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Falcon 2000LX Winglets > RKA's > Flashcards

RKA's Flashcards

1
Q

Monitored doors

A

Cabin

Baggage

Emergency

Fwd service

Aft service

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2
Q

ELT control

A

Remote right side panel

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3
Q

Test not on the TEST Synoptic

A

Fire test

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4
Q

CVR Test

A

Soft key on test synoptic

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5
Q

Door lift operation

A

2 pushbuttons

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6
Q

Main door lift and lowered

A

Electrically lifted, mechanically lowered

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7
Q

Number of MAU power supplies

A

2

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8
Q

Right engine fails, what happens electrically?

A

Essential and Median are untied

Batt 2 powers R Bus and Median bus

Gen 1 powers L Bus

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9
Q

Max Gen output in flight with eng inop

A

400 amps

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10
Q

Ext pwr cart rating

A

28V and 1000V

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11
Q

CVR on ____ Bus

A

Essential

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12
Q

Gen control switch trips when ____ and. ____ ?

A

Overvolt and overamp

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13
Q

Left eng fails what happens electrically?

A

Essential and Median untied

Batt 1 powers L Bus

Gen 2 powers R Bus

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14
Q

Mini Load powers ______

A

Essential Bus

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15
Q

All gens fail pull ________ CBs

A

Orange

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16
Q

Landing light limits on ground

____ min on then ______ min cool

A

15, then 45

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17
Q

Dimming DUs on the _______

A

RCP rev panel

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18
Q

Emer Light position in flight

A

Arm

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19
Q

Emer lighting powered by ___ supplies

A

3

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20
Q

Emer lights tested by ___ position

A

On position

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21
Q

Master Warning Lights tested by ______

A

Soft key

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22
Q

If push Boost 2 pushbutton ______

A

Amber STBY light and STBY pump runs, no operational impact

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23
Q

FUEL LEVEL 1/2

A

1000 lbs remain

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24
Q

X-BP

A

Verify on fuel Synoptic

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25
Q

X-TK turns _____ on automatically

A

X-BP

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26
Q

Low Fuel cas

A

250 lbs remain

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27
Q

X-TK

A

Transfers fuel from tank group to group

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28
Q

Oil quantity check

A

10 mins after shutdown

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29
Q

FADEC funtions

A

FF

Surge protection

Overspeed

Overtemp

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30
Q

If FADEC fails _______ will fail

A

Eng fails

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31
Q

Thrust limit settings

A

Eng synoptic page

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32
Q

Start selector switch remains ________

A

Normal position

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33
Q

N1 turns amber during start, ______

A

Abort

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34
Q

APU Fire cas

A

APU auto shutdown

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35
Q

APU Bleed _____ auto when A/I turned on

A

Closes

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36
Q

When APU Master is on, APU EGT displayed ____

A

In Eng-Trim-Fuel Window

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37
Q

APU gen limits

______

______

______

A

300 to 10

250 10-20

200 20-35

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38
Q

Eng Gen amo limits

______ ground

_______ air

A

300

400

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39
Q

EXT PWR on, what happens

A

Batteries and Gens isloated

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40
Q

Failed APU start wait _____

A

30 seconds

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41
Q

FIRE BAG COMP on

A

Fight with portable extinguisher

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42
Q

Bottles to fight APU and ENG fires

A

1 for apu

2 for either engine

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43
Q

Hot bleed air is cooled to the cabin air by _______

A

ECU

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44
Q

Potable water pressurized from _____

A

Pneumatic air from eng and apu

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45
Q

Fuel tank pressurized from ____

A

Engs

