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Airbus > Differences > Flashcards

Differences Flashcards

1
Q

319 dimensions

A

Length: 111
Width: 111’10”
Nose to main: 36’3”
Between mains: 24’11”

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2
Q

320 dimensions

A

Length: 123’3”
Width: 111’10”
Nose to main: 41’6”
Between mains: 24’11”

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3
Q

321 dimensions

A

Length: 146’
Width: 111’10”
Nose to main: 55’6”
Between mains: 24’11”

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4
Q

Min turning radius for 319/320/321

A

319/320 is 100’
321 is 105’

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5
Q

319/ 320/321
max operating Altitude
Vmo
Mmo
Vlo extension
Vlo retraction
Vle

A

39,000’
350kts
.82mac
250kts
220kts
280kts

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6
Q

319
Max Taxi Weight
Max Takeoff weight
Max Landing weight
Max zero fuel weight

A

167,330
166,448
137,788
128,970

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7
Q

320

Max Taxi Weight
Max Takeoff weight
Max Landing weight
Max zero fuel weight

A

170,637
169,755
142,198
134,481

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8
Q

A321 non sharklet

Max Taxi Weight
Max Takeoff weight
Max Landing weight
Max zero fuel weight

A

205,911
205,029
171,519
162,701

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9
Q

A321-IAE sharklet

Max Taxi Weight
Max Takeoff weight
Max Landing weight
Max zero fuel weight

A

207,014
206,132
171,519
162,701

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10
Q

A321-CFM-sharklet

Max Taxi Weight
Max Takeoff weight
Max Landing weight
Max zero fuel weight

A

207,014
206,132
174,606
166,669

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11
Q

Min crew for A320

A

2 pilots
Up to 4 FA

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12
Q

PED power is automatically removed during _______

A

Takeoff and Landing

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13
Q

Potable water is pressurized by _________system but on ground with no power it is pressurized by _________

A

Pneumatics

Electric compressor pump
or APU or Ground Air port

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14
Q

O2 mask provide 3 types of O2 blends

A

Mixture of O2 and cabin air
Pure O2
O2 under pressure

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15
Q

O2 mask will auto deploy at______ +-________
Manually deployed by pushing __________

A

14000 +250-750

Mask man on

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16
Q

DMC 1,2,3 info goes to

A

Display management system
1-captains PFS, ND and upper ECAM
2- FO PFD, ND, lower ECAM
3- standby computer and any info to each side

17
Q

Blank screen means individual DU has ______or is _______

A

Failed / turned off

18
Q

DMC failure is displayed by _________ on EIS1 and________
Message on EIS 2.

A

Diagonal / invalid

19
Q

Standby instruments gets info from ________ and is powered by

A

Standby PSTatic system
ADIRU 1&3
ILS 1

Aircraft battery

20
Q

Clock right of ECAM is the _______time reference to ________

A

FMGC and other systems

21
Q

The RAT will not produce enough Hyd Pressure below_____for emergency generator

A

140

22
Q

Cargo compartment bottles provide______min of fire suppression

A

60

23
Q

What controls the APU?

A

ECB-electronic control box

24
Q

APU starter motor duty cycle

A

Start/60sec/start/60sec/start/60min

25
Q

A319 non sharklet engines and thrust

A

CFM56-5—-23,500
V2500———24,000

26
Q

A320 engines and TQ

A

CFM56-5——-27,000
V2500———-25,000 or 27,000

27
Q

A321 engines and TQ

A

CFM56-5——-32,000
V2500———-33,000

28
Q

What is EPR

A

Engine Pressure ration

29
Q

How many fuel
Cells in a 319/320
Fuel moves from outer cell by ________

A

5
Transfer valves

30
Q

321 has _____tanks

A

3

31
Q

All aircraft can have 2 additional center fuel tanks
________lbs each

A

5,250

32
Q

Fuel tank weights
Outer
Inner
Center
Act

A

1550
12200
14500
5250

33
Q

Center tank fuel is trapped and unusable if __________fail

A

Both pumps

34
Q

Nose wheel steering is inoperative if not operating with the Green Hyd system
Except on _____aircraft

A

Enhanced

35
Q

A321 has double _________flaps

A

Slotted

36
Q

320 Speed brakes have _______control when hand flying and ________control when Auto pilot is on

319/321 are not this way they always correspond to handle position.

A

Full
1/2

37
Q

Load alleviation is inhibited when

A

Slats or flaps are extended

Airspeed less than 200kts or greater than Vmo +10

Slats/flaps wing tip brakes engaged

Airbus (29 decks)

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