Limitations

Question 1

(LVO) CAT I Minima

Answer 1

RVR 550 m
DH 200 feet

Question 2

(LVO) CAT II minima:

Answer 2

RVR 300m
DH 100 feet

Question 3

(LVO) CAT III minima:

Answer 3

RVR 250m
DH 50 feet

Question 4

(LVO) LVTO Minima:

Answer 4

125 m
No DH

Question 5

The A220-300 is an airplane of approach category:

Answer 5

C

Question 6

Maximum number of PAX seats are

Answer 6

148 or 149

Question 7

A maximum number of __ infants (under the age of 2) can be carried in arms of PAX, provided safety measures are applied:

Answer 7

40

Question 8

PBN Limitations:

Answer 8

RNP AR approaches greater than or equal to 0.3NM and MaP of 1.0 NM accuracy.

Question 9

Maximum ramp weight:

Answer 9

68039 kg

Question 10

MTOW:

Answer 10

67585 kg

Question 11

MLW

Answer 11

58740 kg

Question 12

MZFW:

Answer 12

55792 kg

Question 13

Maximum structural load for cargo compartments:

Answer 13

2446 kg FWD
2606 kg AFT
* maximum load limits must be observed in the wardrobe labels

Question 14

Maximum operating speed sea level - 8000’

Answer 14

300 KIAS

Question 15

Maximum operating speed 10 000’ – 27 500’

Answer 15

330 KIAS

Question 16

Maximum operating speed above 27 500’

Answer 16

M0.82

Question 17

VFEs:

Answer 17

230
210
210
190
170

Question 18

VLO extension:

Answer 18

250 KIAS

Question 19

VLO retraction:

Answer 19

220 KIAS

Question 20

VRA:

Answer 20

280 KIAS or M0.75
— 10 000 ‘ —
265 KIAS

Question 21

The tire limit speed is:

Answer 21

195 KT GS

Question 22

Descending below 10 000’ the maximum speeds allowed are as follows:

Answer 22

IAS: 300 KT
ROD: 3 000 fpm

Question 23

At or below 2 500 ‘ AGL (TAWS advisory “TWENTY FIVE HUNDRED”)

Answer 23

ROD 1500 fpm + Hands on controls

Question 24

Maximum Taxi speeds:

Answer 24

30 KT
(10 KT in 90° turn)

Question 25

At rotation and touchdown, bank angles of _____ can cause an engine nacelle strike.

Answer 25

15°

Question 26

At rotation, pitch of more than ___ can cause a tail strike.

Answer 26

11°

Question 27

At touchdown, pitch angles of __ can cause a tail strike.

Answer 27

10°

Question 28

Maximum PA for TO/LDG :

Answer 28

10 000 feet

Question 29

Maximum PA for AUTOLAND :

Answer 29

8466 feet

Question 30

Maximum Operating Altitude

Answer 30

41 000 ft

Question 31

Maximum temperature approved for LDG:

Answer 31

52.5°C

Question 32

Minimum temperature approved for TO AND LDG

Answer 32

—54°C

Question 33

Manoeuvring limit load factors:

Answer 33

Flaps Up: 2.5G ; -1.0G
Flaps Down: 2.0G ; - 0G

Question 34

Maximum RWY slope for TO AND LDG:

Answer 34

+/- 2%

Question 35

Minimum TWY width is:

Answer 35

15 m

Question 36

Minimum OXY pressure for dispatch:

Answer 36

(2 crew members)
900 psi
950 psi in mountainous region

Question 37

The freezing point of JET A1 is:

Answer 37

—47°C

Question 38

MAX fuel temperature for starting is:

Answer 38

+ 52.5°C

Question 39

Takeoff with fuel indications below __ °C is prohibited.

Answer 39

— 37°C

Question 40

MAX permissible fuel imbalance between tanks is:

Answer 40

454 kg

Question 41

Fuel load in L/R tanks:

Answer 41

3050kg / each

Question 42

Fuel Load in Center tank:

Answer 42

11300 kg

Question 43

Total fuel load:

Answer 43

17 400 kg

Question 44

Maximum and minimum refuelling pressure:

Answer 44

MAX: 55 PSI
MIN: 30 PSI

Question 45

Engine warmup MAX setting:
(Between -6°C and 21°C)

Answer 45

30% N1

Question 46

Engine warmup MAX setting:
(Below -6°C)

Answer 46

IDLE N1

Question 47

Above 29 100 feet, the MAX N1 is __

Answer 47

95.2 %

Question 48

MAX TO EGT:

Answer 48

1054°C

Question 49

Minimum oil temperature for TO is:

Answer 49

+49°C (48 switch to white on EICAS happens)

Question 50

After ___ start attempts, or ___ minutes of continuing cranking, a ___ minute cooling period is required.

Answer 50

3 attempts
4 minutes
30 minute