Limitations

Question 1

Maximum Operating Altitude

Answer 1

25000ft

Question 2

G Limits

Flaps Retracted

Answer 2

-1g to +2.5g

Question 3

G Limits

Flaps Extended

Answer 3

0g to +2g

Question 4

G Limits

Gear Down

Answer 4

0g to +2g

Question 5

Cargo Door Operations

Answer 5

Crosswind 45kt

Question 6

Max Passenger Seats

Answer 6

74

Question 7

Maximum Weight

Taxi

Answer 7

23170kg

Question 8

Maximum Weight

Take-Off

Answer 8

23000kg

Question 9

Maximum Weight

Landing

Answer 9

22350kg

Question 10

Maximum Weight

Zero Fuel

Answer 10

21000kg

Question 11

Vmo

Answer 11

250kt

Question 12

Mmo

Answer 12

0.55

Question 13

Va

Answer 13

175kt

Question 14

Vfe

Flap 15

Answer 14

185kt

Question 15

Vfe

Flap 30

Answer 15

150kt

Question 16

Vle

Answer 16

185kt

Question 17

Vlo RET

Answer 17

160kt

Question 18

Vlo LOW

Answer 18

170kt

Question 19

Vra

Rough Air Speed

Answer 19

180kt

Question 20

Vwo

Wiper Operating Speed

Answer 20

160kt

Question 21

Maximum Tire Speed

Answer 21

165kt (G/S)

Question 22

Vmcl (Flap 30)

Answer 22

98kt (CAS)

Question 23

Vmcl (Flap 15)

Answer 23

98kt (CAS)

Question 24

Tail Wind Limit

Answer 24

15kt

Question 25

Maximum Demonsrated crosswind

Answer 25

35kt

Question 26

Maximum Mean Runway Slope

Answer 26

+- 2%

Question 27

Minimum Runway Width

Answer 27

30m

Question 28

Maximum Demonsrated crosswind (Take-Off)

Answer 28

35kt

Question 29

Maximum Demonsrated crosswind (Landing Flap 30)

Answer 29

35kt

Question 30

Maximum Demonsrated crosswind (Wet)

Answer 30

28kt

Question 31

Starter Time Limits

Answer 31

3 Starts, Max 1:30min Starter Running Time, 4min Off

Question 32

Refueling

Answer 32

50Psi (3.5bars)

Question 33

Usable Fuel

Answer 33

Each Tank 2500kg

Question 34

Maximum Fuel Imbalance

Answer 34

730kg

Question 35

Fuel Feeding

Answer 35

EACH ELECTRIC PUMP IS ABLE TO SUPPLY ONE ENGINE IN
THE WHOLE FLIGHT ENVELOPE

ONE ELECTRICAL PUMP AND ASSOCIATED JET PUMP ARE
ABLE TO SUPPLY BOTH ENGINES IN THE WHOLE FLIGHT
ENVELOPE

Question 36

Max Differential Pressure

Answer 36

6.35psi

Question 37

Max Negative Differential Pressure

Answer 37

-0.5psi

Question 38

Max Differential Pressure for landing

Answer 38

0.35psi

Question 39

Max Differential for OVBD Valve Full Open Selection

Answer 39

1psi

Question 40

Max Altitude For One Bleed Off Operation

Answer 40

20000ft

Question 41

Single DC GEN Operation

Answer 41

If OAT exceeds ISA +25

20000ft

Question 42

MFC Failure

Answer 42

TAKE OFF WITH TWO OR MORE FAILED MFC MODULES IS PROHIBITED.

Question 43

Autopilot Engagement (Take-Off)

Answer 43

100ft

Question 44

Autopilot Engagement (Landing)

Answer 44

160ft

Question 45

Minimum Height For Flight Director Operation

Answer 45

1000ft

Question 46

ITT and Electrical system

Answer 46

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