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46
Q

Cross bleed valve opens when ____ in Auto mode

A

Eng 1 or 2 shut down

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47
Q

Hyd reservoirs pressurized by _____

A

Bleed air

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48
Q

A/I fails ______ with loss of elect pwr

A

Open

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49
Q

Amber mark on N1 gives you _____

A

Adequate bleed air for A/I operation

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50
Q

A/I controls located _____

A

On overhead panel

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51
Q

Eng A/I supplied from ______

A

HP bleed air

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52
Q

Wing A/I supplied from _______

A

Mix of hp and LP bleed air

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53
Q

A/I temp limits

A

10C to -40C

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54
Q

WW speed

A

215

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55
Q

Wing A/I ______ only

Eng A/I _______ and ______

A

In flight

On ground and in flight

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56
Q

EMER Pressure guarded switch _____

A

Control of hot valves only

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57
Q

Remote ECS key ____

A

Gives cabin control ECS

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58
Q

Air cond controls ______

A

Overhead

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59
Q

The air conditioning system regulates ________

A

Flow of air into cockpit, cab and baggage

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60
Q

Air cond heat exchanger in flight

A

Ventilated from vert fin root intake

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61
Q

Recirc valve closes at ______

A

15,000 ft

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62
Q

Ground Air max psi ______

A

50

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63
Q

Pneumatic outflow dump valve needs ____ and _____

A

Electric and pneumatic pressure

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64
Q

Cab Alt is limited to ________

A

14,500 ft

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65
Q

Max diff press _____

A

9.3 psi

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66
Q

To manually control pressurization ______

A

Use MAN Pressure knob

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67
Q

With STBY Pump in auto, cas illuminates after _____

A

60 seconds

68
Q

With #2 HYD eng driven pump failure and HYD 2 Isol valve in auto, the STBY HYD PUMP will power HYD 2 with ________

A

SF extended

69
Q

1 hyd system normally powered by ____ and ____

A

Eng 1 pump and Eng 2 pump 1

70
Q

Hyd reservoirs pressurized by _____

A

LP bleed air

71
Q

To close HYD manually, _______

A

Push fire/shutoff buttons

72
Q

Landing gear hyd power from _____

A

Hyd 1

73
Q

Brake temps are on _____

A

HYD synoptic

74
Q

Normal braking is from _______

A

Hyd 1 and 2

75
Q

SF indications disappear at _____

A

18000 ft

76
Q

During aero braking on ground ______

A

All 6 ABs are extended

77
Q

Ldg gear symbology

A

Green and red

78
Q

1900 psi brake

A

Gives 6 pulls emer brakes

79
Q

Elevator Arthur Unit

A

stab and slats

80
Q

SF speeds

______

______

______

A

200

190

180

81
Q

Man pitch will ______ AP

A

Disengage

82
Q

Ail Zero cas

A

Not neutral

83
Q

Flap Asym

A

Obviously cas flaps

84
Q

_______ actuated and _______ linked flight controls

A

Hyd and mechanically

85
Q

Blue curved arrow

A

Data to set

86
Q

Cursor inhibited

A

In another active screen

87
Q

Red X is ______ fail

A

AGM

88
Q

000000 means ____

A

Man data entry

89
Q

Emer VHF

A

121.5

90
Q

SV brightness on _____

A

Data tab

91
Q

LH PDU from _____

A

FMS 1

92
Q

LH PDU from ______ ____ and ______

A

All 3 FMSs

93
Q

FMS primary approach for _____ approach

A

GPS

94
Q

GA mode is exited by ____

A

Selecting another V mode

95
Q

FMS MSG cleared by

A

Hit the button

96
Q

TD off then FD off if push

A

Button on panel

97
Q

PDU/MDU toggle to ______

A

PNF

98
Q

DUs to fly needed ______

A

3 out 4 and not lower out

99
Q

_____ is default vert mode

A

Path

100
Q

RAD ALT works from

A

-20 to 2,500 ft

101
Q

Accel chevron inside ____ to match speed

A

Thrust vector

102
Q

Blue ADI with red flag ____ failure

A

IRS

103
Q

8.33 spacing on _____

A

Radio window VHF

104
Q

Ox in Override ____

A

Drops reguardless of alt

105
Q

Ox knob closed _______

A

Pax off , crew still on

106
Q

Ox pressure on ECS synoptic _____

A

Bottle pressure

107
Q

Pax masks drop at ______

A

14,500 +- 500

108
Q

TRs work ______

A

Idle

On grounds

30kts full throttle

Fadec auto stow hyd in flight

109
Q

TRs on ______ system

A

HYD 2

110
Q

Va

Payload

Baggage comp

Max ramp

Max t/o

Max Landing

Max z fuel

A

198

5990

1600

43000

42800

39,300

29,700

111
Q

Max tail

Max cross

Max land alt

Max cruise alt

Slope max

A

10

35

14000 to - 1000

FL 470

2%

112
Q

Max starting ITT

A

950

113
Q

T/O thrust lim

A

5 minutes

6990

875 Cool

114
Q

N1 primary for ______

Limit?

