Limitations

Question 1

Runway slope?

Answer 1

+/- 2%

Question 2

Max operating altitude

Answer 2

43,100 Ft pressure altitude

Question 3

Max takeoff and landing altitude

Answer 3

8,400ft pressure altutude

Question 4

Max takeoff and landing tailwind component

Answer 4

15kts

Question 5

Severe turbulent air penetration speed

Answer 5

290Kias / .78Mach, whichever is lower

Question 6

HF limitation

Answer 6

Do not operate during refuelimg

Question 7

FLCH limitation

Answer 7

Do not use on final approach below 1000 AFE

Question 8

The APU starter duty cycle limitation

Answer 8

Maximum of three consecutive starts or attempts within a 60 minute period.

Question 9

Maximum allowable inflight difference between captain and FO altimeter for RVSM?

Answer 9

200Ft

Question 10

Maximum allowable difference between CAPT/FO and field elevation at all altitudes?

Answer 10

75ft

Question 11

Max diffrences between captain and first officer altimeters on the ground?
Sea level 5000ft, and 10,000ft

Answer 11

Sea level: 40ft
5,000ft: 45ft
10 000ft: 50ft

Question 12

weather radar limitation

Answer 12

Avoid operation in hangar

Question 13

Minimum autopilot engagement altitude after takeoff?

Answer 13

200AGL

Question 14

Aileron trim limitation

Answer 14

Prohibited with autopilot engaged

Question 15

Maximum allowable wind speeds when landing weather minima are predicated on autoland operations?

Answer 15

Headwind, crosswind: 25kts

Tailwind: 15kts

Question 16

Engine vibration limitation

Answer 16

Crew shall not blank engine vibration display during takeoff

Question 17

Center tank limitation?

Answer 17

The center tank may contain up to 10,000kg of fuel with less than full main tanks provided center tank fuel weight plus zero fuel weight is less thsn max zero fuel weight and with the cg limit.

Question 18

Reverse thrust limitations

Answer 18

For ground use only and

Question 19

Max altitude with flaps extended

Answer 19

20,000ft

Question 20

AFM limitation
#Avoid rapid.....

Answer 20

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw. (Ex: large side slip angles) as they may result in structual failure at any speed, including below VA.