B777 Flashcards

1
Q

What provides the yaw damping function in normal mode?

A

Turn coordination and Dutch Roll damping

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2
Q

How are the primary flight controls powered?

A

Redundant hydraulic sources

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3
Q

Which hydraulic systems supply the flight controls?

A

Left, right, and center hydraulic systems supply power to the flight controls

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4
Q

Which tank can the DC fuel pump feed from?

A

Single centre tank

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5
Q

During an in-flight second start attempt, at what EGT will the EEC re-introduce fuel?

A

EGT falls below 200 degrees C

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6
Q

What are the maximum allowable wind speeds for autoland?

A

HW: 25 knots TW: 15 knots XW 25 knots

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7
Q

At what N3 RPM does starter cutout occur? (300)

A

25% (start selector releases to the NORM position)

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8
Q

Which spoiler surfaces are mechanically controlled?

A

Spoilers 4 and 11

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9
Q

How is the hot battery bus voltage normally supplied?

A

Main battery charger

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10
Q

What condition will most likely be accompanied with high N1 vibration?

A

Tactile vibration

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11
Q

Which isolation valves are normally open in flight?

A

Left and right (Centre normally closed)

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12
Q

What is the VNAV climb speed when in clean configuration?

A

Speed transition associated with origin airport or Vref+100 whichever higher

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13
Q

Which altimeter setting provides the landing altitude barometric pressure correction?

A

Captains altimeter setting

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14
Q

Which flight control modes allow for autopilot operation?

A

Normal, secondary

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15
Q

What is the backup system for flaps and slats?

A

Electrically powered backup systems

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16
Q

Which main gear axle is steerable?

A

Fwd axle of main gear is steerable

17
Q

How is the ADIRU hot battery bus operation indicated on the ground?

A

Horn in the landing gear wheel well sounds to alert maintenance crew

18
Q

What are the primary engine indications displayed on EICAS?

A

N1 and EGT

19
Q

What is the indication for crossed valve disagreement?

A

CROSSFEED switch VALVE light illuminates and EICAS advisory message FUEL CROSSFEED FWD or AFT displays

20
Q

What is the maximum landing weight for the Boeing 777-300ER?

A

251,290 kg

21
Q

What components make up the ADIRS?

A

ADIRU, SAARU, Air data modules

22
Q

How are TRUs supplied?

A

AC transfer busses powers TRUs (transformer rectifier units)

23
Q

How is tail strike protection achieved?

A

PFCs calculate if a tail strike is imminent and decrease elevator deflection

24
Q

Which hydraulic systems power the stabilizer?

A

Left and center hydraulic systems

25
Q

How many times will autostart attempt on the ground for 777-300?

A

3 attempts