A

Thrust

102.5

115
Q

End start times

______

______

______

Starter cutout _____

A
  1. To N2

20 to light

60 light to started

50% N1

116
Q

Max motor time _____

Tailpipe fire

A

30 sec

Motor starter

117
Q

Norm hyd press

A

3000

+- 200

118
Q

Max fuel imbalance

A

2200

119
Q

MEL

A

B

C

D

A

Spec

3

10

120

120
Q

Vle

Vlo

A

245

190

121
Q

Max tire

A

195

122
Q

Min oil temp for T/O

A

27 Cool

123
Q

Max SF ops

A

20,000

124
Q

Both HYD fail speed and button

A

260 and ISOL

125
Q

All eng out speeds

In cruise

During holding

A

.80/300

DDI

126
Q

Time between firing bottles and speed

A

30 sec and 250

127
Q

Wheel overheat

A

190 lower gear

Then to 245

128
Q

Emer evac

A

Set brake

Notify ATC

Evac pax

129
Q

2 gens fail mem

A

Talk 1

Squak 1

130
Q

Smoke or elect fire

A

Ox mask on 100 emer

Goggles on

Vent valve open

Squak 1

Talk 1

Declare emergency

7700

131
Q

Blank DU

A

Turn DU off

132
Q

Rapid depress

A

Mask on , emer 100

Disc AP, Idle

MMO

AB2

Squak 1

Talk 1

Declare emer

7700

Ox override

133
Q

PDU show

A

Adi

Hsi

Cas window

134
Q

SV on, no _______

A

Yellow attitude ref line

135
Q

HSI pushed down _____

A

During t/o for ros

136
Q

Cyan border for _______ page

A

Active

137
Q

AP is ______ when on

A

Green

138
Q

FPS uncaged below _______

A

20000 ft

139
Q

VOR bearing on ______

A

HSI

140
Q

FMS nav on ______ page

A

Sensors

141
Q

Yellow box ADI means _______

A

Rev mode

142
Q

Active LNAV is inverse ______

A

Green

143
Q

T/O speeds are on the ______

A

T/O data page FMW

144
Q

AGM are inside the _____

A

MAU

145
Q

TD

A

Magenta half circle

146
Q

FD off leaves _______

A

Dot in center

147
Q

HAI in Arc mode to diaplay ________

A

WX radar

148
Q

Auto tune nav from

A

Nav tab

149
Q

Initialize 1 ______ at power up

A

FMS

150
Q

FMS 1 reversion _____

A

FMS 2 in amber

151
Q

P p hold by pressing

A

Aircraft symbol on inav

152
Q

FMS operates in _____ ans ____ mode

A

Synch and single

153
Q

If FMS 1 fails, PF should hit ______

A

FMS 2 for rev mode

154
Q

INav info is from _____

A

PF FMS

155
Q

Fly over waypoint will ____

A

Join course after (F) waypoint

156
Q

Flight plans can be entered for ____ and ____

A

Active and secondary

157
Q

L indicates ____

A

Man left turn

158
Q

3 types of FMS databases ____ _____ ____

A

Perf

Nav

User

159
Q

FMS speed tabs to adjust _____

A

Flap speeds

160
Q

If dicontinuity then LNAV to _____

A

Roll

161
Q

For airplane position FMS uses ____

______

______

_____

A

2 gps

2 dme

2 irs

2 vor

162
Q

Remove batts ______

A

-15 Cool

163
Q

Remove potable water _____

A

Below 0 C

164
Q

Do not service potable water with _____ or _____

A

Distilled or demineralized water

165
Q

Aft water heater CB is in the ____

A

Aft baggage cab supply cb panel

Falcon 2000LX Winglets (1 decks)

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