SYS4 Test Review (Hydraulics)

Question 1

the rudder pedals control both the rudder and nose wheel steering when …

Answer 1

when the nose wheel is extended

Question 2

full forward control column movement will deflect the elevator …

Answer 2

down 12*

Question 3

which control surface is used as both a primary and secondary flight control?

Answer 3

spoilers

Question 4

the rudder boost function is used to help …

Answer 4

with an asymmetric thrust condition

Question 5

T-1 primary flight controls?

Answer 5

rudder, elevator, spoilers

Question 6

what are the secondary flight controls?

Answer 6

flaps, speed brake, 3 trim systems

Question 7

T-1 flap type

Answer 7

electronically controlled, hydraulically actuated double slotted fowler flaps

Question 8

which secondary flight controls are hydraulically actuated?

Answer 8

flaps and speed brakes

Question 9

the max speed for moving flaps from 10 to 30

Answer 9

170 KIAS

Question 10

when does roll trim warning sound?

Answer 10

actuated more than 5 secs

Question 11

which control surface is both primary and secondary?

Answer 11

spoilers

Question 12

V_fe for 30 flap

Answer 12

165 KIAS

Question 13

emergency pitch trim is accomplished ..

Answer 13

electronically with a switch on the pedestal

Question 14

rudder is operated …

Answer 14

mechanically

Question 15

when will speed brakes be automatically retracted?

Answer 15

1: throttles to above 60%N1
2: setting flaps beyond 10

Question 16

speed brake control valve supplies _____ pressure to deploy spoilers on both wings

Answer 16

hydraulic

Question 17

FLAP ASYM indicates

Answer 17

main flap asymmetry ( >7* differential)

Question 18

Pitch attitude controlled by

Answer 18

mechanically actuated elevators

Question 19

emergency pitch trim is ____ of the normal rate of trim

Answer 19

1/3

Question 20

what happens when the hydraulic filter becomes clogged?

Answer 20

fluid bypasses clogged filter (no indication)

Question 21

which hydraulic system is not part of the valve package?

Answer 21

wheel brakes

Question 22

what happens when hydraulic pressure exceeds 1650 psi?

Answer 22

hydraulic pressure relief valve opens, routes excess to return line

Question 23

purpose of bleed air in hydraulic reservoir?

Answer 23

prevents fluid foaming and provides constant supply of fluid to the pumps

Question 24

hydraulic pressure stabilizes at

Answer 24

1500 psi

Question 25

HYD LEVEL LO light turns on when

Answer 25

0.6 gal left in Hydr. reservoir

Question 26

L/R H PUMP PRESS LO lights up when

Answer 26

< 750 psi

Question 27

pilot intervention required if pressure reaches ____ psi

Answer 27

1850

Question 28

hydraulic reservoir should be serviced when gauge level is

Answer 28

below the REFILL line

Question 29

What does the hydr. filter do?

Answer 29

removes contaminants that could damage moving parts

Question 30

What happens to hydr. components if one hydraulic pump is lost?

Answer 30

All hydraulic subsystems operate normally

Question 31

High pressure is indicated by which light?

Answer 31

None, pressure gauge only

Question 32

when does the hydraulic system start operating?

Answer 32

automatically at engine start

Question 33

which systems require hydraulic pressure?

Answer 33

wheel brakes, speed brakes, flaps, gears

Question 34

how do you know if a hydraulic pump has failed?

Answer 34

L/R H PUMP PRESS LO

Question 35

the landing gear handle

Answer 35

sends an electrical signal to the hydraulic valve package to start the gear lowering/retraction sequence

Question 36

max nose wheel deflection

Answer 36

45* using rudder pedals and differential power/braking

Question 37

with flaps at 0 or 10, when will the gear horn sound?

Answer 37

throttle below 70%

Question 38

using rudder pedals only, what is max deflection of nose gear

Answer 38

25*

Question 39

when fully closed, the main gear fuselage doors ____ lock closed

Answer 39

mechanically

Question 40

normal landing gear extension sequence

Answer 40

gears do not extend until inboard main doors are fully open

Question 41

the max airspeed for emergency gear extension is ...

Answer 41

150 KIAS

Question 42

min strut extension for main gear

Answer 42

1.1 inch

Question 43

normal landing gear sequence takes approx. ___ sec

Answer 43

7

Question 44

normal strut extension for nose gear approx.

Answer 44

3.5 inches

Question 45

max altitude for gear extension

Answer 45

20,000 ft MSL

Question 46

when main gears are extended, _____ locks them down

Answer 46

mechanical down lock mechanism

Question 47

which component allows gear handle to be raised if it is stuck down ?

Answer 47

downlink release button

Question 48

during emergency gear extension, nitrogen pressure is used to

Answer 48

close the main gear fuselage doors