Memory Limitations Flashcards

1
Q

Max Operating Pressure Altitude
(787-8, 787-9)

A

43,100 feet

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2
Q

Max Operating Pressure Altitude
(787-10)

A

41,100 feet

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3
Q

Max 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 which is lower

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5
Q

Turbulent Air Penetration Speed
Severe turbulence below 25,000 feet

A

290 knots

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6
Q

Takeoff Crosswind Component
>430,000 lbs Dry Rwy, CG < 20

A

40 knots

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7
Q

Takeoff Crosswind Component
350,000 lbs Dry Rwy, CG < 20

A

40 knots

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8
Q

Takeoff Crosswind Component
< 270,000 lbs Dry Rwy, CG < 20

A

40 knots

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9
Q

Landing Crosswind Component
RWY Dry

A

40 knots

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10
Q

AUTOFLIGHT LIMITATIONS
Autopilot/ Flight Director System
(5)

A
  1. Do not engage the autopilot below a minimum altitude of 200 feet AGL after takeoff
  2. Autoflight capability may only be used for operations to runways at or below 8,400 AFE
  3. Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 135feet AGL
  4. With LAND 2 or LAND 3 annunciated and glidepath angles greater than 3.25, the autopilot
    must be disengaged below 100 feet AGL
  5. Do not use FLCH on final approach below 1000 feet AFE
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11
Q

Max wind component Low Vis HUD Takeoff

A

Headwind 25 knots
Tailwind 15 knots
Crosswind 15 knots

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12
Q

SA CAT I Approach Max Crosswind

A

15 knots

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13
Q

ILS Automatic Landing Max Glideslope Angle

A

3.25

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14
Q

ILS Automatic Landing Min Glidepath Angle

A

2.5

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15
Q

Communication/Fueling Limitation

A

Do not operate the HF radio during fueling operations

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16
Q

Minimum Oil Quantity Prior to Start

A

18 quarts

17
Q

Minimum Oil temp prior to start

A

The oil temp must be greater than -40C for engine start

18
Q

Reverse Thrust Limitations

A
  1. Intentional selection of reverse thrust in flight is prohibited
  2. Backing the plane with use of reverse thrust is prohibited
19
Q

Control Inputs

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