A22-058 Regarding the AFS CONTROL PANEL the letter B applies to:
a. AP, FD, L/FD, and A/THR Controls
b. Lateral Controls
c. Vertical Controls
d. Speed/Mach Controls
A31-022 SIDESLIP INDEX. According to the information displayed in the following image, what of the following is FALSE?
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.
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.
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A26-012 Select the correct sentence about the number of bottles:
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.
A34-045 When any navaid is manually tuned:
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
A27-025 The flap load relief function limits the loads on the flaps if:
a. Vmo is exceeded
b. VFR is exceeded
c. VFE is exceeded.
d. Vmax is exceeded
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.
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)
A22-027 The Flight Envelope (FE) computations take into account:
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
A28-008 About the fuel distribution, choose the RIGHT 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.
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.
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?
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.
Which statement about the breakaway position of the HUD is correct:
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
A80-026 The N2 indicates:
a. The N2 value is not displayed
b. The exhaust gas temperatura
c. The lP shaft rotation speed
d. The vibration of the Engine
A27-012 Choose the wrong answer:
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.
A35-004 About the protective crew oxygen bottles, choose the most correct answer:
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.
A32-023 The main controls of the kneeling system are in the cargo hold area on the: (Choose the wrong answer)
a. LMCP
b. LMWS and LMCP
c. Ditching Hatch
d. LMWS
A22-007 The Automatic flight system (AFS) is designed to :
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.
A31-023 SIDESLIP INDEX. According to the information displayed in the following image, what of the following is FALSE?
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.
A42-015 The avionic network is fully duplicated to ensure redundancy. The two networks are independent.
A22-050 For a Missed Approach the SRS mode engages like at takeoff, and follows a target speed equal to:
a. The current aircraft speed.
b. VAPP as a minimum.
c. maximum ofVLS +25 kt if all engines are operative.
A49-006 Choose the correct answer. The APU is designed for use:
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.
A33-010 Regarding the Beacon/Rendezvous Lights, select the FALSE:
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.
A34-012 The multifunction probes measure:
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.
A31-032 According to the information displayed in the following image, what of the following is TRUE:
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.
A80-017 The LFI:
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.
A22-059 Regarding the AFS CONTROL PANEL the letter C applies to:
a. Lateral Controls
b. Speed/Mach Controls
c. AP,FD,L/FD, and A/THR Controls
d. Vertical Controls.
A28-014 About the fuel system, choose the WRONG answer:
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.
A30-004 Mark the correct one about the ICE DETECTORS:
a. There are four of them, on each engine.
b. There are two of them, in ENG 2 and ENG 3.
c. There are two of them, on each side of the fuselage.
d. There are four of them, on the fuselage and the wing leading edges.
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