0%

Normal DC power is provided to each FADEC and is available for engine starting and all engine operation. After engine start, if normal DC power becomes unavailable, the engine-driven PMA provides AC electrical power to the FADEC.

Correct! Wrong!

The aircraft electrical system does not supply electrical power to the FADEC when using the emergency bus.

Ignition during normal engine start is activated by FADEC when:

Correct! Wrong!

Ignition and boost pump operation during engine start are normally terminated:

Correct! Wrong!

For any flight that exceeds 5 hours, the oil level must be at least:

Correct! Wrong!

It is recommended that the throttles should normally be reduced to the CRU or below position within how many minutes after reaching cruise altitude?

Correct! Wrong!

The normal time to check engine oil is _____ after engine shutdown.

Correct! Wrong!

The throttles should be reduced to the CRU detent or below within 10 minutes after reaching an intermediate or final cruise altitude.

Correct! Wrong!

The use of CLB during normal operations beyond 10 minutes after reaching cruise altitude will significantly decrease engine life and increase operator costs.

If the N1 fan shaft shifts aft:

Correct! Wrong!

When does the OIL PRESS LO L–R CAS message on the MFD illuminate?

Correct! Wrong!

If one ignitor fails during engine start:

Correct! Wrong!

Advertisement

The maximum crosswind component for engine start is:

Correct! Wrong!

What is the minimum oil temperature for engine start?

Correct! Wrong!

ITTs should be allowed to stabilize for how long before engine shutdown?

Correct! Wrong!

When the FADEC start sequence is completed, the N2:

Correct! Wrong!

If the ITT is rapidly approaching 830 deg.C, terminate the engine start by moving the:

Correct! Wrong!

Takeoff thrust is limited to 5 minutes except during emergency situations (i.e., one engine inoperative).

Correct! Wrong!

If the F/W SHUTOFF R CAS message posts when positioning the throttle to CUTOFF, this indicates:

Correct! Wrong!

The primary thrust indicator for the Pratt and Whitney PW615F-A is:

Correct! Wrong!

If normal DC power is not available, the FADEC receives power from the:

Correct! Wrong!

What is the maximum tailwind component for engine start?

Correct! Wrong!

Citation Mustang – Powerplant