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JSX Oral Prep > ORAL PREP GO > Flashcards

ORAL PREP GO Flashcards

1
Q

APU maximum rotor speed

A

108%

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1
Q

Maximum EGT for APU start

A

884 C

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2
Q

Maximum continuous EGT for APU

A

680 C

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3
Q

Maximum continuous EGT for 5 minutes max for APU

A

717 C

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4
Q

Minimum Battery temperature for starting APU

A

-20 C

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5
Q

Maximum ITT engine start

A

800 C

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6
Q

Maximum ITT for takeoff

A

948 C

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7
Q

Maximum continuous ITT

A

901 C

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8
Q

Which bus is IC-600 #1 on?

A

Essential DC Bus 1

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8
Q

Which bus is IC-600 #1 on?

A

Essential DC Bus 1

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8
Q

Which bus is IC-600 #2 on?

A

DC Bus 2

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8
Q

Which bus is IC-600 #1 on?

A

Essential DC Bus 1

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8
Q

Which bus is IC-600 #1 on?

A

Essential DC Bus 1

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8
Q

Which bus is IC-600 #1 on?

A

Essential DC Bus 1

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8
Q

Which bus is IC-600 #1 on?

A

Essential DC Bus 1

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8
Q

Which bus is IC-600 #1 on?

A

Essential DC Bus 1

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9
Q

Which bus are the PFDs on?

A

DC Bus 1

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10
Q

Which bus are the MFDs on?

A

DC Bus 2

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11
Q

Which bus are the RMUs on?

A

RMU 1 - Essential Bus 1
RMU 2 - Essential Bus 2

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12
Q

Which bus is the EICAS on?

A

Essential Bus 1

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13
Q

What is a Data Acquisition Unit?

A

Present information about the engines and other system information to the IC-600 flight computers, which are presented on the EICAS and MFD.

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14
Q

How many Data Acquisition Units are there?

A

Two

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15
Q

How many channels do each Data Acquisition Units have?

A

Two:
Channel A (main, normal)
Channel B (backup, manually selected)

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16
Q

What information does DAU 1 supply?

A

Left Engine Systems
FADEC 1A (normal) / 1B (standby)
Forward Systems

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17
Q

What information does DAU 2 supply?

A

Right Engine Systems
FADEC 2A (normal) / 2B (standby)
Aft Systems

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18
Q

What controls the APU?

A

FADEC

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19
Q

What type of transponder do we have?

A

Mode S

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20
Q

What does TA/RA stand for?

A

Traffic Advisory
Resolution Advisory

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21
Q

What does the Tuning Backup Control Head do?

A

Provides an alternative means to tune COM 2 if both RMUs fail

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22
Q

When does the Cockpit Voice Recorder start to record?

A

When the batteries are turned on

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23
Q

How long does the Cockpit Voice Recorder record for?

A

2 hours

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24
Q

Where is the Cockpit Voice Recorder located?

A

Rear Avionics Bay

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25
Q

How long does the Underwater Location Beacon transmit for?

A

30 days

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26
Q

What is on the AC Bus?

A

EPGWS
Windshear Avoidance
TCAS

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27
Q

What does Amber Windshear indicate?

A

Increasing Performance

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28
Q

HALF

A

Hydraulic Shutoff Valves
Air Bleed Valves
(Engine) Lip Anti-Ice Valve
Fuel Pump Shutoff Valve

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29
Q

HEAP OF

A

Hydraulic Pumps
Electric Generators
Air Turbine Starter
Permanent Magnetic Alternator

Oil Pump
Fuel Pump Metering Unit

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30
Q

What does Red Windshear indicate?

A

Decreasing Performance

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31
Q

Volts and Amps for Generators

A

28 Volts
400 Amps

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32
Q

Volts and Amps for APU

A

28 Volts
400 Amps

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33
Q

Volts and Amps for NiCad Batteries

A

24 Volts
44 Amps

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34
Q

Volts and Amps for Backup Batteries

A

24 Volts
5 Amps

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35
Q

Volts for the GPU

A

26 to 29 Volts

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36
Q

Single Phase Static Inverters converts…?

