Limitations

Question 1

Maximum Operating Pressure Altitude is:
• 43,100 ft.
• 45,100 ft.
• 41,500 ft.
• 41,300 ft.

Answer 1

• 43,100 ft.

Question 2

The maximum landing gross weight is:

• 503,500 pounds.
• 355,000 pounds.
• 380,000 pounds.
• 430,000 pounds.

Answer 2

• 380,000 pounds.

Question 3

Engine oil temperature prior to engine start must be __ degrees or greater.
• There is no minimum
• -22c
• 0c
• -40c

Answer 3

• -40c

Question 4

For 90 degree crosswinds between 40 and 55 kts, limit engine thrust to a setting normally used for taxi (45% N1).
A. True
B. False

Answer 4

A. True

Question 5

Do not extend flaps above:

• 15,000 ft.
• 43,100 ft.
• 20,000 ft.
• 18,000 ft.

Answer 5

• 20,000 ft.

Question 6

Maximum wind component speeds when T/O minima are predicated on HUD takeoff operations are __ .
• 15 kts headwind / 15 kts tailwind / 10 kts crosswind.
• 25 kts headwind / 10 kts tailwind / 5 kts crosswind.
• 25 kts headwind / 15 kts tailwind / 25 kts crosswind.
• 25 kts headwind / 15 kts tailwind / 20 kts crosswind.

Answer 6

• 25 kts headwind / 15 kts tailwind / 20 kts crosswind.

Question 7

Maximum takeoff gross weight is:
• 502,500 lbs.
• 355,000 lbs.
• 380,000 lbs.
• 503,500 lbs.

Answer 7

• 502,500 lbs.

Question 8

Maximum allowable wind speeds for autoland operations are:
• 25 kts headwind, 15 kts tailwind, 25 kts crosswind.
• 20 kts headwind, 10 kts tailwind, 20 kts crosswind.
• 38 kts headwind, 15 kts tailwind, 25 kts crosswind.
• None

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.
• 2.25 max / 3.25 min
• 2.0 max / 3.0 min
• 3.25 max / 2.5 min
• 4.0 max / 2.5 min

Answer 9

3.25 max / 2.5 min

Question 10

The B787 is certified as Category __ for instrument approaches and Category __ for circling approaches.
• D/D
• B/D
• A/C
• D/C

Answer 10

• D/D

Question 11

What is the maximum takeoff and landing pressure altitude?
• 14,000 ft.
• 8,500 ft.
• 10,000 ft.
• 12,500 ft.

Answer 11

• 14,000 ft.

Question 12

What is the maximum unrestricted T/O and Landing tailwind component?
• 5 kts.
• 25 kts.
• 15 kts.
• 20 kts.

Answer 12

• 15 kts.

Question 13

The Ground Proximity Warning System (GPWS) terrain display can be used for navigation.
A. True
B. False

Answer 13

B. False

Question 14

Do not use speed brakes inflight:
A. With flaps extended.
B. When altitude is less than 2000 ft AGL.
C. When altitude is less than 1000 ft AGL.
D. All the above.

Answer 14

C. When altitude is less than 1000 ft AGL.

Question 15

When using Autoland:
A. Either 20, 25, or 30 flaps may be used.
B. Maximum ILS glide slope angle is 2.5 degrees.
C. May land over max landing weight if caution is used.
D. All the above

Answer 15

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

Question 16

The flap placard speed for flaps 1 is:
• 265 kts.
• 235 kts.
• 215 kts.
• 250 kts.

Answer 16

• 250 kts.

Question 17

Category Ill / Autoland is approved for all landing flaps settings only if both engines are operating.
A. True
B. False

Answer 17

B. False

Question 18

Which of the following statements are true regarding autoland operations on the B787?
• Autolandings are certified even if all three hydraulic systems are lost.
• The B787 is not certified for autolandings with the loss of any one of the 3 hydraulic systems.
• Autolandings are not certified with the loss of the right hydraulic system.
• The B787 is not authorized for autolandings when using GLS approach procedures.

