Flight Management System Knowledge Review Flashcards

1
Q

After manually positioning the throttles

with the autothrottle system engaged,

the autothrottle does NOT subsequently

reposition the throttles in which mode?

A

HOLD

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2
Q

During climb, the IAS/MACH window automatically change from IAS to

MACH _____.

A

at .84 MACH

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3
Q

_____ is displayed on the PFD throttle FMA when thrust is set to the selected

thrust limit.

A

THR REF

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4
Q

In flight, TO/GA is armed whenever the ______.

A

Flaps are not retracted or

glideslope captured

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5
Q

At what altitude does VNAV engage if it is armed for takeoff?

A

400 feet

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6
Q

Autothrottle disconnect occurs automatically under what circumstance?

A

A fault in the engaged autothrottle mode is detected

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7
Q

Autopilot rudder commands are added only ______.

A

When LAND 3 or LAND 2 is annunciated

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8
Q

With LAND 2 annunciated on the PFD, ______.

A

a single fault cannot

cause a significant deviation from the flight path

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9
Q

If electrical power is removed from the airplane and the battery switch is turned

OFF, the _____ continues to supply electrical power to the ADIRU.

A

hot battery bus

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10
Q

At cruise altitude,

Lthe FMC sets cruise speed at the default or pilot entered speed

until reaching the top-of-descent point.

What are the other two alternate cruise speed options?

A

Long range LRC and

Engine out ENG OUT

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11
Q

All flight management computing tasks are accomplished by _____.

A

The active FMC

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12
Q

The VNAV, LNAV, LOC,

and APP modes can be disarmed by _____.

A

pushing the mode switch a second time before capture

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13
Q

Regarding thrust management, the second push of the TO/GA switch in flight ______.

A

engages autothrottles in THR REF mode to provide

full-rated go around thrust

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14
Q

The FMC determines present position from the _____.

A

ADIRS, GPS, and navigation radios

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15
Q

The ADIRU and SAARU receive air data from the _____.

A

left, center, and right pitot, and static systems

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