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175 LIMITATIONS > 175 GROUND SCHOOL > Flashcards

175 GROUND SCHOOL Flashcards

1
Q

DVDR TEST IS GOOD TEST?

A

NO FAIL MSGE ON EICAS

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2
Q

WHAT TEST BEGINS WHEN AC POWER IS APPLIED?

A

E-PBIT

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3
Q

HOW DO YOU KNOW P-BIT TEST IS RUNNIG?

A

FLT CONTROL TEST IN PROGRESS STATUS MSG.

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4
Q

HOW LONG DOES E-PBIT TEST TAKE

A

3 MIN

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5
Q

WHAT DOES E PBIT CHECK

A

DETECT OUT OF TOLERANCE DON AND FAILURES IN THE FCMS, P-ACE AND SF-ACE

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6
Q

WHAT INTERRUPTS THE E PBIT TEST?

A

AC POWER INTERRUPTION
FLIGHT MODE SWITCH CYCLED
HYD PUMPS ON

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7
Q

WHAT TEST BEGINS ALL THREE HYD SYSTEMS ARE PRESSURIZED?

A

H-PBIT

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8
Q

HOW DO WE KNOW IT IS RUNNING

A

FLT CTRL TES IN PROG STATUS MSG

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9
Q

HOW LONG TAKE TO COMPLETE

A

1 MIN

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10
Q

WHAT DOES H-PBIT CHECK

A

FUNCTIONAL TEST OF FLT CONTROL ACTUATORS

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11
Q

WHAT INTERRUPTS H-PBIT TEST?

A

MOVEMENT OF FLT CONTROLS

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12
Q

ALL FLT CONTROLS EXCEPT AILERONS ARE?

A

FBW

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13
Q

EXPLAIN SIGNAL PATH FROM CONTOL COLUM TO ELEVATOR IN NORMAL MODE?

A

YOKE TO PACE TO FCM TO ACTUATOR

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14
Q

SIGNAL PATH IN DIRECT MODE

A

YOKE TO P-ACE TO ACTUATOR

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15
Q

WHAT IS PURPOSE OF ACE

A

CONNECT CONTROL COLUMN ELECTRONICALLY TO THE RESPECTIVE CONTROL SURFACE, PROVIDING DIRECT ANALOG CONTROL FO THE SURFCE

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16
Q

PURPOSE OF FCM?

A

PROVIDE SOFTWARE BASED ASSISTANCE TO P-ACE AND IS REQUIRED FOR NORMAL MODE OPERATION OF FLT CONTROL SYSTMS

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17
Q

NAME A FEW IMPORTANT HIGHER LEVEL FUNCTIONS?

A 
AOA LIMITING
AUTO THRUST COMPENSATION 
RUDDER AIRSPEED GAIN 
ROLL SPOILER SCHEDULING WITH AIRSPEED
CONFIG CHANGE COMPENSATION 
ELEVATOR CONTROL LAW SCHEDULING
YAW DAMPER AND COORDINATION VIA AFCS
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18
Q

FLAPS ARE _________ ACTUATED THROUGH THE SF-ACE

A

ELECTRONICALLY THROUGH THE PDUS

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19
Q

WHAT IS THE DIFFERENCE BETWEEN FLAPS 4 AND FLAPS 6

A

4 IS FOR T/O

5 IS FOR LANDING

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20
Q

WHAT FLAP SETTINGS ARE USE FOR T/O LANDING GO AROUND

A

T/O. 1 2 4
LANDING 5 AND FULL
GO AROUND. 5 TO 2. AND FULL TO 4

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21
Q

SPEED BRAKES ARE _____ ACTIVATED AND ______ ACTUATED

A

ELECTRONICALLY ACTIVATED

HYDRAULICALLY ACTUATED

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22
Q

WHAT IS THE DIFFERENCE BETWEEN GROUND SPOILERS AND MULTIFUNCTION SPOILERS?

A

GROUND SPOILERS ONLY DEPLOY ON LANDING

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23
Q

SPEED BRAKES AUTOMATICALLY RETRACT IN FLIGHT

A

AIRSPEED LESS THAN 180
FLAPS 2 OR GREATER
THRUST LEVER ANGE 70 DEGREES

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24
Q

FUNCTIONS OF THE MULTIFUNCTION SPOILERS?

A

ASSIST IN ROLL OF AIRCRAFT
AIRBORNE SPEED BRAKES
GROUND SPOILERS

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25
Q

ALL PILOT TRIM COMMANDS LIMIT OF TILL CUTS OUT

A

3 SEC

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26
Q

WHAT DOES PRESSING SYS1 AND 2 CUT OUT BUTTONS DO?

