Limitations

Question 1

Category for Approaches?

Answer 1

Category D both Straight In and Circling

Question 2

Max Operating Pressure Altitudes

787-8?
787-9?
787-10?

Answer 2

787-8,9 43,100 ft

787-10 41,100 ft

Question 3

Max TO and LDG ALT?

Answer 3

14,000 ft

Question 4

Max Runway Slope?

Answer 4

+/- 2%

Question 5

Max Tailwind, TO and LDG?

Answer 5

15 kts

Question 6

Max Landing Gear Speed?

VLO?
VLE?

Answer 6

270 kts / .82 Mach for both

Question 7

Turbulent Air Penetration Speed

At and Above 25,000 ft?

Below 25,000 ft?

Answer 7

At and Above 25,000

310 KIAS / .84 Mach, whichever lower

Below 25,000

290 KIAS

Question 8

Takeoff Crosswind Guidelines

Answer 8

40 kts all types, all weights on dry runway

starred

Question 9

LANDING CROSSWIND GUIDELINE

Answer 9

40 knots for all operations, single engine and all engine, all types and weights

Question 10

Gross Takeoff Weights?

787-8

787-9

787-10

Answer 10

787-8 502.5

787-9 561.5

787-10 560

Question 11

Max Landing Weights

787-8

787-9

787-10

Answer 11

787-8 380

787-9 425

787-10 445

Question 12

Max differential pressure?

For TO and LDG?

Answer 12

9.9 PSI

.11 PSI

Question 13

Minimum ALT for autopilot engagement after TO?

Answer 13

200 ft

Question 14

Max Airfield Elevation for Autoland?

Answer 14

8,400 ft

Question 15

Without LAND 2 or LAND 3, when must autopilot be disengaged?

Answer 15

135 ft AGL

Question 16

If LAND 2 or LAND 3, but glide slope is >3.25 degrees, when must autopilot be disengaged?

Answer 16

100 ft AGL

Question 17

If glidepath > 3.77 degrees, when must autopilot be disengaged?

Answer 17

No later than 50 ft below DH/MDA

Question 18

Min ALT for FLCH on approach?

Answer 18

1,000 ft AFE

Question 19

Max Wind Component for takeoff with HUD?

Headwind?

Tailwind?

Crosswind?

Answer 19

Headwind 25 kts

Tailwind 15 kts

Crosswind 15 kts

Question 20

Max Wind for ILS Autoland

Headwind?

Tailwind?

Crosswind?

Answer 20

Headwind 25 kts

Tailwind 15 kts
(10 kts CAT II/III)

Crosswind 25 kts
(15 kts CAT II/III)

Question 21

Max glide slope angle for autoland?

Answer 21

3.25 degrees

Question 22

Min glide slope angle for autoland?

Answer 22

2.5 degrees

Question 23

Can you Autoland from a GLS approach?

Answer 23

No, even if LAND 2 or LAND 3

Question 24

What flap configuration may be used with Autoland?

Engine Inoperative?

Above Max Landing Wt?

Answer 24

Flaps 20, 25, or 30

Both engines or one engine inoperative

Autoland not certified above max landing weight

Question 25

APU Start Cycle Limitation?

Answer 25

If APU does not start after 2nd attempt, 5 minute cooling period.

Question 26

HF Radio Limitation?

Answer 26

Do not use HF during fueling operations.

Question 27

Minimum Oil Quantity prior to Start? ***

Answer 27

18 quarts

Question 28

Min Oil Temp for Start? ***

Answer 28

-40 degrees C

Question 29

Reverse thrust in flight? ***

Answer 29

Intentional selection of reverse thrust in flight is prohibited

Question 30

Use of reverse thrust for backing the aircraft? ***

Answer 30

Prohibited

Question 31

Engine thrust Limitation for ground operations ***

Answer 31

No more than taxi thrust (45%) for more than 40 kt crosswinds No more than taxi thrust (45%) for 35 kt winds w/ a tailwind component greater than 5 kts

Question 32

Limits on Control Inputs? ***

Answer 32

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

Question 33

Max TO and LDG tailwind component if EECs in ALT mode

Answer 33

10 kt tailwind

Question 34

Flight maneuvering loads

Answer 34

Flaps up...........+2.5g to -1.0g Flaps down......+2.0g to 0.0g

Question 35

Max ALT for flap operation?

Answer 35

20,000 feet

Question 36

Min ALT for Speed Brake Usage?

Answer 36

1,000 ft AGL

Question 37

Does ISFD meet RVSM requirements?

Answer 37

No.

Question 38

What are the restrictions for the EGPWS?

Answer 38

Do not use for navigation. Use of look-ahead terrain alerting and terrain display functions prohibited within 15 NM of TO, approach or LDG at airport not contained in the GPWS database.

Question 39

Maximum altimeter differences for RVSM operation

Answer 39

Before takeoff, both captain’s and FO’s altimeters must indicate within 75 feet of field elevation. In flight, altimeters must agree within 200 feet.

Question 40

Min/Max Fuel temps - Jet A?

Answer 40

-37 deg C / 49 deg C In flight fuel tank temp must be 3 degrees warmer than minimum fuel temp.

Question 41

Maximum fuel tank imbalance | Taxi, takeoff and landing

Answer 41

Total main tank fuel > 68,300 lbs: 1,500 lbs difference Total main tank fuel < 41,900 lbs 2,500 lbs difference

Question 42

Fuel jettison / Flap setting?

Answer 42

Do not jettison fuel with Flaps 30

Question 43

Fuel density restriction?

Answer 43

Fuel density must be 6.3 to 7.1 lb/gal

Question 44

Fuel in Center Tank

Answer 44

If Center tank empty, use main tanks with all operable main tank pumps on, cross feeds closed. If Center Tank > 16,000#, use center tank fuel for all ops with all pumps on and cross feeds closed If Center Tank < 16,001#, use main tank fuel with main pumps on and cross feeds closed In cruise, if FUEL IN CENTER msg displays, burn center tank fuel until FUEL LOW CENTER displays.

Question 45

Max Tire Speed for TO

Answer 45

204 kts GS

Question 46

Max Tire Speed for LDG

Answer 46

226 kts GS

Question 47

Approximate fuel quantities

Answer 47

787-8 Main Tanks 37.3 Center Tank 148.7 Total 223.4 787-9, 10 Main Tanks 37.0 Center Tank 149.7 Total 223.6