Limitations

Question 1

Max runway slope

Answer 1

+/- 2%

Question 2

Max landing and takeoff tailwind component

Answer 2

15 kts

Question 3

Max operating altitude

Answer 3

43,100

Question 4

Max takeoff and landing altitude

Answer 4

8,400

Question 5

Turbulent air penetration speed

Answer 5

270 kts below 25000 feet, 280 or M0,82 whichever is lower at 25000 feet and above.

Question 6

Minimum airspeed for turbulent air penetration

Answer 6

15 kts above minimum maneuvering speed when airspeed below M0,82

Question 7

When shall the HF-radio not be operated?

Answer 7

During refuelling.

Question 8

When shall the WX-radar not be operated?

Answer 8

In a hangar (test mode ok) or within 15m of any fuel spill.

Question 9

Max allowable difference between captain and F/O’s altimeter prior to takeoff for RVSM operations is?

Answer 9

75 feet.

Question 10

What are the restrictions on the standby altimeter?

Answer 10

It does not meet RVSM accuracy requirements.

Question 11

What runway width are crosswind limits based on?

Answer 11

45 m or greater.

Question 12

When is a rolling takeoff strongly adviced?

Answer 12

With crosswinds over 20 kts.

Question 13

What are the takeoff crosswind limits for dry, wet and contaminated runway? Restrictions for weight and CG?

Answer 13

40 / 34 / 24. Reduce limit by 1 kt for every 5000 kg below 250 000 kg. Reduce limit by 10 kts for CG greater than 39%.

Question 14

Can takeoff or landing on untreated snow be accomplished?

Answer 14

Only when no melting is present.

Question 15

Are there differences between normal and EO crosswind landing limits?

Answer 15

No.

Question 16

What are the crosswind landing limits for: dry / wet / contaminated / contaminated ice?

Answer 16

45 / 40 / 20 / 17.

Question 17

Crosswind landing limit corrections are?

Answer 17

For a a landing on a wet or contaminated runway with asymmetric reverse thrust, reduce crosswind limit by 5 kts. Sideslip only technique is not allowed with crosswinds over 30 kts (200 and F) or 35 kts (300).

Question 18

Max differential pressure in flight and for takeoff and landing?

Answer 18

9.1 psi / 0,11 psi for takeoff and landing.

Question 19

Without LAND 2 or LAND 3, when must the A/P be disengaged?

Answer 19

Below 200 ft AGL.

Question 20

Allowable wind speeds for autoland are?

Answer 20

Headwind 25, tailwind 15, crosswind 25.

Question 21

Max/min glideslope for autoland?

Answer 21

3,25 / 2,5

Question 22

Oil temperature limits for RR engines?

Answer 22

-40 degrees C for start, 50 degrees C for takeoff.

Question 23

What are the fuel temperature limitations?

Answer 23

Max temp 49 degrees C. Must be above -41 degrees C for takeoff and 3 degrees C above fuel freezing temperature in-flight.

Question 24

What is max latitude for ADIRU alignment?

Answer 24

78 deg

Question 25

How much fuel may be in the center tanks with less than full main tanks?

Answer 25

1360 kg

Question 26

VNAV approach validation.

Answer 26

In nav database. Final approach course within 3 deg. of published. FAF to RW/MAWP within 1 nm. Minimum crossing altitude infringement max 10 ft. G/S within +/- 0.10.

Question 27

What are GE engines warm up requirements and recommendations?

Answer 27

Requirement, oil temperature above bottom of scale. Recommendation is to run for 3 mins with thrust for taxi operations.

Question 28

When shall A/P at latest be disengaged for RNAV visual approach without DA/MDA?

Answer 28

300 ft AAL

Question 29

When will LNAV engage in case of a missed approach?

Answer 29

Above 50 ft with A/P not engaged, above 200 ft with A/P engaged.

Question 30

GE cooldown recommendations?

Answer 30

3 mins at taxi thrust.

Question 31

Which control movements need confirmation from both pilots during non-normals?

Answer 31

1. A/T arm switch 2. Thrust lever of failed engine 3. Fuel control switch 4. Engine/APU fire switch or cargo fire arming switch 5. Generator drive disconnect

Question 32

Cooldown time for RR and GE engines?

Answer 32

1 min and 3 minutes.

Question 33

For a VNAV approach, final approach course shall be checked to be within how many degrees of published approach course?

Answer 33

3 degrees.

Question 34

VNAV app: minimum crossing altitude may be infringed by?

Answer 34

10 feet

Question 35

Max cabin altitude for cruise is?

Answer 35

8000 ft

Question 36

When does pressurization information show on EICAS? When does it turn red?

Answer 36

Cabin altitude above 8500 ft. Above 10000 ft.