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Latitude > Ch: 12 > Flashcards

Ch: 12 Flashcards

1
Q

Crosswind Dry or Wet T/O

A

30

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2
Q

Crosswind Contaminated >/= 150

A

15

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3
Q

Crosswind Contaminated < 150

A

10

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4
Q

Max Tailwind for T/O

A

10

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5
Q

Max Ramp / Taxi Weight

A

31,050

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6
Q

Max T/O Weight

A

30,800

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7
Q

Max Landing Weight

A

27,575

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8
Q

Max Operating Altitude

A

45,000

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9
Q

Min Altitude Speedbrake Extension

A

500’

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10
Q

Turbulent Air Penetration

A

225 / .73

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11
Q

Max Landing Gear Operating (V LO)

A

210

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12
Q

Max Flaps 1

A

250

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13
Q

Max Flaps 2

A

200

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14
Q

Max Flaps FULL

A

175

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15
Q

Min Holding Icing

A

180

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16
Q

APU Starter Operation

A

3 within 30m, 90s cooling

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17
Q

Max Airspeed APU Start

A

305

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18
Q

Max Altitude APU Start

A

20k

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19
Q

Max APU Operating Altitude

A

30k

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20
Q

AP min Enroute Altitude

A

1k

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21
Q

AP Min ILS LPV Altitude

A

160

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22
Q

AP Min Approach Alt

A

200

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23
Q

AP T/O / Climb Altitude

A

400

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24
Q

If not already engaged during TO, do not engage auto throttle ____ on the ground, and not until ____

A

Above 65

Above 400

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25
Q

Disengage auto throttle prior to landing without ____

A

FULL flaps

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26
Q

Voltage for engine start

A

Displayed Green

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27
Q

Max GPU voltage

A

30

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28
Q

Max Fuel Imbalance

A

400

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29
Q

Max time for PITOT/STATIC on ground

A

2 minutes

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30
Q

Approach Category

A

B

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31
Q

Max Tailwind Engine Start

A

10

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32
Q

Max Time TO Thrust AEO

A

5m

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33
Q

Max time TO Thrust OEI

A

10m

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34
Q

Max Time Reverse Thrust

A

5m
30s APU Running

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35
Q

Transient N1

A

106 for 20s

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36
Q

Transient N2

A

106 for 20s

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37
Q

Transient ITT

A

950 for 20s

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38
Q

Transient 20s Oil PSI

A

0-20 psi

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39
Q

Engine Start Attempts and Cooldown

A

2m, 5m, 30m

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40
Q

BAT only motoring limit

A

20s

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41
Q

BAT w/ gen assist or 1000A GPU

A

15

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42
Q

Starter Motoring Limit GPU 1500A

A

7s

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43
Q

Evacuation

A

Parking Brake - PF - ON
L & R Engine - PF - STOP

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44
Q

Start Malfunction On Ground

A

L/R Engine - LP - Stop

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45
Q

Smoke/Fire/Fume

A

O2 Mask and Goggles - Don/Emer
Crew Communication - Establish

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46
Q

Inflight Reverser Deploy

A

L/R TR Emer Stow - Press

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47
Q

Jammed Pitch/ Roll

A

Stabilizer Trim - Actuate
Yoke - Relax Pressure
Pitch/Roll Disconnect - Pull Until Latched
Operative Yoke - Identify

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48
Q

Stab Trim Runaway

A

AP/Trim/NWS Disc - PF - Press and Hold

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49
Q

Cabin Alt - Emer Descent

A

O2 Mask - Don/100%
Crew Communications - Establish

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50
Q

Battery O’Temp

A

L/R Batt - LP - Off

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51
Q

Engine Start Sequence Numbers

A

ITT Rise - Start
:20 - Oil Pressure Rise
40% N2 - N1 Rise
90s - Stable (57%, N1 Bugs, CAS Message Out)

