Limitations

Question 1

Runway slope

Answer 1

+/- 2%

Question 2

Max operating altitude

Answer 2

41,000’ pressure altitude

Question 3

Maximum TOLD altitude

Answer 3

8,400’ pressure altitude

Question 4

ViaSat inflight connectivity system fitted: FMC derived EO CRZ Max Altitude is required?

Answer 4

To be reduced by 400’

Question 5

Operations on narrow runways
(<45m but not less than 30m)

Answer 5

Vis: RCL shall be clearly visible in the prevailing conditions
Systems: not allowed nose gear steering inop or 1 thrust reverser inop.

If an alternate ​airport is available with a runway at least 45m wide, diversion to that alternate ​shall be performed in case of jammed or restricted flight​ controls, trailing edge ​flap asymmetry, leading edge flap/slat asymmetry,​ or loss of system A​ or B ​hydraulics

Question 6

Ground wind limits for all doors

Answer 6

-40KT while opening or losing
-65KT while open

Question 7

Altitude display limits for RVSM operations

Answer 7

-standby altimeters do not meet altimeter accuracy requirements for RVSM
-Max allowable in-flight difference between the C and FO is 200’
-Max allowable on-the-ground (SL-5000’) difference between C and FO is 50’. Between the C or FO and field elevation is 75’.

Question 8

VXA-VXU max weights

Answer 8

MTW 79242kg
MTOW 79015kg
MLW 66360kg
MZFW 61688kg

Question 9

VYA-VZE max weights

Answer 9

MTW 75296kg
MTOW 75069kg
MLW 66360kg
MZFW 61688kg

Question 10

VYZ, VZF-XZP max weights

Answer 10

MTW 79242kg
MTOW 79015kg
MLW 66360kg
MZFW 62731kg

Question 11

Max cabin differential pressure

Answer 11

9.1psi

Question 12

Aileron trim with the autopilot engaged?

Answer 12

Prohibited

Question 13

Autopilot engagement for TO

Answer 13

Not below 400’ AGL

Question 14

Single channel operation during approach, the autopilot shall not remain engaged below?

Answer 14

50’AGL

Question 15

Max and min GS angles for autoland

Answer 15

3.25 and 2.5

Question 16

Autoland capability may only be used:

Answer 16

F30 or F40 and both engines operative

Question 17

LVL CHG restriction on final approach?

Answer 17

Do not use below 1000’ AFE

Question 18

Engine ignition must be on:

Answer 18

-TO
-LDG
-operation in +RN
-AI operation

Question 19

Reverse thrust

Answer 19

Intentional selection in flight is prohibited

Question 20

Thrust for TO with anti-skid inoperative

Answer 20

ATM is not permitted

Question 21

APU INFLIGHT: bleed + electrical load max alt

Answer 21

10000’

Question 22

APU bleed max alt

Answer 22

17000’

Question 23

APU electrical load max alt

Answer 23

41000’

Question 24

APU bleed air valve must be closed when:

Answer 24

-ground air connected and isolation valve open
-engine 1 bleed valve open
-Isolation and engine 2 bleed valves open

Can be open during engine start, but avoid engine power above idle.

Question 25

After 3 consecutive aborted APU start attempts, what cooling period is required?

Answer 25

15 minutes

Question 26

How long should the APU be run before using it as a bleed air source?

Answer 26

2 full minutes

Question 27

Max altitude with flaps extended?

Answer 27

20000’

Question 28

Holding in icing conditions with flaps extended?

Answer 28

PROHIBITED

Question 29

Sbeedbrakes

Answer 29

Do not deploy in flight at <1000’RA

Question 30

Alternate flap duty cycle

Answer 30

-when extending or retracting flaps with ALTERNATE FLAPS position switch, allow 15 secs after releasing before moving switch again to avoid damage to the alternate flap motor clutch
-after a complete extend/retract cycle, allow 5 mins cooling before attempting another extension.

Question 31

Maximum fuel tank temperature

Answer 31

49C