GO_2

Question 1 of 27

1

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

Select one of the following:

a. AP, FD, L/FD, and A/THR Controls
b. Lateral Controls
c. Vertical Controls
d. Speed/Mach Controls

Explanation

Question 2 of 27

1

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

Select one of the following:

a. The ADRs provide the sideslip and the lateral acceleration
b. Indicates the sideslip in the case of one engine out (displayed below the FPV)
c. Appears when one engine fails during takeoff, or go-around
d. The PRIMs provide the beta target information.

Explanation

Question 3 of 27

1

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.

Select one of the following:

Verdadero
Falso

Explanation

Question 4 of 27

1

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

Select one of the following:

a. The APU has only one bottle and one discharge valve.
b Each engine has one bottle and two discharge valves.
c The Lavatories has only one autonomous fire extinguish bottle
d. All of the above.

Explanation

Question 5 of 27

1

A34-045 When any navaid is manually tuned:

Select one of the following:

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

Explanation

Question 6 of 27

1

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

Select one of the following:

a. Vmo is exceeded
b. VFR is exceeded
c. VFE is exceeded.
d. Vmax is exceeded

Explanation

Question 7 of 27

1

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.

Select one of the following:

a. The Door Control and Monitoring Unit (DCMU)
b. The Autonomous Standby Power Supply Unit (ASPSU)
c. The Ramp and Cargo Door Controller (RCDC)
d. The Doors Control and Monitoring System (DCMS)

Explanation

Question 8 of 27

1

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

Select one of the following:

a. Aircraft performance selection (Normal Operating Standard (NOS), Reduced Operating Standard (ROS) and Military Operating Standard (MOS)
b. Flight phases
c. Aircraft parameters (speed, bank angle, angle-of-attack, etc.)
d. All of the above

Explanation

Question 9 of 27

1

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

Select one of the following:

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.
b. If the logistic fuel distribution sequence is selected, the FEED TKs are filled below full capacity in order to maximize aircraft structural efficiency
c. In automatic refuel mode, depending on the mission, the crew can choose between three fuel distribution sequences LOGISTIC, TACTICAL or TANKER.
a. If no fuel distribution sequence is selected, the FAMS assumes it is a tactical distribution.

Explanation

Question 10 of 27

1

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?

Select one of the following:

a. Under the cockpit stairs and in the wardrobe of the cockpit.
b. In the Load-master Workstation.
c. Beside the crew door.
d. In the ramp.

Explanation

Question 11 of 27

1

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

Select one of the following:

a. the flight crew can use the associated HUD provided that the flight crew stows then redeploys the combiner in the locked position
b. the PFD is automatically displayed on the associated cockpit side
c. All are correct
d. The breakaway position avoids a possible injury of the flight crew's head in case of crash

Explanation

Question 12 of 27

1

A80-026 The N2 indicates:

Select one of the following:

a. The N2 value is not displayed
b. The exhaust gas temperatura
c. The lP shaft rotation speed
d. The vibration of the Engine

Explanation

Question 13 of 27

1

A27-012 Choose the wrong answer:

Select one of the following:

a. lf the master PRIM degrades, another PRIM will replace it and becomes the master computer.
b. All 3 PRIMS are identical
c. Only PRIMS 1 and 2 can be master PRIMS
d. One computer (either PRIM or SEC) is sufficient to fly the aircraft.

Explanation

Question 14 of 27

1

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

Select one of the following:

a. From one to four high pressure oxygen bottles can be installed in the right side of the aircraft.
b. The pressure value can be checked through a window from outside of the aircraft fuselage.
c.The pressure value is continuously indicated in the DOOR/CARGO/OXYGEN SD.
d. From two to four high pressure oxygen bottles can be installed in the left side of the aircraft.

Explanation

Question 15 of 27

1

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

Select one of the following:

a. LMCP
b. LMWS and LMCP
c. Ditching Hatch
d. LMWS

Explanation

Question 16 of 27

1

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

Select one of the following:

a. Assist the pilot in flying the aircraft within the normal flight envelope.
b. Enhance safety.
c. Help the flight crew in the management of an optimized flight profile.
d. All of the above.