A

28 Volts DC into 115 Volts AC

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37
Q

What does the Electrical Distribution Logic do?

A

EDL is a two channel computer that controls the electrical system by opening and closing channels.

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38
Q

What is powered when all generators fail?

A

Central Bus
Essential Bus
Avionics Bus
Hot Bus

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39
Q

Which systems use air from the Pneumatic System?

A

Pressurization
AC
Thermal Anti Ice
Engine Starting

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40
Q

What is powered when we only have 1 or 2 generators?

A

Everything but the shed buses

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41
Q

Main batteries require maintenance when below:

A

19 Volts

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42
Q

Batteries provide how many minutes of reserve power?

A

40 minutes

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43
Q

How many volts are required to start the APU?

A

24 Volts

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44
Q

How many Shed Buses are there?

A

Two

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45
Q

How many Avionic Buses are there?

A

Six

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46
Q

How many starts of the APU do we have on essential power?

A

Three

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47
Q

How long does the Digital Flight Data Recorder record for?

A

25 hours

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48
Q

When does the Digital Flight Data Recorder start to record?

A

When the Red Beacon is on
When the aircraft is airborne

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49
Q

Fire Detection Test EICAS messages

A

APU Fire
Eng 1(2) Fire
Bagg Smoke
APU Firedet Fail
E1(2)Firedet Fail

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50
Q

How many halon fire extinguisher bottles are there for the APU?

A

One

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51
Q

How many halon fire extinguisher bottles are there per engine?

A

Two

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52
Q

How many halon fire extinguisher bottles are there for the baggage compartment?

A

Two.
One Rapid, one Slow Release (50 minutes)

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53
Q

How many fuel pumps are there?

A

6 (3 per wing)

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54
Q

With a Fuel Low EICAS message, how much flight time is remaining?

A

30 minutes

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55
Q

Engines have a high bypass ratio of…?

A

5:1

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56
Q

What does Compressor Variable Geometry do?

A

Prevents engine surges and compressor stalls

57
Q

How many FADECs do we have?

A

Two - A and B

58
Q

What happens if both FADECs fail?

A

Engine shutdown

59
Q

How many hydraulic pumps are there?

A

Four

60
Q

When do the Electric Hydraulic Pumps activate?

A

When hydraulic pressure is below 1600 psi.

61
Q

How many liters are in the Hydraulic Reservoir?

A

6 liters

62
Q

What do the Hydraulic Accumulators control for System 1?

A

Landing Gear
Main Door
Steering

63
Q

What do the Hydraulic Accumulators control for System 2?

A

Emergency Brakes

64
Q

When does the landing gear warning activate?

A

1200 RA, Flaps less than 22 and thrust lever angle is below 59 degree.
Flaps 45.
RA failure.

65
Q

What brake protection do we get?

A

Anti-Skid
Locked Wheel Protection (above 30 knots)
Touchdown Protection (50 knots / 3 seconds)

66
Q

What types of flaps do we have?

A

Double-Slotted Fowler Flaps

67
Q

CPAM

A

Cabin Pressure Acquisition Module

68
Q

Spoiler Control Unit automatically deploys ground spoilers when:

A

On the ground
Landing gear below 25 knots
Both Thrust Lever Angles below 30 degrees
Both Engine N2 below 56%

69
Q

Speed Brakes Open if:

A

Thrust Levers below 50%
Flaps 0-9
Speed Brake Handle Open

70
Q

Elevator Tabs

A

Outer Tabs - Servo Tabs - Low Speed
Inner Tabs - Spring Tabs - High Speed

71
Q

Rudders will automatically decrease hydraulic power if:

A

Rudder is deflected more than 5 degrees
130# on the rudder pedals
Both engines are running 56% or less N2

72
Q

Both hydraulic systems power the rudders when below:

A

135 knots

73
Q

Pneumatic and Pressurization systems are supplied by:

A

Engines
APU
Ground Source

74
Q

Left side Pneumatic System powers:

