ENR 1.7 ALTIMETER SETTING PROCEDURES


1.7.1 Introduction

1.7.1.1. The altimeter setting procedures in use generally conform to those contained in ICAO Doc 8168, Vol. I , Part 6 and are given in full below. Differences are shown in heavy black type.
1.7.1.2. The transition altitude ( TA ) is given:
  1. in the AD 2.17 tabulation, for the aerodrome but only for those aerodromes outside the Jeddah FIR which are , therefore, non standard (see 1.7.2.1.1 below); and
  2. on all instrument approach charts.
1.7.1.3. QNH and temperature data, for use in determining adequate terrain clearance, are included in ATIS broadcasts, where provided, or are available on request from the appropriate ATS unit. QNH values are given in hectopascals (millibars), rounded down to the nearest whole unit.

1.7.2 Basic altimeter setting procedures

1.7.2.1 General

1.7.2.1.1. A common TA of 13 000 FT and a fixed transition level (TL) of FL 150 are established for the whole of Jeddah FIR airspace.
 
Note 1 : The altitude equivalent of FL 150, calculated from the lowest known MSL pressure in Saudi Arabia (986 HPA), is 14 265 FT and, therefore, a minimum of 1 000 FT of vertical separation exists in the transition layer under all surface atmospheric pressure conditions; thus, simultaneous flight at both TA and TL is always permissible, but level flight within the layer is prohibited.
 

Note 2 : The classification of the airspace within the transition layer assumes the classification of the airspace within which it resides.
1.7.2.1.2. The vertical position of aircraft is expressed in terms of:
  1. altitude, when at or below the TA and when descending through the transition layer; and
  2. flight level, when at or above the TL and when climbing through the transition layer.
1.7.2.1.3. Flight level zero is located at the atmospheric pressure level of 1 013.2 HPA. Consecutive flight levels are separated by a pressure interval corresponding to 500 FT (152.4 M) in the ICAO International Standard Atmosphere ( ISA ).

1.7.2.2 Take-off and climb

1.7.2.2.1. A QNH altimeter setting is available either:
  1. in routine departure information, by ATIS ( where applicable ) or RTF, at aerodromes with ATS units; or
  2. from Jeddah ACC , Dammam Approach , Abha APP, Riyadh Approach or Tabuk APP, as appropriate, for aerodromes without ATS units.
1.7.2.2.2. Vertical position of aircraft during climb is controlled by reference to altitude until reaching the TA, and by reference to flight level above the TA.

1.7.2.3 Vertical separation enroute

1.7.2.3.1. Vertical separation of aircraft enroute is controlled by reference to:
  1. altitude, when at and below the TA; and
  2. flight level, when at and above the TL.
1.7.2.3.2. Vertical separation is applied by requiring aircraft to fly at the appropriate hemispherical level prescribed in ICAO Annex 2, Appendix 3, according to the magnetic track of the aircraft, except that non hemispherical levels are also assigned on one way airways if necessary to improve traffic flow or avoid double level changes, as shown below:
 


IFR ALTITUDES 13 000 FT AND BELOW
359°  
  000°
EVEN  
  ODD
2 000  
4 000  
6 000 1 000
8 000 3 000
10 000 5 000
12 000 7 000
  9 000
  11 000
  13 000
180°  
  179°

 
IFR FLIGHT LEVELS FL 150 UP TO FL 290
 
359°  
  000°
EVEN  
  ODD
160  
180  
200 150
220 170
240 190
260 210
280 230
  250
  270
180°  
  179°

 

 

 

 

 

 

VFR ALTITUDES BELOW 13 000 FT
 
359°  
  000°
EVEN  
  ODD
2 500  
4 500  
6 500 1 500
8 500 3 500
10 500 5 500
12 500 7 500
  9 500
  11 500
180°  
  179°


IFR FLIGHT LEVELS (FL290 - FL410) INCLUSIVE IN RVSM AIRSPACE "APPLY 2000 INTERVALS"
 
359°  
  000°
   
EVEN  
300 ODD
320 290
340 310
360 330
380 350
400 370
430 390
470 410
510 450
550 490
590 530
  570
   
180°  
  179°

Note 1 : Aircraft operating on ATS routes above FL 600 or below ALT 11 500 FT will be outside controlled airspace and, therefore, will be provided with flight information service only.
 

