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Citation Latitude Memory Items > Oral Questions > Flashcards

Oral Questions Flashcards

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
Q

Main hydraulic accumulator

A

Landing gear

26
Q

AUX pump

A

Parking break only

27
Q

WING X FLOW

A

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
Q

Turn on ENG/STAB

What comes on

A

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
Q

Windshield anti-ice system

A

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
Q

When does boos pump come on?

A

Engine start
X-feed
Low fuel pressure
APU start

31
Q

Lose DC power during x-feed what happens?

A

?

32
Q

Bleed air provides anti-ice for

A

Wings
Horizontal Stabilizer
Engines

33
Q

Heated electrically

A 
Pitot tubes
Static ports
Angle of attack vanes
RAT Ryanair temp probes
Windshields
34
Q

FADEC propulsion page shows

A

FADEC A or B

35
Q

1 FADEC per engine

A

2 channels

36
Q

Landing gear & brakes have a backup

A

Pneumatic system if all hydraulic pressure is lost

37
Q

Back up gear extension

A

Pneumatic blowdown &

Manual extension

38
Q

Main gear unlocks hold gear in

A

Retracted position

39
Q

Landing gear hydraulic system

PSI?

A

3,000 PSI

40
Q

Gear warning Annunciation

Horn activated

A 
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
Q

NWS steering accumulator pressure gauge in

A

Left nose compartment

42
Q

How to check brakes?

A

Parking brake set

Check brake wear pin indicators

43
Q

Antiskid inop

A

No anti skid

Incr landing distance by x 1.35

44
Q

Bus tie

Relay on the ground

A

Bus tie operates automatically

Relay closes when engine or APU start button is pressed

45
Q

Bus tie

In flight bus tie operates

A

Manually

Close in flight for APU start

46
Q

Bus tie connects

A

L & R bus systems at EMER BUSES

28 V eng gen @ 300 AMPS

47
Q

Batteries

A

2 25 V, 44 Amp Nicad Batteries

48
Q

Batteries provide power to all systems for

A

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
Q

Circuit breakers

3 sections

A

Avionics
Electrical
EMER/STBY

50
Q

Min ___ V for engine start

A

24 V

51
Q

Danger with NICAD batteries?

A

Thermal runaway

52
Q

Left battery

A

Cabin door

Nosewheel bleed down

53
Q

Bus tie on ground

A

Left gen & APU cannot be on at the same time

54
Q

Bus tie on ground

A

Left gen & APU cannot be on at the same time

55
Q

Lap children may only be held in seats

A

3 or 4

Citation Latitude Memory Items (5 decks)

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