Limitations

Question 1

Maximum Operating Pressure Altitude
1) 787-8/9
2) 787-10

Answer 1

1) 43,100 ft
2) 41,100 ft

Question 2

Maximum T/O and Landing tailwind component

Answer 2

15 kts

Question 3

Turbulent Air Penetration speed
1) At or above 25,000 ft
2) Below 25,000 ft

Answer 3

1) 310 kts / .84 Mach
2) 290 KIAS

Question 4

Maximum Crosswind Dry runway (6 RCC) T/O & Land

Answer 4

40 kts

Question 5

Icing Condition exist:
1) On the ground
2) In the air

Answer 5

1) OAT is 10°C or below
2) TAT is 10°C or below
AND
-Visible moisture is present
OR
-Standing water, ice, slush, snow, etc. is present on surfaces

• Use TAT to determine EAI selection on the ground to avoid nuisance EICAS messages

Question 6

Minimum autopilot engagement altitude after T/O

Answer 6

200 ft AGL

Question 7

Maximum runway altitude for autoland

Answer 7

8,400 ft field elevation

Question 8

Without LAND 2 or LAND 3 annunciated the autopilot must be disengaged below _____

Answer 8

135 ft AGL

Question 9

With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25°, the auto pilot must be disengaged below____

Answer 9

100 ft AGL

Question 10

Do not use FLCH ____

Answer 10

on final approach below 1000 ft AFE

Question 11

Low visibility (HUD) T/O (RVR <500)
1) Headwind
2) Tailwind
3) Crosswind

Answer 11

1) 25 kts
2) 15 kts
3) 15 kts

Question 12

SA CAT 1 approach max crosswind

Answer 12

15 kts

Question 13

Max Glideslope angle for an ILS autoland

Answer 13

3.25°

Question 14

Min glideslope angle for an ILS autoland

Answer 14

2.50°

Question 15

Do not operate HF radios during _____

Answer 15

Fueling operations

Question 16

Minimum Oil quantity for start

Answer 16

18 qts

Question 17

Minimum oil temp for engine start

Answer 17

-40°C

Question 18

Intentional selection of reverse thrust in flight is _______

Answer 18

Prohibited

Question 19

Backing the airplane up with reverse thrust is _____

Answer 19

Prohibited

Question 20

Avoid large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw as they may result in structural failure at any speed, including below VA

Question 21

If the glide path angle for approach is greater than 3.77°, the autopilot must be disengaged no later than ___

Answer 21

50 ft below DH/MDA

Question 22

Maximum Wind Component Speeds
ILS Automatic Landing
1) Headwind
2) Tailwind
3) Crosswind

Answer 22

1) Headwind 25kts
2) Tailwind 15 kts (10 kts CAT II/III)
3) Crosswind 25 kts (15 kts for Cat II/III)

Question 23

Which of the following are limitations on the use of speed brakes? [1.30]

A. Do not use the speed brakes with flaps 25 or 30.
B. Do not use speed brakes with the gear down.
C. Speed brakes can be used at any altitude.
D. Do not use the speed brakes inflight below 1000 feet.

Answer 23

D. Do not use the speed brakes inflight below 1000 feet.