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NETJETS CITATION LATITUDE STUDY 1 > Latitude Jeopardy > Flashcards

Latitude Jeopardy Flashcards

(99 cards)

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1
Q

The cabin entry lights are powered from the:

A

Right Battery Bus

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2
Q

What is the single-point refueling pressure limits?

A

10 to 55 psi

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3
Q

What is the maximum elevation limit for T/O?

A

14,000

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4
Q

At what altitude must WING ANTI-ICE buttons be selected off?

A

Above FL410

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5
Q

Which external doors are monitored via CAS message:

A 
Nose Compartment Doors L - R
Cabin Entry
Baggage Door
Emergency Exit
Tailcone Access Door
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6
Q

Bus tie functions are _____ on the ground and _____ in flight.

A

Automatic on the ground

Manual in flight

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7
Q

The 680AS tail height rounded up to the nearest foot?

A

21’

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8
Q

An amber FUEL CROSSFEED CAS message indicates crossfeed is selected and a ___ pound imbalance has developed in the _____ direction.

A

60 Pound

Wrong Direction

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9
Q

The Max APU generator amperage is:

A

275 Amps

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10
Q

With the EMER LTS armed, the cabin emergency lights will illuminate automatically when:

A

Loss of Main DC Power
5g Impact Switch
Pax Safety Selected ON

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11
Q

The APU hours and cycles are displayed on the:

A

MFD > Aircraft Systems > Propulsion page with the

APU switch in the ON position.

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12
Q

Auto-throttle maintains _____ in VS mode and ___ in FLC mode.

A

Airspeed

MCT

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13
Q

Battery switches should be selected OFF after 30 seconds of engine shutdown to allow data to transfer from the:

A

EEC to the EDU

Electronic Engine Controller (EEC) to the Electronic Diagnostics Unit (EDU)

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14
Q

If a thrust reverser inadvertently deploys in flight, the thrust reverser EMER STOW buttons will _____ until pushed, then will display _____.

A

Flash

Steady

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15
Q

When the hydraulic pump buttons are selected to UNLOAD, the unload valve ____ and an amber ____ _____ _____ L-R CAS message is displayed.

A

Opens

HYD PRESS LOW

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16
Q

What happens if the APU FIRE button is not pressed after an APU fire indication?

A

After 8 seconds, the APU will shut down and the shared APU/Baggage fire bottle will discharge automatically.

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17
Q

Landing elevation for the pressurization system is normally derived from:

A

Flight Plan Destination Altitude

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18
Q

Electric cabin pressure control is accomplished by modulating a single _____ _____ on the aft pressure bulkhead.

A

Outflow Valve

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19
Q

Cabin dump will dump the cabin to _____ feet in auto mode and ____ feet in manual mode.

A

13,700

14,200

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20
Q

What is the maximum Zero Fuel Weight?

A

21,430

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21
Q

The APU can be started up to _____ feet, operated to _____ feet, and _____ KIAS.

A

20,000’
30,000’
305 kias

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22
Q

Oxygen pressure is monitored on MFD GTC > Aircraft Systems > _____ page.

A

Summary

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23
Q

What runway conditions are thrust reversers and speedbrakes calculated for the takeoff performance?

A

Wet runway

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24
Q

Baggage fire detection is accomplished by:

