Required Knowledge Areas Flashcards

1
Q
  • Prior to take off and landing the main air valves must
A

Must be closed

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2
Q
  • Abnormal annunciators that indicate a fault condition
A

Are yellow

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3
Q
  • To ease isolation in event of smoke or fire, CBs that provide protection for un switched PE circuits
A

Are labeled with a white square background

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4
Q
  • Lower Static vents
A

Have no electrical heating

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5
Q
  • Emergency escape hatch
A

is fourth window on right side

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6
Q

Max nose wheel angle

A

45 Degrees each side

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7
Q
  • What is a caution
A

an operating procedure that could result in damage to equipment if not carefully followed

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8
Q
  • What is a warning
A

– Could result In loss of life if not carefully followed

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9
Q
  • How do you manually disconnect gen from its bus
A

Switch GEN switch to trip then release

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10
Q
  • What opens both battery contactors when starting
A

– depressing either end 1 or 2 green operating buttons

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11
Q
  • BATT 1 or 2 CNTCTR
A

indicates either emergency contactor or battery contactor is open

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12
Q

Placing battery switch to EMERG does what

A

provides power to No 1 and 2 batteries to close both emergency contactors

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13
Q
  • When powered from PS1 and PS2 bus, the inverters 1 and 2
A

produce 115 VAC at 400hz

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14
Q
  • A and B windshield panels and stall vanes are heated by what
A

eng driven alternators that produce 208v three phase, wild frequency power

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15
Q
  • What is normal battery voltage
A

24 DC

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16
Q
  • What happens when you press either BATT ISOLATE switch
A

either BATT 1 or BATT 2’s contactor will open

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17
Q
  • Bus voltages under 24.5 and above 29.5 will
A

automatically open the bus tie when both gens are powering the bus system and bus tie is closed

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18
Q
  • When does NO SMOKING come on automatically
A

when in AUTO and the nose landing gear locks down

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19
Q
  • The entry light switch controls
A

Main entrance door lighting and powered by battery No.1

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20
Q
  • Red annunciator
A

indicates hazardous fault condition that requires immediate action

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21
Q
  • What bus powers master warning system
A

PE

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22
Q
  • 7 master warning annunciators have arrows that point to overhead panel, which one does not point
A

– DUCT OVHT, it points to a guage

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23
Q
  • White annunciators
A

Provide an advisory or system status indication

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24
Q
  • How many water drains
A

5

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25
Q
  • When does ventral tank transfer valve open
A

when AUX fuel transfer lever is placed to transfer

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26
Q
  • Left and right wing tanks
A

– have electric boost pumps

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27
Q
  • What does the surg tank NACA anti ice ram air assembly provide
A

positive pressure for vent system in flight

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28
Q
  • The PE bus bar provides power when left and right boost pump switches
A

are in EMER

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29
Q
  • PS1 and 2 bus bars provide power when left and right boost pump switches are
A

Are ON

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30
Q
  • What do the wing tank fuel boost pumps use to pull fuel into their no. 1 compartment
A

Use jet pump action

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31
Q
  • Where is the maintenance panel that includes an oil bypass indicator
A

Rear equipment bay next to hydraulic accumulators

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32
Q
  • What does the IGN ON mean
A

– Power is available to the ignition unit, this also comes on when HP cock is moved to the on position

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33
Q
  • What provides engine cranking
A

Starter Generator

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34
Q
  • Mechanical governor provides overspeed protection at
A

105% n2

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35
Q
  • What eng does the 900xp have
A

TFE-731-50R-1H

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36
Q
  • What are the two APR control switches
A

