Limitations

Question 1

Maximum Takeoff and Landing Tailwind Component

Answer 1

15 knots

Question 2

Severe turbulent air penetration speed (in severe turbulence) is defined as:

Answer 2

270 knots below 25,000 feet,
280 knots or 0.82 Mach whichever is lower at 25,000 feet and above.
Maintain a minimum speed of 15 knots above the minimum maneuvering speed at all altitudes when airspeed is below 0.82 Mach.

Question 3

Do not operate HF radios

Answer 3

during refueling operations

Question 4

Avoid weather radar operation in a hangar or within…….. of fueling operations or a fuel spill.

Answer 4

50 feet (15.25 meters)

Question 5

The autopilot must not be engaged below a minimum engage altitude of

Answer 5

200 feet AGL after takeoff.

Question 6

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged

Answer 6

below 200 feet AGL.

Question 7

Maximum allowable Headwind for an Autoland is

Answer 7

25 knots

Question 8

Maximum allowable Tailwind for an Autoland is

Answer 8

15 knots

Question 9

Maximum allowable crosswind for an Autoland is

Answer 9

25 knots (USA – 15 knots)

Question 10

The maximum glideslope angle for an Autoland is

Answer 10

3.25 degrees.

Question 11

The minimum glideslope angle for an Autoland is

Answer 11

2.5 degrees.

Question 12

Automatic landings can be made using flaps 20 or 30, with both engines operative or one engine inoperative. The autopilot flight director system (AFDS) autoland status annunciation must display LAND 2 or LAND 3 and the ………message must not be present.
…………….must not be displayed.

Answer 12

SLATS DRIVE EICAS

SGL SOURCE DISPLAYS, RAD ALT or ILS

Question 13

Do not use FLCH on final approach below

Answer 13

1,000 feet AFE.

Question 14

G-YMMA - G-YMMU
# Oil temperature must be greater than .......for engine start and ..........before advancing thrust levers to takeoff power.

Answer 14

-40 degrees C

50 degrees C

Question 15

Intentional selection of reverse thrust in flight is.

Answer 15

prohibited

Question 16

Backing the airplane with use of reverse thrust is.

Answer 16

prohibited

Question 17

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may

Answer 17

result in structural failure at any speed, including below VA.

Question 18

The maximum altitude with flaps extended is

Answer 18

20,000 feet.

Question 19

Land climb limit weight:-
There is no requirement to check the Landing Climb Limit Weight chart if you are making a normal weight approach below the WAT limit.
Neither would it be necessary if you are planning to land with Flap 20. Eg SE

So, when should the LCW chart be checked?

Answer 19

IF Landing Overweight AND a Flap 25 or Flap 30 landing is planned.
Or as above with a normal landing above the WAT limit

When you do the Overweight Landing NNC you will notice that at weights over approximately 267T for a -200 and 310T for a -300 you will not be able to use Flap 30.