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52
Q

FADEC Abort Start

A

1000 Degrees
Insufficient ITT

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53
Q

“IGN” means ____

A

Power applied, not necessarily igniting

54
Q

NWS Degrees

A

81% Tiller
7% Pedals
88% Cumulative

55
Q

Norm sets Bleed to HP ____

A

Above 37k
Above 25k w/ Anti Ice On

56
Q

Emer Press Source and Conditions

A

HP Left Engine
ACM bleed leak or over temp
14.5k

57
Q

Crew Brief Trigger

A

Crew Assembled

58
Q

Arrival and Approach Brief Trigger

A

FL180 or prior to commencing

59
Q

Departure Briefing Trigger

A

Cockpit Prep Checklist Complete

60
Q

Takeoff Brief Trigger

A

Both Pilots seated

61
Q

Acft Acceptance Flow Trigger

A

Pilot change
First Flight of Duty
Mx

62
Q

Power On Checklist Trigger

A

Electrical power is established for the purpose of aircraft movement

63
Q

Exterior Preflight Trigger

A

Acft Acceptance Flow Complete

64
Q

Interior Preflight Flow Trigger

A

Acft Acceptance Flow completed

65
Q

Cockpit Prep Flow Trigger

A

Power On Checklist complete (Postflight Flow for next flight)

66
Q

Before Start Flow Trigger

A

Ready to Start Engines

67
Q

Engine Start Trigger

A

Completion of Before Start Checklist

68
Q

After Start Flow Trigger

A

Both Engines Started

69
Q

Taxi Flow Trigger

A

Clear of obstacles, established on taxi route

70
Q

Before TO Flow

A

Approaching TO Runway

71
Q

After TO Flow Trigger

A

PF calls for Flap Retraction

72
Q

10K Flow Trigger

A

10K

73
Q

Nose Door Open L / R CAS message micro switch is located on?

A

4 mechanical latches

74
Q

Cabin entry door lift motor is powered by?

A

Left Battery Bus

75
Q

How long is the door held close by the motor?

A

10s

76
Q

The emergency exit can be removed from inside or outside the aircraft?

A

Both

77
Q

Baggage compartment heated or pressurized?

A

Not heated, not pressurized

78
Q

1 battery turned off with generators online?

A

Battery is isolated, DC is powered by generators

79
Q

REMOTE CB TRIPPED

A

CB not accessible by crew has tripped

80
Q

Primary DC Sources

A

APU, GEN, EPU

81
Q

Batteries during engine start?

A

Both batteries for every start (except windmilling)

82
Q

Bus tie opens and closes?

A

Auto on ground, manually in flight

83
Q

DC GEN OFF L / R

A

QRH

84
Q

APU power is supplied to?

A

Bus if respective GEN is unavailable

85
Q

BUS TIE CLOSED CAS displays?

A

In flight if bus tie button is selected closed, both GENs are online, and 5 minutes has elapsed.

86
Q

When is the BUS TIE auto in flight?

A

Closed to Open if overcurrent

87
Q

BATTERY O’ TEMP L / R temp?

A

63

88
Q

ACFT main electrical system is?

A

Split bus system, 2 DC GENs, 2 DC Batteries (25V / 44A)

89
Q

White AVAIL on the EPU switch means?

A

Connected and correct voltage (not necessarily correct amperage)

90
Q

BAT voltage before engine start?

A

Indicate green digits

91
Q

GEN switches for ENG start?

A

ON (off is checklist driven, normally ON)

92
Q

INTERIOR button?

A

Adds or removes all cabin power except EMER ARM lights (3 overhead, 5 floor, 6 exit)

93
Q

Will the APU come online (be used) with the L GEN on?

A

No, L GEN will take priority and power the system (will power left side if R GEN is online)

94
Q

TRU selected on means?

A

Windshield loses AC power so ALT can provide DC power (via TRU)

95
Q

Will the interior lights illuminate on battery power?

A

Yes

96
Q

The cabin entry light button is on which bus?

