ENR 1.7  ALTIMETER SETTING PROCEDURES

1. INTRODUCTION

The Altimeter Setting Procedures in use generally conform to those contained in ICAO Doc 8168 - Procedures for Air Navigation Services - Aircraft Operations (PANS-OPS), Volume III, Section 2 and are given in full below.

Information on the QNH and air temperature for use in determining adequate terrain clearance and transition level is provided in MET reports, ATIS broadcasts or transmitted by the appropriate ATS unit.

QNH values are given in hectopascals (HPA) rounded down to the nearest lower whole hectopascal.

2. BASIC ALTIMETER SETTING PROCEDURES

2.1 Transition altitude

The transition altitude within the entire Riga FIR is 5000 ft (1500 m) AMSL.

2.2 Transition level

The transition level is the lowest flight level available for use and located at least 1000 ft (300 m) above the transition altitude to permit the transition altitude and the transition level to be used concurrently in cruising flight, with vertical separation ensured, and it will be calculated according to the following table:

Transition altitude 5000 FT

QNH value

Transition level

901 - 942

85

943 - 959

80

960 - 977

75

978 - 995

70

996 - 1013

65

1014 - 1031

60

1032 - 1050

55

1051

50


2.3 Take-off and climb

A QNH altimeter setting is made available to aircraft during taxi clearance, prior to take-off. QFE values will be given on request only.

Vertical positioning of aircraft during climb is expressed in terms of altitudes until the transition altitude is reached above which vertical positioning is expressed in terms of flight levels.

2.4 En-route

For en-route flight which implies that the aircraft will be flying at an altitude equal to or lower than the transition altitude, ATS unit will inform aircraft about the altimeter setting to be used within the area concerned.

2.5 Approach and landing

A QNH altimeter setting is made available during approach clearance and during clearance to enter the traffic circuit.

QFE altimeter settings will be given on request only.

Vertical positioning of aircraft during approach is controlled by reference to flight levels until the transition level is reached, below which vertical positioning is controlled by reference to altitudes.

2.6 Missed approach

The relevant portions of 2.3 and 2.5 shall be applied in the event of a missed approach.

3. DESCRIPTION OF ALTIMETER SETTING REGION(S)

3.1 Altimeter setting regions

Lateral limits of altimeter setting regions within Riga FIR are corresponding to the GAMET/AIRMET areas in GEN 3.5.

3.2 Regional QNH

Regional QNH is a forecast of minimum value of QNH within Riga FIR sub-areas for a specified time period.

Forecast of the minimum QNH values for sub-areas is provided in GAMET according to GEN 3.5.4.

3.3 Description of aerodrome related QNH areas

During flight at or below the transition altitude the following pressure shall be set on altimeter:

a. within Riga CTR, Liepaja FIZ Sector B and FIZ Sector A - QNH of the aerodrome;

b. within Riga TMA B and a layer 1000 ft (300 m) below* - QNH of aerodrome Riga;

c. within Riga TMA C and a layer 1000 ft (300 m) below* - QNH of aerodrome Lielvarde;

d. all other airspace is part of the forecast QNH altimeter setting region system.

* It concerns flights in airspace just below the lower limit of TMA, during which it could come to unintended and undesirable penetration of TMA when the pressure is set up incorrectly.

3.4 Lower limit of controlled airspace

Lower limit of controlled airspace defined by altitude (AMSL) is always references to the QNH of:

a. Riga TMA A - Regional QNH;

b. Riga TMA B - Riga aerodrome QNH;

c. Riga TMA C - Lielvarde aerodrome QNH.

4. PROCEDURES APPLICABLE TO OPERATORS (INCLUDING PILOTS)

4.1 Flight planning

The levels at which a flight is to be conducted shall be specified in a flight plan:

1. In terms of flight levels if the flight is to be conducted at or above the transition level, and

2. In terms of altitudes if the flight is to be conducted at or below the transition altitude.

Note: Flight levels and altitudes are specified in a flight plan by number not in terms of FT or M.

4.2 Corrections of altimeter setting

The pilot is responsible for corrections to altimeter settings as described in Doc 8168 (PANS-OPS). If an aircraft is cleared by ATC to an altitude which the pilot-in-command finds unacceptable due to low temperature or any other operational requirement then the pilot-in-command shall request an alternative altitude. If such a request is not received ATC will consider that the clearance has been accepted and will be complied with.

5. TABLE OF CRUISING LEVELS

The cruising levels to be observed when so required are as follows:

MAGNETIC TRACK

From 000 degrees to 179 degrees

From 180 degrees to 359 degrees

IFR Flights

VFR Flights

IFR Flights

VFR Flights

Altitude

Altitude

Altitude

Altitude

FL

Metres

Feet

FL

Metres

Feet

FL

Metres

Feet

FL

Metres

Feet

010

300

1000

-

-

-

020

600

2000




030

900

3000

035

1050

3500

040

1200

4000

045

1350

4500

050

1500

5000

055

1700

5500

060

1850

6000

065

2000

6500

070

2150

7000

075

2300

7500

080

2450

8000

085

2600

8500

090

2750

9000

095

2900

9500

100

3050

10000

105

3200

10500





110

3350

11000

115

3500

11500

120

3650

12000

125

3800

12500

130

3950

13000

135

4100

13500

140

4250

14000

145

4400

14500

150

4550

15000

155

4700

15500

160

4900

16000

165

5050

16500

170

5200

17000

175

5350

17500

180

5500

18000

185

5650

18500

190

5800

19000

195

5950

19500

200

6100

20000

205

6250

20500





210

6400

21000

215

6550

21500

220

6700

22000

225

6850

22500

230

7000

23000

235

7150

23500

240

7300

24000

245

7450

24500

250

7600

25000

255

7750

25500

260

7900

26000

265

8100

26500

270

8250

27000

275

8400

27500

280

8550

28000

285

8700

28500

290

8850

29000


300

9150

30000






310

9450

31000


320

9750

32000




330

10050

33000


340

10350

34000




350

10650

35000


360

10950

36000




370

11300

37000


380

11600

38000




390

11900

39000


400

12200

40000








410

12500

41000


430

13100

43000




450

13700

45000


470

14350

47000




490

14950

49000


510

15550

51000




etc.

etc.

etc.


etc.

etc.

etc.