010.07 ATS and ATM .02.06 + .02.07 + .02.08 + .02.09 (speed instructions, wake turbulence) Flashcards
.02.06 Horizontal speed control instructions .02.07 Change from IFR to VFR flight .02.08 Wake turbulence .02.09 Altimeter-setting procedures
In order to facilitate a (…), aircraft may, subject to conditions specified by the appropriate authority, be instructed to adjust speed in a specified manner.
In order to facilitate a (safe and orderly flow of traffic), aircraft may, subject to conditions specified by the appropriate authority, be instructed to adjust speed in a specified manner.
Arriving aircraft should be permitted to operate in a clean configuration for as long as possible. Below FL 150, speed reductions for turbojet aircraft to not less than (…) kt IAS may be used.
Arriving aircraft should be permitted to operate in a clean configuration for as long as possible. Below FL 150, speed reductions for turbojet aircraft to not less than (220) kt IAS, which will normally be very close to the minimum speed of turbojet aircraft in a clean configuration, may be used.
Only minor speed adjustments not exceeding plus/minus (…) kt IAS should be used for aircraft on intermediate and final approach.
Only minor speed adjustments not exceeding plus/minus (20) kt IAS should be used for aircraft on intermediate and final approach.
Speed control should not be applied to aircraft after passing a point (…) NM from the threshold on final approach.
Speed control should not be applied to aircraft after passing a point (4) NM from the threshold on final approach.
If a PIC cancels his IFR flight with the expression “CANCELLING MY IFR FLIGHT”, no reply, other than the acknowledgment (…), should normally be made by an air traffic services unit.
If a PIC cancels his IFR flight with the expression “CANCELLING MY IFR FLIGHT”, no reply, other than the acknowledgment (“IFR FLIGHT CANCELLED AT … (time)”), should normally be made by an air traffic services unit.
Wake turbulence separation minima shall be based on a grouping of aircraft types into three categories according to the (…) mass as follows:
a) HEAVY (H) — all aircraft types of (…) kg or more;
b) MEDIUM (M) — aircraft types less than (…) kg but more than (…) kg; and
c) LIGHT (L) — aircraft types of (…) kg or less.
Wake turbulence separation minima shall be based on a grouping of aircraft types into three categories according to the (maximum certificated take-off) mass as follows:
a) HEAVY (H) — all aircraft types of (136 000) kg or more;
b) MEDIUM (M) — aircraft types less than (136 000) kg but more than (7 000) kg; and
c) LIGHT (L) — aircraft types of (7 000) kg or less.
For aircraft in the heavy wake turbulence category the word “Heavy” shall be included immediately after the aircraft call sign in (all/the initial) radio contact between such aircraft and ATS units.
For aircraft in the heavy wake turbulence category the word “Heavy” shall be included immediately after the aircraft call sign in (the initial) radio contact between such aircraft and ATS units.
Altimeter settings provided to aircraft shall be rounded (up/down) to the nearest (half/whole) hectopascal.
Altimeter settings provided to aircraft shall be rounded (down) to the nearest (whole) hectopascal.
Letter A in the table is (…) min.
A: 2 min, B: 3 min
C: 4 NM, D: 5 NM, E: 6 NM, F: 5 NM
G: 2 min, H: 3 min, I: 3 min
Letter B in the table is (…) min.
A: 2 min, B: 3 min
C: 4 NM, D: 5 NM, E: 6 NM, F: 5 NM
G: 2 min, H: 3 min, I: 3 min
Letter C in the table is (…) NM.
A: 2 min, B: 3 min
C: 4 NM, D: 5 NM, E: 6 NM, F: 5 NM
G: 2 min, H: 3 min, I: 3 min
Letter D in the table is (…) NM.
A: 2 min, B: 3 min
C: 4 NM, D: 5 NM, E: 6 NM, F: 5 NM
G: 2 min, H: 3 min, I: 3 min
Letter E in the table is (…) NM.
A: 2 min, B: 3 min
C: 4 NM, D: 5 NM, E: 6 NM, F: 5 NM
G: 2 min, H: 3 min, I: 3 min
Letter F in the table is (…) NM.
A: 2 min, B: 3 min
C: 4 NM, D: 5 NM, E: 6 NM, F: 5 NM
G: 2 min, H: 3 min, I: 3 min
Letter G in the table is (…) min.
A: 2 min, B: 3 min
C: 4 NM, D: 5 NM, E: 6 NM, F: 5 NM
G: 2 min, H: 3 min, I: 3 min