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777 > Memory Items > Flashcards

Memory Items Flashcards

1
Q

The maximum altitude with flaps extended is___

A

20,000 feet

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2
Q

APU to pack takeoffs are prohibited at airport altitudes above ____.

A

6,900 feet

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3
Q

Do not use FLCH on final approach below ___

A

1,000 feet AFE

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4
Q

Maximum landing weight

A

575,000 lbs

260,815 kgs

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5
Q

FIRE ENG L, R

A

Fire is detected in the engine

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
5) If the FIRE ENG message stays shown:
Engine fire switch (affected side) - Rotate to the stop and hold for 1 second

If after 30 seconds the FIRE ENG message stays shown:
Engine fire switch (affected side) - Rotate to the other stop and hold for 1 second

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6
Q

Maximum zero fuel weight

A

547,000 lbs

248,115 kgs

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7
Q

ENG SVR DAMAGE / SEP L, R

A

One or more of these occur:
• Airframe vibration with abnormal engine indications
• Engine separation

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

Max takeoff and landing tailwind component

A

10 knots

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9
Q

Do not use the autopilot below ___ RA at airport pressure altitudes above ____

A

100 feet / 8500 feet

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10
Q

Max glide slope angle with autoland

A

3.25°

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11
Q

AIRSPEED UNRELIABLE

A

Airspeed or Mach indications are suspected to be unreliable.

1) Autopilot disengage 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° and 85% N1
Flaps up - 4° and 70% N1

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13
Q

Do not operate the ____ in a hangar or within ____ of any fuel spill.

A

Weather radar / 50 feet (15.25 meters)

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14
Q

ABORTED ENGINE START L, R

A

During a ground start, an abort start condition occurs

1) FUEL CONTROL switch (affected side) - CUTOFF

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15
Q

Do not operate ___ during refueling operations

A

HF radios

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17
Q

The maximum demonstrated takeoff and landing crosswind

A

38 knots

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18
Q

ENG LIM / SURGE / STALL L, R

A

One or more of these occur:
• Engine indications are abnormal
• Engine indications are quickly nearing or showing and 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

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

19
Q

Max winds with auto land operations:

Headwind
Tailwind
Crosswind
Crosswind CAT II/CAT III

A

Headwind 25 knots
Tailwind 10 knots
Crosswind 25 knots
Crosswind CAT II / CAT III 15 knots

21
Q

Ground wind limits for doors:

Opening or closing
While open

A

40 knots opening or closing

65 knots while open

22
Q

CABIN ALTITUDE

A

Cabin Altitude is excessive

1) Don the oxygen masks
2) Establish crew communications
3) Check the cabin altitude and rate
4) If the cabin altitude is uncontrollable:
SUPRNMRY OXYGEN switch - Push to ON and hold for 1 second

Without delay, descend to the lowest safe altitude or 10,000’, whichever is higher

To descend:
      Move the thrust levers to idle
      Extend the speed brakes
      If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads
      Descend at Vmo/Mmo
24
Q

DUAL ENG FAIL/STALL

A

Engine Speed for both engines is below idle.

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

25
Q

Maintain a minimum speed of ______ above the minimum maneuvering speed at all times when airspeed is below _____

A

15 knots / 0.82 Mach

25
Q

The autopilot must not be engaged below a minimum engaged altitude of _____ after takeoff.

A

200 feet AGL

25
Q

Min glide slope angle with autoland

A

2.5°

26
Q

Maximum takeoff weight

A

N774SA, N775SA: 766,000 lbs

N714SA, N777SA/N778SA: 766,800 lbs / 347,451 kgs

27
Q

Maximum taxi weight

A

N774SA, N775SA: 768,000 lbs

N714SA, N777SA/N778LA: 768,800 lbs / 348,358 kgs

28
Q

Turbulent air and penetration speed (in severe turbulence) is defined as:

A

270 knots below 25,000 feet

280 knots or 0.82 Mach whichever is lower at 25,000 feet and above

28
Q

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

A

200 feet AGL

28
Q

Prohibited maneuvers

A

Intentional selection of reverse thrust in flight

Backing the airplane with the use of reverse thrust

28
Q

Avoid ___ and ___ 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 ___ speed, including below ___.

A

Rapid / large alternating / any / Va

29
Q

ENGINE AUTOSTART L, R

A

During a ground start, one of these occurs:
• AUTOSTART did not start the engine
• Fuel Control switch is in RUN at low engine RPM with the autostart switch OFF

FUEL CONTOL switch (affected side) - CUTOFF

31
Q

STABILIZER

A

One of these occurs:
• Stabilizer movement without a signal to trim
• The stabilizer is failed

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

32
Q

Max Runway slope?

A

+/- 2°

33
Q

Max T/O and landing altitude?

A

9,800’ pressure altitude

34
Q

Max field elevation?

A

9,650’

35
Q

APU starter motor duty cycle?

Time between starts?

A

3 starts in a 60 min period

1min wait between each start (electric and air turbine)

777 (23 decks)

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