400 questions good luck

Question 1

how many gallons of HYD fluid in A vs B

Answer 1

A = 4.7 us gallons
B = 7.2 us gallons

Question 2

if there is a leak in the engine driven A pump how much fluid will be left?

what about the electric?

Answer 2

22% left for the electric driven pump

outta luck butter cup nothing left

Question 3

if the #1 engine RPM fails below 56%, gear is not up and commanded up, what happens

Answer 3

the LGTU operates from the b system to raise the gear

Question 4

if a leak occurs in the B system engine HYD pump what happens?

what about the electric pump?

Answer 4

the fluid will drain to the top of the engine driven HYD pump stand pipe leaving about 40%

it leaks to the top of the electric pump standpipe which is about empty but enough fluid is left over for the PTU

Question 5

if the standby HYD system has a leak how much will the B reseivor decrease to?

Answer 5

64%

Question 6

if either flight control switch is not in the STBY RUD position and the ALT Flaps switch is not in the arm position, the stand by system will do what?

Answer 6

the standby system will auto shut off when the flaps are retracted in flight

Question 7

with the Loss of A and B HYD what flight controls are powered and how?

Answer 7

Ailerons and elevators thru manual reversion and the rudder is via the standby system

Question 8

how many flight spoilers do we have? what HYD system power which ones?

Answer 8

4 // the inboard flight spoilers via the A system and the outboard via the B system

Question 9

how many ground spoilers are there?

Answer 9

3

Question 10

if the B system is completly inop what provides pressure to the leading edge devices?

Answer 10

the stand by system

Question 11

are the rudder pressure reducer (RDR) and the rudder pressure limiter (RDL) the same thing ?

Answer 11

yes, the RDR is on the a system and RDL is on the B system

both limit the hydraulic pressure to the rudder when full rudder is not required

Question 12

when is rudder pressure reduced?

Answer 12

it is reduced at 1000agl and remains reduced until descending below 700ft agl

it also makes the ailerons and flight spoilers more effective in the event that the more counter active force is needed

Question 13

when will the rudder pressure return to normal

Answer 13

loss of system B

a difference in N1 between the thrust levers that exceeds more than 45%

Question 14

if the RPR fails to come back on descending trough 700RA what happens?

Answer 14

the FLT control low pressure limit is illuminated and the standby sytem will activate, open standby rudder valve power the standby PCU

Question 15

a runaway trim can be caused by?

Answer 15

uncommanded operation of the main electric trim
uncommanded operation of the autopilot trim system
or a failure of the brake portions of the main and autopilot trim systems, which allow stabillizer float

Question 16

what do you do if you have runaway stabilizer float?

Answer 16

it may be neccessary to not do opposite control forces as it may make the situation worse

trim will stop the uncontrolled motion of the stabilizer

this is one situation where grabbing the stabilizer trim wheel would be neccessary as far as i can find

Question 17

the lower cargo compartment must have operating smoke detection and fire suppresion with 3 exceptions.. what are these exceptions

Answer 17

empty cargo handling equipment, ballast and or fly away kits

Question 18

how many smoke detectors in the forward cargo compartment? how many in the aft?

Answer 18

4 in the forward // 6 in the aft // each unit has a dual loop configuration a and b

Question 19

if one fire detection loop fails what happens?

Answer 19

it goes into single loop mode automatically

Question 20

how many agent bottles do we have for the lower cargo? what about in 311?

Answer 20

1 // 2

Question 21

what must you do while doing the cargo fire procedure?

Answer 21

proceed to nearest suitable airport

Question 22

how many circuit breakers are there for the lower cargo suppresion and detection system?

Answer 22

3 // p6-2 panel /

Question 23

how is lower cargo compartment smoke detection powered? what about lower cargo suppresion?

Answer 23

DC bus 1 and 2 /// hot battery bus

Question 24

when will a detection fault light illuminate during a cargo fire test?

Answer 24

when one or more of the detectors in the selected loops have failed

Question 25

how many smoke detectors in the main deck cargo

Answer 25

12 detectors

Question 26

what lights will illuminate with a main deck cargo fire?

Answer 26

MAIN CARGO SMOKE (lower right or left) and the associated smoke detector will illuminate.. THERE IS NO MASTER CAUTION OR MASTER FIRE WARNING OR FIRE BELL

Question 27

if you have a main deck fire what are some of the steps the QRH would direct you to do?

Answer 27

Move the CABIN AIR SHUTOFF switch to closed.
- this action uses two valves, powered by the number 2 DC main bus, to close off ECS air supplied from the mix manifold

there is no fire suppresion / fighting ability except for reducing the amount of oxygen to the fire

Question 28

why does the QRH direct the flight crew to descend to (and reise the cabin alitutde) FL250 during a main deck cargo fire?

Answer 28

maintaining 250 as long as practable minimizes oxygen available to the fire while accomidating flight crew physiological limits for extended flight on supplementary oxygen

Question 29

what is the MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR SYSTEM test?

Answer 29

1: main deck cargo compartmennt smoke detector panel
- press to test switch: press and hold
- verify 12 smoke detector lights are on
- verify both MAIN CARGO SMOKE (red) lights - on

NOTE: the MAIN CARGO SMOKE red lights are located on each pilots lower instrument panel

Question 30

MAIN CARGO COMPARTMENT AIR SUPPLY SHUTOFF test?

Answer 30

Cabin air shutoff control panel

1: cabin air shutoff switch guard = move up
2: cabin air shutoff control swtich = closed
- verify cabin air shutoff closed indicator (amber) light = on
3: cabin air shutoff control switch = open
4: cabin air shutoff switch guard = move down
- verify cabin air shutoff indicator (amber) light = off