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Boeing 787 > Limitations -9 (# items) + Nice to Know > Flashcards

Limitations -9 (# items) + Nice to Know Flashcards

1
Q

Runway slope

A

+/- 2%

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2
Q

(#) Maximum Takeoff and Landing Tailwind
Component

A

15 knots

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3
Q

Maximum Operating Altitude

A

43.100 ft pressure altitude

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4
Q

Maximum Takeoff and Landing Altitude

A

14.000 ft pressure altitude

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5
Q

(#) Do not operate HF radios __________.

A

when refueling

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6
Q

Verify that an operational check of the Flight Deck Access System has been accomplished according to approved procedures once ___________.

A

each flight day

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7
Q

The maximum demonstrated crosswind for takeoff is _________ (gust included).

A

33 knots

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8
Q

The maximum demonstrated crosswind component for landing is _______ (gust included).

A

40 knots

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9
Q

(#) Severe turbulent air penetration speed (in severe turbulence) is defined as:

A
  • 290 KIAS below 25,000 feet
  • 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet.
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10
Q

(#) Avoid ________________ in a hangar.

A

weather radar operation

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11
Q

Prior to takeoff the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation is ________.

A

75 feet

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12
Q

Maximum Taxi Weight

A

253.558 kg

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13
Q

Maximum Takeoff Weight

A

252.650 kg

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14
Q

Maximum Landing Weight

A

192.776 kg

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15
Q

Maximum Zero Fuel Weight

A

181.436 kg

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16
Q

(#) The autopilot must not be engaged below a minimum engage altitude of __________ after takeoff.

A

200 feet AGL

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17
Q

(#) Autoland capability may only be used for operations into runways _______________ airport field elevation.

A

at or below 8400 feet

18
Q

(#) Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged ________.

A

below 135 feet AGL

19
Q

(#) With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged __________.

A

below 100 feet AGL

20
Q

If the glidepath angle for approach is greater than 3.77 degrees, the autopilot must be disengaged __________________.

A

no later than 50 feet below DH/MDA

21
Q

Low Visibility (HUD) Takeoff
(#) Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations (headwind, crosswind, tailwind):

A

Headwind: 25 knots
Crosswind: 20 knots
Tailwind: 15 knots

22
Q

Automatic Landing
(#) Maximum wind component speeds when landing weather minima are predicated on autoland and CAT II/III operations (headwind, crosswind, tailwind):

A

Headwind: 25 knots
Crosswind: 25 knots
Tailwind: 10 knots

23
Q

Automatic Landing
For USA operations the Crosswind component is reduced to ___________.

A

15 knots

24
Q

(#) The maximum glideslope angle is _____ degrees.

A

3.25

25
Q

(#) The minimum glideslope angle is ______ degrees.

A

2.5

26
Q

Autoland capability may be used with flaps ____________, with both engines operative or with one engine inoperative.

A

20, 25, or 30

27
Q

(#) Do not use FLCH on final approach below

A

1,000 feet AFE

28
Q

(#) Oil temperature must be greater than _____ for engine start.

A

-40° C

29
Q

(#) What AFM limitations should we observe regarding the use of thrust reversers?

A

Intentional selection of reverse thrust in flight is prohibited.
Backing the airplane with use of reverse thrust is prohibited.

30
Q

(#) What AFM limitation should we observe regarding the use of flight controls?

A

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.

31
Q

The maximum altitude with flaps extended is _________.

A

20,000 feet

32
Q

Flap placard speeds

A

1 - 260 kt
5 - 250 kt
10 - 230 kt
15 - 220 kt
17 - 215 kt
18 - 215 kt
20 - 210 kt
25 - 190 kt
30 - 180 kt

33
Q

Maximum tank fuel temperature at takeoff is _________ for Jet A, Jet A-1, JP-5, JP-8 or TS-1.

A

49° C (120° F)

34
Q

Tank fuel temperature prior to takeoff must not be less than ___________.

A

-29° C (-20° F)

35
Q

Before Takeoff Procedure
Engine warm up requirements:
Run the engines for at least _____ minutes.

A

5

36
Q

Before Takeoff Procedure
Engine warm up requirements:
Engine oil temperature must be _________ before takeoff.

A

above the lower amber band

37
Q

After Landing Procedure
Engine cooldown recommendations:
Run the engines for at least _____ minutes

A

5

38
Q

Minimum pavement width for a 180-degree turn

A

47,0 meters

39
Q

Principal dimensions (length, height, wingspan)

A

Length: 62,8 meters
Height: 17,0 meters
Wingspan: 60,1 meters

40
Q

Thrust Rating Rolls-Royce Trent 1000J

A

74.400 pounds BET

41
Q

In-flight tank fuel temperature must be maintained __________________ of the fuel being used.

A

at least -42° C, as well as 3° C
above the freezing point

Boeing 787 (6 decks)

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