更多"[单选题]MODE SEL pushbutton sw of fuel"的相关试题:
[单选题]Amber FAULT light on MODE SEL pushbutton of fuel mode will turn on when：
A. Fuel feed pressure descends
B. CTR is above 250kg, any wing tank is below 5000kg
C. Two CTR Pumps selects OFF position
[单选题]On fuel control panel of cockpit, MODE SEL pushbutton controls
A. CTR transfer valve and Wing pump
B. CTR transfer valve
C. Wing pump
[单选题]When ground fuel transfers, the mode of fuel control panel selects ：
A. manual
B. automatic
C. transfer is not related to mode selection
[单选题]How many main fuel pumps exist in fuel system?
A.6
B.8
C.12
[单选题]After landing, will pressurization system automatically transfer?
A. No, another system must be chosen
B. Yes, it will immediately transfer at touchdown
C. Yes, after touching ground 70 seconds
[单选题]Which part of outer procedure signal does Automatic Pressurization System receive？
A. FMGS
B.ECAM
C.FAC
[单选题]TRIP FUEL is：
A. The weight of the fuel necessary to cover the normal leg without reserves.
B. Enroute fuel consumption + enroute reserve fuel
C. Enroute fuel consumption + enroute reserve fuel + 45 min holdingfuel
[单选题]( ) feed APU fuel
A. CTR Pump, not engine pump
B. APU pump
C. All of above
[单选题]Model Sel功能的作用是 （ ）
A.反向通道
B.失控保护
C.模型切换
[单选题]Engine LP fuel valve closes when
A. the pressure of fuel pressurization pump descends
B. engine shut-down or engine fire alarm pushbutton out
C. engine fire alarm detection system detects ENG FIRE PUSH
[单选题]During fast alignment, MODE sel should be change from OFF to NAV in ____.
A. A. 3s
B. B. 5s
C. C. 7s
[单选题]Transponder Mode sel at AUTO, how does it operate?
A. A. In flight, selected transponder operates.
B. B. Selected transponder only operates in mode S (Selective aircraft interrogation mode).
C. C. Both correct
[单选题]Fuel quantity detection value would be different in different aircraft pitch attitude, it might cause overweight landing. According to Chief Pilot Advisory, to prevent overweight landing, current aircraft weight should be less than MLW - （）KG when captured LOC.
A.200
B.150
C.100
[单选题] Fuel quantity detection value would be different in different aircraft pitch attitude, it might cause overweight landing. According to Chief Pilot Advisory, to prevent overweight landing, current aircraft weight should be less than MLW - （）KG when captured LOC.
A.200
B.150
C.100
[单选题]When ATT HDG and AIR DATA sel at NORM, which is correct?
A. A. ADIRU 1 supplies data to PFD 1, ND 1; ADIRU 2 supplies data to PFD 2, and ND2
B. B. ADIRU 1 supplies data to PFD 1, ND 1, RMI and VOR/DME; ADIRU 2 supplies data to PFD 2, and ND2
C. C. ADIRU 1 supplies data to PFD 1; ADIRU 2 supplies data to PFD 2
[单选题]ZERO FUEL WEIGHT（ZFW）is：
A. The weight obtained by addition of the total traffic load and the dry operating weight.
B. The weight obtained by addition of the total traffic load and the operational empty weight.
C. The weight obtained by addition of the total traffic load and the manufacturer’s empty weight.
[单选题]The calculated fuel consumption for the APU installed on the A320 is
A. 130KG/H or 290LB/H
B. 11.5 KG/MIN or 25LB/MIN
C. 20KG/MIN or 45LB/MIN
[单选题]All fuel pumps are fitted with pressure relief sequence valve to ensure
A. the center tank pumps will deliver fuel preferentially
B. inner tank pump will deliver fuel preferentially
C. the center tank pumps and inner tank pump deliver fuel at the same time
[单选题]Which of the following fuel supply sequence is correct?
A. Firstly, the central fuel tank (the system automatically selects the CTR TK PUMP off when the inner tank is full. The wing tank pumps will feed until the engine have used approximately 500kg (1 100 lb) of fuel when the fuel level reaches the underfull sensors. The logic circuits then restart the center tank pumps, and then inner fuel tank (each inner tank empties down to 750 kg), and the last one is outer tank.
B. Firstly, the inner tank (each inner tank empties to 750 kg), then center tank, and the last one is outer tank.
C. Firstly, central tank and inner tank feed at the same time, when inner fuel tank empties to 750kg, and then use the outer tank.
