Limitations

Question 1

Maximum take-off tailwind

Answer 1

10kts

Question 2

Maximum landing tailwind

Answer 2

15 kts

Question 3

Crosswind PVD take-off

Answer 3

15kts

Question 4

Bird strike Protection speed

Answer 4

Do not exceed 313kts below 8,000ft

Question 5

Turbulent air penetration speed

Answer 5

290kts / .78 Mach, whichever is lower.

Question 6

After take-off, the autopilot must not be engaged below

Answer 6

500 feet AGL.

Question 7

Use of aileron trim with autopilot engaged

Answer 7

Is prohibited.

Question 8

Max autoland Headwind

Answer 8

25kts

Question 9

Max autoland Tailwind

Answer 9

15kts

Question 10

Max autoland crosswind

Answer 10

25kts

Question 11

Max autoland crosswind USA Ops

Answer 11

15kts

Question 12

In an approach using v/s mode, the autopilot must be disengaged

Answer 12

At or above 250 feet ARTE (above runway threshold elevation)

Question 13

On a single channel ILS approach, disengage the autopilot at

Answer 13

Not less than 150 feet ARTE

Question 14

Maximum operating altitude?

Answer 14

43,100 feet

Question 15

The Autopilot must be disengaged in severe turbulence

Answer 15

Unless CWS is installed and selected.

Question 16

The maximum & minimum glide slope angle for automatic landings are

Answer 16

3.1 degrees & 2.5 degrees

Question 17

Automatic landings may be made with flaps

Answer 17

25 or 30 only.

Question 18

For automatic landings how may hydraulic systems must be operating?

Answer 18

All three.

Question 19

For automatic landing how many electrical systems must be operating?

Answer 19

Two electrical systems (the APU generator may be used to power one system.

Question 20

For automatic landing the inertial reference system IRS associated with the engaged autopilots

Answer 20

Must be in NAV mode.

Question 21

For automatic landing what autoland status annunciations and how many autopilots engaged below 600 feet?

Answer 21

At least 2 autopilots & LAND 2 or LAND 3

Question 22

Do not use FLCH

Answer 22

on final approach below 1000 feet AFE.

Question 23

The auto throttle on a single engine approach

Answer 23

must not be used.

Question 24

Continuous ignition must be on (engine start selector in the CONT position)

Answer 24

while operating in severe turbulence.

[Note: continuous ignition is automatically provided in icing conditions when engine anti-ice is on.]

Question 25

Max engine EGT TAKEOFF

Answer 25

785 degrees C 5 mins [increased to 10 mins provides this use is restricted to situations where an engine failure actually occurs, and there is an obstacle in the takeoff flight path.]

Question 26

Max engine EGT Maximum Continuous

Answer 26

733 degrees C

Question 27

Max engine EGT Starting

Answer 27

600 degrees C

Question 28

Max engine EGT Overtemperature

Answer 28

805 degrees C 20 seconds

Question 29

Fuel imbalance, wing tanks less than 21,773 kg

Answer 29

1134 kg [linear reduction between figures[

Question 30

Fuel imbalance, wing tanks more than 36,200 kg

Answer 30

680 kg [linear reduction between figures]

Question 31

Reverse thrust

Answer 31

Ground use only.

Question 32

The maximum altitude for flap extension is

Answer 32

20,000 feet