A220 Limitations

Question 1

Max Pressure Altitude TO & Landing

Answer 1

10,000 ft

Question 2

Max Operating Altitude

Answer 2

FL410

Question 3

Maneuvering Load Limits

Answer 3

Flaps Up -1.0 to 2.5 g
Flaps Down 0.0 to 2.0 g

Question 4

Max TO Weight

Answer 4

149,000 lbs.

Question 5

Max Landing Weight

Answer 5

129,500 lbs.

Question 6

Max Zero Fuel Weight

Answer 6

123,000 lbs.

Question 7

Min Flight Weight

Answer 7

80,000 lbs.

Question 8

Mmo

Answer 8

.82 m

Question 9

Turbulent Air Penetration Speed
At or Above 10,000ft.

Answer 9

280 kts. / .75m

Question 10

Tire Limit Ground Speed

Answer 10

195 kts.

Question 11

Maximum windshield wiper speed

Answer 11

250 kts 

Question 12

Maximum gear extension speed Vlo extend

Answer 12

250 kts

Question 13

Maximum gear, retraction speed

Answer 13

220 kts

Question 14

Maximum gear extended speed

Answer 14

250 kts

Question 15

Vfe Flaps 1

Answer 15

230 kts

Question 16

Vfe Flaps 2

Answer 16

210 kts

Question 17

Vfe Flaps 3

Answer 17

210 kts

Question 18

Vfe Flaps 4

Answer 18

190 kts

Question 19

Vfe Flaps 5

Answer 19

170 kts

Question 20

Direct Mode Maneuvering Speed

Answer 20

300 / .80m

Question 21

Crosswind Limit RCAM 5 & 6
Takeoff

Answer 21

32 kts

Question 22

Crosswind Limit RCAM 5 & 6
Landing

Answer 22

29 kts

Question 23

Max Tailwind

Answer 23

10 kts including gusts

Question 24

Definition of Icing Conditions

Answer 24

Icing conditions exist when outside air temperature on the ground/takeoff or TAT in Flight is 10° C or less with visible moisture.

Question 25

When should Cowl anti-system be activated on the ground?

Answer 25

The cowl anti-ice system must be activated when the OAT is 10° C or less and icing conditions exist 

Question 26

When must the wing anti-ice system be activated for takeoff? 

Answer 26

The wing anti-ice system must be activated for takeoff when the OAT is 5° C or less and icing conditions exist

Question 27

Holding in icing conditions

Answer 27

Do not hold in icing condition with slats/flaps extended 

Question 28

Fuel Capacity L/R Wing Center Total

Answer 28

L/R 6,725 lbs Center 24,900 lbs Total 38,350 lbs

Question 29

Max fuel imbalance L and R Main Tanks

Answer 29

800 lbs.

Question 30

Can manual transfer and gravity cross flow be on for takeoff?

Answer 30

No

Question 31

Either L or R Bleed must be ON for takeoff when temps are at or below:

Answer 31

15° C

Question 32

Either L or R Pack must be on when temps are at or below:

Answer 32

15° C

Question 33

Use of ______ spoilers is prohibited except in an emergency.

Answer 33

Max

Question 34

During an approach and landing with auto throttle, the approach speed must be increased by ____ kts.

Answer 34

5

Question 35

Man Speed must be used when flying _______ in the final landing configuration.

Answer 35

Vapp

Question 36

Oil Temp in Amber Range

Answer 36

Do not take off. Oil temps less than 20° C trust limits apply.

Question 37

Engine cool down time

Answer 37

3 mins

Question 38

Maximum tailwind for engine start

Answer 38

18 kts