A

DISABLES HS-ACE

AND TRIM DISC FUNCTION IN THE AP/TRIM DISC BUTTON

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27
Q

WHEN WILL EDP START

A

ENGINE START AUTOMATICALLY

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28
Q

ACMP TURN ON AUTOMATICALLY

A

INFLIGHT:
EDP2 OR ENG2 FAILURE OR
FLAPS GREATER THAN 0

GROUND
FLAPS GREATER THAN 0 AND
THRUST LEVERS T/O OR GROUND SPEED GREATER THAN 50 KTS
DURING T/O THRUST LEVERS TOGA PUMPS RUN FOR 60 SEC

ALSO ENG 1 ON WITH PARKING BRAKE RELEASED. ENG AT 40% N2 AND PARKING BRAKE SET LESS THAN 6 MIN

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29
Q

HYD PUMPS 3 ARE?

A

ELECTRIC

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30
Q

WHEN WILL ACMP 3B TURN ON AUTOMATICALLY?

A

IN FLIGHT IN AUTO WHEN 3 A FAILS

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31
Q

PURPOSE OF PTU

A

ASSISTS IN LANDING GEAR EXTENSION AND RETRACTION SHOUND ENG2 OR EDP2 FAIL

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32
Q

WILL THE PTU RUN ON THE GROUND IN AUTO?

A

NO

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33
Q

WHEN SILL PTU RUN IN FLIGHT IN AUTO?

A

FLAPS NOT SET TO 0 OR
LANDING GEAR NOT UP AND LOCKED
EDP1 NOT FAILED
HYD RESERVOIR ABOVE 12%

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34
Q

WHAT TYPE OF HYDRAULIC PUMPS ARE IN SYSTEM 2

A

EDP
ACMP
PTU

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35
Q

WHAT TYPE OF HYD PUMPS ARE IN SYSTEM 1

A

EDP

ACMP

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36
Q

After starting life engine with APU on what generator will power AC buS 2?

A

APU

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37
Q

What memory aid used to remember the AC electrical power priority?

A

Onside
Inside
Outside
Cross side

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38
Q

Items on HOT BAT BUTS 1 and 2 include?

A

Engine Fire Ext

Pressure refueling Panel

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39
Q

Leaving the GPU button pressed in after being disconnected from AC external power will?

A

Not allow you to re-connect to ground power until first pushing out the button

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40
Q

With non-annunciated aft cargo fire on the ground, how many times do you need to press the AFT cargo button to discharge the low-rate fire bottle?

A

3

41
Q

With an annunciated aft cargo fire in the air, how many time do you need to press the AFT cargo button to discharge the low rate bottle?

A

1

42
Q

Upon aircraft start up, you notice BAT 1 voltage of 20.7 and BAT 2 volt of 23.1. You should?

A

call MX

43
Q

Minimum battery volt for normal operations is?

A

22.5 v

44
Q

Before pressing the fire test button

A

Wait for EICAS to populate

45
Q

Primary purpose of the TRU’s?

A

Convert AC power to DC power

46
Q

Primary purpose of the Invertter

A

Convert DC to AC

47
Q

What areas have fire protection and detection?

A

Engines
APU
Cargo Compartments
Lavatory

48
Q

List Flt Deck emergency Equipment?

A 
Escape rope
Crash Axe
Fire Ext
Life jackets
PBE
Flashlights
Oxygen masks
49
Q

Docs check in plane?

A 
QRC
QRH
Airworthiness
Registration
Radio license
Mx can
50
Q

Turning Batt on and auto what 3 things looking for?

A

Screens 2 and 3 on
IESS align 90 sec
BAT voltage

51
Q

What voltage battery recharge procedure be accomplished?

A

21.0 to 22.5
22.5 your okay
Below 21.0 call Mx

52
Q

Why wait 30 sec after batteries on?

A

fault msg. May be displayed on EICAS

53
Q

List all items that are part of the fire ext panel test?

A

Engines
APU
Cargo

54
Q

How many halon bottles serve engine fire suppression?

A

2 Halon bottles that can be direct into one or both engines

55
Q

Pulling the fire handle does what?

A 
Closes 
Fuel
Hyd
Bleed 
Cross bleed shut off
56
Q

Rotating fire handle does what

A

Counter clock wise fires bottle A

clock wise bottle b

57
Q

How many bottles APU fire suppression?

A

One

58
Q

APU emergency stop do?

A

Closes APU fuel SOV

White striped bar illuminates lower half

59
Q

What button do I press to discharge halon to the APU?

A

APU fire ext push button

60
Q

Will the APU automatically shut down for a fire, if so when?

A

10 sec after fire cond on ground

61
Q

How many fire detectors are in each cargo bin? Smoke detectors?

A

Forward 3

Aft has 2

62
Q

Cargo how many halon bottles?

A

2
One high rate
One low rate

63
Q

Will any cargo bottle automatically discharge at any time?

A

Low rate bottle discharges automatically after high rate?

One minute only in air.

