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Citation Latitude > Latitude Jeopardy > Flashcards

Latitude Jeopardy Flashcards

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
Q

if an amber A/I (_) HOT CAS message for WING, STAB, ENGINE displays, the associated valve will _____.

A

Close

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26
Q

During start, the RUN/STOP button should be set to run at __ % N2.

A

9

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27
Q

Roll control is normally achieved by mechanical ____ and hydraulic ____ ____.

A

ailerons

roll spoilers

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28
Q

The APU generator will supply power directly to the:

A

Left Emergency Bus

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29
Q

Pressing an ENG FIRE button accomplishes:

A
  • 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
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30
Q

The Interior button will remove power from the aft cabin with the exception of:

A

Emergency Lights
Pax Safety
Cabin Entry Lights

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31
Q

Primary trim is accomplished by a movable _____ _____.

A

horizontal stabilizer

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32
Q

The amber LAVATORY DOOR CAS message will display whenever the sliding pocket door is not secured:

A
  1. On the ground

2. In flight, below 18,000 feet with either main gear down – locked and/or flaps out of up.

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33
Q

What is the maximum Takeoff Weight?

A

30,800

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34
Q

Cockpit and cabin temperature control can be operated either _____ or _____.

A

Automatically or Manually

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35
Q

With the APU generator ON, DC electrical power is provided on the :

A

Left EMER Bus

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36
Q

Power for the NWS accumulator bleed valve is from the ___ ___ ___.

A

Left Battery Bus

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37
Q

Minimum battery temperature for engine start is:

A

-10 degrees C

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38
Q

The use of the AUX PUMP is prohibited __ _____ and below ____.

A

In flight

-40 degrees C

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39
Q

When will EDM activate?

A
  • Autopilot engaged
  • Aircraft above 30,000’
  • Cabin altitude above 14,500’
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40
Q

Can takeoff be initiated with a RED CAS message?

A

NO

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41
Q

What is the maximum total weight in the tailcone baggage compartment?

A

1,000 lbs

42
Q

Amber / White CAS messages can be scrolled using:

A

UP and DOWN arrows on the left or right PFD GTCs.

43
Q

When selecting the PASS OXY knob to Auto, the passenger oxygen masks will automatically drop with a cabin altitude above _____ feet.

A

14,500

44
Q

The PITCH/ROLL disconnect releases the interconnect between the _____ and _____ _____, and between the left and right _____.

A

Ailerons and roll spoilers

Elevators

45
Q

A red CABIN ALTITUDE CAS message will be displayed with a cabin altitude above _____ feet in normal mode and _____ feet in high altitude mode.

A

9,650

14,500

46
Q

Emergency pressurization will automatically activate with:

A
  • ACM O’TEMP
  • ACM BLD LEAK
  • Cabin Altitude above 14,500 feet
47
Q

Normal indications of crossfeed are White _____ and White _____ _____ _____ _____CAS message.

A

CROSSFEED

FUEL BST PUMP ON

48
Q

The pressurization source selector controls bleed air for:

A

environmental and pressurization

49
Q

The standby battery will power the standby flight display for ___ minutes with no other power source
available.

A

180 minutes

50
Q

The ENG/STAB buttons must be selected to ON whenever in visible moisture and temperature between:

A

+10 to -35 degrees C RAT (SAT on ground)

51
Q

The cabin entry door lift motor is powered by the ____ ____ ____?

A

Left Battery Bus

52
Q

With a main DC power failure, all anti-ice valves open except:

A

WING XFLOW VALVE

53
Q

What is the definition of Takeoff Field Length?

The greatest of:

A
  • Accelerate-Stop distance
  • Engine-Out accelerate-go distance to 35 feet
  • 115% of the 2-Engine takeoff distance to 35 feet
54
Q

Automatic temperature control can be changed on either MFD GTC > Aircraft Systems > ____ ____.

A

Temp Page

55
Q

The engine start sequence and stabilized idle is indicated by:

A
  • White ENGINE SHUTDOWN L or R CAS message clearing

* Engine bugs posted on the N1 gauges

56
Q

With auto-throttle use on takeoff, a green ____ must be seen by __ KIAS.

A

HOLD

65

57
Q

With the boost pump switch in NORM, automatic activation of the electric boost pump occurs when:

A

Engine Start
Crossfeed
Low Fuel Pressure
APU operation with right engine not running.

58
Q

The results of auto test are displayed:

A

MFD GTC > Aircraft Systems > Summary Synoptic page

59
Q

Pushing the TO/GA button will direct the command bars to __° nose up on the ground and __° nose up in flight.

A

10

7.5

60
Q

The oxygen bottle is a standard ___ cubic feet.

A

77

61
Q

The PAX safety button illuminates:

A

No Smoking - Return to Seats signs

Emergency Lights

62
Q

Service air is used for:

A
  • Low limit temperature valve (ACM)

* Recirc valve operation

63
Q

To achieve a proper indication of brake wear, the brakes must be ___.

