2.1 General
2.1.1 The transition altitude for
BangkokTAIRSPACE;CODE_ID;114 FIR is 11000 ft.
2.1.2 The transition level for
BangkokTAIRSPACE;CODE_ID;114 FIR is flight level 130 (FL130).
2.1.3 The transition layer is located between the transition altitude and the transition level.
2.1.4 The vertical position of aircraft operating at or below the transition altitude shall be expressed in terms of altitudes, which are determined from an altimeter set to sea level pressure (
QNH).
Note: This does not preclude a pilot using a QFE setting for terrain clearance purposes during the final approach to the runway.
2.1.5 The vertical position at or above the transition level shall be expressed in terms of flight levels, which are surfaces of constant atmospheric pressure based on an altimeter setting of 1013.2 hPa or 29.92 inHg
2.1.6 While passing through the transition layer, vertical position shall be expressed in terms of:
2.1.6.1 flight levels when climbing; and
2.1.6.2 altitudes when descending.
2.1.7 Cruising within the transition layer is not permitted unless specifically cleared by the
ATS unit providing control services for that portion of airspace.
2.1.8 While operating in the transition layer, vertical position shall be expressed in terms of flight levels or altitudes as advised by
ATC.
2.1.9 Flight level zero is located at the atmospheric pressure level of 1013.2 hPa (29.92 inHg). Consecutive flight levels are separated by a pressure interval corresponding to 500 ft (152.4 m) in the International Standard Atmosphere.
2.1.10 For all flights operating at or below the transition altitude, altimeter shall be set to the appropriate
QNH derived from an available source.
2.2
QNH for aircraft operating at or below the transition altitude
2.2.1 Pilot who operating an aircraft at or below the transition altitude shall set an altimeter to the currently reported
QNH of the nearest station along the route of flight, except as provide in
2.2.2 and
2.2.3.
2.2.2 Pilot who operating an aircraft operating in a terminal control area or a terminal control zone shall set an altimeter to the currently reported
QNH of the major aerodrome of that airspace, which will be given by
ATC.
2.2.3 When there is no appropriate available station, pilot shall set an altimeter to the elevation of the departure aerodrome until the appropriate
QNH can be obtained.
Note: Pressure-altitude-derived level information displayed to the controller and level received from a pilot by radiotelephony might be vary due to different pressure setting.ATC shall comply with criteria as stated in ICAO doc 4444 paragraph 8.5.5 Level information based on the use of pressure-altitude information.
2.3 Take-off and climb
2.3.1 Altimeter setting is made available to aircraft in the routine takeoff and climb instructions.
2.3.2 Vertical displacement of aircraft during climb is controlled by reference to altitude until passing the transition altitude above which vertical displacement is controlled by reference to flight level.
Note: The word “controlled” is used in a composite sense in that a pilot will wish to fly his aircraft on predetermined flight levels or altitudes and ATS will wish to advise a pilot the availability of flight levels or altitudes: both are concerned with vertical position of aircraft.
2.4 Vertical Separation - en-route
2.4.1 Aircraft en-route in the
BangkokTAIRSPACE;CODE_ID;114 FIR (irrespective of whether
IFR or
VFR) shall be flown at flight levels or altitudes where appropriate.
2.4.2 When complying with the table of cruising levels in Civil Aviation Board (CAB) Regulation on Rules of the air, or for
VFR flight above 900 metres (3 000 feet), aircraft shall be flown at levels corresponding to the tracks shown in the following table:
TRACK |
---|
From 000 degrees to 179 degrees | From 180 degrees to 359 degrees |
---|
IFR Flights | VFR Flights | IFR Flights | VFR Flights |
---|
Level | Level | Level | Level |
---|
FL | Feet | Meters | FL | Feet | Meters | FL | Feet | Meters | FL | Feet | Meters |
---|
| 1000 | 300 | - | - | - | | 2000 | 600 | - | - | - |
| 3000 | 900 | | 3500 | 1050 | | 4000 | 1200 | | 4500 | 1350 |
| 5000 | 1500 | | 5500 | 1700 | | 6000 | 1850 | | 6500 | 2000 |
| 7000 | 2150 | | 7500 | 2300 | | 8000 | 2450 | | 8500 | 2600 |
| 9000 | 2750 | | 9500 | 2900 | | 10000 | 3050 | | 10500 | 3200 |
110 | 11000 | 3350 | 115 | 11500 | 3500 | 120 | 12000 | 3650 | 125 | 12500 | 3800 |
130 | 13000 | 3950 | 135 | 13500 | 4100 | 140 | 14000 | 4250 | 145 | 14500 | 4400 |
150 | 15000 | 4550 | 155 | 15500 | 4700 | 160 | 16000 | 4900 | 165 | 16500 | 5050 |
170 | 17000 | 5200 | 175 | 17500 | 5350 | 180 | 18000 | 5500 | 185 | 18500 | 5650 |
190 | 19000 | 5800 | 195 | 19500 | 5950 | 200 | 20000 | 6100 | 205 | 20500 | 6250 |
210 | 21000 | 6400 | 215 | 21500 | 6550 | 220 | 22000 | 6700 | 225 | 22500 | 6850 |
230 | 23000 | 7000 | 235 | 23500 | 7150 | 240 | 24000 | 7300 | 245 | 24500 | 7450 |
250 | 25000 | 7600 | 255 | 25500 | 7750 | 260 | 26000 | 7900 | 265 | 26500 | 8100 |
270 | 27000 | 8250 | 275 | 27500 | 8400 | 280 | 28000 | 8550 | 285 | 28500 | 8700 |
290 | 29000 | 8850 | | | | 300 | 30000 | 9150 | | | |
310 | 31000 | 9450 | | | | 320 | 32000 | 9750 | | | |
330 | 33000 | 10050 | | | | 340 | 34000 | 10350 | | | |
350 | 35000 | 10650 | | | | 360 | 36000 | 10950 | | | |
370 | 37000 | 11300 | | | | 380 | 38000 | 11600 | | | |
390 | 39000 | 11900 | | | | 400 | 40000 | 12200 | | | |
410 | 41000 | 12500 | | | | 430 | 43000 | 13100 | | | |
450 | 45000 | 13700 | | | | 470 | 47000 | 14350 | | | |
490 | 49000 | 14950 | | | | 510 | 51000 | 15550 | | | |
etc. | etc. | | | | | etc. | etc. | etc. | | | |
2.5 Approach and landing
2.5.1 A
QNH altimeter setting is made available in the routine approach and landing instructions.
2.5.2 A
QFE altimeter setting is made available on request in approach and landing clearance but reports to
ATC are to be made in altitude.
2.5.3 Vertical displacement of aircraft during approach is effected by reference to flight level until passing the transition level below which vertical displacement is controlled by reference to altitude, except as provided in
2.5.4.
2.5.4 After approach clearance has been issued and the descent to land is commenced, the vertical position of an aircraft above the transition level may be by reference to altitude (
QNH) provided that level flight above the transition altitude is not indicated or anticipated.