Oral Prep Questions (1/30/2018) Flashcards

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1
Q

How many engine fire extinguishers are they and where are they located?

A

2, in the tail cone

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2
Q

How much does a motorized mobility unit weigh?

A

100 Lbs

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3
Q

When will you not get a stick pusher?

A
Above 200knots
Below 200’
Quick Disconnect Button Pushed
1 Channel inop
On th ground 
Less than .5 G
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4
Q

DAU 1 takes info from?

A

Engine 1, and forward A/C Systems

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5
Q

How much does a Segway weigh?

A

193 Lbs

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6
Q

How much does a non motorized mobility unit weigh?

A

60 Lbs

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7
Q

How many fire extinguishers are there for the APU and where are they located?

A

1, tail one

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8
Q

Maximum Standing Water on runway?

A

1/2 an inch

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9
Q

What Gas senses overheating?

A

Helium

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10
Q

How many motors are controlled by pitch trim?

A

2

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11
Q

What busses are powered in an electrical emergency?

A

The essential bus

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12
Q

What must be considered when shooting an approach with 3/4 mile visibility or 4000 RVR?

A

Add 15% to the min. Required runway length, all weather markings on runway, or Centerline lights

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13
Q

Maximum amount of slush?

A

1/2 inch

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14
Q

What do you add to your alternate airport’s minimums with 2 approaches?

A

200’, 1/2 mile

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15
Q

What is inhibition logic for take-off?

A

V1-15 Knots
Below 400’
Wheel speed less than 60knots
1 Minute after wheels up

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16
Q

How are the emergency lights powered?

A

4 Dedicated Batteries for 15 Minutes

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17
Q

What happens if 1 flap motor fails?

A

Flaps lower at half speed

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18
Q

A/C Height

A

22’ 2”

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19
Q

What is the purpose of the collector box?

A

To keep the fuel pumps submerged in fuel.

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20
Q

Components of the stall protection System

A

2 AOA vanes
One Computer with 2channels
One stick Pusher
2 Stick Shakers

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21
Q

What is a rudder hardover?

A

Uncommanded deflection of the rudder

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22
Q

What happens if their is flap asymmetry?

A

Both flaps stop working. EICAS flap position will read actual angle of flaps at their failed position

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23
Q

Aircraft Length

A

98’

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24
Q

When will you get a low fuel indication?

A

Below 500lbs

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25
Q

When do we do an anti-ice take off?

A

When temperature is below 10°C with visible moisture and the ceiling is below 1500’ AGL

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26
Q

When so the remaining pumps begin cycling?

A

When fuel pressure in the

One drops below 6.5 PSI

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27
Q

Approaches that cannot use the “APP “ Button on the flight guidance controller

A

RNAV, ILS OTS, Circle to land

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28
Q

When do we anti-ice?

A

When you want to prevent ice from adhering to the Aircraft

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29
Q

What Busses power the fire extinguishing of both Engines?

A

The Hot Batteries

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30
Q

How are flaps powered?

A

Electrically

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31
Q

How long does it take to depressurization the door when locked?

A

2 Minutes

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32
Q

When will you get a take off configuration warning?

A

With TLA above 60%

Flaps not in take off position
Parking Brake On
Pitch Trim
Spoilers open

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33
Q

At 37,000’, if you press Dump in the automatic mode of pressurization what happens? Manual?

A

Automatic Mode= dumps cabin to 14,500’ +/- 500’

Manual Mode= Nothing happens

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34
Q

How is Ram air used?

A

Ram air is used to flow over the primary and secondary heat exchangers to keep them cool. In the event of a dual pack failure, the ram air will enter the cabin bypassing the packs.

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35
Q

What ensures there is fuel in the collector box at all times?

A

Ejector Pumps and Flap valves

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36
Q

3 ways to get wind shear escape guidance

A

1) Manually= Pressing the Go Around Buttons in Windshear
2) Automatically = when encountering windshear in T/O GA Mode
3) Automatically= with TLA above 78% and decreasing performance

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37
Q

A/C Width

A

LR/LR2= 65’ 9”

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38
Q

Hat does the DC Electrical System Consist of?

A
4 Generators
APU Starter Generator
2 NiCad Batteries
1 Lead Acid Battery
GPU
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39
Q

When does your holdover time start?