A

Optical smoke detectors

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25
if an amber A/I (_) HOT CAS message for WING, STAB, ENGINE displays, the associated valve will _____.
Close
26
During start, the RUN/STOP button should be set to run at __ % N2.
9
27
Roll control is normally achieved by mechanical ____ and hydraulic ____ ____.
ailerons roll spoilers
28
The APU generator will supply power directly to the:
Left Emergency Bus
29
Pressing an ENG FIRE button accomplishes:
* Fuel F/W Shutoff closes * Hydraulic F/W Shutoff closes * Engine generator is deactivated * Both fire bottles are armed * affected engine thrust reverser is deactivated
30
The Interior button will remove power from the aft cabin with the exception of:
Emergency Lights Pax Safety Cabin Entry Lights
31
Primary trim is accomplished by a movable _____ _____.
horizontal stabilizer
32
The amber LAVATORY DOOR CAS message will display whenever the sliding pocket door is not secured:
1. On the ground | 2. In flight, below 18,000 feet with either main gear down – locked and/or flaps out of up.
33
What is the maximum Takeoff Weight?
30,800
34
Cockpit and cabin temperature control can be operated either _____ or _____.
Automatically or Manually
35
With the APU generator ON, DC electrical power is provided on the :
Left EMER Bus
36
Power for the NWS accumulator bleed valve is from the ___ ___ ___.
Left Battery Bus
37
Minimum battery temperature for engine start is:
-10 degrees C
38
The use of the AUX PUMP is prohibited __ _____ and below ____.
In flight -40 degrees C
39
When will EDM activate?
* Autopilot engaged * Aircraft above 30,000’ * Cabin altitude above 14,500’
40
Can takeoff be initiated with a RED CAS message?
NO
41
What is the maximum total weight in the tailcone baggage compartment?
1,000 lbs
42
Amber / White CAS messages can be scrolled using:
UP and DOWN arrows on the left or right PFD GTCs.
43
When selecting the PASS OXY knob to Auto, the passenger oxygen masks will automatically drop with a cabin altitude above _____ feet.
14,500
44
The PITCH/ROLL disconnect releases the interconnect between the _____ and _____ _____, and between the left and right _____.
Ailerons and roll spoilers Elevators
45
A red CABIN ALTITUDE CAS message will be displayed with a cabin altitude above _____ feet in normal mode and _____ feet in high altitude mode.
9,650 14,500
46
Emergency pressurization will automatically activate with:
* ACM O’TEMP * ACM BLD LEAK * Cabin Altitude above 14,500 feet
47
Normal indications of crossfeed are White _____ and White _____ _____ _____ _____CAS message.
CROSSFEED | FUEL BST PUMP ON
48
The pressurization source selector controls bleed air for:
environmental and pressurization
49
The standby battery will power the standby flight display for ___ minutes with no other power source available.
180 minutes
50
The ENG/STAB buttons must be selected to ON whenever in visible moisture and temperature between:
+10 to -35 degrees C RAT (SAT on ground)
51
The cabin entry door lift motor is powered by the ____ ____ ____?
Left Battery Bus
52
With a main DC power failure, all anti-ice valves open except:
WING XFLOW VALVE
53
What is the definition of Takeoff Field Length? | The greatest of:
* Accelerate-Stop distance * Engine-Out accelerate-go distance to 35 feet * 115% of the 2-Engine takeoff distance to 35 feet
54
Automatic temperature control can be changed on either MFD GTC > Aircraft Systems > ____ ____.
Temp Page
55
The engine start sequence and stabilized idle is indicated by:
* White ENGINE SHUTDOWN L or R CAS message clearing | * Engine bugs posted on the N1 gauges
56
With auto-throttle use on takeoff, a green ____ must be seen by __ KIAS.
HOLD 65
57
With the boost pump switch in NORM, automatic activation of the electric boost pump occurs when:
Engine Start Crossfeed Low Fuel Pressure APU operation with right engine not running.
58
The results of auto test are displayed:
MFD GTC > Aircraft Systems > Summary Synoptic page
59
Pushing the TO/GA button will direct the command bars to __° nose up on the ground and __° nose up in flight.
10 7.5
60
The oxygen bottle is a standard ___ cubic feet.
77
61
The PAX safety button illuminates:
No Smoking - Return to Seats signs | Emergency Lights
62
Service air is used for:
* Low limit temperature valve (ACM) | * Recirc valve operation
63
To achieve a proper indication of brake wear, the brakes must be ___.
Set
64
Hydraulic system pressure is used for:
