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Citation Latitude > Latitude Jeopardy > Flashcards

Latitude Jeopardy Flashcards

(100 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
100
How are the forward refreshment center and aft vanity sink drains heated?
Use main DC power. Electrically heated drains prevent ice formation that might impair normal drainage of water from the aircraft. The drain heating elements are powered when the left ANTI-ICE PITOT STATIC button is in the ON position.

Citation Latitude (16 decks)

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