GOS

Question 1

highest priority checklist

Answer 1

evacuation

highest chance for loss of life

Question 2

What is a sign of incapacitation

Answer 2

if you ask a question twice with no response

Question 3

AED location

Answer 3

aft overhead left

Question 4

“will carry” hazmat

Answer 4

dry ice
bio substance category B
lithium batteries (with vaccines)

Question 5

engine

Answer 5

Gen electric CF34-8E5

CF commercial fan
34 model number
8E5 embraer

Question 6

Describe N1

Answer 6

single stage (big fan up front)
shaft through center
low pressure reaction turbine (4 stage at back)

Question 7

Describe N2

Answer 7

10 stage axial flow compressor
powered by 2 stage high pressure reaction turbine

Question 8

Cold section

Answer 8

N2 compressor forward

Question 9

hot section

Answer 9

N2 compressor backward

Question 10

annular combustion chamber

Answer 10

exciters and igniters
(like magnetos and spark plugs)

Question 11

vgigv

Answer 11

variable geometry inlet guide veins
behind big fan
automatically adjust pitch (regulates engine airflow)

actuated by fuel pressure going into engine

Question 12

what engine stage does bleed air come from

Answer 12

6 and 10

Question 13

accessory gear box

Answer 13

air turbine starter (ATS)
powered by bleed air, arms overcome spring tension, starts spinning N2

integrated drive generator (IDG)
creates 3 phase AC

Question 14

thrust reversers

Answer 14

cascading reversers
slides cowling back and redirects airflow

Question 15

thrust reverser usage

Answer 15

lift up on trigger and pull back
locked until weight on wheels
2 settings, only ever use max

Question 16

t/f
slats / flats move independently

Answer 16

false
they are synced

Question 17

t/o flap settings

Answer 17

1, 2, 4

Question 18

landing flap settings

Answer 18

3, 5, full

Question 19

in flight APU will auto shut down for

Answer 19

overspeed, underspeed, fadec critical fault

Question 20

FADEC info

Answer 20

3 total
only controls designated engine
dual channel (info in info out)
FADEC gone = engine gone
intake side of engine

Question 21

T/F
in flight if the engine control is set to stop, the FADEC will shutdown the engine

Answer 21

false

engine will only shutdown with engine lever at idle

Question 22

T/F
there is no mechanical connection between the thrust levers and the engine

Answer 22

True
uses rheostats

Question 23

APU

Answer 23

hamilton sunstrand aps 2300

bleed air for:
AC
engine start
pressurization

Question 24

what spots have zero icing protection

Answer 24

inboard slats (don’t produce enough lift comparatively)

tail (vibrations should shake off)

Question 25

bleed air ice protection

Answer 25

outer 3 slats engine intake lip

Question 26

electric ice protection

Answer 26

windscreens probes

Question 27

under what situation can you restart an engine after a flameout

Answer 27

flameout caused by weather

Question 28

CAMI

Answer 28

confirm activate monitor intervene

Question 29

Who has to have an FCC in order to operate

Answer 29

only one under exemption 11498 otherwise both

Question 30

who is authorized to run and taxi an aircraft

Answer 30

any authorized personal

Question 31

who is responsible for ensuring off line handling gets done

Answer 31

company determines if airport has it captain responsibility to decide if it gets used

Question 32

Information to obtain from icing crew

Answer 32

start time of final application mixture ratio fluid type

Question 33

ice pellet table

Answer 33

comply 365 holdover table

Question 34

who is in charge of pushback

Answer 34

person in direct communication with the captain is in charge of the pushback operation

Question 35

minimum holding speeds

Answer 35

found in the performance manual not FOM

Question 36

if enroute to airport and weather drops to minimums, do you divert

Answer 36

not yet contact dispatch