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BOEING 787 > LIMITATION B787 > Flashcards

LIMITATION B787 Flashcards

1
Q

MAX RWY SLOPE?

A

+/- 2%

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2
Q

MAXIMUM TAKE OFF AND LANDING TAILWIND COMPONENT?

A

+/- 10 KTS

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3
Q

MAXIMUM OPERATING ALTITUDE?

A

43100 FT

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4
Q

MAXIMUM TAKE OFF AND LANDING ALTITUDE

A

14000FT

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5
Q

CNA YOU FLY RVSM WITH ISFD?

A

NO

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6
Q

WHEN NOT TO USE THE HF?

A

WHILE REFUELLING

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7
Q

SA-SB MAX CROSSIWINDS?

A

TAKE OFF 35KTS LANDING 33 KTS DEMOSTRATED

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8
Q

SC-SI MAX DEMOSTRATED TAKE OF AND LANDING CROSSWINDS?

A

TAKE OFF 29 KTS LANDING 35 KTS

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9
Q

SEVERE TURBULENCE SPEED?

A

290 KTS BELOW 25000FT

310kts or .84 M ABOVE 25000ft

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10
Q

WHAT IS THE MAX DIFFERENCE IN BETWEEN CPT AND FO ALTIMETERS AND FIELD ?

A

75 FEET

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11
Q

WHEN IS FORBIDDEN TO USE THE WEATHER RADAR?

A

IN HANGAR, OR WITHIN 15 MTRS FROM FUELING OPERATIONS,AVOID TO USE WHEN PERSONNEL ARE CLOSED TO THE PLANE

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12
Q

MAX TAXI WEIGHT 788

A

228,383 KG

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13
Q

MAX TAXI WEIGHT 789

A

251,743 KGS

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14
Q

MAX TO WEIGHT 788

A

227,930 KGS

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15
Q

MAX TAKE OFF WEIGHT 789

A

250,863 KGS

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16
Q

MAX LDG WEIGHT 788

A

172,365 KGS

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17
Q

MAX LDG WEIGHT 789

A

192.776 KGS

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18
Q

MAX ZFW 788

A

161.025 KGS

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19
Q

MAX ZFW 789

A

181.436 KGS

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20
Q

WHAT IS THE MINIMUM ALTITUDE TO ENGAGE THE A/P?

A

200FT

21
Q

MAX AUTOLAND CAPABILITY ALTITUDE?

A

8400 FT

22
Q

WITH OUT LAND 2/3 SHOWN A/P MUST BE DISENGAGED BY ?

A

100FT

23
Q

WITHOUT LAND 2/3 ON B787-9 AT WHICH ALTITUDE THE A/P MUST BE DISENGAGED?

A

135 FT

24
Q

WITH LAND 2 AND LAND 3 ANNUNCIATED WITH GS MORE THEN 3.25 DEGREES WHEN TO DISCONNECT THE A/P?

A

100 FT

25
Q

WITH GS GRATER THE 3.77 DEGREES WHEN TO DISCONNECT THE A/P?

A

DISENGAGE NOT LATER THEN 50 FT BELOW MDA/DH

26
Q

LOW VISIBILITY HUD TAKE OFF MAX WIND TAKE OFF

A

HEADWIND 25 KTS

TAIL 10 KTS

CROSS 20 KTS

27
Q

MAX LDG WIND FOR AUTOLAND

A

HEAD 25 KTS

TAIL 10KTS

CROSS 25 KTS

28
Q

MAX GS ANGLE?

A

3.25

29
Q

MINIMUM GS ANGLE?

A

2,5

30
Q

AUTOLAND FLAP CAPABILITY?

A

20/25/30 BOTH ENGINE OR ENGINE OUT

31
Q

WHEN NOT TO USE FLCH?

A

IN FINAL APPROACH BELOW 1000 FT AFE

32
Q

OIL TEMPERATURE LIMIT TO START?

A

GREATER THEN -40

33
Q

CROSSWIND 40 KTS HOW MUCH U LIMIT THE TRUST TOO?

A

45 %

34
Q

TAIL GREATER THE 5 KTS AND WIND GREATER THEN 35KTS TRUSTI LIMIT?

A

45 %

35
Q

WIND GREATER THEN51 KTS TRUST LIMIT ON GRD?

A

IDLE

36
Q

MAX ALTITUDE WITH FLAP EXTENDED?

A

20000FT

37
Q

MAX FUEL TEMP AT TAKE OFF?

A

49 *c

38
Q

In flight fuel temp limit?

A

-65*c

39
Q

Tank fuel temperature prior takeoff not less then?

A

-29*c

40
Q

Which temperature in flight to be maintained by the fuel?

A

At least 3 *c above freezing point

41
Q

How much fuel can be loaded ion the center tank with main tanks not full?

A

Up to 10000 kgs provided that the center tank fuel weight plus actual zfw doesn ‘t exceed the maximum zfw and cg respected

42
Q

When is prohibited to use LOOK AHEAD TERRAIN?

A

15 nm range in take off landing approach in airport not in the database

43
Q

AIRSPEED UNRELIABLE MAX SPEED

A

ABOVE 40000FT 250 KTS

40000FT AND 38000FT 260KTS

38000FT TO 35000FT 270 KTS

BELOW 35000FT 290KTS

44
Q

WHEN USING ALTN GEAR EXTENSION AND FLAPS ARE 20 WHAT IS THE SPEED LIMIT?

A

190 KTS

45
Q

MAX CABIN PRESSURE POSITIVE RELIEF VALVE VALUE>?

A

9.9 PSI

46
Q

MAX DIFF PRESS TO AND LDG?

A

0.11 PSI

47
Q

FLAP LIMIT FOR JETTISON

A

DO NOT JETTISON WITH FLAP 30

48
Q

MAX G

A

FLAP UP +2.5 AND -1.0

FLAP DOWN +2.0 AND 0.0

49
Q

MAX IMBALANCE FUEL

A

WITH 30000KG OF FUEL MAX IS 680 KG

WITH 19000 KG FUEL MAX IMBALANCE 1100KGS

BOEING 787 (12 decks)

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