limitations Flashcards

1
Q

MAXIMUM OPERATING PRESSURE ALTITUDE

A

787-8, 787-9
43,100 feet
787-10
41,100 feet

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2
Q

MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT

A

15 knots

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3
Q

Severe turbulence at and above 25,000 feet

A

310 knots/.84 Mach (whichever is lower)

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4
Q

Severe turbulence below 25,000 feet

A

290 KIAS

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5
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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6
Q

Do not engage the autopilot below a minimum engagement altitude of

A

200 feet AGL after takeoff.

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7
Q

Autoland capability may only be used for operations to runways at or below

A

8400 feet airport field elevation

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8
Q

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below

A

135 feet AGL

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9
Q

With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25°,

A

the autopilot must be disengaged below 100 feet AGL.

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10
Q

Do not use FLCH on final approach below

A

1000 feet AFE

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11
Q
LOW VISIBILITY (HUD) TAKEOFF
 Headwind
A

25 knots

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12
Q

LOW VISIBILITY (HUD) TAKEOFF (RVR <500)

Tailwind

A

15 knots

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13
Q

LOW VISIBILITY (HUD) TAKEOFF (RVR <500)

Crosswind

A

15 knots

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14
Q

ILS AUTOMATIC LANDING Maximum wind component speeds: Headwind

A

25 knots

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15
Q

ILS AUTOMATIC LANDING Maximum wind component speeds Tailwind

A

15 knots (◘ 10 knots for CAT II/III)

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16
Q

ILS AUTOMATIC LANDING Maximum wind component speeds Headwind

A

25 knots

17
Q

ILS AUTOMATIC LANDING Maximum wind component speeds Crosswind

A

25 knots (◘ 15 knots for CAT II/III)

18
Q

The maximum glideslope angle is.

A

3.25°

19
Q

The minimum glideslope angle is .

A

2.50°

20
Q

Oil Quantity Minimum prior to start

A

18 quarts

21
Q

Oil temperature must be greater than ? for engine start.

A

-40°C

22
Q

REVERSE THRUS
Intentional selection of reverse thrust in flight is
Backing the aircraft with use of reverse thrust is .

A

prohibited