B787 Limitations

Front 1

Max Runway Slope

Back 1

+ or - 2%

Front 2

# Max Tail-wind on take-off / landing

Back 2

15 knots

Front 3

Maximum operating altitude

Back 3

43,100 ft

Front 4

Maximum takeoff or landing altitude

Back 4

14,000ft

Front 5

Optimum Turbulent penetration speed

Back 5

290kts below 25,000ft and 310 / 0.84M (whichever is lower) at and above 25,000ft

Front 6

Max crosswind for takeoff and landing

Back 6

35 kts for takeoff and 33 knots for landing

Front 7

# Minimum operational Weather radar distance of a hanger and fuel spill

Back 7

Avoid operation of Weather Radar in hanger or 50ft of refuelling or a fuel spill

Front 8

If your altimeters failed and you only had the ISFD operating, can you fly in RVSM airspace?

Back 8

No

Front 9

If the captains altimeter was reading 20ft and the FO's read 100ft is the plane allowed to be dispatched?

Back 9

No. The maximum difference allowable is 75ft discrepancy.

Front 10

Max Taxi (ramp) Weight

Back 10

228,383kgs

Front 11

Max Takeoff weight

Back 11

227,930kgs

Front 12

Max Landing weight

Back 12

172,365kgs

Front 13

Max zero fuel weight

Back 13

161,025kgs

Front 14

# Minimum height allowable to engage the autopilot

Back 14

200ft

Front 15

# Max height allowable to use auto land ops

Back 15

8,400ft

Front 16

# Without LAND 3 or LAND 2 annunciation, what is the height you must disconnect the AP below?

Back 16

You must disconnect the AP below 100ft AGL.

Front 17

# With LAND 2 or LAND 3 annunciated, and the glide slope greater than 3.25*, at what height must you disconnect the AP?

Back 17

You must disconnect the AP below 100ft

Front 18

If the glide path angle is more than 3.77 degrees, when must the autopilot be disconnected?

Back 18

50ft below the MDA

Front 19

If the main tanks are not fuel, are you allowed to load the centre tank?

Back 19

No, however the centre tank may contain up to 10,000kgs of fuel with the main tanks not full provided that the center tank fuel weight plus the actual Zero fuel weight does not exceed the maximum Zero fuel weight

Front 20

In what phase of flight cant you use FLCH?

Back 20

On final approach below 1000ft AGL

Front 21

What is the lowest oil temperature needed for engine start?

Back 21

-40•C

Front 22

Are you authorised to back an aeroplane with reverse thrust?

Back 22

No

Front 23

Can you deploy reverse thrust in flight?

Back 23

No

Front 24

When taxiing what is the N1 limit?

Back 24

45%

Front 25

For winds greater than 55 kts on taxi, what should the N1 be?

Back 25

Limit engine thrust to idle

Front 26

Maximum altitude flap extension?

Back 26

20,000ft

Front 27

What is the maximum and minimum fuel temperature (JET a-1) for takeoff

Back 27

49•C

Front 28

What is the maximum inflight temperature?

Back 28

65•C and -29•C