A

Engine 1
APU
ECU 1
Left Wing Piccolo Tube
Both Horizontal stabilizers piccolo tubes

75
Q

Right side Pneumatic System powers:

A

Engine 2
Ground Start Cart Port
ECU 2
Right Wing Piccolo Tube

76
Q

Cross bleed valve opens when:

A

Engine 2 is being started
Engine 1 is being started with Engine 2 bleed air

77
Q

14th stage bleed air is used for:

A

Low thrust operations
Icing conditions
X-Bleed starts
Engine Inlet heating

78
Q

Gasper fan provides air to:

A

Air outlets
Rear electronic compartments
Oxygen Compartments
Relay Box Ventilation

79
Q

Electric Pressurization maintains the cabin at:

A

15,000 feet

80
Q

What is considered “icing conditions”?

A

10 C or below
Visible moisture
Less than 1 sm visibility

81
Q

What does does the thermal anti ice system provide?

A

Wings
Horizontal Stabilizer
Engine Lip Inlets

82
Q

When in icing conditions below 24,600 feet, what closes?

A

Pack 1 valve

83
Q

What groundspeed must you be at for anti ice to work?

A

25 knots

84
Q

EICAS messages for ice detection test?

A

Ice Detection 1 Fail
Bleed 1 Low Temp
Ice Condition

85
Q

Electronic Anti Ice powers which systems?

A

Windshields
Pitot Tubes
AOA Sensors
TAT Sensors
ADC Static Ports
Pressurization
FADEC

86
Q

Engine cooling between start attempts?

A

1-4 cycles: 1 minute on, 1 minute off
5th cycle: 1 minute on, 5 minutes off

87
Q

Engine warm up times?

A

4 minute run for cold engine.
2 minute run for warm engine.

88
Q

When is an engine considered cold?

A

When it is shut down more than 90 minutes.

88
Q

When is an engine considered cold?

A

When it is shut down more than 90 minutes.

89
Q

APU cooling between start attempts?

A

Three start attempts: 1 minute off
After that: 30 minutes off before another three start attempts

90
Q

Minimum maneuvering speed in icing conditions?

A

200 knots

91
Q

Minimum maneuvering speed in clean configuration?

A

180 knots

92
Q

Minimum speed, flaps 9?

A

160 knots

93
Q

Minimum speed flaps 22 and 45?

A

140 knots

94
Q

Hot Battery Bus powers what?

A

Courtesy lights
Main Door
Fueling Panel
Engine Fire Bottles

95
Q

APU Bleed is used for what?

A

Pressurization
Engine Start
Air Conditioning

96
Q

Fuel Pump power sources?

A

A: Essential
B: Essential
C: DC Bus 1/2

97
Q

A fuel pump fails when it goes below:

A

6.5 psi

98
Q

How many fuel pumps are necessary for both engines and the APU? (except Go Around and Takeoff)

A

One

99
Q

How long can vibration be in the yellow?

A

5 minutes in TOGA.
10 seconds all other times.

100
Q

PMA supplies power to:

A

FADEC
Ignition

101
Q

Hydraulic Quantity is considered low when at:

A

1 liter

102
Q

During landing gear retraction, the brake control unit:

A

Applies a 6 second application to stop the wheels before retraction.

103
Q

Elevator is controlled by:

A

Mechanics, no hydraulics

104
Q

Ailerons and Rudders are controlled by:

A

Ailerons: both hydraulic systems
Rudders: Both at low speeds, system 2 at high speeds (135 knots)

105
Q

TO Config checks:

A

Pitch Trim
Flaps
Parking Brake
Spoilers

106
Q

Speed Brakes automatically retract when:

A

Flaps 22 and above.
TLA is greater than 50.

107
Q

White stall speed

A

1.23 VSO

108
Q

Yellow stall speed

A

1.13 VSO

109
Q

What is Total Air Temperature?

A

Air that is brought to the relative speed of the aircraft before being measured.

110
Q

What is Static Air Temperature?

A

Temperature that is unaffected by the velocity of the aircraft.

