Powerplant Flashcards

1
Q

_____ engines are installed on the Challenger 300

A

AS907-HTF 7000-1-1A

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2
Q

_____ engines are installed on the Challenger 350.

A

AS907-HTF 7350-2-1A

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3
Q

The normal thrust rating for the Challenger 300 is _____.

A

6,826 lb at SL to ISA + 86°F (15°C)

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4
Q

The normal thrust rating for the Challenger 350 is _____.

A

7,323 lb at SL to ISA + 86°F (15°C)

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5
Q

APR provides rated thrust up to a temperature of _____.

A

ISA + 95°F (20°C)

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6
Q

_____% is the minimum N2 ground idle.

A

46

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7
Q

The FADEC is DC electrically powered during engine start. As N2 increases above 45%, the FADEC power is taken over by the ______.

A

Permanent Magnet Alternator (PMA)

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8
Q

The Takeoff Thrust time limit is _____ minutes.

A

5 Mins

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9
Q

Auto APR is armed when _____.

A

the Auto APR switch is on and Thrust Levers
are placed in TO detent

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10
Q

The Auto APR is armed when ______.

A

the Auto APR switch is on and Thrust Levers are placed in TO detent

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11
Q

The Auto APR time limit is _______.

A

10 min, after which exceedances are recorded

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12
Q

The Manual APR time limit is _____.

A

5 min, after which exceedances are recorded

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13
Q

An engine start can be accomplished on the ground via _____, _____, and _____.

A

APU; Crossbleed; External Air Source

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14
Q

APR can be activated in two ways: _____ and _____.

A

Manually, by selecting the thrust levers into the APR detent;

Automatically, when there is an N2
mismatch in excess of 15%, or FADECs stop cross-communicating, and the throttles are in TO detent

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15
Q

If a thrust reverser becomes unstowed in flight, _____.

A

the FADEC will command the engine to idle

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16
Q

Engine sync is available with _____.

A

CRZ or CLB power and N 1s within 5%

17
Q

Mach Hold is available with _____.

A

CRZ thrust, ALT or ALTS mode, Sync on—
automatically adjusts N 1 ± 3%

18
Q

The 7 components mounted on the Engine Accessory Gearbox include: _____.

A

-Oil Pump
-Oil Reservoir
-Hydraulic Pump
-Generator
-Hydro-mechanical Fuel Metering Unit (HFMU),
-Air Turbine Starter (ATS),
-Permanent Magnetic Alternator (PMA).

19
Q

The 10 FADEC controls engine functions including _____.

A

-2 channels—Fuel scheduling
-bleed air extraction
-ignition
-engine starting
-limits for N 1/N2/ITT
-overspeed protection
-idle for ground/flight/reverse
-APR
-engine sync
-thrust annunciations

20
Q
A