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B777 Type Rating > Memory Items & Limitations > Flashcards

Memory Items & Limitations Flashcards

1
Q

What is the wingspan?

A

212’ 7”

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2
Q

What is the height?

A

62’ 4”

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3
Q

What is the length?

A

209’ 1”

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4
Q

What is the main wheelbase distance?

A

42’ 4”

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5
Q

What is the minimum width of pavement needed for a 180 turn?

A

157’ 4”

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6
Q

You should not attempt to make a turn away from an obstacle within how many feet of the WINGTIP?

A

15’

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7
Q

You should not attempt to make a turn away from an obstacle within how many feet of the NOSE?

A

55’

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8
Q

What is the runway slope limitations?

A

+/-2%

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9
Q

What is the maximum takeoff and landing tailwind component?

A

15kts

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10
Q

What is the maximum operating altitude?

A

43,100ft

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11
Q

What is the maximum takeoff and landing altitude?

A

8,400ft (pressure altitude)

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12
Q

What is the maximum demonstrated takeoff and landing crosswind?

A

38kts

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13
Q

What is the severe turbulent air penetration speed below 25,000ft?

A

270kts

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14
Q

What is the severe turbulent air penetration speed above 25,000ft?

A

280kts or 0.82 Mach (Whichever is lower)

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15
Q

What is the minimum speed at all altitudes when airspeed is below 0.82 Mach?

A

15kts above the minimum manoeuvring speed

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16
Q

When shouldn’t HF radios be used?

A

During fuelling operations

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17
Q

When should the use of weather radar be avoided?

A
  • In a hangar; or
  • Within 50ft of fuelling operations or a fuel spill.
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18
Q

What is the maximum allowable difference between Captain’s and First Officer’s attitude display and field elevation for RVSM operations?

A

75ft

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19
Q

What is the maximum total number of persons carried?

A

9
- 2 on-duty flight crew;
- 2 off-duty flight crew;
- 5 Supernumeraries (if there is approved seating installed)

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20
Q

What is the maximum taxi weight?

A

768,000lbs

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21
Q

What is the maximum takeoff weight?

A

766,000lbs

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22
Q

What is the maximum landing weight?

A

575,000lbs

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23
Q

What is the maximum zero fuel weight?

A

547,000lbs

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24
Q

Autopilot must not be engages below what altitude after takeoff?

A

200ft

25
Q

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

A

200ft

26
Q

When shouldn’t FLCH (Flight Level Change) be used?

A

On approach below 1,000ft AFE (Above Field Elevation)

27
Q

What is the maximum tank fuel temperature?

A

49°C

28
Q

What should the fuel tank temperature be prior to takeoff?

A

Not less than -40°C or 3°C above the fuel freezing point whichever is higher.

29
Q

When is the use of thrust reversers prohibited

A
  • In flight
  • To back the aircraft
30
Q

In tailwinds and crosswinds between 30 and 45kts, what should engine power be limited to?

A

70% N1

31
Q

What is the APU stater attempt limit?

A

3 start attempts within 60 minutes

32
Q

How long should you wait between APU starter attempts?

A

1 minute

33
Q

What is the maximum altitude with flaps extended?

A

20,000ft

34
Q

If there is fuel in the centre tank, how much fuel should be in the main tanks?

A

Full

35
Q

What is the minimum oxygen pressure for crew?

A

1,100 psi

36
Q

What is the minimum oxygen pressure for supernumerary?

A

1,300 psi

37
Q

What is the minimum oxygen pressure for portable bottles?

A

1,200 psi

38
Q

What is the maximum allowable headwind for an automatic landing?

A

25kts

39
Q

What is the maximum allowable crosswind for an automatic landing?

A

25kts

40
Q

What is the maximum allowable tailwind for an automatic landing?

A

15kts

41
Q

When is the use of the ground manoeuvring camera system prohibited?

A

Take-off, approach and landing

42
Q

When must main tanks be scheduled full?

