Questions FSI - Feuille updated Flashcards
The Emergency Descent mode is automatically activated anytime a cabin depressurization is detected and the aircraft altitude is greater than \_\_\_\_\_ ft A - 15 000 B - 20 000 C - 25 000 D - 30 000
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What components are responsible for the processing power of ACE avionics system? A - MAU 1 and MAU 2 B - MFD 1 and MFD 2 C - Autopilot 1 and Autopilot 2 C - DCPU 1 and DCPU 2
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.......... generate the data presented on the flight display units. A - Pilot flight dispay B - Modular avionics units C - Multifunction controllers C - Advanced graphics modules
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The ........... button on the Multiofunction controller calls up a secondary windows providing additionnal data related to the selected item. A - DETAIL B - PAGE C - CLR D - MFD
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MFS messages are cleared using the …………
A – CRV TEST/ERASE button on the left side console
B – Msg clear pushbutton on the glareshield
C – DEL button on the Multifunction controller
D - Msg Clear softkey on the right side of the INAV display
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An active and coupled navigation source will be display in........... A – Green B – Cyan C – Magenta D - White
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(Refer to figure 11) Referencing the provided Passager Moment Table, what is the moment value, (lb. in.) for a passager that weighs 220 lbs, and is seated is ROW 2? A –29,610 B –32,900 C –55,930 D -72,380
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The PC-24 measures ............... in height, which must be noted in case the aircraft is to be parked in a hangar overnight. A – 10 ft. 11 in. (3,3 m) B – 17 ft. 4 in. (5,3 m) C – 23 ft. 1 in. (7 m) D - 55 ft. 9 in. (17 m)
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Purging of the water tank assembly is completed by using the connections on the ………..
A – Ground Service Panel
B – Refuel/Defuel Panel
C – Status indication Panel on the vacuum Toilet Assembly
D - ECS Synoptic Page
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The first memory item for the Engine fire on-groud / Tail Pipe Fire non-annunciated Emergency procedure is ………..
A – THRUST LEVER……….. IDENTITY/IDDLE
B – ENG SWITCH ……. OFF
C – ENG START ……… Push to motor
D - FIRE XTING Pushbutton ….. Push to activate
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The Emergency Descent Mode (EDM) provides guidance to turn the aircraft 90° from current heading and performs VMO/MMO SPD descend to .......... A –Minimum Off-Route Altitude B – Emergency Safe Altitude C – 10 000 ft D - 15 000 ft
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The ........ button on the flight Controller allows the pilot to select which PFD navigation data is coupled with flight director A – SENSOR B – L/R C – FMS/MAN D - PFD
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The Utilities Management System (UMS) is made of in part of ………….
A – Two air graphics modules (AGMs)
B – Four data concentrator processing units (DCPUs)
C – Four pneumatics check valves
D - Two electrical power distribution units (EPDUs)
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The COM shortcut key on the multifunction controller set the cursor focus on the ............. A – Lower 1/6 window on Pilot's PFD B – INAV display C – Next waypoint in the list D - DIR field for entry of a waypoint
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The ................ provides control of Electronic Circuit Breakers (ECBs) and also provides load shedding when required? A – CAS Window B – Modular Avionics Unit (MAU) C – Utiity management System (UMS) D - Power Conversion Units (PCU)
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The predictive RAIM page can be accessed via the ………….
A – PRAIM softkey on the INAV waypoint list
B – STAR/L/dg Tab of the flight Management Window
C – PRAIM softkey on the GPS Sensors Window
D - Electrical Synoptic page
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The maximum cargo load limit is ................ A – 500 lb. (227 kg) B – 1 000 lb. (454 kg) C – 1250 lb. (567 kg) D - 2500 lb (1135 kg)
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As long as the conditions for a CAS message are valid, the .............. will continue to transmit the message as active. A – Modular Avionics Unit (MAU) B – Radio Tuning Unit C – PFD Controller D - Primary Flight Display
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Processing the AP button on the flight Controller will engage/activate the ………….
A – Autopilot only
B – Autopilot and Autothrottle
C –Yaw damper only
D - Autopilot, Pitch autotrim function and Yaw damper (if not currently active)
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When the flight crew oxygen masks are operated in the Emergency mode, the system supplies ……………
A – 100 % oxygen with positive pressure
B – A mixture of ambiant air to oxygen under pressure
C – Ambient air with positive pressure
D - Only ambient air while wearing the mask (Oxygen saver feature)
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When the Passenger Oxygen Control valve (POCV) is set to the AUTO position, the passenger oxygen masks will deploy when the cabin altitude reaches .............. +/-150 ft. A – 8000 B – 10 500 C – 12 850 D - 14 800
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When the Passager Oxygen Control Valve (POCV) is selected to the ............. position, the passager masks will drop and deliver oxygen regardless of cabin pressure. A – EMER B – ON C – OFF D - AUTO
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The Oxygen system is designated for enough gaseous oxygen to supply for ………… maximum.
