oral prep Flashcards

(40 cards)

1
Q

how many IRUs

A

3

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2
Q

how do you ALIGN the IRUs

A

switch to NAV

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3
Q

how long does the alignment process take

A

About 10min

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4
Q

how can you tell how much longer until the alignment is complete

A

HDG counts down from 7 min

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5
Q

what is the initialization priority

A

GPS postion, gate postion, last postion and ARP, otherwise put in the LAT/LONG for the gate, then ARP

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6
Q

how can you force in a position

A

on the 3rd attempt it will accept the position entered

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7
Q

why does the ON DC illuminate momentarily during power up

A

part of a self test

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8
Q

IRU ALIGN light stays on for 30 seconds during shutdown. Why?

A

part of the shutdown process and the IRU is saving the LAST POS

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9
Q

the RAT provides HYD pressure to?

A

Spoilers
Autopilot servos
Flight controls (primary)
Elevator feel
Trim for stabilizer
Yaw damper

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10
Q

which HYD system does the RAT get its fluid from

A

the center system

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11
Q

when does the RAT deploy

A

when both engines fail

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12
Q

what is the min speed for the RAT to produce pressure

A

130kts

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13
Q

which system is the normal brakes on

A

right

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14
Q

which system are the alternate brakes on

A

center

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15
Q

how many HYD systems control the flight controls

A

all 3

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16
Q

where do you read the HYD quantity indicator

A

EFIS 2

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17
Q

what does RF mean

18
Q

what quantity will cause the gauge to switch to RF

19
Q

(HYD) what quantity will cause it to say QTY

20
Q

when do demand pumps run automatically

A

when there is a high HYD demand condition

21
Q

what is the main reason for the C HYD SYS demand pump

A

to assist in getting the main landing gear doors up sooner

22
Q

what is on the hot bat bus

A

clock
fire extinguisher bottles
APU fuel valve
spar fuel valves
parking break

23
Q

with EXT power AVAIL light illuminated, what buses are powered

A

HOT BAT and ground handling buses

24
Q

how many batteries are there

A

2 - the main and APU battery

25
when does UTIL BUS shedding occur
BOSS Both thrust levers advanced to T/O range on the ground with engines shut down Overload-electrical load exceeds power available Starting engines Single generator source (gen or eng failure)
26
with a left AC BUS light fault, will the captains flight instruments fail?
no, automatically powered from the right main AC BUS
27
what is the purpose of the BUS TIE system?
PPI-Prevent, provide and Isolate Prevent paralleling of the left and right main buses Provide power to both main buses Isolate faults
28
when can a disconnected IDG be reconnected?
only on the ground
29
what does the HDG provide power to?
BATT and HOT BATT buses left and right AC transfer buses Standby AC and DC buses captains FLT INSTR
30
what are the 5 times that pilot verification is required prior to pilot action
initial position GEN DRIVE thrust levers fuel control switches fire switches
31
is it possible to shed the galley bus and not the utility bus
yes
32
how does the APU get its fuel
left FWD AC pump or the DC pump in the left tank
33
what happens when you move the APU start switch ON?
the fault light cycles on then off the APU door opens the APU fuel valve opens turns on the DC or AC fuel pumps arms APU bleed valve to open
34
how long is the main A/C battery capable of powering the STBY PWR system
30 min
35
at what altitude must a single pilot be on oxygen
25,000ft
36
where do we load pets
BULK cargo compartment
37
when are AUTO BRAKES activated during takeoff
above 85kts and BOTH thrust levers at IDLE
38
which brake systems have anti-skid capability
All of them
39
when the APU RUN light flashes twice, what does this mean?
it is testing both APU circuits
40
what happens when you turn on the fuel jettison nozzle switches are selected ON?
jettison transfer valves open jettison pumps operate (if installed) sheds side window heat equip cooling switches to overboard