111
Q

Maximum Runway Slope

A

Plus/Minus 2 degrees

112
Q

Maximum tailwind

A

10 knots

113
Q

Maximum Takeoff and Landing Pressure Altitude

A

-1,000 feet to 8,000 feet

114
Q

Service Ceiling

A

37,000 feet

115
Q

Maximum operational Static Air Temperature

A

ISA + 35 degrees

116
Q

Maximum and Minimum SAT for takeoff and landing

A

-40 C to 52 C

117
Q

Vmo / Mmo

A

Up to 8,000 feet: 250 knots
10,000 feet to 26,000: 320 knots
Above 10,000 feet: .78 M

118
Q

Va

A

200 knots

119
Q

Turbulent Air Penetration Airspeeds

A

Below 10,000 feet: 200 knots
Above 10,000 feet: 250 knots / .63 M, whichever is lower

120
Q

When does a Oxygen Low Pressure message show up on the EICAS?

A

Below 400 psi
About 12 minutes

121
Q

Oxygen Tank Pressure Levels

A

Full - 1,850 psi
Two - 1,500 psi
Three - 1,100 psi

122
Q

What cabin altitude will the oxygen masks automatically deploy?

A

14,000 feet

123
Q

What does the manual position do for the passenger oxygen panel?

A

Deploy the oxygen masks regardless of altitude.

124
Q

How many Protective Breathing Equipment do we have?

A

Three

125
Q

How long do PBE supply oxygen?

A

15 minutes

126
Q

How many minutes does a rechargeable flashlight last?

A

45 minutes

127
Q

How many rechargable flashlights do we have?

A

Four

128
Q

How long does the ELT transmit a distress signal?

A

72 hours

129
Q

How long will the batteries last if they have to power the entire electrical system?

A

10 to 20 minutes

130
Q

Where are the main batteries located?

A

On the left side of the nose

131
Q

Maximum battery temperature

A

70 C

132
Q

Thermal runaway can occur when the battery temperature drops below

A

-20 C

133
Q

Battery 1 is connected to which generators

A

1 and 3

134
Q

Maintenance is required on the batteries when they go below:

A

19 Volts

135
Q

APU starter generator is rated at how many amps?

A

Above 30,000 - 300
Below 30,000 - 400

136
Q

DC bus powers what?

A

Essential buses
Shed buses
Avionic buses
AC Inverter

137
Q

DC bus is powered by what?

A

DC bus 1 - battery 1 and generators 1 / 3
DC bus 2 - battery 2 and generators 2 / 4

138
Q

What does the Central bus do?

A

Takes power FROM the APU / GPU and battery 2
TO the rest of the electrical system
Also connects both electrical networks

139
Q

Hot bus is always powered by:

A

The batteries
(3 per battery)

140
Q

Shed buses power what?

A

Nose landing light
Taxi lights
Recirculation fan
Galley power
Rechargable flashlight
Windshield 2 heat

141
Q

Ground Service Bus powers what?

A

Cabin lights
Lavatory
Galley
Courtesy lights
Dome light
Baggage lights

142
Q

APU generator is available when:

A

APU RPM is above 95% for 7 seconds

143
Q

In order for the thrust reversers to activate, you need:

A

Wheel speeds greater than 25 knots
OR
Ground signal from the nose gear

144
Q

Minimum acceptable oil quantities:

A

Before Pushback: 8 qts
Before Takeoff: 6 qts

145
Q

Minimum oil temperature to start the engine

A

-40 C

146
Q

To increase N2 above 83%, oil temperature must be at least

A

40 C
OR
has been running for at least 8 minutes

147
Q

Minimum and Maximum Oil Pressure Limits

A

34 to 110 psi

148
Q

What does APU bleed do?

A

Provides bleed air to operate ATS for engine starting
Run the two Environmental Control Units for AC when engine bleed air is not available

149
Q

APU will initiate an automatic shutdown when rotor speed reaches

A

104%

150
Q

APU receives fuel from which fuel tank?

A

Right Wing Tank

JSX Oral Prep (1 decks)

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