the 0 -degree temperature line (also known as an

isotherm) five times (near 900 mb, 860 mb, 775 mb, 725 mb, and 675 mb).

Figure 25-23. Skew-T Diagram—Multiple Freezing Level Example

25.3.2.3.2 Cloud Top Example

Figure 25-24 is the radiosonde observation from Vandenberg Space Force Base (VSFB), California, for

1200 UTC for a typical coastal stratus cloud.

At about 950 mb, the temperature profile (bold red line) and dewpoint profile (bold green line) almost touch

each other. This is the profile of a cloud top. The temperature and dewpoint quickly diverge, representing

a change from the cool, moist air (and associated strat us cloud) to the dry and warmer air (cloud free)

above.

Figure 25-24. Skew-T Diagram—Cloud Top Example

Chapter 25, Analysis 25-23

25.4 Freezing Level Analysis

The freezing level is the lowest altitude in the atmosphere over a given location at which the air temperature

reaches 0°C. This altitude is also known as the height of the 0°C constant-temperature surface.

The initial analysis is updated hourly. The colors represent the height in hundreds of feet above MSL of the

lowest freezing level. Regions with white indicate the surface and the entire depth of the atmosphere are

below freezing. Hatched or spotted regions (if present) represent areas where the surface te mperature is

below freezing with multiple freezing levels aloft.

More information on the freezing level forecast graphics is available on the AWC’s website.

See Section 27.12 for additional information on freezing level forecast graphics.

25.5 Icing Analysis [Current Icing Product (CIP)]

The NWS produces icing products that are derived from NWS computer model data combined with

observations with no forecaster modifications. One of these products is the CIP.

The CIP combines weather satellite, weather radar, METAR, PIREPs and NWS model data to provide an

hourly 3D diagnosis of the icing environment. This information is displayed on a suite of graphics available

for the CONUS, much of Canada and Mexico, and their respective coastal waters.

The CIP [and its forecast counterpart Forecast Icing Product ( FIP) (see Section 27.13)] provide a

broad-brush approach to describing icing intensity using estimated liquid water content , drop size, and

temperature to depict ice accumulation rate. The intensity of ice accumulation rate varies by aircraft wing

shape. Hence, the icing intensity categories depicted in CIP s and FIPs (e.g., none, light, moderate, heavy)

is only a broad -brushed indication of ice accumulation rate, and not necessarily of aircraft performance.

The icing terms used in SIGMETs and AIRMETs do refer to icing impact on aircraft.

CIPs will continue to evolve over the coming years with increased model resolutions, additional horizontal

layers, and improvements to the algorithms and/or data sets used to produce the products. Along with these

improvements may come a change in references to the product update version. Users can find additional

information on these products and any changes on the AWC’s website.

The CIP suite as it appears on the AWC’s website consists of three graphics, including:

• Icing Probability (see Section 27.13.1 for additional information).

• Icing Severity (see Section 27.13.2 for additional information).

• Icing Severity plus SLD (see Section 27.13.3 for additional information).

The CIPs are generated for select altitudes from 1,000 ft MSL to FL300.

The CIPs can be viewed at single altitudes and FLs or as a composite of all altitudes from 1,000 ft MSL to

FL300, which is referred to as the “maximum” or “max.”

The CIP can be used to identify the latest and forecast 3D probability and intensity of ice accumulation rate.

The CIP should be used in conjunction with the report and forecast information contained in an AIRMET

and SIGMET.

The Icing Severity plus SLD product can help in determining the threat of SLD, which is particularly

hazardous to some aircraft.

Icing PIREPs are plotted on a single -altitude CIP graphic if the PIREP is within 1,000 ft of the selected

altitude and has been observed within 75 minutes of the chart ’s valid time. Icing PIREPs for all altitudes

(i.e., 1,000 ft MSL to FL300) are displayed, except negative reports are omitted to reduce clutter. The

PIREP legend is located on the bottom of each graphic.

