問題一覧
1
A. BAT 1 and 2 pushbuttons must be selected to ON
2
C. With a delay if the bleed air was in use
3
B. Energize the starter, the ignition turns ON. When N = 60% the starter is de-energized and the ignition turns OFF
4
True
5
A. Electric power goes to the APU system, the ECB performs a power-up test, air intake flap opens, the fuel isolation valve opens, if no fuel tank pump is running the fuel pump operates
6
B. If a fuel spill occurs, perform a normal APU shutdown
7
C. a single-shaft gas turbine
8
A. N = 95%
9
True
10
A. If the ENG 1 FIRE pb-sw is pushed
11
False
12
B. Fire on ground only
13
B. 20 000 ft
14
A. Within aircraft operational envelop
15
A. Within aircraft operational envelop
16
A. After three consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt
17
B. Electric power goes to the APU system; the ECB performs a power-up test
A-320 Chapter № 21. Engines
A-320 Chapter № 21. Engines
Popovich · 37問 · 1ヶ月前A-320 Chapter № 21. Engines
A-320 Chapter № 21. Engines
37問 • 1ヶ月前A-320 Chapter № 19. APU
A-320 Chapter № 19. APU
Popovich · 17問 · 1ヶ月前A-320 Chapter № 19. APU
A-320 Chapter № 19. APU
17問 • 1ヶ月前A-320 Chapter № 14. Lights
A-320 Chapter № 14. Lights
Popovich · 11問 · 1ヶ月前A-320 Chapter № 14. Lights
A-320 Chapter № 14. Lights
11問 • 1ヶ月前A-320 Chapter № 13. Landing gear
A-320 Chapter № 13. Landing gear
Popovich · 37問 · 1ヶ月前A-320 Chapter № 13. Landing gear
A-320 Chapter № 13. Landing gear
37問 • 1ヶ月前A-320 Chapter № 12. Indicating / Recording
A-320 Chapter № 12. Indicating / Recording
Popovich · 38問 · 1ヶ月前A-320 Chapter № 12. Indicating / Recording
A-320 Chapter № 12. Indicating / Recording
38問 • 1ヶ月前A-320 Chapter № 10. Hydraulic
A-320 Chapter № 10. Hydraulic
Popovich · 17問 · 1ヶ月前A-320 Chapter № 10. Hydraulic
A-320 Chapter № 10. Hydraulic
17問 • 1ヶ月前A-320 Chapter № 8. Flight Controls
A-320 Chapter № 8. Flight Controls
Popovich · 42問 · 1ヶ月前A-320 Chapter № 8. Flight Controls
A-320 Chapter № 8. Flight Controls
42問 • 1ヶ月前A-320 Chapter № 3. Autoflight
A-320 Chapter № 3. Autoflight
Popovich · 40問 · 1ヶ月前A-320 Chapter № 3. Autoflight
A-320 Chapter № 3. Autoflight
40問 • 1ヶ月前A-320 Chapter № 21. Engines
A-320 Chapter № 21. Engines
Popovich · 37問 · 11ヶ月前A-320 Chapter № 21. Engines
A-320 Chapter № 21. Engines
37問 • 11ヶ月前A-320 Chapter № 15. Navigation and Surveillance
A-320 Chapter № 15. Navigation and Surveillance
Popovich · 30問 · 11ヶ月前A-320 Chapter № 15. Navigation and Surveillance
A-320 Chapter № 15. Navigation and Surveillance
30問 • 11ヶ月前A-320 Chapter № 8. Flight Controls
A-320 Chapter № 8. Flight Controls
Popovich · 42問 · 11ヶ月前A-320 Chapter № 8. Flight Controls
A-320 Chapter № 8. Flight Controls
42問 • 11ヶ月前A-320 Chapter № 3. Autoflight
A-320 Chapter № 3. Autoflight
Popovich · 40問 · 11ヶ月前A-320 Chapter № 3. Autoflight
A-320 Chapter № 3. Autoflight
40問 • 11ヶ月前д31
д31
ユーザ名非公開 · 50問 · 1年前д31
д31
50問 • 1年前Літерні позначення в електричних схемах
Літерні позначення в електричних схемах
ユーザ名非公開 · 50問 · 1年前Літерні позначення в електричних схемах
Літерні позначення в електричних схемах
50問 • 1年前Оператор ППД
Оператор ППД
ユーザ名非公開 · 70問 · 1年前Оператор ППД
Оператор ППД
70問 • 1年前СЭД
СЭД
Aisulu2006 Dulat · 69問 · 1年前СЭД
СЭД
69問 • 1年前Характеристики/роуминг
Характеристики/роуминг
Анастасия Финогентова · 33問 · 2年前Характеристики/роуминг
Характеристики/роуминг
33問 • 2年前問題一覧
1
A. BAT 1 and 2 pushbuttons must be selected to ON
2
C. With a delay if the bleed air was in use
3
B. Energize the starter, the ignition turns ON. When N = 60% the starter is de-energized and the ignition turns OFF
4
True
5
A. Electric power goes to the APU system, the ECB performs a power-up test, air intake flap opens, the fuel isolation valve opens, if no fuel tank pump is running the fuel pump operates
6
B. If a fuel spill occurs, perform a normal APU shutdown
7
C. a single-shaft gas turbine
8
A. N = 95%
9
True
10
A. If the ENG 1 FIRE pb-sw is pushed
11
False
12
B. Fire on ground only
13
B. 20 000 ft
14
A. Within aircraft operational envelop
15
A. Within aircraft operational envelop
16
A. After three consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt
17
B. Electric power goes to the APU system; the ECB performs a power-up test