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Airbus A220-300 > Limitations > Flashcards

Limitations Flashcards

1
Q

Dimensions.
L, H, wingspan, main wheels, Main - Nose wheel, Pod Clearance

A

L= 38.7m
H= 11.5m
Wingspan = 35.1m
Main wheels = 6.7m
Main - Nose wheel = 15.2m
POD Clearance = 0.51m

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2
Q

180deg turn min radius

A

23.5m

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3
Q

Flight in icing conditions

A

Up to 35000’

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4
Q

NWS Deflection

A

80degrees L&R

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5
Q

Max approach angle

A

3.5 degrees

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6
Q

Weights.
MRW, MTOW, MLW, MZFW, MFW

A

MRW= 71214
MTOW = 70896
MLW = 58740
MZFW = 55792
MFW = 36287

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7
Q

Max operating Alt

A

41000’

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8
Q

Vmo/Mmo

A

> 8000’ = M0.82/330kts

<8000’ = 300kts

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9
Q

Vmo/Mmo in Direct Mode

A

M0.80/300kts

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10
Q

Max Alt for TO/LDG

A

10000’

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11
Q

Vfe for F1, 2, 3, 4, 5

A

F1 = 230
F2= 210
F3= 210
F4= 190
F5= 170

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12
Q

Vloe
Vlor
Vle

A

Vloe = 250
Vlor= 220
Vle = 250

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13
Q

Vra TB penetration for Mod & Svr

A

<10000’ = 265kts
>10000’ = 280/0.75 whichever is less

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14
Q

Windshield wiper operation

A

250kts

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15
Q

Tire limit speed

A

195kt ground speed

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16
Q

Max & Min temp for TO & LDG

A

52.5 degrees C
-54 degrees C

17
Q

Maneuvering load limits for Flaps Up and Down

A

Flaps up = -1.0g - 2.5g

Flaps down = 0.0g - 2.0g

18
Q

RWY slope

A

+/- 2%

19
Q

Tailwind TO & LDG

A

10kts

20
Q

Max positive cabin diff
Max negative cabin diff

A

Positive = 8.8 psid

Negative = -0.5 psid

21
Q

At touchdown, cabin pressure diff must be less than

A

1.0 psid

22
Q

Min height for Autopilot engagement

A

400’ AGL

23
Q

Min height for Autopilot use

A

80’ AGL

24
Q

APU starter duty cycle

A

Max 3 attempts in 1 hour

2 mins between start attempts

25
Q

APU bleed max altitude

A

23000’

26
Q

APU bleed operation for TO

A

APU bleed must be off for takeoff when OAT is at or below 15 degrees C

27
Q

Max AC continuous generator load

A

75KVA

28
Q

Max continuous load on TRU 1&2.

Max continuous load on TRU 3

A

350amps

225amps

29
Q

Max Alt with flaps and slats extended

A

20000’

30
Q

Min height with spoilers extended

Min speed with spoilers extended

A
  • 300’ AGL
  • Vref +10

Use of max spoilers is prohibited except in emergencies

31
Q

Left & Right main Fuel tank max Imbalance

A

454kg

32
Q

Fuel quantity.
Left and Right main tank
Centre tank
Total

A

Left main = 3770L (3050kg @ 0.809kg/l)
Right main = 3770L (3050kg)
Centre = 13968L (11300kg)

Total = 21508L (17400kg)

33
Q

Minimum fuel quantity for go around

A

442kg per wing and max climb attitude of 10 degrees nose up.

34
Q

Max and Min fuel temp for starting and operating

A

52.5 degrees C

Takeoff with fuel temp below -37 degrees C is prohibited

Airbus A220-300 (2 decks)

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