Chapter 25, Analysis 25-24

Finally, while the “C” in CIP stands for “current,” the product does not show the current conditions, rather

it depicts the computer ’s expected conditions at the valid time shown on the product. This valid time can

be an hour old or more depending on when it is received by the user.

See Section 27.13 for additional information on the FIP.

25.6 Turbulence (Graphical Turbulence Guidance Nowcast (GTG-N))

The GTG Nowcast (GTG-N) product has been developed as a tactical aid for aviation. GTG-N provides a

nowcast of the current turbulent state of the atmosphere over the CONUS in near real-time, updating every

15 minutes. The basis for the nowcast is the most recently available short -term (one-hour) forecast from

the GTG product whose valid time is closest to the current update time. Recent observations of turbulence

are then used to update the GTG forecast and create a blended nowcast (expressed as EDR).

Current inputs include PIREPs, automated in situ EDR reports, and EDR estimated from ground -based

radar observations via the Next-Generation Radar (NEXRAD) Turbulence Detection Algorithm (NTDA).

In future upgrades, lightning, wind/gust observations from METARs, and EDR derived from ADS -B

vertical rate data will be assimilated as well.

GTG-N is available at 100 ft MSL, 1000 ft MSL, then every 1000 ft up to FL500.

See Section 27.14 for additional information on the GTG forecast.

25.7 Real-Time Mesoscale Analysis (RTMA)

RTMA is an hourly analysis system by the NWS ’ Environmental Modeling Center that produces analyses

of surface weather elements. The FAA has determined that RTMA temperature and altimeter setting

information is a suitable replacement for missing temperature and altimeter setting observations for a subset

of airports. RTMA temperature and altimeter setting information is intended for use by operators, pilots,

and aircraft dispatchers when an airport lacks a surface temperature and/or altimeter setting report from an

automated weather system (e.g., ASOS or AWOS sensor) or human observer. Airports with RTMA data

available are located in Alaska, Guam, Hawaii, Puerto Rico, and the CONUS.

RTMA is issued by the NWS every hour, 24 hours a day. Temperatures and altimeter settings are reported

for an airport station including the latitude and the longitude. Temperatures are reported in degrees Celsius.

Altimeter setting is reported in inches of mercury. See Figure 25-25 for an example RTMA temperature

and altimeter setting report.

Chapter 25, Analysis 25-25

25.7.1 Adjustments

The values found at the RTMA site are 95 percent accurate throughout the United States for both

temperature and altimeter setting when using the following mitigations:

• Temperature requires adding 4°C to the RTMA-derived temperature.

• Altimeter setting requires increasing the minimum descent altitude (MDA) or decision height

(DH) value on the approach chart by 100 ft and increasing the required flight visibility minimums

by ½ SM.

*****************************************************************

RTMA 2m-temperature (degrees Celsius) and altimeter setting

(inHg)

COMPUTED: 1239Z 25 Jan 2024

VALID: 1239Z 25 Jan 2024 to 1339Z 25 Jan 2024

*****************************************************************

Station Lat Lon 2m-T ALT

KABE 40.65 -75.44 3.43 30.19

KABI 32.41 -99.68 7.31 30.08

KABQ 35.04 -106.61 1.67 N/A

KABR 45.45 -98.42 -2.06 30.02

KABY 31.54 -84.19 19.07 30.15

KACK 41.25 -70.06 8.98 30.14

KACT 31.61 -97.23 10.00 30.06

KACV 40.98 -124.11 9.74 30.22

KACY 39.46 -74.58 11.59 30.17

KADS 32.97 -96.84 8.69 N/A

KAEX 31.33 -92.55 15.29 29.96

KAFW 32.99 -97.32 8.40 30.06

KAGS 33.37 -81.96 18.85 30.21

KAHN 33.95 -83.33 16.51 30.23

KAIA 42.05 -102.80 -4.11 29.94

KALB 42.75 -73.80 3.18 30.09

KALN 38.89 -90.05 3.02 30.12

KALO 42.56 -92.40 1.03 30.10

Figure 25-25. RTMA Surface Temperature and Altimeter Setting Example

Original source PDFPublished from pages 362–367 of the recorded source chapter.
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