Which mode has the spoiler actuator if the hydraulic pressure is lost? 27-009
a. There is damping mode. The spoiler panel can be moved to retract and to extend positions by the aerodynamic forces.
b. There is locked mode. The spoiler panel can only be moved towards the retracted position, pushed by the aerodynamic forces.
c. There is biased mode. The spoiler panel retracts electrically.
What will happen with the Trimmable Horizontal Stabilizer (THS) control in case of total loss of the green and yellow hydraulic pressure? 27-062
a. The THS will have an ability to be controlled by the Pitch Trim Actuator electric motors.
b. The THS will have an ability to be controlled by the manual control.
c. The THS will be kept in the last specified position without any ability to be controlled.
20. The available modes of the aileron servo actuator are:
a. Active and centering modes.
b. Active and damping modes.
c. Active, damping and centering modes.
ATA 27A. FLIGHT CONTROLS System Operation:
Electrical/Fly-by-Wire (LVL 3)
If both ELACs fail, what controls the elevator and stabilizer? 27A-012
a. SEC 1 or 2 depending of the status
b. Elevator and stabilizer revert to mechanical backup
c. Backup mode of ELAC's
In the event of electrical control loss of one servo controls of elevator surface: 27A-007
a. The elevator surface stays and is held in the last position
b. The elevator surface is brought back in the 0 zero position
c. The elevator surface is still controlled by adjacent servo control.
ATA 29. HYDRAULIC POWER SYSTEMS (LVL 3)
The hydraulic hand pump used for the cargo door operation is installed on the... 29-027
a. Green system service panel.
b. Yellow system service panel.
c. Blue system service panel.
Where is the ground service panel for the Green system located? 29-002
a. Aft of the main landing gear bay on the LH side
b. Aft of the main landing gear bay on the RH side
c. Fwd of the main landing gear bay on the RH side
Which of the following requirements must be performed to refill the Yellow hydraulic system reservoir? 29-026
a. The Reservoir Filling Selector on the Green service panel is turned to YELLOW position and hand pump on the Yellow service panel is operated.
b. The Reservoir Filling Selector on the Green service panel is turned to YELLOW position and hand pump on the Green service panel is operated.
c. The Reservoir Filling Selector in the Yellow hydraulic system bay is turned to YELLOW position and hand pump on the Yellow service panel is operated.
|
|
|
When the blue electric pump will run, if one engine is running? 29-003
a.In case of the ELECtric (ELEC) PUMP P/B set to AUTO.
b.In case of the ELECtric (ELEC) PUMP P/B set to OFF.
c.In case BLUE PUMP OverRiDe (OVRD) P/B is set to ON
Which hydraulic systems have engine driven pumps? 29-016
a. Green and yellow.
b. Blue and yellow.
c. Green and blue.
When is the PTU operation inhibited?
a. When the aircraft is on the ground.
b. When the cargo door is electro-hydraulically operated only.
c. On the ground when the cargo doors are operated or at one engine start.
Which hydraulic system is not powered from engine
a) Yellow and Blue
b) Blue
c) Yellow
ATA 29A. HYDRAULIC POWER SYSTEMS MONITORING and INDICATING (LVL 3)
30.Each of three hydraulic systems has a pressure transducer which gives data… 29A-008
a. on the ECAM for pressure indication and sends information to
ELevator Aileron Computers (ELACs) 1 and 2.
b. on the related pressure gage located in the Main Landing Gear wheel well.
c. on the Flight Management and Guidance Computer (FMGC) 1 and 2 for good flight control.
31.The hydraulic temperature transmitters monitor the hydraulic fluid temperature in the … 29A-003
a. related hydraulic system pressure line.
b. related hydraulic system return line.
c. related hydraulic system case drain line.
ATA 51. Airframe structure (LVL 3)
Which of the fuselage skin panels are made of titanium alloys? 51-010
a. The skin panels which installed just above and below the emergency escape hatches.
b. The skin panels which installed just above the cargo compartments doors.
c. The skin panels which installed just above the cockpit windshields
ATA 52. Doors (LVL 3)
The When the Emergency Control Handle is in the ARMED position, what part of the emergency escape slide release mechanism does fasten the slide? 52-003
|
|
|
a) The girt bar fittings
b) The cam disk
c) The girt bar
Дата добавления: 2019-02-22; просмотров: 144; Мы поможем в написании вашей работы! |
Мы поможем в написании ваших работ!