Lim

Question 1

Maximum Operating Pressure Altitude is:

Answer 1

43,100 ft.

Question 2

The maximum landing gross weight is:

Answer 2

380,000 pounds.

Question 3

Engine oil temperature prior to engine start must be ____ degrees or greater.

Answer 3

-40 C

Question 4

For crosswinds greater than 37 knots, limit engine thrust to a setting normally used for taxi (45% N1).

Answer 4

A. True

Question 5

Do not extend flaps above:

Answer 5

20,000 ft.

Question 6

Maximum wind component speeds whe T/O minima are predicted on HUD takeoff operations are ____.

Answer 6

25 kts headwind / 15 kts tailwind / 15 kts crosswind.

Question 7

Maximum takeoff gross weight is:

Answer 7

502,500 lbs.

Question 8

Maximum allowable wind speeds for autoland operations in other than CAT 2 or CAT 3 conditions are:

Answer 8

25 kts headwind, 15 kts tailwind, 25 kts crosswind.

Question 9

The maximum and minimum glidepath angle for ILS/GLS automatic landing (or approaches using IAN) is ____ degrees.

Answer 9

3.25 max / 2.5 min

Question 10

The B787 is certified as Category ____ for instrument approaches and Category ____ for circling approaches.

Answer 10

D / D

Question 11

What is the maximum takeoff and landing pressure altitude?

Answer 11

14,000 ft.

Question 12

What is the maximum unrestricted T/O and Landing tailwind component?

Answer 12

10 kts.

Question 13

The Ground Proximately Warning System (GPWS) terrain display can be used for navigation.

Answer 13

B. False

Question 14

Do not use speed brakes inflight:

Answer 14

C. When altitude is less than 1000 ft AGL.

Question 15

When using Autoland:

Answer 15

A. Either 20, 25, or 30 flaps may be used.

Question 16

The flap placard speed for flaps 1 is:

Answer 16

250 kts.

Question 17

Category III / Autoland is approved for all landing flaps settings only if both engines are operating.

Answer 17

B. False

Question 18

Which of the following statements are true regarding autoland operations on the B787?

Answer 18

The B787 is not authorized for autolandings when using GLS approach procedures.

Question 19

Maximum Cabin Differential Pressure is:

Answer 19

9.9 psi.

Question 20

The autopilot must not be engaged:

Answer 20

below 200ft. after takeoff

Question 21

The Turbulent Air Penetration Speed is:

Answer 21

A. 290 KIAS below 25,000 feet.

Question 22

The maximum flap placard speed for flaps 30 is:

Answer 22

170 kts.

Question 23

What is the maximum ramp weight?

Answer 23

503,500 lbs.

Question 24

What is the maximum zero fuel weight?

Answer 24

355,000 lbs.

Question 25

The flap placard speed for flaps 5 is:

Answer 25

230 kts.

Question 26

The flap placard speed for flaps 15 is:

Answer 26

215 kts.

Question 27

The flap placard speed for flaps 20 is:

Answer 27

210 kts.

Question 28

The flap placard speed for flaps 25 is:

Answer 28

180 kts.

Question 29

Use of reverse thrust is prohibited:

Answer 29

B. For backing the aircraft.

C. Inflight.

Question 30

Use of JP4 and Jet B is prohibited?

Answer 30

A. True

Question 31

The maximum fuel temperature at takeoff is:

Answer 31

+49 degrees C.

Question 32

Inflight fuel temperature is limited to ____ (Jet A, A1, JP-5 or JP-8).

Answer 32

+65 degrees C.

Question 33

For aircraft 901 through 904, the fuel tank temperature for T/O is between -23 degrees C and -29 degrees C, each main and cennter tank fuel must be less than 22,000 lbs.

Answer 33

A. True

Question 34

The center fuel tank may contain up to 22,000 lbs. of fuel with less than full main tanks provided:

Answer 34

A. Center tank fuel weight is added to the actual ZFW and the combined total does not exceed the maximum ZFW.
C. Center of gravity remains within limits.

Question 35

For SATCOM conference calls, only the Center Audio Control Panel may be used.

Answer 35

A. True