Limitations Flashcards

B787 Limitations

1
Q

MAXIMUM OPERATING PRESSURE ALTITUDE (787-8, 787-9)

A

43,100 feet

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2
Q

MAXIMUM OPERATING PRESSURE ALTITUDE
(787-10)

A

41,100 feet

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3
Q

MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT

A

15 knots

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4
Q

TURBULENT AIR PENETRATION SPEED (Severe turbulence at and above 25,000 feet)

A

310 knots/.84 Mach (whichever is lower)

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5
Q

TURBULENT AIR PENETRATION SPEED (Severe turbulence below 25,000 feet)

A

290 KIAS

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6
Q

Takeoff Crosswind Guidelines

A

40 knots Crosswind Component

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7
Q

Landing Crosswind Guidelines (Valid for all engine and one engine inoperative operations at any weight and CG)

A

40 knots Crosswind Component

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8
Q

ICING CONDITIONS DEFINITION

A

Icing conditions exist when OAT (ground) or TAT (flight) is 10°C or below.

Note: Use TAT to determine EAI selection during ground operations to avoid nuisance ANTI-ICE ON EICAS messages.

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9
Q

Autopilot minimum engagement altitude after takeoff (OpSpec C071)

A

200 feet AGL

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10
Q

Maximum Airfield Elevation for Autoland

A

8400 feet

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11
Q

Autopilot Disengagement Height, without LAND 2 or LAND 3 annunciated

A

“…the autopilot must be disengaged below 135 feet AGL.” (1.30.4)

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12
Q

Autopilot Disengagement Height with LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25° (OpSpec C071)

A

“…the autopilot must be disengaged below 100 feet AGL.” (1.30.4)

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13
Q

Do not use FLCH on final approach below 1000 feet AFE. (T/F)

A

TRUE

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14
Q

LOW VISIBILITY (HUD) TAKEOFF (RVR <500) Wind Components

A

25 knots headwind
15 knots tailwind
15 knots crosswind

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15
Q

SA CAT I APPROACHES
Maximum wind component speed

A

15 knots crosswind

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16
Q

Maximum glideslope angle

A

3.25º

17
Q

Minimum glideslope angle

A

2.50º

18
Q

Do not operate HF radio during fueling operations (T/F)

A

TRUE

19
Q

Minimum Oil Quantity prior to start

A

18 quarts

20
Q

Minimum Oil Temperature for Engine Start

A

-40ºC

21
Q

Intentional selection of reverse thrust in flight is prohibited. (T/F)

A

TRUE

22
Q

Backing the airplane with use of reverse thrust is prohibited. (T/F)

A

TRUE

23
Q

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. (T/F)

A

TRUE