11-20 Flashcards

(10 cards)

1
Q

An APU FUEL SOV FAIL Caution message is displayed after the EICAS is fully energized, what do you do?

A

APU SWITCH ON
APU SWITCH OFF

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2
Q

Is it permissible to simultaneously use the APU bleed and HP cart?

A

NO, Prohibited

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3
Q

When should the TO DATA SET MENU on the MCDU be set to ENG?

A

-When OAT is from 5C to 10C and,
-When there is any possibility of encountering visible moisture up to 1700 ft AFE -When operating on ramps, taxiways, or runways when surface snow, ice,
standing water, or slush may be ingested by the engines, freeze on engines, nacelles, or engine sensor probes.

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4
Q

When should the TO DATA SET MENU on the MCDU be set to ALL?

A

-When OAT is less than 5C and,
-When there is any possibility of encountering visible moisture up to 1700 ft AFE -When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, freeze on engines, nacelles, or engine sensor probes.

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5
Q

What is the SOPM definition of “visible moisture”?

A

Clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals

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6
Q

What are the Starter Cranking Limits on the ground?

A

1 & 2: 90 seconds ON / 10 seconds OFF 3 - 5: 90 seconds ON / 5 minutes OFF

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7
Q

What are the Dry Motoring Cycle Limits?

A

1: 90 seconds ON / 5 minutes OFF 2 -5: 30 seconds ON / 5 minutes OFF

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8
Q

During engine start you experience a hung start, what are the indications and what action do you take?

A

N1 and/or N2 failing to accelerate to stable idle speed (hung start)

AFFECTED ENGINE
START / STOP SELECTOR - STOP (ENGINE ABNORMAL START)

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9
Q

What other conditions require aborting a start?

A

10, 50, 30, HOT, LOP, Hung, EPS

• No positive oil pressure indication within 10 seconds after N2 speed starts to increase.

• During engine start with a tailwind, when a positive increase of N1 is not indicated before starter cutout (50% N2). In this case, the airplane is repositioned prior to engine start to minimize tailwind effects.

• No ITT indication within 30 seconds after initiation of fuel flow (no light off).

• ITT exceeds start limit (815°C - Hot).

• Oil pressure stabilizes below the engine limits.

• N1 and/or N2 failing to accelerate to stable idle speed (hung start).

• An intermittent electrical pneumatic or starter malfunction occurs before the starter disengagement.

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10
Q

At idle engine thrust, the engine exhaust danger area can extend to approximately 90 feet
behind the aircraft with a jet blast velocity reaching?

A

65 mph (SOPM CH 2)

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