* Landing gear * Brakes * Nose wheel steering * Speed brakes * Roll Spoilers * Thrust reversers
65
Hydraulic fluid volume is displayed on the:
Hydraulic Synoptic
66
What happens with APU bleed and MAX COOL selected ON?
* Recirc Fan commanded to HI * Temp Control Valves Close * APU Bleed Valve commanded to Full Open * In flight, Mass Flow Valves bias to a higher flow
67
Failure of the engine fire detection system is indicated by a:
FIRE DETECT FAIL L or R CAS message
68
What is trim air?
Hot and cold air mixed together
69
Throttles must be decreased to idle reverse position by ___ KIAS during landing rollout.
65
70
To cool generators, the engine must be operated at ____ with the generator load less than ___ amps for __ minutes prior to shutdown, or do not restart engines for ___ minutes.
IDLE 75 amps 4 minutes 35 minutes
71
The maximum (green display) differential pressure is _____.
10.2 psid
72
The amber CHECK DOORS CAS message indicates a monitor has not been properly tested or has failed. Identify monitored doors:
Nose Compartment Doors L - R Cabin Entry Door Baggage Door
73
APU bleed air can be used in place of engine bleed air except for:
* Anti-Ice | * Emergency Pressurization
74
Touch down protection prevents power brake application until _?_ or _?_.
Main wheels spin up Main squat switches indicate on the ground for 3 seconds or more.
75
What is the maximum landing gear operating/extended speed (VLO / VLE)?
210
76
On the ground, the pilot must abort the start if:
``` • No oil pressure within 20 seconds of ITT rise • No N1 by 40% N2 • No stabilized idle by 90 seconds of ITT rise ```
77
Engine-driven hydraulic pumps can deliver ____ psi hydraulic pressure.
3,000
78
The no takeoff items are displayed:
MFD GTC > Aircraft Systems > Summary Synoptic page
79
The GARMIN system will inhibit non-critical CAS messages for certain phases of flight such as:
TOPI, LOPI, Bus Inhibit, and Engine shutdown.
80
When will the the recirculation valve close automatically?
* Recirculation fan is selected OFF * Loss if bleed air to the ACM * Duct failure * Pressure Source not in NORM
81
With the loss of hydraulic pressure, the nose wheel steering accumulator will supply:
2 full sweeps of NWS operation
82
What are the 5 ways to illuminate the wing inspection lights?
``` WING INSP button – ON EMER LTS switch – ON EMER LTS switch ARM: - PAX SAFETY - ON - 5g impact - Loss of normal DC power ```
83
What is the maximum engine oil consumption?
1 Quart per 8 Hours
84
Airspeed must be decreased to ____ KIAS to allow an inadvertently deployed thrust reverser to be stowed.
150
85
What is the maximum runway gradient used in the performance data?
2% uphill and 2% downhill
86
A satisfactory preflight test of the thrust reverser system must be accomplished:
* First flight of the day * After any mx has been performed * If performance is predicated on their use
87
Rudder bias uses bleed air to assist with lateral rudder control during ____ ____ ____.
Single engine operations
88
With the exception of ___ ___ ___, all other BLD LEAK CAS messages will automatically close the associated valve.
TAIL BLD LEAK
89
Where is control of the navigation and beacon lights located?
The MFD GTC > Aircraft Systems > Exterior Lights page
90
The transponder is controlled using either ___ ___.
MFD GTC
91
Thrust reverser deployment for more than ___ seconds with an operating APU is prohibited.
30
92
Pushing the baggage fire button will discharge the Shared APU/Baggage fire bottle and Low rate squib on the ___ bottle.
MDR | Metered Discharge Rate
93
The amber APU OIL LEVEL LOW CAS message allows operation of the APU for ___ hours.
20
94
Power for windshield heat is supplied by:
Engine driven alternators
95
What is heated with the PITOT/STATIC button ON:
* Left / Right / Standby Pitot Tubes * Left / Right / Standby Static Ports * both AOA Vanes
96
What two methods can be used to fuel the Latitude?
Single Point Refueling | Over-wing Refueling
97
When selecting the PASS OXY knob to ON, _____ _____ will immediately drop the passenger masks.
oxygen pressure
98
The amber FUEL IMBALANCE CAS message indicates that there is a difference of more than ___ pounds between the right and left fuel tanks.
400 pounds
99
The control lock mechanically locks _____ , _____ and _____, and restricts movement of the ___ throttle.
Ailerons, Elevators and Rudder Left

NETJETS CITATION LATITUDE STUDY 1 (15 decks)

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