GO_2

Question 1

A22-058 Regarding the AFS CONTROL PANEL the letter B applies to:

Accepted Answer

b. Lateral Controls

Answer

a. AP, FD, L/FD, and A/THR Controls

Answer

c. Vertical Controls

Answer

d. Speed/Mach Controls

Question 2

A31-022 SIDESLIP INDEX. According to the information displayed in the following image, what of the following is FALSE?

Accepted Answer

a. The ADRs provide the sideslip and the lateral acceleration

Answer

b. Indicates the sideslip in the case of one engine out (displayed below the FPV)

Answer

c. Appears when one engine fails during takeoff, or go-around

Answer

d. The PRIMs provide the beta target information.

Question 3

A27-004 The maneuver load alleviation function reduces the wing bending moments during high load factor maneuvers. It is achieved by deflecting the ailerons upward that modifies the wing spanwise load distribution.

Accepted Answer

Verdadero

Answer

Falso

Question 4

A26-012 Select the correct sentence about the number of bottles:

Accepted Answer

d. All of the above.

Answer

a. The APU has only one bottle and one discharge valve.

Answer

b Each engine has one bottle and two discharge valves.

Answer

c The Lavatories has only one autonomous fire extinguish bottle

Question 5

A34-045 When any navaid is manually tuned:

Accepted Answer

a.a "M" letter near the navaid ident

Answer

b. a "M" letter near the navaid ident and a "MANUAL NAVAID" on MEMOS

Answer

c. a "MANUAL NAVAID" near the navaid ident and a "M" letter on MEMOS

Answer

d. a "MANUAL NAVAID" on MEMOS

Question 6

A27-025 The flap load relief function limits the loads on the flaps if:

Accepted Answer

c. VFE is exceeded.

Answer

a. Vmo is exceeded

Answer

b. VFR is exceeded

Answer

d. Vmax is exceeded

Question 7

A56-004 What is the name of the system in charge of monitoring and controlling all fuselage doors, emergency exits, and peripherals of the aircraft.

Accepted Answer

d. The Doors Control and Monitoring System (DCMS)

Answer

a. The Door Control and Monitoring Unit (DCMU)

Answer

b. The Autonomous Standby Power Supply Unit (ASPSU)

Answer

c. The Ramp and Cargo Door Controller (RCDC)

Question 8

A22-027 The Flight Envelope (FE) computations take into account:

Accepted Answer

d. All of the above

Answer

a. Aircraft performance selection (Normal Operating Standard (NOS), Reduced Operating Standard (ROS) and Military Operating Standard (MOS)

Answer

b. Flight phases

Answer

c. Aircraft parameters (speed, bank angle, angle-of-attack, etc.)

Question 9

A28-008 About the fuel distribution, choose the RIGHT answer:

Accepted Answer

a. If tactical fuel distribution sequence is selected, the FQMS fills first each tank below full capacity in order to minimize the consequences of bullets impact. The airspace of each tank protects the tanks against hydrodynamic ram. Then the TKs can be filled to the maximum capacity if necessary.

Answer

b. If the logistic fuel distribution sequence is selected, the FEED TKs are filled below full capacity in order to maximize aircraft structural efficiency

Answer

c. In automatic refuel mode, depending on the mission, the crew can choose between three fuel distribution sequences LOGISTIC, TACTICAL or TANKER.

Answer

a. If no fuel distribution sequence is selected, the FAMS assumes it is a tactical distribution.

Question 10

A25-007 The medical equipment is used for first aid or in case of emergency medical situations. It includes two first aid kits and an emergency medical kit. Where are they located?

Accepted Answer

a. Under the cockpit stairs and in the wardrobe of the cockpit.

Answer

b. In the Load-master Workstation.

Answer

c. Beside the crew door.

Answer

d. In the ramp.

Question 11

Which statement about the breakaway position of the HUD is correct:

Accepted Answer

c. All are correct

Answer

a. the flight crew can use the associated HUD provided that the flight crew stows then redeploys the combiner in the locked position

Answer

b. the PFD is automatically displayed on the associated cockpit side

Answer

d. The breakaway position avoids a possible injury of the flight crew's head in case of crash

Question 12

A80-026 The N2 indicates:

Accepted Answer

c. The lP shaft rotation speed

Answer

a. The N2 value is not displayed

Answer

b. The exhaust gas temperatura

Answer

d. The vibration of the Engine

Question 13

A27-012 Choose the wrong answer:

Accepted Answer

c. Only PRIMS 1 and 2 can be master PRIMS

Answer

a. lf the master PRIM degrades, another PRIM will replace it and becomes the master computer.

Answer

b. All 3 PRIMS are identical

Answer

d. One computer (either PRIM or SEC) is sufficient to fly the aircraft.

