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.
The transition altitude within the entire Riga FIR is 5000 ft (1500 m) AMSL.
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 |
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.
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.
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.
The relevant portions of 2.3 and 2.5 shall be applied in the event of a missed approach.
Lateral limits of altimeter setting regions within RIGA FIR are corresponding to the GAMET/AIRMET areas in GEN 3.5.
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.
During flight at or below the transition altitude the following pressure shall be set on altimeter:
a. within RIGA CTR, LIEPAJA TIA and TIZ - 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.
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.
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.
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.
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. |
|
|
|