A – One pilot and four passengers
B – One pilot and eight passengers (optional)
C – Two pilots and six passengers
D - Two pilots and ten passengers (optional)
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The maximum airspeed to retract the landing gear (VLo - Retract), is ....... KIAS. A – 165 B – 195 C – 200 D - 250
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Operation of the weather radar is prohibited ............ A – In icing conditions B – During an approach C – Within a hangar or other enclosure D - Anything during ground operations
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The minimum height for autopilot engagement after takeoff is ........... feet AGL. A – 200 B – 400 C – 600 D - 1000
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The auto throttle system must be disengaged prior to ............... A – Takeoff B – Landing C – Descend D - An approach
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The minimum Outside Air temperature (OAT) limit at sea level is ..........°C A – -54 B – -50 C – -44 D - +40
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The maximum operating speed limit (VMO) is ......... kts. for altitudes 28.230 feet and below. A – 290 B – 295 C – 300 D - 310
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The maximum tailwind component for takeoff and landing is .......... kts. A – 13;448 lb. (6,100 kg.) B – 16,250 lb. (7,370 kg.) C – 17, 650 lb (8,005 kg.) D - 17,750 lb (8,050 kg.)
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The maimum crosswind component for engine start is ........... knots (estimated steady wind conditions). A – 10 B – 15 C – 20 D - 25
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An engine start must be aborted when N1 fails to increase by ..........% N2. A – 15 B – 25 C – 29 D - 45
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The term ............. means to land without delay at the nearest airport where a safe approach and landing is reasonably assured. A – Land as soon as possible B – Circle-to-land C – Land as soon as practical D - Land when able
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The first memory item for fire, Smoke or Fumes in Cockpit/Cabin is, ………………
A – Oxygen Mask…… DON/100%/Check EMERG
B – Smoke goggles ……….. DON
C – CPCS ………….. DUMP
D - PASSENGER OXYGEN …….ON. Instruct passengers to don down masks
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The first memory item for an Emergency Descent is, ……………..
A – Crew Oxygen Marks ………… DON / 100 % / Establish COMM
B – AIRBRAKE lever ………………..OUT
C – SEAT BELTS ……………………..ON
D - THRUST Levers ………………..IDLE
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The memory for the All Brakes Fail Warning CAS message is, ……………
A – Differential braking …………….. Use to stop aircraft
B – Wheel brakes / EMER brake…………… Use if available to stop aircraft
C – Aircraft, ……………………………………. Use NWS to avoid obstacles
D - L+R ENG switches ………….OFF
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The memory item for an Emergency Evacuation is, ………………
A – ATC/distress message ………. Notify
B – ENG L+R switches ……………… Both OFF
C – CPCS DUMP pushbutton …………… Press DUMP
D - Park Brake ……………Set
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The first memory item for a Rejected takeoff is, ……………….
A – THRUST levers ……………. IDLE
B – BRAKES ………………… Max Braking / As Required
C – ATC …………………….. INFORM
D - THRUST levers …………………ATR
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In the event that an Essential Bus circuit breaker trips in flight, only ............ attempt (s) is/are permitted to reset the circuit breaker if the pilot in command dertermines that the system or equipment is needed for safe completion of the flight. A – One B – Two C – Three D - Four
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The selected Navigation Source is displayed in the ................... A – Upper right of the HSI B – Upper right of the INAV C – System Summary synoptic D - Top left portion of the PFD
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A stored FPI.N can be selected and inserted via the ………………… on the Flight Management Window.
A – Arrival Phase of Flight - Tcomp Tab
B – Departure Phase of Flight - Runway/SID button
C – INIT Phase of Flight - Data Bases Tab
D - Preflight Phase of Flight - Flight Plan Tab
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If FMSI has been seclected as the navigation source on the both PFDs, the FMSI source annunciator on the top right of the HSI will return ............ in color. A – White B – Red C – Amber D - Magenta
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An amber “MSG” annunciation will appear on the PFD when ………………
A – Caution CAS messages appear in the CAS Window
B – Warning CAS messages appear in the CAS Window
C – FMS messages are displayed on the INAV
D - FMS messages are displayed on the PFD Radio Window
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Factored Landing Distance for a Dry runway is ............x the Actual Landing Distance. A – 1,15 B – 1,33 C – 1,67 D - 1,92
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V-Speeds for the approach and landing phases of flight are entered into the ACE system via the ……………
A – STAR/L.dg tab of the Flight Management Window (FMW)
B – SID /Takeoff Tab of the flight Management Window (FMW)
C – ECS synoptic page
D - Manual Speed knob on the Flight Controller
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