Answer 18

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

Question 19

Maximum Cabin Differential Pressure is:
• 0.11 psi.
• 1.0 psi.
• 8.5 psi
• 9.9 psi.

Answer 19

• 9.9 psi.

Question 20

The autopilot must not be engaged:
• below 200 ft after takeoff.
• If NO AUTOLAND is displayed.
• On non-precision approaches below 1000ft.
• If the EICAS Message FLAP PRIMARY is displayed.

Answer 20

• below 200 ft after takeoff.

Question 21

The Turbulent Air Penetration Speed is:
A. 290 KIAS below 25,000 feet.
B. 310 KIAS / .84 Mach at and above 25,000 feet.
C. 250 KIAS.
D. Both A and B.

Answer 21

D. Both A and B.

Question 22

The maximum flap placard speed for flaps 30 is:
• 185 kts.
• 190 kts.
• 170 kts.
• 160 kts

Answer 22

• 170 kts.

Question 23

The use of VNAV and/or LNAV with QFE selected is prohibited.
A. True
B. False

Answer 23

A. True

Question 24

What is the maximum ramp weight?

• 380,000 lbs.
• 460,000 lbs.
• 503,500 lbs.
• 502,500 lbs.

Answer 24

• 503,500 lbs.

Question 25

What is the maximum zero fuel weight?
• 355,000 lbs.
• 502,500 lbs.
• 380,000 lbs.
• 460,000 lbs.

Answer 25

• 355,000 lbs.

Question 26

What considerations must be made when using QFE instead of QNH as an altitude reference?
A. The altitude reference for the PFD/HUD (QFE vs. QNH) must be selected in the FMC.
B. Vertical (VNAV) navigation is not allowed.
C. The use of IAN procedures is prohibited.
D. All the above.

Answer 26

D. All the above.

Question 27

The flap placard speed for flaps 5 is:
• 230 kts.
• 215 kts.
• 190 kts.
• 210 kts.

Answer 27

• 230 kts.

Question 28

The flap placard speed for flaps 15 is:

• 235 kts.
• 195 kts.
• 215 kts.
• 185 kts.

Answer 28

• 215 kts.

Question 29

The flap placard speed for flaps 20 is:
• 230 kts.
• 210 kts.
• 190 kts.
• 170 kts.

Answer 29

• 210 kts.

Question 30

The flap placard speed for flaps 25 is:
• 170 kts.
• 180 kts.
• 190 kts. 
• 215 kts.

Answer 30

• 180 kts.

Question 31

Use of reverse thrust is prohibited:
A. Below 80 kts.
B. For backing the aircraft.
C. lnflight.
D. Both B and C

Answer 31

D. Both B and C

Question 32

Use of JP4 and Jet B is prohibited?
A. True
B. False

Answer 32

A. True

Question 33

The maximum fuel temperature at takeoff is:
• + 37 degrees C.
• + 47 degrees C.
• + 49 degrees C.
• There is no maximum.

Answer 33

• + 49 degrees C.

Question 34

lnflight fuel temperature is limited to __ (Jet A, A1, JP-5 or JP-8).
• + 65 degrees C
• + 49 degrees C
• + 15 degrees C
• + 37 degrees C

Answer 34

• + 65 degrees C

Question 35

The fuel tank temperature for T/O is between -23 degrees C and -29 degrees C, each main and center tank fuel load must be less than 22,000 lbs.
A. True
B. False

Answer 35

A. True

Question 36

The center fuel tank may contain up to 22,000 lbs of fuel with less than full main tanks provided:
A. Center tank fuel weight is added to the actual ZFW and the combined total does not exceed the maximum ZFW.
B. Maximum imbalance between left and right main tanks does not exceed 4500 lbs.
C. Center of gravity remains within limits.
D. Both A and C.

Answer 36

D. Both A and C.