Exam

Question 1

On the ground when does the ground crew horn sound?

Answer 1

When the forward equipment cooling is inoperative

Question 2

Standby Electric System can supply

Answer 2

AC and DC power to selected flight instruments, communication and navigation systems FCOM6.20.11

Question 3

The correct sequence of fuel flow through the engine is

Answer 3

Spar fuel valve ,stages ,heat exchanger, fuel filter ,fuel metering unit, engine fuel valve FCOM7.20.12

Question 4

Which are characteristics of the bank angle protection

Answer 4

Provides opposite wheel force at excessive bank angels and begins at 35 FCOM9.20.14

Question 5

In direct mode, yaw damping is degraded or can even be inoperative for some failures

Answer 5

True FCOM9.20.17

Question 6

crossfeed valve

Answer 6

3 FCOM12.10.2

Question 7

Main Gear Steering advisory message appears if:

Answer 7

Either main gear steering actuator is not locked in the centered position. FCOM 14.20.3

Question 8

OVRD is illuminated amber on the EQUIP COOLING switch:

Answer 8

The equipment cooling system is in override mode. FCOM2.10.5

Question 9

cross HASSA at 9000ft

Answer 9

True

Question 10

fire ext

Answer 10

both disch and fire extinguish

Question 11

The Autoslat system enhance airplane stall

Answer 11

Only in primary slat mode and armed when flaps 1,5,15,20 FCOM9.20.20

Question 12

Which statement true about non-normal checklist que

Answer 12

It allows you to select which checklist perform next

Question 13

Roll control

Answer 13

Flaperons Ailerons Spoilers

Question 14

Primary ice detection

Answer 14

engine nacelle inlet and wing icing FCOM3.20.1

Question 15

Statement

Answer 15

All above

Question 16

EICAS Advisory TCAS OFF

Answer 16

Both A&B

Question 17

Comm messages

Answer 17

Are displayed white, prefaced white dot cant be cancelled by pushing CANC/RCL switch

Question 18

pred-eta

Answer 18

2045z

Question 19

track bug

Answer 19

false

Question 20

tail strike pitch attitude

Answer 20

10 -8.9

Question 21

In flight both transfer busses unpowered APU starts automatically.

Answer 21

True

Question 22

Engine driven pumps are primary

Answer 22

True

Question 23

Tail skid

Answer 23

Retracts and extends along the landing gear + main landing gear actuation system.

Question 24

Dry windshield

Answer 24

False

Question 25

Engine Bleed air supplied from

Answer 25

High stage during descend and low setting FCOM2.40.1

Question 26

correct statement

Answer 26

only one center demand pump is required to be operating during landing.

Question 27

Aural Fire Bell

Answer 27

All of above