Oral Questions Flashcards

(55 cards)

1
Q

ER lights, when do they come in?

A
5-G impact
Lose DC power
Taxi
Activate manually 
Pax safety button on in ARM position
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2
Q

Doors outside monitored?

A
Nose
Cabin
(ER door)
Baggage
Hell hole
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3
Q

Wing X-flow

When do you use it?

A

Used for engine failure

SE leading edge of wings only

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4
Q

Engine/Stab

Anti-ice on

A
3 inboards inlet, stab, stator vanes 
RAT probe ( electric) comes on when you turn on engine stab 

Bullet ( bleed air) on when engines are running

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5
Q

COM 1

A

121.5 Emergency

Puts it in the active

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6
Q

Standard O2 bottle

A

77 cubic feet

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7
Q

APU

Why wait 10 seconds before starting the APU?

A

The “self test” may fail

No message if started before 10 seconds

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8
Q

Event marker

A

5 min before

1 minute after

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9
Q

If APU fire bottles

Auto shutdown discharges after 8 seconds

A

Engine SOV
Hydraulic SOV
Engine Gen deactivated
Both fire bottles armed

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10
Q

Max cool button

A

Cools faster on the ground than normal
Straight cold air from ACM
Recurved fan on
Or cool faster w engines

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11
Q

APU will not start if

A

Baggage fire bottle fired.

The APU shares the same bottle for baggage fire and it automatically shuts the APU off if baggage fire bottle is pressed

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12
Q

Max amps APU on the ground

A

275 amps

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13
Q

Secondary trim

What do you lose?

A

Primary stab

Autopilot

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14
Q

Type of electrical system?

A

Split bus system

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15
Q

Where do you see battery temp?

A

On electrical page

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16
Q

How does the bus tie operate?
Ground
Flight

A

Ground auto closed

Flight manual

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17
Q

Nose gear up lock

When pulled allows

A

Gear to free fall

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18
Q

Landing gear

A

Electrically controlled

Hydraulically actuated

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19
Q

Emergency descent mode

When does it activate?

A

Above 30,000 feet
Autothrottes engaged
Autopilot on
Cabin altitude greater than 14,500 ft

90 deg left
Descent
VMO about 10 kts
Set 7700

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20
Q

Control lock locks what 4 items?

A

Left throttle
Rudder pedals
Yoke

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21
Q

Cabin Dump

A

30,000 -13,700

Manual mode 14,300. 14,500

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22
Q

Can APU be used for EMER pressurization?

A

No

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23
Q

Hydraulic Pump

L ENG. R ENG

A
Spoilers
Landing gear
NWS nosewheel steering
Thrust reversers 
Brakes
24
Q

Accumulator

A

Helps w spike/surges

3,000 psi syst

25
Main hydraulic accumulator
Landing gear
26
AUX pump
Parking break only
27
WING X FLOW
Supplies engine bleed air to both L & R wing leading edges from a single engine Bleed air only provided to the wing Leading edges
28
Turn on ENG/STAB | What comes on
Horizontal Stab leading edges Stator vanes Nose cone ( inboard) Wing leading edges incl first 36 inches of winglets Activated 2 RAT probes-heated electrically in each inlet
29
Windshield anti-ice system
Heated electrically w engines running & TRU’s are off L ALT L windshield & R side window R ALT R window & L side window Current for heating windows is provided by the alternators I
30
When does boos pump come on?
Engine start X-feed Low fuel pressure APU start
31
Lose DC power during x-feed what happens?
?
32
Bleed air provides anti-ice for
Wings Horizontal Stabilizer Engines
33
Heated electrically
``` Pitot tubes Static ports Angle of attack vanes RAT Ryanair temp probes Windshields ```
34
FADEC propulsion page shows
FADEC A or B
35
1 FADEC per engine
2 channels
36
Landing gear & brakes have a backup
Pneumatic system if all hydraulic pressure is lost
37
Back up gear extension
Pneumatic blowdown & | Manual extension
38
Main gear unlocks hold gear in
Retracted position
39
Landing gear hydraulic system | PSI?
3,000 PSI
40
Gear warning Annunciation Horn activated
``` Any gear not down & locked Flaps greater than 24 deg RA less than 500’ AGL Both throttle lever angles less than 8.7 deg Any gear not down and licked TLA’s less than 8.7 deg Both AOA’s greater than 0.4 ```
41
NWS steering accumulator pressure gauge in
Left nose compartment
42
How to check brakes?
Parking brake set | Check brake wear pin indicators
43
Antiskid inop
No anti skid | Incr landing distance by x 1.35
44
Bus tie Relay on the ground
Bus tie operates automatically Relay closes when engine or APU start button is pressed
45
Bus tie In flight bus tie operates
Manually | Close in flight for APU start
46
Bus tie connects
L & R bus systems at EMER BUSES 28 V eng gen @ 300 AMPS
47
Batteries
2 25 V, 44 Amp Nicad Batteries
48
Batteries provide power to all systems for
20 minutes or EMER Buses for 60 min If both L& R electrical buttons are selected to EMER within 5 min of losing gen power
49
Circuit breakers 3 sections
Avionics Electrical EMER/STBY
50
Min ___ V for engine start
24 V
51
Danger with NICAD batteries?
Thermal runaway
52
Left battery
Cabin door | Nosewheel bleed down
53
Bus tie on ground
Left gen & APU cannot be on at the same time
54
Bus tie on ground
Left gen & APU cannot be on at the same time
55
Lap children may only be held in seats
3 or 4