MEMORY ITEMS / LIMITATIONS Flashcards

1
Q

Aborted Engine Start L, R

A
  1. FUEL CONTROL Switch (affected side) - CUTOFF
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2
Q

Airspeed Unreliable

A
  1. Autopilot disconnect switch - Push
  2. A/T ARM switches (both) - OFF
  3. F/D switches (both) - OFF
  4. Set the following gear up pitch attitude and thrust:
  • Flaps extended - 10° degrees and 85% N1
  • Flaps up - 4° degrees and 70% N1
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3
Q

[] CABIN ALTITUDE

A
  1. Don oxygen masks.
  2. Establish crew communications.
  3. Check the cabin altitude and rate.
  4. IF the cabin altitude is uncontrollable:
  • PASS OXYGEN switch - Push to ON and hold for 1 second
  • Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
  • To descend:
    • Move the thrust levers to idle;
    • Extend the speedbrakes;
    • IF structural integrity is in doubt, limit airspeed and avoid high maneuvering loads.
    • Descend at Vmo/Mmo.
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4
Q

Dual Eng Fail / Stall

A
  1. FUEL CONTROL switch (both) - CUTOFF, then RUN
  2. RAM AIR TURBINE switch - Push and hold for 1 second
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5
Q

[] ENG AUTOSTART L, R

A
  1. FUEL CONTROL switch (affected side) - CUTOFF
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6
Q

Eng Lim / Surge / Stall L, R

A
  1. A/T ARM switch (affected side) - Confirm - OFF
  2. Thrust lever (affected side) - Confirm - Retard until engine indications stay within limits or the thrust lever is at idle
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7
Q

Eng Svr Damage / Sep L, R

A
  1. A/T ARM switch (affected side) - Confirm - OFF
  2. Thrust lever (affected side) - Confirm - Idle
  3. FUEL CONTROL switch (affected side) - Confirm - CUTOFF
  4. Engine fire switch (affected side) - Confirm - Pull
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8
Q

[] FIRE ENG L, R

A
  1. A/T ARM switch (afected side) - Confirm - OFF
  2. Thrust lever (affected side) - Confirm - Idle
  3. FUEL CONTROL switch (affected side) - Confirm - CUTOFF
  4. Engine fire switch (affected side) - Confirm - Pull
  5. IF the FIRE ENG message shows:
  • Engine fire switch (affected side) - Rotate to the stop and hold for 1 second.
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9
Q

[] STABILIZER

A
  1. STAB cutout switches (both) - CUTOUT
  2. Do not exceed the current airspeed
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10
Q

Maximum Takeoff and Landing Tailwind Component

A

15 knots

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11
Q

Severe Turbulent Air Penetration Speed

A
  • 270 knots below 25,000 feet;
  • 280 knots or 0.82 Mach whichever is lower at 25,000 feet and above;
  • Maintain a minimum speed of 15 knots above the minimum maneuvering speed at all altitudes when airspeed is below 0.82 Mach.
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12
Q

HF Radio

A

Do not operate HF radios during refueling operations.

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13
Q

Weather radar

A

Avoid weather radar operation in a hangar.

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14
Q

Autopilot minimum engage altitude

A

200 feet AGL after takeoff

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15
Q

Autopilot must be disengaged…

A

Below 200 feet AGL, without LAND 2 or LAND 3 annunciated.

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16
Q

Maximum allowable wind speeds (including gusts) on autoland operations

A
  • Headwind - 25 knots
  • Tailwind - 15 knots
  • Crosswind - 25 knots (15 - USA)
17
Q

Maximum and minimum glideslope angle for Automatic Landing:

A

Maximum - 3.25° degrees

Minimum - 2.5° degrees

18
Q

FLCH on final approach

A

Do not use it below 1,000 feet AFE

19
Q

Reverse Thrust limitations…

A
  1. Intentional selection of reverse thrust in flight is prohibited;
  2. Backing the airplane with use of reverse thrust is prohibited.
20
Q

Control inputs (AFM Limitations)

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.

21
Q

Maximum altitude with flaps extended

A

20,000 feet

22
Q

Minimum oil quantity limit

A

No minimum (FCTM Chapter 8)

23
Q

Condition statement for Eng Lim/Surge/Stall non-normal checklist

A

One or more of these occur:

  • Engine indications are abnormal;
  • Engine indications are quickly nearing or show an exceedance;
  • abnormal engine noises are heard, possibly with airframe vibration;
  • There is no response to thrust lever movement or the response is abnormal;
  • Flames in the engine inlet or exhaust are reported.