A

Right battery, 15 minute timer

97
Q

PAX SAFETY with EMER ARM illuminates?

A

Interior and Exterior Emergency Lights

98
Q

EMER lights, when ARMED, come on with?

A

Loss of DC power (ARM before BAT on)
5G impact
PAX SAFETY on

99
Q

Red CAS messages do what when posted?

A

Flash until acknowledged by Master Warning button

100
Q

Amber CAS messages do what when posted?

A

Flash amber and illuminate the steady amber Master Caution

101
Q

How does the NO TAKEOFF message act

A

White CAS, then red w/ aural NO TAKEOFF when throttles are moved to TO

102
Q

Engine Shutdown Inhibit (ESDI)

A

Activated when a pilot shuts down the engine or white ENGINE SHUTDOWN CAS posts
Deactivated when engine reaches idle

103
Q

Max Fuel Capacity Over Wing and SPPR

A

11,390 / 10,720

104
Q

SPPR Precheck must be completed?

A

Before every SPPR operation

105
Q

CAS message for L ENG low fuel pressure?

A

FUEL BOOST PUMP ON L (amber)

106
Q

Crossfeed from left tank to right engine may not occur if what CAS is displayed?

A

FUEL MOTIVE VALVE R (amber)

107
Q

Boost Pump in NORM comes on?

A

Low fuel pressure
APU w/ R ENG off
Cross feed
Engine Start

108
Q

APU Fire Light sequence

A

APU shuts down
BAG/APU fire bottle is discharged after 8s if APU FIRE button is not pressed

109
Q

APU provides?

A

DC power
Bleed Air (service air, environmental/ pressurization)

110
Q

APU oil level is monitored by?

A

CAS message (no gauge)

111
Q

Check engine oil by?

A

OIL LEVEL LOW L / R CAS (amber)

112
Q

N1 gauge inward pointing line indicates

A

FADEC setting for CRU

113
Q

FADEC will abort start when stabilized IDLE is not achieved by?

A

90s

114
Q

If the engine does not start, but the QRH has you dry motor, how long before you try another start?

A

2 minutes before the dry motor, 5 minutes before the start

115
Q

Prior to shutdown, the engine must be at idle power for ____ prior to shutdown

A

2 minutes

116
Q

Generator cooling times

A

Eng idle with load < 75 amps for 4 minutes
Or
Wait 35 minutes before restart

117
Q

____ squat switches must indicated on ground for TRs to deploy

A

All 3

118
Q

TRs at idle by what speed?

A

65

119
Q

Type of fire sensor in baggage

A

2 optical smoke sensors

120
Q

FIRE DETECT FAIL L

A

Failure of the fire detect loop on left engine

121
Q

Areas monitored by fire detection system

A

Engines (heat)
APU (heat)
Baggage Compartment (smoke)

122
Q

L ENG FIRE button shuts off?

A

Fuel
Hyd
GEN
Bottles (armed)
TR

123
Q

BAGGAGE FIRE button causes?

A

BAG-APU fire bottle in the tail cone, and the low discharge function of the fire bottle in the nose, to discharge

124
Q

PRESS SOURCE controls bleed air

A

From engines for environmental/ pressurization

125
Q

L/R ENG BLD AIR NORM selects HP and LP when?

A

HP - low throttle setting, > 14500, 25k w/ anti-ice, 37k anytime, wing XFLOW, default if input signals are invalid

126
Q

TAIL BLD LEAK

A

Only overtemp that won’t automatically close associated bleed air valve

127
Q

ENG BLD AIR first enters

A

Pylor precooler

128
Q

EMER PRESS auto when?

A

ACM Bleed air leak
ACM Overtemp
Cabin > 14500

129
Q

IFR Fuel Reserve

A

1464

130
Q

Emergency Fuel

A

1100

131
Q

Runway length, width and slope

A

4k, 70, 2%

Latitude (2 decks)

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