64
Q

How do I discharge the low-rate bottle for a non-annunciated fwd cargo fire on the ground?

A

Depress button 3 times

65
Q

Briefly explain how LAV SMOKE EICAS msg would appear?

A

LAV smoke detector activated

66
Q

Does LAV SMOKE mean the halon bottle has discharged?

A

NO

67
Q

List af few important items on HOT BAT BUS 1 and 2

A

Pressure refueling panel

Fire protection system

68
Q

What type of CB does this plane have and how do I access them?

A

Thermal (Cockpit)
Electronic (SPADAs)
Cockpit for non remote and MCDU for SPDAs electronic

69
Q

Purpose of TRU

A

AC power to DC power

70
Q

Electrical emergency batteries will provide at least

A

10 min of electrical power

22.5 volts

71
Q

RAT purpose

A

Converts kinetic energy to AC power (115, 115 volts, 400 Hz, three phase) power to AC ESS BUS and ESS DC BUS through the ESS TRU. Power ACMP 3A for flight controls.

72
Q

DC GPU can replace _____ for APU Starts

A

Battery 2 only

73
Q

sources of AC Power?

A

IDG 1 and 2
APU GEN
EXT AC
RAT

74
Q

Electrical power priority?

A

Onside
Inside
Outside
Cross side

75
Q

After starting the left engine with APU on what gen will power AC BUS 2

A

APU

76
Q

Which of the following Flt controls are fly by wire?

A

Rudder
Elevator
Flaps

77
Q

Pushing these red guarded buttons does what

A

Inhibits the respective FCM, enabling Direct mode

78
Q

What is purpose of FCM

A

Provide software-based assistance to P-ACE and is required for normal Mode operation of the Flt controls.

79
Q

Speed Brakes/Spoilers are_____ activated and ______ actuated.

A

Electrically

Hydraulically

80
Q

The ERJ 170 has a stick pusher

A

FALSE

81
Q

Primary purpose of PTU?

A

Assist in landing gear extension and retraction in the event of EDP2 or Engine 2 failure.

82
Q

The PTU will automatically start in flight when engine 2 or EDP2 fails and ?

A

Hyd reservoir 2 quantity above 12%
Flaps not set to zero OR landing gear not up and locked. (Coming into land do you need some help)
EDP 1 not failed

83
Q

SE taxi on engine two?

A

ACMP 1 must stay on for taxi

84
Q

SE taxi on engine One?

A

No action necessary

85
Q

When will ACMP 2 turn on with the knob in AUTO

A

In Flt when flaps greater than 0
On GND with flaps greater than 0 and thrust set to TOGA or ground speed greater than 50kt
In flight when either EDP2 fails or engine 2 fails
On the ground when EDP 1 is running and the parking brake is off
On the ground when EDP 1 is running and the parking brake was set less than six min ago

86
Q

ADSP probe should be turned on as per GND school?

A
  1. 0 degrees visibly moisture
  2. ADSP probe visibly contaminated on external inspection.
  3. PFD indicates incorrect information. Ex. 300fpm climb on ground.
87
Q

Audio Control panel should be all what color?

A

Green

88
Q

Manual Manifest what weight is put into MTOW

A

The Higher weight you could use on the Release for your performance on the specific RWY.

89
Q

If the Crew Oxygen is showing CYAN can we still T/O?

A

yes, just can’t take a jump seater

90
Q

The approved weight for an adult Summer time is?

A

190

91
Q

A ticketed bag is entered into the manifest by?

A

Entering the weight of a child for the appropriate season on the “non-standard weight” column to the appropriate zone.

92
Q

In the performance if it says ECS on should the APU be left on or off for T/O?

ECS OFF means APU is?

A

OFF

ON for T/O

93
Q

In Flight the APU will shut down for?

A
  1. Under speed
  2. Fadec critical fault
  3. Over speed
94
Q

On Ground the APU will automatically shut down for?

A
  1. Sensor Failure
  2. High Oil Temp
  3. EGT Over temp
  4. Low Oil Press
  5. Fire
    +
  6. Under speed
  7. Fadec critical fault
  8. Over speed
95
Q

With Battery 1 missing, what is needed to start the APU?

A

APU cannot be started.

96
Q

Where does the APU get fuel from to start?

  1. Batteries Only
  2. AC power available
  3. Both engines running
A
  1. DC pump (right wing)
  2. AC pump (right wing)
  3. Main ejector pump.
97
Q

While powered by DC power only is it possible to view the temperature of the batteries?
Which synoptic page displays battery temp?

A

Must have AC power to see temp

Electrical synoptic page

98
Q

With only the batteries available what fuel pump is powered?
Where is it located in the aircraft?

A

DC fuel pump.

Right fuel tank right wing collector tank.

99
Q

How long IESS to align?

Can the aircraft be moved?

A

90 sec

NO

175 LIMITATIONS (21 decks)

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