A

As soon as application of De icing/anti icing fluid begins

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40
Q

How many pitch trim motors are working at the same time?

A

1

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41
Q

What is a rudder overboost?

A

When above 135 Knots, both hydraulic systems going to the rudder remain active. HS1 did not shut down.

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42
Q

Can you use alt-t/o 1 thrust on a wet runway?

A

Yes

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43
Q

Maximum amount of Dry snow on the runway?

A

2 Inches

44
Q

What Bus powers APU fire extinguishing?

A

Essential 2

45
Q
Which Bus is IC-600 #1 on?
#2?
A

Essential 1.

DC2

46
Q

When do the No Smoking Signs/ Seatbelt Signs come on automatically?

A

Sudden Cabin depressurization above 14,000’

47
Q

How many motors do the flaps have?

A

2

48
Q

What is required for 6/6/6 Take off

A

High intensity runway lights and center

Line lights

49
Q

What Powers the Engine 1, Engine 2, APU fire detection?

A

ENG1= Essential 1

ENG2 &APU= Essential 2

50
Q

What Doors or Hatches are pressurized?

A
Under Cockpit Hatch
Main Cabin Door
Service Door
Overwing Exits
Rear Electronic Compartment
51
Q

Explain Baggage smoke detection

A

2 smoke detectors detect smoke
Fan stops
Bag ext. light illuminates
Bag smoke EICAS Message appears
——————-
When button is pressed, 2 bottles are deployed.
1 Immediate discharge, 1 metered discharge to last for 50 Minutes

52
Q

How is pressure refueling powered when aircraft is :

Powered
Unpowered

A

Powered: DC1
Unpowered: a Hot Bus

53
Q

What is the IC-600?

A

The Symbol Generator

54
Q

How are the electric fuel pumps powered?

A
A= on side Essential
B= opposite side Essential
C= on side DC
55
Q

What gas senses high intensity heat ( fire)

A

Hydrogen

56
Q

How does the FMS get it’s positioning?

A

GPS, DME to DME, VOR DME, IRS if installed

57
Q

What are circling minimums?

A

1,000’ ceiling, 3 mile visibility

58
Q

Hat does windshear escape guidance do?

A

Prevents Stalling, Descending, and Overspeeding (in that order)

59
Q

When does the anti-icing equipment turn off again?

A

After the 60 second cycle, it will remain off unless icing conditions exist

60
Q

What do the packs do and where do they get air from?

A

Packs provide pressurization and air conditioning to the cabin. They receive their air either from APU or Engine bleed air.

61
Q

What happens when the fir detect button test is pressed?

A

Audible bells
Lighted T Handles and Bag Smoke Light
Warning and caution lights on dash light up

EICAS Messages:

ENG FIRE1
ENG FIRE2
APU FIRE
ENG1 FIRE DETECT FAIL
ENG2 FIRE DETECT FAIL
62
Q

When do we de-ice?

A

When Ice has collected on the aircraft and we need to remove it to provide a clean surface

63
Q

What do the batteries do during an APU Start?

A

Battery 1= Provides stead power to Sensitive Systems

Battery 2= Start Power for the APU

64
Q

Is Type one fluid heated? Type 4?

A

Type 1= yes

Type 4= no

65
Q

Explain the IC-600 Built in Tests

A

Power up
Continuous
Pilot-initiated

66
Q

What do you add to your alternate airport’s minimums with 1 approach?

A

400’, 1 mile visibility

67
Q

What indications do you get in the cockpit that you’re collecting ice?

A

When Ice is detected by the ice detectors, an EICAS message is displayed and the anti-icing system will activate by using bleed air to head the surfaces for 60 seconds. If the ice detectors do nor continue to detect ice after 60 seconds, the anti-icing system will deactivate.

68
Q

LAHSO on a wet runway

A

Prohibited

69
Q

Minimum ceiling and visibility for LAHSO

A

1,000’ ceiling and 3 mile visibility if PAPI or VASI is available

70
Q

Is LAHSO Authorized if windhshear has been reported within 20 Minutes?

A

No

71
Q

LAHSO limitation for tailwind

A

3 knots

72
Q

Are RVR Reports required for CAT II?