Note 2 : Since VFR is not permitted above FL 150, the highest usable VFR level is ALT 12 500 FT.
 

Note 3 : Some of the lower levels shown above may not be usable due to terrain clearance requirements.
1.7.2.3.3. Current QNH reports are used to determine the terrain clearance for flights operating at or below the TA. The chart on page ENR 6.11 Altimeter Setting Observing Stations - Index Chart depicts the network of observing stations, which report QNH hourly; these reports are provided direct to ATS units established at aerodromes and, in the form of an hourly METAR bulletin, to Jeddah ACC, Dammam Approach, Abha Approach , Riyadh Approach and Tabuk APP.

1.7.2.4 Approach and landing

1.7.2.4.1 A QNH altimeter setting is available either:

  1. in routine approach and landing information, by ATIS (where applicable) or RTF, at aerodromes with ATS units ; or
  2. from Jeddah ACC, Dammam Approach, Abha Approach, Riyadh Approach or Tabuk APP, as appropriate, for aerodrome without ATS units.

Note: At present there is no observing station at Jubail; the Dammam QNH is authorized for remote use.
1.7.2.4.2. A QFE altimeter setting is available on request at aerodromes with ATS units; QFE is NOT readily available at other aerodromes. Where available, the QFE reference datum is either:
  1. runway threshold elevation - for all precision runways and those non-precision runways with a threshold elevation 7 FT or more below aerodrome elevation; or
  2. aerodrome elevation - for all other runways.
1.7.2.4.3. Vertical positioning of aircraft during approach is controlled by reference to flight levels until reaching the TL, and by reference to altitude below the TL. However, this does not preclude pilots from using either:
  1. QNH setting from top of descent, provided that level flight above the TA is neither indicated nor anticipated; or
  2. QFE setting, where available, for terrain clearance purposes during final approach to the runway. 

1.7.2.5 Missed approach

The relevant portions of the preceding paragraphs apply in all cases of missed approach.

1.7.3 Description of altimeter setting region

The altimeter setting regions are shown on the Altimeter Setting Observing Stations Index Chart ENR 6.11.

1.7.4 Procedures applicable to operators (including pilots)

1.7.4.1 Flight planning

1.7.4.1.1. The levels at which a flight is to be conducted shall be specified in a flight plan in terms of:
  1. flight level, when the flight is to be operated at or above the TL; and
  2. altitude, when the flight is to be operated at or below the TA.
1.7.4.1.2. The levels selected should:
  1. ensure adequate terrain clearance for the entire route; and
  2. satisfy ATC requirements; and
  3. be compatible with those shown in paragraph 2.3.2.

Note 1 : The information required to determine the lowest level which will ensure adequate terrain clearance may be obtained from the appropriate services unit, e.g. ATS, AIS or MET.

Note 2 : The levels selected will depend upon the accuracy with which the vertical position of such levels relative to the terrain can be estimated which, in turn, is dependent upon the type of meteorological information available. A lower level may be used with confidence when its position is based on current information relevant to the particular route to be flown and when it is known that amendments to this information will be available in flight; but a higher level will be needed when based on information less relevant to the particular route to be flown and the time at which the flight is to be conducted. See chart on page ENR 6.11.

Note 3 : Flights over level terrain may often be conducted at one level, whereas flights over mountainous terrain may require several changes in levels to account for changes in the elevation of the terrain. The use of several levels may also be needed in order to comply with ATS requirements.
 

