010.06 AIRCRAFT OPS .04 (approach procedures) Flashcards
.04 Approach procedures - ICAO Doc 8168, Volume I
Aircraft performance has a direct effect on the airspace and visibility required for the various manoeuvres associated with the conduct of instrument approach procedures. The most significant performance factor is (…).
Aircraft performance has a direct effect on the airspace and visibility required for the various manoeuvres associated with the conduct of instrument approach procedures. The most significant performance factor is (aircraft speed).
Vat is (…)
VSO is (…)
VS1g is (…)
Vat is (indicated airspeed at threshold)
VSO is (stall speed in landing configuration)
VS1g is (stall speed at 1g load factor)
Vat is equal to VSO • (…) or VS1g • (…).
If both VSO and VS1g are available, the (higher/lower) resulting Vat shall be applied.
Vat is equal to VSO • (1.3) or VS1g • (1.23).
If both VSO and VS1g are available, the (higher) resulting Vat shall be applied.
Aircraft categories based on approach speed (Vat):
When the Vat is 166 kt or more but less than 211 kt, the aircraft category is (…)
Category A <91 kt
Category B 91 kt - 120 kt
Category C 121 kt - 140 kt
Category D 141 kt - 165 kt
Category E 166 kt - 210 kt
Aircraft categories based on approach speed (Vat):
When the Vat is 141 kt or more but less than 166 kt, the aircraft category is (…)
Category A <91 kt
Category B 91 kt - 120 kt
Category C 121 kt - 140 kt
Category D 141 kt - 165 kt
Category E 166 kt - 210 kt
Aircraft categories based on approach speed (Vat):
When the Vat is 121 kt or more but less than 141 kt, the aircraft category is (…)
Category A <91 kt
Category B 91 kt - 120 kt
Category C 121 kt - 140 kt
Category D 141 kt - 165 kt
Category E 166 kt - 210 kt
Aircraft categories based on approach speed (Vat):
When the Vat is less than 91 kt, the aircraft category is (…)
Category A <91 kt
Category B 91 kt - 120 kt
Category C 121 kt - 140 kt
Category D 141 kt - 165 kt
Category E 166 kt - 210 kt
Aircraft categories based on approach speed (Vat):
When the Vat is 91 kt or more but less than 121 kt, the aircraft category is (…)
Category A <91 kt
Category B 91 kt - 120 kt
Category C 121 kt - 140 kt
Category D 141 kt - 165 kt
Category E 166 kt - 210 kt
A standard instrument arrival (STAR) route permits transition from (…) to (…). It ends at the (IAF/IF/FAF/MAPt).
A standard instrument arrival (STAR) route permits transition from (the en-route phase) to (the approach phase). It ends at the (IAF).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Manouvre D shown in the figure is a (…).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Manouvre D shown in the figure is a (racetrack procedure).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
The intermediate approach segment starts at the (IAF/IF/FAF/MAPt) and ends at the (IAF/IF/FAF/MAPt).
The intermediate approach segment starts at the (IF) and ends at the (FAF or FAP).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Manouvre C shown in the figure is a (45°/180° procedure turn / 80°/260° procedure turn / base turn / racetrack procedure).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Manouvre C shown in the figure is a (base turn).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Manouvre B shown in the figure is a (45°/180° procedure turn / 80°/260° procedure turn / base turn / racetrack procedure).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Manouvre B shown in the figure is a (80°/260° procedure turn).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Manouvre A shown in the figure is a (45°/180° procedure turn / 80°/260° procedure turn / base turn / racetrack procedure).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Manouvre A shown in the figure is a (45°/180° procedure turn).
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
The initial approach segment provides at least (…) ft of obstacle clearance in the primary area, reducing laterally to zero at the outer edge of the secondary area.
The initial approach segment provides at least (1 000) ft of obstacle clearance in the primary area, reducing laterally to zero at the outer edge of the secondary area.
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
45°/180° procedure turn, starts at a facility or fix and consists of:
1) a straight leg with track guidance. This straight leg may be timed or may be limited by a radial or DME distance;
2) a 45° turn;
3) a straight leg without track guidance. This straight leg is timed. It is:
i) (…) minute(s) from the start of the turn for Category A and B aircraft; and
ii) (…) minute(s) (…) seconds from the start of the turn for Category C, D and E aircraft; and
4) a 180° turn in the opposite direction to intercept the inbound track.
45°/180° procedure turn, starts at a facility or fix and consists of:
1) a straight leg with track guidance. This straight leg may be timed or may be limited by a radial or DME distance;
2) a 45° turn;
3) a straight leg without track guidance. This straight leg is timed. It is:
i) (1) minute(s) from the start of the turn for Category A and B aircraft; and
ii) (1) minute (15) seconds from the start of the turn for Category C, D and E aircraft; and
4) a 180° turn in the opposite direction to intercept the inbound track.
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
During the intermediate approach, the obstacle clearance requirement reduces from (…) ft to (…) ft in the primary area, reducing laterally to zero at the outer edge of the secondary area.
During the intermediate approach, the obstacle clearance requirement reduces from (1000) ft to (500) ft in the primary area, reducing laterally to zero at the outer edge of the secondary area.
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Where an operational advantage can be obtained, an ILS procedure may include a dead reckoning (DR) segment from a fix to the localizer. The DR track will intersect the localizer at (…)° and will not be more than (…) NM in length.
Where an operational advantage can be obtained, an ILS procedure may include a dead reckoning (DR) segment from a fix to the localizer. The DR track will intersect the localizer at (45)° and will not be more than (10) NM in length.
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 1 in the attachment is (OCH/OCA/MDH/DH/MDA/DA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 1 in the attachment is (OCH)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 2 in the attachment is (OCH/OCA/MDH/DH/MDA/DA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 2 in the attachment is (OCA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 3 in the attachment is (OCH/OCA/MDH/DH/MDA/DA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 3 in the attachment is (MDH)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 4 in the attachment is (OCH/OCA/MDH/DH/MDA/DA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 4 in the attachment is (MDA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 4 in the attachment is (OCH/OCA/MDH/DH/MDA/DA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 4 in the attachment is (DA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 3 in the attachment is (OCH/OCA/MDH/DH/MDA/DA)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf
Height or altitude 3 in the attachment is (DH)
source: http://www.chcheli.com/sites/default/files/icao_doc_8168_vol_1.pdf