Previous Page Page 472 Next Page  
background image

AIM

4/3/14

7−1−44

Meteorology

TBL 7

−1−7

PIREP Element Code Chart

PIREP ELEMENT

PIREP CODE

CONTENTS

1.

3−letter station identifier

XXX

Nearest weather reporting location to the reported phenomenon

2.

Report type

UA or UUA

Routine or Urgent PIREP

3.

Location

/OV

In relation to a VOR

4.

Time

/TM

Coordinated Universal Time

5.

Altitude

/FL

Essential for turbulence and icing reports

6.

Type Aircraft

/TP

Essential for turbulence and icing reports

7.

Sky cover

/SK

Cloud height and coverage (sky clear, few, scattered, broken, or

overcast)

8.

Weather

/WX

Flight visibility, precipitation, restrictions to visibility, etc.

9.

Temperature

/TA

Degrees Celsius

10. Wind

/WV

Direction in degrees magnetic north and speed in knots

11. Turbulence

/TB

See AIM paragraph 7−1−23

12. Icing

/IC

See AIM paragraph NO TAG

13. Remarks

/RM

For reporting elements not included or to clarify previously

reported items

EXAMPLE

1. KCMH UA /OV APE 230010/TM 1516/FL085/TP
BE20/SK BKN065/WX FV03SM HZ FU/TA 20/TB LGT

NOTE

1. One zero miles southwest of Appleton VOR; time
1516 UTC; altitude eight thousand five hundred; aircraft
type BE200; bases of the broken cloud layer is six thousand
five hundred; flight visibility 3 miles with haze and smoke;
air temperature 20 degrees Celsius; light turbulence.

EXAMPLE

2. KCRW UV /OV KBKW 360015

−KCRW/TM

1815/FL120//TP BE99/SK IMC/WX RA/TA M08 /WV
290030/TB LGT

−MDT/IC LGT RIME/RM MDT MXD

ICG DURC KROA NWBND FL080

−100 1750Z

NOTE

2. From 15 miles north of Beckley VOR to Charles-
ton VOR; time 1815 UTC; altitude 12,000 feet; type
aircraft, BE

−99; in clouds; rain; temperature minus

8 Celsius; wind 290 degrees magnetic at 30 knots; light to
moderate turbulence; light rime icing during climb
northwestbound from Roanoke, VA, between 8,000 and
10,000 feet at 1750 UTC.

7

1

21. PIREPs Relating to Airframe Icing

a.

The effects of ice on aircraft are cumulative-

thrust is reduced, drag increases, lift lessens, and

weight increases. The results are an increase in stall

speed and a deterioration of aircraft performance. In

extreme cases, 2 to 3 inches of ice can form on the

leading edge of the airfoil in less than 5 minutes. It

takes but 

1

/

2

 inch of ice to reduce the lifting power of

some aircraft by 50 percent and increases the

frictional drag by an equal percentage.

b.

A pilot can expect icing when flying in visible

precipitation, such as rain or cloud droplets, and the

temperature is between +02 and −10 degrees Celsius.

When icing is detected, a pilot should do one of two

things, particularly if the aircraft is not equipped with

deicing equipment; get out of the area of

precipitation; or go to an altitude where the

temperature is above freezing. This “warmer”

altitude may not always be a lower altitude. Proper

preflight action includes obtaining information on the

freezing level and the above freezing levels in

precipitation areas. Report icing to ATC, and if

operating IFR, request new routing or altitude if icing

will be a hazard. Be sure to give the type of aircraft to

ATC when reporting icing. The following describes

how to report icing conditions.

1. Trace.

Ice becomes perceptible. Rate of

accumulation slightly greater than sublimation.

Deicing/anti-icing equipment is not utilized unless

encountered for an extended period of time (over

1 hour).

  Previous Page Page 472 Next Page