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787 > 787 > Flashcards

787 Flashcards

1
Q

Turbulence penetration speed

A

290 KTS below FL250 - Lower of 310 / 0.84 above

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2
Q

Max flap extension altitude

A

20000 FT

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3
Q

Gear VLE/VLO

A

270 KTS

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4
Q

Speedbrake MIN ALT

A

800 FT

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5
Q

MAX tailwind

A

15 KTS(-8) / 10 KTS(-9)

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6
Q

MAX crosswind TO/LDG

A

40 / 37 (-8) // 33 / 40 (-9)

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7
Q

Autoland wind limits

A

25 KTS H-WIND + X-WIND

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8
Q

CAT II/III X-Wind limits

A

15 KTS

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9
Q

Left VS right altimeter difference limit

A

100 FT

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10
Q

Primary VS standby altimeter difference limit

A

200 FT

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11
Q

Primary altimeter VS field elevation difference limit

A

75 FT

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12
Q

Primary headings VS compass

A

+/- 10 degrees

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13
Q

Engine A/I ON - Ground operations

A

+10 C or less and visible moisture

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14
Q

Runup required

A

+3 C or less and visible moisture
40% N1 for 5 seconds every 60 minutes
(50-55% N1 if high engine vibrations occur)

Within 5 minutes of, or in conjunction with takeoff

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15
Q

T/O ALT range

A

377nm (60min) or ETOPS-754 (120min)

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16
Q

ETOPS 60 / 180 range

A

458nm / 1317nm

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17
Q

Engines on time required before T/O

A

3 minutes

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18
Q

MAX runway slope

A

+/- 2%

19
Q

MAX deviation without reroute

A

128nm

20
Q

MAX fuel load error

A

-0 / +400 KGS

21
Q

MAX WAT T/O weight error

A

+0 / -5000 KGS

22
Q

No ATM

A

1) Windshear or temperature inversion below 1500 AGL
2) Contaminated with slush, standing water or 25% snow or ice

23
Q

No Derate

A

Windshear below 1500 AGL

24
Q

Manual thrust landing REF speed

A

Half the steady state wind + the whole gust factor
(Wind 15 gust 20 = 7.5 + 5)

Headwind additive is bled off approaching the flare.
Gust factor additice is maintained to touchdown.

25
Q

Center tank fuel pump ON quantity

A

7.3

26
Q

Max rate of climb

A

VREF 30 +140

27
Q

Fuel burn KG/MIN

A

90 KG/MIN AIR / 22 KG/MIN GND

28
Q

Fuel required at ETOPS ALTN

A

Fuel to hold at 1500’ for 15 min and conduct an approach

29
Q

HDG REF to TRUE

A

Northern control area or 70N

30
Q

Waypoint sequencing max distance

A

21nm off track sequencing. OFST 99nm. 120nm total.

31
Q

RVSM check __ hours

A

1.0

32
Q

Fuel check __ hours

A

1.5

33
Q

Position report __ hours

A

2.0

34
Q

Fan ice removal

A

Prolonged flight in moderate / severe icing conditions with N1 at or below 70%, or when fan ice suspected due to engine vibrations…
Every 15 minutes, one engine at a time, reduce N1 to idle, then increase to 70% for 10-30 seconds.

35
Q

Severe damage indications

A

Airframe vibrations with abnormal engine indications

36
Q

APP mode selection criteria

A

Inside 18NM (ILS) or 23NM (GLS)
Tuned and identified
On intercept heading (maximum 120 degrees)
LOC and GS pointers appear in correct position

37
Q

ENG Oil Check

A

Less than 4 hours - 13L
4 hours or more - 18L

38
Q

Oxygen Check

A

1200 PSI Minimum

39
Q

Service Check

A

48 hours between each check. Must not expire airborne.
Always prior to…
ETOPS
T/O ALT beyond 60min
Departure from a maintenance base
Overseas to/from Canada

Service check within 2 hours of crew arrival = No walkaround

40
Q

FMC True Track Check

A

Track within +/- 1 degrees
Distance within +/- 2 NM (3 NM for North/South tracks)

41
Q

%MAC AFT Runup Limits

A

(-8) - 25.3
(-9) - 23.1

Refer to AOM if static runup required.

42
Q

Oil temperature for engine start

A

Greater than -40 degrees

43
Q

Maximum OAT for dual engine start

A

Greater than +40 degrees

44
Q

Fuel temperature prior to takeoff

A

Not less than -29 C

787 (1 decks)

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