A

If centre tank fuel is loaded

43
Q

When can the main tanks be less than full with fuel in the centre tank?

A

The centre tank can contain up to 3000lbs of fuel with less than full main tanks if the centre tank fuel weight plus the actual fuel weight is less than the maximum zero fuel weight.

44
Q

How long is the minimum oxygen pressure able to supply undiluted oxygen to the crew? How many crew members?

A

180 minutes each (4)

45
Q

How long is the minimum oxygen pressure able to supply undiluted oxygen to the supernumeraries? How many supernumeraries?

A

180 minutes each (5)

46
Q

Aborted Engine Start L,R

Condition: On the ground, an aborted engine start is needed.

A
  1. FUEL CONTROL switch (affected side)………………………CUTOFF
47
Q

Dual Eng Fail/Stall

Condition: Engine speed for both engines is below idle.

A
  1. FUEL CONTROL switches (both)…………….CUTOFF, then RUN
  2. RAM AIR TURBINE switch…………Push and hold for 1 second
48
Q

[ ] ENG AUTOSTART L, R

Condition: 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

A
  1. FUEL CONTROL switch (affected side)……………………..CUTOFF
49
Q

Eng Lim/Surge/Stall L, R

Condition: 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 air frame vibration
* There is no response to thrust lever movement or the response is abnormal
* Flames in the engine inlet or exhaust are reported

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
50
Q

Eng Svr Damage/Sep L, R

Condition: One or more of these occur:
* Airframe vibrations with abnormal engine indications
* Engine separation

A
  1. A/T ARM switch
    (affected side)……………………….Confirm………………………..OFF
  2. Thrust lever
    (affected side)……………………….Confirm…………………………Idle
  3. FUEL CONTROL switches
    (affected side)………………………Confirm…………………..CUTOFF
  4. Engine fire switch
    (affected side)………………………Confirm…………………………Pull
50
Q

Eng Svr Damage/Sep L, R

Condition: One or more of these occur:
* Airframe vibrations with abnormal engine indications
* Engine separation

A
  1. A/T ARM switch
    (affected side) ……………………….Confirm………………………..OFF
  2. Thrust lever
    (affected side)……………………….Confirm…………………………Idle
  3. FUEL CONTROL switches
    (affected side)………………………Confirm…………………..CUTOFF
  4. Engine fire switch
    (affected side)………………………Confirm…………………………Pull
51
Q

[ ] FIRE ENG L, R

Condition: Fire is detected in the engine.

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
  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

52
Q

[ ] STABILIZER

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

A
  1. STAB cutout switches (both)…………………………………………….CUTOUT
  2. Do not exceed the current airspeed.
53
Q

Airspeed Unreliable

Condition: The airspeed or Mach indications are suspected to be unreliable.

A
  1. Autopilot disengage switch………………………………………..Push
  2. A/T ARM switch………………………………………………………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
54
Q

[ ] CABIN ALTITUDE

Condition: Cabin altitude is excessive.

A
  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 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

55
Q

ENGINE FAILURE ON THE GROUND

A
  1. FUEL CONTROL switch (affected engine)………………………….CUTOFF
56
Q

ENGINE FIRE ON THE GROUND

A
  1. FUEL CONTROL switch (affected engine)…………………………..CUTOFF

DO NOT PROCEED UNTIL ENGINE SHUTDOWN HAS OCCURRED.

If FIRE indication persists after engine shutdown:

  1. Engine Fire switch (affected engine)……………………………………………Pull
  2. Engine Fire switch (affected engine)………………………………………. Rotate

After a momentary delay:

  1. Engine Fire switch (affected engine)………………….Rotate (to other bottle)
57
Q

LOWER CARGO FIRE ON THE GROUND

A
  1. CARGO FIRE ARM switch (affected compartment)……………………Push
  2. CARGO FIRE DISCH switch……………………..Push and hold for 1 second

B777 Type Rating (1 decks)

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