1.7.4.2 Pre-flight operational test

1.7.4.2.1. The following test should be performed by flight crew members prior to take-off; the purpose of this test being to establish whether or not the altimeter readout is within the permissible range for that instrument.
1.7.4.2.2. With the aircraft at a known elevation on the aerodrome, set the altimeter pressure scale to the appropriate current value (QNH or QFE). Vibrate the instrument by tapping unless a mechanical vibration is provided. A serviceable altimeter will indicate either:
  1. QNH - the elevation of the point selected plus the height of the altimeter above this point; or
  2. QFE - the height of the altimeter in relation to the QFE reference datum;

within a tolerance of plus/minus 60 FT or 80 FT for altimeters with test ranges up to 30 000 FT or 50 000 FT respectively.

Note 1 : When the altimeter does not indicate the reference elevation or height exactly, but is within the specified tolerance, no adjustment of this indication should be made either by means of the pressure adjustment knob or other adjustment on the altimeter at any stage of a flight. Furthermore, any error that is within tolerance, noted during pre-flight check on the ground, should be ignored by the pilot during flight.

Note 2 : The tolerances specified above are considered acceptable for aerodrome elevations up to 3 500 FT ISA. The tables below indicate the permissible range for different aerodrome elevations and when pressure is lower than ISA.
 

Table 1
  Tolerances for altimeters
with test range up to
30 000 FT.
 
AD
ELEV
(FT)
Permissible
Range
(FT)
2 000 1 940 to 2 060
3 000 2 930 to 3 070
4 000 3 925 to 4 075
5 000 4 920 to 5 080
6 000 5 915 to 6 085
7 000 6 905 to 7 095
 

Table 2
  Tolerances for altimeters
with test range up to
50 000 FT.
AD
ELEV
(FT)
Permissible
Range
(FT)
2 000 1 900 to 2 100
3 000 2 895 to 3 105
4 000 3 885 to 4 115
5 000 4 875 to 5 125
6 000 5 865 to 6 135
7 000 6 855 to 7 145

1.7.4.3 Take off and climb

1.7.4.3.1. Prior to take-off, one altimeter shall be set to the latest QNH available for the aerodrome.
1.7.4.3.2. During climb, all references to the vertical position of the aircraft in air-ground communications shall be expressed in terms of:
  1. altitude, up to and while at the TA ; and
  2. flight level, above the TA.
1.7.4.3.3. The reference to vertical position of the aircraft shall be changed from altitude ( QNH ) to flight level ( ISA 1 013.2 HPA ) when leaving or passing the TA.

1.7.4.4 Enroute

1.7.4.4.1. Vertical separation during enroute flight is accomplished as follows:
  1. at or below the TA, aircraft shall be flown at altitudes and references to vertical position in air-ground communications shall be expressed in such terms; and
  2. at or above the TL , aircraft shall be flown at flight levels and references to vertical position in air-ground communications shall be expressed in such terms.
1.7.4.4.2. It is essential that all aircraft operating in the same airspace segment use the same altimeter setting reference to ensure that vertical separation is not infringed and, therefore, aircraft flown entirely in accordance with paragraph 1.7.4.4.1 a) above shall set QNH as follows:
  1. within a TMA, the QNH provided for the area by the controlling ATS unit except that aircraft destined to other aerodromes within that same TMA shall set the appropriate aerodrome QNH when entering the relevant ATZ or, where no ATZ is established, the aerodrome traffic circuit; or
  2. elsewhere, the QNH for the nearest on track station, the changeover from the station QNH behind the aircraft to that ahead being made at the mid point between the two stations.

Note : This does not preclude aircraft using off-track QNH reports to assess terrain clearance in accordance with paragraph 1.7.4.4.3 below.
 
1.7.4.4.3. Terrain clearance shall be assessed using the latest and most appropriate QNH altimeter setting reports available.


