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145 > 145 CAE > Flashcards

145 CAE Flashcards

1
Q

How many fans are there in the air conditioning system

A

TWO RECIRCULATING FANS AND ONE GASPER FAN

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2
Q

The ECU’s normally distribute conditioned air as follows

A

LEFT SYSTEM TO THE COCKPIT AND CABIN, RIGHT SYSTEM TO CABIN.

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3
Q

In manual mode the electro pneumatic outflow valve

A

IS KEPT CLOSED

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4
Q

When the co-pilots side window is not properly locked

A

A YELLOW PIN PROTRUDES NEAR THE OPENING HANDLE

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5
Q

If the door BLOCKED inscription is showing

A

IT SHOULD BE CLARDE BY OPERATION OF THE ALTERNATIVE OPENING VALVE

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6
Q

What controls the APU

A

AN ESU/FADEC

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7
Q

What is true regarding the APU:

A

NORMAL APU INDICATIONS AND CAUTION/WARNING MESSAGES ARE PRESENTED ON EICAS

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8
Q

The aural warning “Auto-pilot” will occur

A

AT ANYALTITUDE BUT IS SELF-CANCELLING ABOVE 25,000 FT

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9
Q

The Go-around mode is:

A

BOTH VERTICAL AND LATERAL

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10
Q

The vertical default mode is

A

PITCH HOLD MODE

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11
Q

Which types of approach may b made using the navigation back-up page of the RMU:

A

ADF, RAW DATA VOR, RAW DATA LOC, RAW DATA ILS

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12
Q

The RMU page menu includes:

A

1 BACK UP NAVIGATION PAGE AND 2 ENGINE BACK UP PAGES

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13
Q

How are the AHRS powered

A

NO.1 AHRS BY THE NO.1 ESS BUS. NO.2 AHRS BY THE NO.2 DC BUS

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14
Q

to erase the CVR you have to be on the ground and

A

THE PARKING BRAKE MUST BE APPLIED

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15
Q

Battery overtemp is indicated on the:

A

ON THE MFD ELEC PAGE AND THE EICAS

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16
Q

The EICAS message APU GEN OVLD indicates

A

APU GENERATOR CURRENT IS ABOVE 400A

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17
Q

What is the purpose of the essential power switch:

A

ALLOWS MANUAL CONNECTION OF ESSENTIAL BUSSES IF THEY FAIL TO CONNECT AUTOMATICALLY DURING AN ELECTRICAL EMERGENCY

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18
Q

The ELT can be activated

A

AUTOMATICALLY OR MANUAL;Y VIA REMOTE PANEL IN COCKPIT OR VIA TRANSMITTER ON/OFF SWITHC

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19
Q

With how many escape straps ropes in the EMB 135/145 equipped

A

2, ONLY IN THE COCKPIT

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20
Q

The PMA has sufficient power for ignition and for powering the FADECS at N2 of

A

10% IGNITION & 50% FADEC.

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21
Q

The fuel system contains a FCOC. what is its purpose in term of the fuel

A

HEATS THE FUEL BEFORE IT GOES THROUG THE FILTER.

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22
Q

How are the engine started normally:

A

AIR TURBINE STARTER SUPPLIED BY APU, GROUND AIR OR CROSS BLEED

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23
Q

Compressor bleed air are available for aircraft use at which stages 9th and 14th. Pulling an engine fire handle

A

SHUTS OFF FUEL, HYDRAULICS, BLEED AIR AND THE ENGINE ANTI ICE BLEED.

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24
Q

As a part of the automatic shut off system rudder hard over protection function selects mechanical reversion dependent upon

A

Pedal input forces, rudder deflection and aircraft engine operation

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25
Q

why is ADC information provided to the HSCU’s

A

IN ORDER THAT TRIMMING RATE CAN BE VARIED DEPENDING ON AIRSPEED.

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26
Q

Will the stick pusher work if there is a disconnection of the elevator systems, with a jam in the left side

A

NO.

