Limitations Flashcards

(18 cards)

1
Q

What is the Maximum Takeoff and Landing Tailwind Component Limit?

A

10 knots (RX Limitation)

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2
Q

What is the limitation regarding HF radios use?

A

Do not operate HF radios when refueling

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3
Q

What is the Severe turbulence air penetration speed?

A
  • 290 KIAS below 25,000 feet
  • 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet
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4
Q

What is the limitation regarding weather radar use?

A

Avoid weather radar operation in a hangar

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5
Q

What is the minimum altitude to engage the autopilot after T/O?

A

200’ ft.

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6
Q

What is the maximum Autoland capability altitude?

A

8400’ ft.

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7
Q

If LAND2 or LAND3 is not displayed, when must the Autopilot be disengaged?

A

Below 135’ ft. AGL

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8
Q

If the G/S angle is more than 3.25 and LAND2 or LAND3 displayed, when must the Autopilot be disengaged?

A

Below 100’ ft. AGL

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9
Q

What are the wind limitations when a Low Visibility HUD T/O is conducted?

A
  • Headwind 25 knots
  • Tailwind 10 knots (RX Limitation)
  • Crosswind 20 knots
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10
Q

What are the Limitations when landing weather minimums are predicted on Autoland operations?

A
  • Headwind 25 knots
  • Tailwind 10 knots (RX Limitation)
  • Crosswind 25 knots
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11
Q

What is the maximum glideslope angle when landing weather minimums are predicted on Autoland operations?

A

3.25 degrees

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12
Q

What is the minimum glideslope angle when landing weather minimums are predicted on Autoland operations?

A

2.5 degrees

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13
Q

What is the limitation regarding FLCH use?

A

Do not use FLCH on final approach below 1,000 feet AFE

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14
Q

What is the minimum Oil temperature for engine start?

A

Oil temperature must be greater than -40° C for engine start

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15
Q

What are the limitations regarding Reverse Thrust use?

A
  • Intentional selection of reverse thrust in flight is prohibited
  • Backing the airplane with use of reverse thrust is prohibited
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16
Q

What are the limitations on alternating control inputs?

A

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (eg, larger side slip angles) as they may result in structural failure at any speed, including below VA.

17
Q

Who is responsible for performing the exterior inspection?

A

Before each flight the Captain or First Officer must verify that the airplane condition is satisfactory for flight

18
Q

What in general is crewmember checking in exterior inspection?

A
  • Surfaces and structures are clear, not damaged, not missing parts
  • Tires are not too worn, not damaged, and there is no tread separation
  • Gear struts are not fully compressed
  • Engine inlets and tailpipes are clear, access panels are secured
  • Exterior is not damaged, reversers are stowed
  • Doors and access panels that are not in use are latched
  • Probes, vents, and static ports are clear and not damaged
  • Antennas are not damaged
  • Light lenses are clean and not damaged