 
1.7.4.4.4. Where the adequacy of terrain clearance cannot be assessed with an acceptable degree of accuracy by means of the QNH reports available, other information shall be obtained from the appropriate services unit for checking the adequacy of terrain clearance.
 

1.7.4.5 Approach and landing

1.7.4.5.1. Prior to descending below the TL, the latest QNH altimeter setting for the aerodrome shall be obtained.
 
1.7.4.5.2. On descending below the TL, the reference for vertical position shall be changed from flight level (ISA 1 013.2 HPA) to altitude (QNH) and, thereafter, the vertical position of the aircraft shall be expressed in terms of altitude.

Note : This does not preclude a pilot using either:
  1. QFE for terrain clearance during final approach in accordance with 1.7.4.5.3 below; or
  2. the change of reference for vertical position from flight level to altitude above the TL, when so cleared by the appropriate ATS unit, after approach clearance has been issued and the descent to land commenced, provided that level flight above the TA is neither indicated nor anticipated.
1.7.4.5.3. When an aircraft is cleared as number one to land and is completing its approach using QFE, vertical position shall be expressed in terms of height, above the aerodrome reference datum used in establishing OCH, during that portion of its flight for which QFE may be used.
 
The relevant portions of the preceding paragraphs apply in all cases of missed approach.

1.7.5 Tables of cruising levels

The cruising levels to be observed when so required are as follows:
  1. in areas where, on the basis of regional air navigation agreement and in accordance with conditions specified therein, a vertical separation minimum (VSM) of 300 M (1 000 FT) is applied between FL 290 and FL 410 inclusive:*
     
TABLE A
 
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
-90     -- -- -- 0     -- -- --
10 300 1000 -- -- -- 20 600 2000 -- -- --
30 900 3000 35 1050 3500 40 1200 4000 45 1350 4500
50 1500 5000 55 1700 5500 60 1850 6000 65 2000 6500
70 2150 7000 75 2300 7500 80 2450 8000 85 2600 8500
90 2750 9000 95 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      
530 16150 53000       550 16750 55000      
570 17350 57000       590 18000 59000      
etc. etc. etc.       etc. etc. etc.      
 
* Except when, on the bases of regional air navigation agreements, a modified table of cruising levels based on a nominal vertical separation minimum of 300 M ( 1000 FT ) is prescribed for use, by aircraft operating above FL 410 within designated portion of the airspace.
** Magnetic track, or in polar areas at latitudes higher than 70 degrees and within such extensions to those areas as may be prescribed by the appropriate ATS authorities, grid tracks as determined by a network of lines parallel to the Greenwich Meridian superimposed on a polar stereo graphic chart in which the direction towards the North Pole is employed as the Grid North.
***Except where, on the basis of regional air navigation agreements, from 090 to 269 degrees and from 270 to 089 degrees is prescribed to accommodate predominant traffic dircetions and appropriate transition procedures to be associated therewith are specified.
TABLE B
 
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
-90     -- -- -- 0     -- -- --
10 300 1000 -- -- -- 20 600 2000 -- -- --
30 900 3000 35 1050 3500 40 1200 4000 45 1350 4500
50 1500 5000 55 1700 5500 60 1850 6000 65 2000 6500
70 2150 7000 75 2300 7500 80 2450 8000 85 2600 8500
90 2750 9000 95 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      
490 14950 49000       510 15550 51000      
530 16150 53000       550 16750 55000      
etc. etc. etc.       etc. etc. etc.      
 
* Except when, on the bases of regional air navigation agreements, a modified table of cruising levels based on a nominal vertical separation minimum of 300 M (1 000 FT) is prescribed for use, by aircraft operating above FL410 within designated portion of the airspace.
** Magnetic track, or in polar areas at latitudes higher than 70 degrees and within such extensions to those areas as may be prescribed by the appropriate ATS authorities, grid tracks as determined by a network of lines parallel to the Greenwich Meridian superimposed on a polar stereo graphic chart in which the direction towards the North Pole is employed as the Grid North.