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27
Q

Which hydraulic system provides actuation of the ailerons

A

BOTH

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28
Q

Ground spoilers are enabled when

A

WOW, WHEEL SPEED ABOVE 25 KNOTS, TLA<30

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29
Q

THE ATTITUD AND HEADING INFRMATION ON THE PFD IS SUPPLIES

A

BY THE AHRS

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30
Q

The airspeed trend vector is an indication of the acceleration direction and it represents the airspeed which the aircraft would attain in:

A

10 SECONDS

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31
Q

When will the Flight data Recorder operate without any pilot selection

A

WHEN THE AIRCRAAFT BECOMS AIRBORN.

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32
Q

After a total loss of electrical power to the SBY attitude indicator, how many minutes of useful attitude information can you expect to get:

A
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33
Q

What is the purpose of the Collector Box:

A

PROVIDES A MEAN OF KEEPING THE ELECTRICAL PUMPS SUBMERGD AT LOW FUEL LEVELS

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34
Q

During a fuel crossfeed operation:

A

The crossfeed switch should be selected to the lower side

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35
Q

What is required for a takeoff or a go-around:

A

AT LEAST ONE ELECTRIC FUEL PUMP FOR EACH ENGINE AND THE APU

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36
Q

INDICATIONS OF HYTDRAULIC SYSTEM STATUS APPEAR ON THE

A

MFD AND SHOW QUANTITY, PRESSURE AND ELECTRIC PUMP STATUS

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37
Q

The electric pumps of both systems are located in the main hydraulics compartments. they deliver fluid at a pressure of

A

2900 PSI

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38
Q

The Hydraulic reservoirs have a capacity of:

A

6 LITERS

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39
Q

In automatic mod the pitot and static heating is applied:

A

WHENEVER AL LEAST ONE ENGINE IS RUNNING

40
Q

With the ice protection OVERRIDE switch set at ENG

A

Engine anti-ice is provided at all times on the ground and in flight.

41
Q

With the aircraft stationary at the holding point and the ice-detection override switch set to ALL

A

ONLY ENGINE ANTI-ICE WILL BE ON.

42
Q

What item is provided in the L/G system to prevent retraction on the ground:

A

A BAULK INSIDE THE LANDING GEAR HANDLE REMOVED BY A SOLENOID IN FLIGHT

43
Q

Which unit provides signals to the landing gear electro-valve

A

THE LGEU.

44
Q

The indication of a landing leg position disagreement is:

A

HATCHED RED AND BLACK INDICATION OR RED LAEL UP OR DN IN RED BOX

45
Q

How is the parking brake applied

A

PRESS PEDALS, WHILST PRESSED PULL UP AND ROTATE HANDLE 90 DEG

46
Q

The batteries supply all emergenci lights approximately for

A

15 MINUTES

47
Q

If the navigation light is U/S:

A

A BACK UP NAV LIGHT CAN BE MANUALLY SELECTED ON THE MAINTENANCE PANEL

48
Q

The oxygen generator is activated

A

WHEN ANY MASK IN THE ASSOCIATED SIPENSING UNIT HS PULLED DOWN

49
Q

The cylinder is protected from over pressurization by a safety disk set to rupture at high psi. if the safety disk has ruptured it can be visually verified from the outside. The disk charge indicator is normally

A

GREEN

50
Q

After failure of the IC-600-2:

A

THE RH PILOT’S INFORMATION WHULD BE RESTORDE AFTER REVERSIONAY SWITCHING

51
Q

What is the power source for the LH PFD

A

NO.1 DC BUS.

52
Q

A number of EICAS messages are inhibited during take-off. The inhibition starts at V1-15Kts and finishes at

A

400 FT RADIO ALTITUDE

53
Q

What is the maximum take-off and landing tailwind components

A

10KT

54
Q

What is the turbulant Air Penetration Speed at or below 10,000 ft:

A

200KT

55
Q

What is the Maximum Landing Mass of the Embraer 145?:

A

18,700KG STD/ 19,300Kg LR

56
Q

What is the maximum start altitude of the Auxiliary Power Unit (APU)?:

A

30,000FT

57
Q

What is the reference temperature, at or below which, pilot should to set the Ice Detection override knob to the ENG position in case of visible moisture

A

:+10 deg. celsius

58
Q

What is the maximum permitted fuel imbalance

A

363 Kg(800lbs)

59
Q

What is the minimum engagement height of the Auto Pilot

A

1,000 Ft

60
Q

What is the minimum engine oil temperature in order to be able to increase N2 above 83% (warm up)?