Question 14

A35-004 About the protective crew oxygen bottles, choose the most correct answer:

Accepted Answer

c.The pressure value is continuously indicated in the DOOR/CARGO/OXYGEN SD.

Answer

a. From one to four high pressure oxygen bottles can be installed in the right side of the aircraft.

Answer

b. The pressure value can be checked through a window from outside of the aircraft fuselage.

Answer

d. From two to four high pressure oxygen bottles can be installed in the left side of the aircraft.

Question 15

A32-023 The main controls of the kneeling system are in the cargo hold area on the: (Choose the wrong answer)

Accepted Answer

c. Ditching Hatch

Answer

a. LMCP

Answer

b. LMWS and LMCP

Answer

d. LMWS

Question 16

A22-007 The Automatic flight system (AFS) is designed to :

Accepted Answer

d. All of the above.

Answer

a. Assist the pilot in flying the aircraft within the normal flight envelope.

Answer

b. Enhance safety.

Answer

c. Help the flight crew in the management of an optimized flight profile.

Question 17

A31-023 SIDESLIP INDEX. According to the information displayed in the following image, what of the following is FALSE?

Accepted Answer

b. None is correct.

Answer

a. On ground, indicates the lateral acceleration of the aircraft

Answer

c. In flight, indicates the sideslip of the aircraft. If the sideslip is not available, indicates the lateral acceleration of the aircraft.

Answer

d. The ADRs provide the sideslip and the lateral acceleration.

Question 18

A42-015 The avionic network is fully duplicated to ensure redundancy. The two networks are independent.

Answer

true

Question 19

A22-050 For a Missed Approach the SRS mode engages like at takeoff, and follows a target speed equal to:

Accepted Answer

d. All of the above.

Answer

a. The current aircraft speed.

Answer

b. VAPP as a minimum.

Answer

c. maximum ofVLS +25 kt if all engines are operative.

Question 20

A49-006 Choose the correct answer. The APU is designed for use:

Accepted Answer

a. On ground or in flight throughout the whole aircraft operating envelope.

Answer

b. On ground or in flight until 25000ft.

Answer

c. On ground only.

Answer

d. In flight only.

Question 21

A33-010 Regarding the Beacon/Rendezvous Lights, select the FALSE:

Accepted Answer

d. The beacon/rendezvous lights flash in white. When both beacon/rendezvous and strobe/anti-collision lights are turned on, they alternately flash.

Answer

a. The beacon/rendezvous lights flash in red. When both beacon/rendezvous and strobe/anti-collision lights are turned on, they alternately flash.

Answer

b. Each beacon/rendezvous light has normal and covert lights.

Answer

c. The beacon/rendezvous lights enable the receiver aircraft to visually identify the tanker aircraft.

Question 22

A34-012 The multifunction probes measure:

Accepted Answer

a. AOA, TAT and total pressure.

Answer

b. AOA, TAT, total pressure and side slip angle.

Answer

c. AOA, TAT, and static pressure.

Answer

d. AOA, TAT and side slip angle.

Question 23

A31-032 According to the information displayed in the following image, what of the following is TRUE:

Accepted Answer

a. The size of the STATUS page exceeds the display capability.

Answer

b. Indicates if there are DEFERRED PROCs and the associated applicable flight phases.

Answer

c. Indicates ifany LIMITATIONS apply.

Answer

d. The flight crew displays the next STATUS page via the MORE pb on the ECP.

Question 24

A80-017 The LFI:

Accepted Answer

a. Reduces the pitch of the propeller to use it as an airbrake. That's why it could be used to perform a steep descent.

Answer

b. Itis automatically activated when an engine fails.

Answer

c. Means Low Fuel Injection.

Answer

d. It is used to reduce noise during cruise.

Question 25

A22-059 Regarding the AFS CONTROL PANEL the letter C applies to:

Accepted Answer

d. Vertical Controls.

Answer

a. Lateral Controls

Answer

b. Speed/Mach Controls

Answer

c. AP,FD,L/FD, and A/THR Controls

Question 26

A28-014 About the fuel system, choose the WRONG answer:

Accepted Answer

d. The crossfeed valves enable the isolation of each engine from the feed network.

Answer

a. The crossfeed valves enable any MAIN or STBY pump to feed any engine/or APU.

Answer

b. Each engine has a Low Pressure (LP) valve to isolate its corresponding engine from the feed network.

Answer

c. The crossfeed valves enable to balance fuel between wings.

Question 27

A30-004 Mark the correct one about the ICE DETECTORS:

Accepted Answer

c. There are two of them, on each side of the fuselage.

Answer

a. There are four of them, on each engine.

Answer

b. There are two of them, in ENG 2 and ENG 3.

Answer

d. There are four of them, on the fuselage and the wing leading edges.

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