787 Limitations

Question 1

Maximum altitude 787 8/9

Answer 1

43,100 feet

Question 2

Maximum altitude 787 10

Answer 2

41,100 feet

Question 3

Maximum Takeoff and Landing Tailwind Component

Answer 3

15 Knots

Question 4

Turbulent Air Penetration Speed

Answer 4

Severe Turbulence at and above 25,000 ft = 310/.84 Mach whichever is lower

Severe Turbulence below 25,000 feet = 290 knots

Question 5

Takeoff Crosswind 8/9/10

Answer 5

40 knots

Question 6

Landing Crosswinds Guideline

Answer 6

40 knots

Slide slip not recommended > 25 knots

Question 7

Icing Conditions Definition

Answer 7

Icing conditions exist when OAT (ground) or TAT (flight) is 10°C or below.

Question 8

Do not engage the autopilot below a minimum engagement altitude of_____ft AGL after takeoff

Answer 8

200

Question 9

Autoland capability may only be used for operations to runways at or below________feet AFE

Answer 9

8400

Question 10

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below _____ feet AGL.

Answer 10

135

Question 11

With LAND 2 or LAND 3 annunciated and glide slope angles greater than 3.25°, the autopilot pilot must be disengaged below _____ feet AGL.

Answer 11

100

Question 12

Do not use FLCH on final approach below _____ feet AFE

Answer 12

1000

Question 13

Maximum low visibility HUD takeoff wind components

Answer 13

Headwind 25 knots
Tailwind 15 knots
Crosswind 15 knots

Question 14

ILS Automatic Landing maximum and minimum glideslope angle is:

Answer 14

Maximum 3.25°
Minimum 2.50°

Question 15

Communication Limitations

Answer 15

Do not operate HF radio during fueling operations.

Question 16

Minimum oil quantity prior to start

Answer 16

18 quarts

Question 17

Minimum oil temperature

Answer 17

Greater than -40° C for engine start

Question 18

Reverse thrust in flight

Answer 18

Is prohibited

Question 19

Reverse Thrust for backing the airplane is

Answer 19

Prohibited

Question 20

Flight Control Inputs

Answer 20

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