A

40 deg

61
Q

What is the maximum time limit with vibration in the amber range below 25 IPS LP/SP spool during T/O or G/A ?:

A

5 minutes

62
Q

What is the Maximum speed for flaps 22 extension?

A

200 KIAS

63
Q

What is teh maximum airspeed for landing gear extension (VLE)?:

A

250 KIAS

64
Q

What is the maximum speed for operating the windshield wipes?:

A

170 KIAS

65
Q

What is the APU starter liimit between three consecutive attempts?:

A

1 MINUTE

66
Q

What is the maximum EGT when starting the APU?:

A

884 deg

67
Q

What is the maximum battery temperature?:

A

70 deg

68
Q

What is the maximum airspeed at 10,000 ft?:

A

320 Kt

69
Q

What is the Go-around thrust setting limit?

A

5 min

70
Q

What is the Take Off thrust setting time limit?

A

5 min

71
Q

What is the maximum permissable thrust setting for T/O named

A

T/O-1

72
Q

How will AFT CG compared to FWD CG affect your margin vs Stall Speed

A

Increase margin

73
Q

A continous bell rings together with an EICAS warning message and FIRE message and FIRE
warning light on the No.1 Engine Fire Handle. What are the RECALL items

A

No.1 Thrust lever - IDLE, .1 No.1 Start/Stop Selector - STOP, No.1 Fire extinguisher Handle - PULL (DO NOT ROTATE).

74
Q

What is the memory Items for a Steering Runaway

A

Steer Diseng Button - PRESS

75
Q

The correct drill for an Engine Hot Start is

A

Start/Stop selector to STOP

76
Q

During takeoff and below V1 an EICAS message E1 (2) LOW N1 appears. What is your immediate action?

A

Reject Takeoff Procedure - ACCOMPLISH

77
Q

Where in the QRH is the Emergency Evacuation procedure located?:

A

The last page of the QRH

78
Q

During takeoff an EICAS warning comes up: ATTCS FAIL what is the recall item?:

A

Thrust Levers - MAX

79
Q

When airborne, what are the initial actions following a “WINDSHEAR” warning?:

A

MAX THRUST, Press TOGA: follow FD pitch demand

80
Q

What are the immediate actions for a pitch ranaway?

A

Quick disc button - PRESS AND HOLD

81
Q

The dark and quiet cockpit principle assumes that when in flight with systems normal:

A

Panel have no lights on, no aural warnings, selector knobs positioned 12 o’clock.

82
Q

On the EICAS display there is an arrow pointing down with numbers next to it. What does this signify?:

A

There are more than 15 messages on the screen. to read them select cursor to the EICAS then using the message scroll either up or down

83
Q

The handling pilots PFD has failed, how can the display be regained

A

The handling pilot will have to revert manually using he reversionary panel

84
Q

About what Calibrated Airspeed (CAS) will the “AIRSPEED ROLLING DIGITS” be displayed?

A

40 Kts

85
Q

Airspeed on the current airspeed displayed in amber signify?

A

A trend vector exeeds VMO/MMO.

86
Q

A amber MSG label is displayed on the PFD. What does it signify?:

A

There is message available on the FMS panel

87
Q

If the pilot airspeed indication fails

A

The indicator in error is removed and a red X superimposed in place

88
Q

what is true regarding the caution messages on the EICAS

A

Follows warning messages in criticality level and in display

89
Q

In which data base is pilot entered waypoints stored? :

A

Custom Data

90
Q

When is an active flight plan considered closed

A

The last waypoint is the destination

91
Q

The NAV data base is updated every

A

28 Days

92
Q

If position information is lost from all sensors or inhibited how will the FMS system react

A

The FMS will go into DR mode using AHRS/IRS heading and airspeed and wind data.

93
Q

To select FMS as navigation source on the PFD and MFD you have to press

A

The FMS button on the Display Control Panel

94
Q

On the PFD FMA which of the following represents the correct color code for normal operation?

A

Magenta - FMS Mode, White - Armed mode

95
Q

What is the ocntrol interfae between the FMS and the pilot?

A

The CDU

96
Q

FMS position information uses the most accurate sensors available. what is the sensor order of priority

A

GPS, DME/DME, IRS

145 (1 decks)

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