A

No, but if available, reports are controlling

TDZ = 1200 RVR
MID= 600
Rollout= 300
73
Q

Lowest RVR to shoot a CATII Approach with only TDZ RVR

A

1600 RVR

74
Q

Required lighting for CATII

A

HIRL, TDZ Lighting, CL lights, ALSF-1 or-2

75
Q

Minimum Runway requirements for a 600/600/600

A

HIRL and CL lights

76
Q

When do you need a take off alternate?

A

When weather at Departure airport is below CAT 1 Minimums

77
Q

Standard Mins for take off for aircraft with 2 Engines or less

A

1SM or 5000 RVR

78
Q

What is the definition of marginal weather?

A

Ceiling of less than 1000’ OR Visibility of less than 3 Miles at Destination
——-AND———

Ceiling less than 600’ OR Visibility less than 2 miles at the alternate

79
Q

When do you need a SECOND Alternate?

A

Any time weather at destination and 1st alternate meet definition of marginal weather

80
Q

How do you calculate Bingo Fuel

A

Total Flight Plan Burn - Fuel Used + Alternate + Reserve = Bingo

81
Q

Landing Inhibition

A

200’ RA
WOW+ 3 seconds
1 Minute on the ground

82
Q

Anti-Ice ON Flight Idle Rescheduling Inhibition

A

Gear Down and Locked below 15,000’

83
Q

What do the T Handles shut off?

A

Hydraulics
Bleed Air
Lip Anti Ice
Fuel

84
Q

When does 14th stage bleed open?

A

Low Thrust
Anti-Aging
Cross Bleed

85
Q

Brake wheel protection

A

< 10 Knots Wheel Speed

Wheel Speed above 30 knots

Touchdown
------------------
WOW + 3 Seconds
OR 
Wheel Speed 50 knots
(Prevents Landing with Brakes on)
86
Q

PMA Provides power for

A

FADEC (Below 50% N2)

Igniters

87
Q

When do BOTH Igniters lite automatically?

A

In flight engine start

Engine Failure in flight (N2 drops less than 56.4%)

88
Q

What’s on the Accessory Gear Box

A
Fuel
Pma
Hydraulic Pump
Oil Pump
Generators
Starter (Air Turbine Starter)
89
Q

Weight on wheels operate at…

A

WOW & Wheel Speed 25knts

MLG & NLG WOW and Thrust levers idle.

90
Q

What Instruments are powered by 115 V AC

A

EGPWS

Windshear

91
Q

What EICAS Messages appear during an Ice test

A

ICE DET 1/2 Fail
BLD 1/2 Low Temp
Ice Condition
CROSS BLD OPEN

92
Q

How is the elevator powered

A

Mechanically

93
Q

How are the ailerons powered

A

Mechanical with hydraulic assist

94
Q

How is the rudder powered?

A

Hydraulically with mechanical reversion

95
Q

How is rudder hardcover protection activated

A

Rudder Deflection > 5° in one direction
> 130 Lbs of force on opposite rudder pedal
Both engines running >56.4%

96
Q

What powers the Parking/ Energency Brake?

A

2 Accumulator

97
Q

How many uses of the brake do you get from the Accumulator?

A

6 Applications

24 Hours of Parking Brake Pressure.

98
Q

What is the Engine Start Sequence

A

Ignition on at 15% N2
Oil Pressure Rising
Fuel Flow (28.5%)
Light Off (ITT Rising within 10 seconds of fuel flow)
Ignition Out (56%)
Oil Pressure ( at least 34 PSI after idle)

99
Q

At what N2 speed does the PMA provide power to the igniters?

A

10%

100
Q

What Powers the Fadec?

A

Below 50% DC Essential

Above 50% PMA

101
Q

How long does it take to charge the Emergency Lights?

A

15 minutes

102
Q

What does the PMA power?

A

Ignition, FADEC, Thrust Levers, Thrust Rating Buttons

103
Q

Why do we have a priority valve for HS1?

A

Flight Controls

104
Q

Which Screens run on essential power? (Electrical Emergency)

A

Eicas and Both RMUs

105
Q

If you have to make a quick return to the airport, do you need to de pressurize the cabin?

A

No, you have 15 minutes.

106
Q

If you have Amber Dashes, what failed?

A

DAU