APR OVRD and APR ARM

37
Q
  • If the eng computer has failed, what happens to the surge bleed valve
A

will default to the 1/3 OPEN position

38
Q
  • What happens if there is an APU fire
A

APU fire extinguisher will automatically discharge

39
Q
  • What is max gen load for the APU
A

.8

40
Q
  • How long can you engage the APU starter
A

No more than 30 seconds

41
Q
  • APU is provided fuel from which tank
A

Left

42
Q
  • What does the fire extinguisher switch do on the APU panel
A

Discharge a separate fire extinguisher into APU shroud

43
Q
  • What provides electrical power for shot 1
A

PE

44
Q
  • What provides electrical power for shot 2
A

PS2

45
Q
  • Which Shot do you fire first
A

1 then 2

46
Q
  • Where are the 3 smoke detector
A

Forward baggage, aft baggage, and lav vanity

47
Q
  • How many lights does the fire detection test illuminate
A

– 6 or 7 and a bell

48
Q
  • What happens when you switch main air valve to LP ON
A

valve will open but HP air will not happen

49
Q
  • Do the main air valves have to be on for the no 1 and 2 bleed air to work with the rudder bias
A

NO

50
Q
  • What happens when you switch main air valve to Open
A

HP air supplements LP air in mixing valve

51
Q
  • What happens when HP AIR 1 or 2 OVHT comes on
A

If the mixing valve that mixes HP air with LP air fails to open

52
Q
  • ADC 1 may fail to operate properly if
A

Left pitot heat is inoperative

53
Q
  • How long can you use the engine anti ice above 10c
A

10 seconds

54
Q
  • How long does the Tks give you ice protection for if full
A

108 Mins

55
Q
  • If the right pitot heat is inoperative what might happen
A

ADC 2 and the standby airspeed indicator may fail

56
Q
  • How do you heat the stall vane
A

PITOT/STALL VANE HEAT switch

57
Q
  • What controls cabin air temp
A

– cabin temp control valve

58
Q
  • What powers the CABIN TEMP MANUAL mode
A

PE

59
Q
  • What happens when there is too much bleed air present in the AC
A

a 40 psi press switch closes no 2 main air valve to protect ACM from overseeding

60
Q
  • What happens when you have a duct temperature of about 115c
A

the duct limiter automatically gives partial reduction in temp and illuminates the DUCT OVHT

61
Q
  • What operates the auto controller
A

– a cabin air venturi, which is on the forward right hand side of the fuselage behind baggage compartment

62
Q
  • How can the pilot provide emer pressuriziation
A

positioning F/DK VLV to open

63
Q
  • What is suction to the outflow valves powered by
A

fan operated venturi which is powered by XS2

64
Q
  • What happens when you lose both hydraulic eng driven pumps and all accumulators are working properly
A

Both HYD LO PRESS annunciators will illuminate and pressure will indicate 2300 psi

65
Q

Can 1 eng hydraulic pump acuate all systems?

A

yes

66
Q
  • What happens is just one hydraulic pump fails
A

HYD LO PRESS will illuminate and pressure will indicate 3000 psi

67
Q
  • What does the auxiliary hydraulic system do
A

– it is an alternative source of hydraulic pressure for emergency extension of the gear and flaps

68
Q
  • Backup pressure for the brakes is provided by what
A

emergency accumulator

69
Q
  • Why is the air pressurized in the reservoir
A

To prevent pump cavitation

70
Q
  • What happens to the brakes and stick pusher if both pumps fail
A

the main accumulator will provide pressure for normal brakes with anti skid and stick pusher

71
Q

Without hydraulic pressure, what if the emergency brake accumulator charged with

A

1000 psi of nitrogen

72
Q
  • Without hydraulic pressure, the thrust reverser accumulator is charged with
A

1500 psi of nitrogen

73
Q
  • What happens when you have 3 green and 3 red lights
A

– landing gear down and locked with gear lever in up position

74
Q
  • What stops inadvertent retraction of the gear on the ground
A

solenoid locking mechanism

75
Q
  • What happens to the gear inboard door when the gear is either retracted or extended
A

it is closed

76
Q
  • No green and no red indicate what
A

that the gear is up and locked and the gear doors are closed

77
Q
  • When you apply takeoff power and you see ELEV/AIL TRIM ann
A

– indicates the elevator trim is more than one unit from center

78
Q
  • What do you need in order to use Lift dump
A

Flaps 45

79
Q
  • What heats the rudder bias heater muffs
A

PITOT/VANE HEAT switches provide DC power

80
Q
  • What heats the upper static plates
A

PITOT/VANE HEAT and its PS2

81
Q
  • Where are the engine instruments displayed
A

normally on the captains MFD

82
Q
  • Where are the fuel indications displayed
A

normally on the co pilots MFD

83
Q
  • How do you allow oxygen to flow to the contents indicator and pressure regulator
A

turn on master supply valve

84
Q
  • How do you isolate oxygen supply to the cabin drop down masks
A

close passenger supply valve

85
Q
  • What does a red indication mean on an eng indicator
A

– A max or min eng limit has been exceeded

86
Q
  • Thrust in excess of reverse idle must not be selected below speed of ____ except in emergency
A

50 kts

87
Q
  • How long is maximum takeoff thrust limited to
A

5 mins

88
Q
  • How long will the batteries last if all generators are shut down –
A

30 mins

89
Q
  • What will you see if there is an APU fire
A

APU FIRE on apu panel, MWS APU FIRE annunciator, and fire bell