Ejet E1 - SOPM

Question 1

During the Power Up what should pilot do if only displays 2 and 3 are available?

Answer 1

The pilot must not proceed with the flight because the airplane is not dispatchable with this condition.

Question 2

Which Emergency Equipment shall be checked in the cockpit during Internal Inspection?

Answer 2

• Protective Breathing Equipment (PBE).
• Fire Extinguisher
• Crash Axe.
• Life Vests.
• Escape Ropes.
• Flashlights.

Question 3

If the crew received the airplane already powered up, which item shall be verified?

Answer 3

• FIRE EXTINGUISHER Panel
• DVDR CONTROL Panel
• Electronic CBs.

Question 4

What should you check before moving the aircraft during the power up?

Answer 4

I must check if the IESS is initialized.

Question 5

What should you do if the batteries voltage are between 21 and 22V?

Answer 5

Recharge the batteries prior to takeoff, through any AC source. (including engines during taxi) for:

• 30 min batteries temperature is >= 0° C
• 35 min batteries temperature is >= -5° C and < 0° C
• 40 min batteries temperature is >= -10° C and < -5° C
• 50 min batteries temperature is < -10° C.

Question 6

What should you do if the batteries voltage are below 21 V?

Answer 6

Report to maintenance!

Question 7

teser

When does the Electrical PBIT start and how long does it take to complete?

Answer 7

The Electrical PBIT is automatically performed after the airplane is powered by any AC source and takes about
3 minutes to complete.

Question 8

What would cause the Electrical PBIT to be interrupted?

Answer 8

• any hydraulic system ELEC PUMP is running;
• the FLIGHT CONTROLS MODE Panel buttons are cycled, or
• AC power is interrupted while the test is running.

Question 9

[ROLL / YAW] trimming should be performed after the airplane has been trimmed for [ROLL / YAW]

Answer 9

ROLL trimming should be performed after the airplane has been trimmed for YAW.

Question 10

A ______________ EICAS message may be displayed on ground if airplane is powered by only one AC power source and indicated airspeed is at or above _____ kt.

Answer 10

A LOAD SHED EICAS message may be displayed on ground if airplane is powered by only one AC power source and indicated airspeed is at or above 50 kt.

Question 11

After starting the engines APU shutting down can only be performed after confirmation of the power transfer. How could pilot do it?

Answer 11

Through the Electrical Synoptic page or waiting 30 seconds after %N2 stabilizes

Question 13

After starting the engines what is acceptable difference between N1 given by FADEC (indicated on EICAS) and the computed value (ePerf)?

Answer 13

Must be zero or positive and lower than or equal to 0.5%.

Question 14

After takeoff in case of F-BUG disappears what should pilot do?

Answer 14

Use the Green dot + 10 kt as reference.