A

Set

64
Q

Hydraulic system pressure is used for:

A
  • Landing gear
  • Brakes
  • Nose wheel steering
  • Speed brakes
  • Roll Spoilers
  • Thrust reversers
65
Q

Hydraulic fluid volume is displayed on the:

A

Hydraulic Synoptic

66
Q

What happens with APU bleed and MAX COOL selected ON?

A
  • 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
Q

Failure of the engine fire detection system is indicated by a:

A

FIRE DETECT FAIL L or R CAS message

68
Q

What is trim air?

A

Hot and cold air mixed together

69
Q

Throttles must be decreased to idle reverse position by ___ KIAS during landing rollout.

A

65

70
Q

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.

A

IDLE
75 amps
4 minutes
35 minutes

71
Q

The maximum (green display) differential pressure is _____.

A

10.2 psid

72
Q

The amber CHECK DOORS CAS message indicates a monitor has not been properly tested or has failed. Identify monitored doors:

A

Nose Compartment Doors L - R
Cabin Entry Door
Baggage Door

73
Q

APU bleed air can be used in place of engine bleed air except for:

A
  • Anti-Ice

* Emergency Pressurization

74
Q

Touch down protection prevents power brake application until ? or ?.

A

Main wheels spin up

Main squat switches indicate on the ground for 3 seconds or more.

75
Q

What is the maximum landing gear operating/extended speed (VLO / VLE)?

A

210

76
Q

On the ground, the pilot must abort the start if:

A 
• No oil pressure within 20   
    seconds of ITT rise 
• No N1 by 40% N2
• No stabilized idle by 90 seconds
    of ITT rise
77
Q

Engine-driven hydraulic pumps can deliver ____ psi hydraulic pressure.

A

3,000

78
Q

The no takeoff items are displayed:

A

MFD GTC > Aircraft Systems > Summary Synoptic page

79
Q

The GARMIN system will inhibit non-critical CAS messages for certain phases of flight such as:

A

TOPI, LOPI, Bus Inhibit, and Engine shutdown.

80
Q

When will the the recirculation valve close automatically?

A
  • Recirculation fan is selected OFF
  • Loss if bleed air to the ACM
  • Duct failure
  • Pressure Source not in NORM
81
Q

With the loss of hydraulic pressure, the nose wheel steering accumulator will supply:

A

2 full sweeps of NWS operation

82
Q

What are the 5 ways to illuminate the wing inspection lights?

A 
WING INSP button – ON
EMER LTS switch – ON
EMER LTS switch ARM: 
    - PAX SAFETY - ON
    - 5g impact
    - Loss of normal DC power
83
Q

What is the maximum engine oil consumption?

A

1 Quart per 8 Hours

84
Q

Airspeed must be decreased to ____ KIAS to allow an inadvertently deployed thrust reverser to be stowed.

A

150

85
Q

What is the maximum runway gradient used in the performance data?

A

2% uphill and 2% downhill

86
Q

A satisfactory preflight test of the thrust reverser system must be accomplished:

A
  • First flight of the day
  • After any mx has been performed
  • If performance is predicated on their use
87
Q

Rudder bias uses bleed air to assist with lateral rudder control during ____ ____ ____.

A

Single engine operations

88
Q

With the exception of ___ ___ ___, all other BLD LEAK CAS messages will automatically close the associated valve.

A

TAIL BLD LEAK

89
Q

Where is control of the navigation and beacon lights located?

A

The MFD GTC > Aircraft Systems > Exterior Lights page

90
Q

The transponder is controlled using either ___ ___.

A

MFD GTC

91
Q

Thrust reverser deployment for more than ___ seconds with an operating APU is prohibited.

A

30

92
Q

Pushing the baggage fire button will discharge the Shared APU/Baggage fire bottle and Low rate
squib on the ___ bottle.

A

MDR

Metered Discharge Rate

93
Q

The amber APU OIL LEVEL LOW CAS message allows operation of the APU for ___ hours.

A

20

94
Q

Power for windshield heat is supplied by:

A

Engine driven alternators

95
Q

What is heated with the PITOT/STATIC button ON:

A
  • Left / Right / Standby Pitot Tubes
  • Left / Right / Standby Static Ports
  • both AOA Vanes
96
Q

What two methods can be used to fuel the Latitude?

A

Single Point Refueling

Over-wing Refueling

97
Q

When selecting the PASS OXY knob to ON, _____ _____ will immediately drop the passenger masks.

A

oxygen pressure

98
Q

The amber FUEL IMBALANCE CAS message indicates that there is a difference of more than ___ pounds between the right and left fuel tanks.

A

400 pounds

99
Q

The control lock mechanically locks _____ , _____ and _____, and restricts movement of the ___ throttle.

A

Ailerons, Elevators and Rudder

Left

100
Q

How are the forward refreshment center and aft vanity sink drains heated?

A

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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