Explanation

Question 17 of 27

1

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

Select one of the following:

a. On ground, indicates the lateral acceleration of the aircraft
b. None is correct.
c. In flight, indicates the sideslip of the aircraft. If the sideslip is not available, indicates the lateral acceleration of the aircraft.
d. The ADRs provide the sideslip and the lateral acceleration.

Explanation

Question 18 of 27

1

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

Select one of the following:

True
False

Explanation

Question 19 of 27

1

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

Select one of the following:

a. The current aircraft speed.
b. VAPP as a minimum.
c. maximum ofVLS +25 kt if all engines are operative.
d. All of the above.

Explanation

Question 20 of 27

1

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

Select one of the following:

a. On ground or in flight throughout the whole aircraft operating envelope.
b. On ground or in flight until 25000ft.
c. On ground only.
d. In flight only.

Explanation

Question 21 of 27

1

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

Select one of the following:

a. The beacon/rendezvous lights flash in red. When both beacon/rendezvous and strobe/anti-collision lights are turned on, they alternately flash.
b. Each beacon/rendezvous light has normal and covert lights.
c. The beacon/rendezvous lights enable the receiver aircraft to visually identify the tanker aircraft.
d. The beacon/rendezvous lights flash in white. When both beacon/rendezvous and strobe/anti-collision lights are turned on, they alternately flash.

Explanation

Question 22 of 27

1

A34-012 The multifunction probes measure:

Select one of the following:

a. AOA, TAT and total pressure.
b. AOA, TAT, total pressure and side slip angle.
c. AOA, TAT, and static pressure.
d. AOA, TAT and side slip angle.

Explanation

Question 23 of 27

1

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

Select one of the following:

a. The size of the STATUS page exceeds the display capability.
b. Indicates if there are DEFERRED PROCs and the associated applicable flight phases.
c. Indicates ifany LIMITATIONS apply.
d. The flight crew displays the next STATUS page via the MORE pb on the ECP.

Explanation

Question 24 of 27

1

A80-017 The LFI:

Select one of the following:

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.
b. Itis automatically activated when an engine fails.
c. Means Low Fuel Injection.
d. It is used to reduce noise during cruise.

Explanation

Question 25 of 27

1

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

Select one of the following:

a. Lateral Controls
b. Speed/Mach Controls
c. AP,FD,L/FD, and A/THR Controls
d. Vertical Controls.

Explanation

Question 26 of 27

1

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

Select one of the following:

a. The crossfeed valves enable any MAIN or STBY pump to feed any engine/or APU.
b. Each engine has a Low Pressure (LP) valve to isolate its corresponding engine from the feed network.
c. The crossfeed valves enable to balance fuel between wings.
d. The crossfeed valves enable the isolation of each engine from the feed network.

	Created by Jose Antonio Vazquez over 2 years ago

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Question 1 of 27

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

Select one of the following:

Explanation

Question 2 of 27

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

Select one of the following:

Explanation

Question 3 of 27

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.

Select one of the following:

Explanation

Question 4 of 27

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

Select one of the following:

Explanation

Question 5 of 27

A34-045 When any navaid is manually tuned:

Select one of the following:

Explanation

Question 6 of 27

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

Select one of the following:

Explanation

Question 7 of 27

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.

Select one of the following:

Explanation

Question 8 of 27

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

Select one of the following:

Explanation

Question 9 of 27

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

Select one of the following:

Explanation

Question 10 of 27

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?

Select one of the following:

Explanation

Question 11 of 27

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

Select one of the following:

Explanation

Question 12 of 27

A80-026 The N2 indicates:

Select one of the following:

Explanation

Question 13 of 27

A27-012 Choose the wrong answer:

Select one of the following:

Explanation

Question 14 of 27

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

Select one of the following:

Explanation

Question 15 of 27

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

Select one of the following:

Explanation

Question 16 of 27

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

Select one of the following:

Explanation

Question 17 of 27

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

Select one of the following:

Explanation

Question 18 of 27

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

Select one of the following:

Explanation

Question 19 of 27

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

Select one of the following:

Explanation

Question 20 of 27

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