B-787 Limitations

Question 1

Turbulent air penetration speed
At and above 25,000 feet

Answer 1

310 knots / .84 Mach
(Whichever is lower)

Question 2

Turbulent air penetration speed below 25,000 feet

Answer 2

290 KIAS

Question 3

Maximum operating pressure altitude 787–8, 787–9

Answer 3

43,100 feet

Question 4

Maximum operating pressure altitude is 787–10

Answer 4

41,100 feet

Question 5

TAKEOFF Crosswind guidelines 787–8, 787–9, 787–10
ALL WEIGHTS

Answer 5

40 knots

Question 6

LANDING crosswind guidelines
DRY,
RW condition code 6

Answer 6

40 knots

Question 7

Autoflight limitations
5

Answer 7

Do not engage the autopilot below a minimum engagement altitude of 200 feet AGL after takeoff

Autoland capability may only be used for operations to runways at or below 8400 feet AFE

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 135 feet AGL.

Without LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25°, the autopilot must be disengaged below 100 feet AGL.

Do not use FLCH on final approach below 1000 feet AFE

Question 8

LOW visibility (HUD) takeoff
(RVR <500)
MAX WINDS

Answer 8

Headwind 25 knots
Tailwind 15 knots
Crosswinds 15 knots

Question 9

SA CAT I APPROACHES
Maximum X-wind component speed

Answer 9

15 knots

Question 10

AUTO-LAND, maximum wind component speeds
Cat I, II, & III

Answer 10

CAT I
Headwind 25 knots
Crosswind 25 knots
Tailwind 15 knots

CAT II & III
Headwind 25 knots
Crosswind 15 knots
Tailwind 10 knots

Question 11

AUTO-LAND
Maximum slope angle

Answer 11

3.25°

Question 12

AUTO-LAND
Minimum glideslope angle

Answer 12

2.50°

Question 13

Minimum oil quantity PRIOR to start

Answer 13

18 quarts

Question 14

Minimum oil temperature must be greater than ____ for engine start

Answer 14

-40° C

Question 15

When is REVERSE THRUST prohibited?

Answer 15

Intentional selection of reverse thrust in flight is prohibited

Back in the airplane with use of reverse thrust is prohibited

Question 16

Control inputs to avoid

Answer 16

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, role, or yaw. As they may result in structural failure at any speed, including below VA.

Question 17

Do not use speed brakes below ______ feet AGL

Answer 17

1,000 feet AGL

Question 18

Maximum G load flaps up

Answer 18

2.5g to - 1.0g

Question 19

Maximum G load flaps down

Answer 19

+2.0g to -0.0g

Question 20

Maximum altitude flaps extended

Answer 20

20,000 feet

Question 21

Do not exceed ____% N1 during static engine run up.

Answer 21

55% N1

Question 22

Do not release brakes with N1 greater than ___%. A tip up can occur and directional control can be reduced.

Answer 22

55% N1

Question 23

Icing conditions exist when
OAT (ground) or TAT (flight) is ____ ‘°C or below

Answer 23

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

Question 24

Do not exceed ___% in one within congested areas and less cleared by an appropriate personnel.

Answer 24

35%