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SkyWest E175 SV Gouge Questions and Answers
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SkyWest E175 SV Gouge Questions and Answers While approaching the airport, you are 15 miles from the runway at 3,000' AFL. As you begin to configure the aircraft for landing, when would you expect the hydraulic ACMP's 1 and 2 to turn on? When flaps are selected to any position greater than 0 ...

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  • August 11, 2024
  • 15
  • 2024/2025
  • Exam (elaborations)
  • Questions & answers

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  • skywest e175 sv gouge questions and answers
  • while approaching the airport you are 15 miles fr
  • the crew elects to single engine taxi on engine 2
  • the backup hydraulic pumps for systems 1 and 2 are

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SkyWest E175 SV Gouge Questions and
Answers
While approaching the airport, you are 15 miles from the runway at 3,000' AFL. As you
begin to configure the aircraft for landing, when would you expect the hydraulic ACMP's
1 and 2 to turn on? - answer When flaps are selected to any position greater than 0

The crew elects to single engine taxi on Engine #2. With the flaps extended, the parking
bake released, and no other action is taken, which hydraulic pump(s) will be operating?
- answer ACMP 3A and Engine driven pump #2

The backup hydraulic pumps for systems 1 and 2 are the - answer ACMPs (AC
Motor Pumps)

What is the primary purpose of the PTU? - answer Assists gear extension or
retraction should the right engine or right EDP fail

The H-PBIT will run automatically when all 3 hydraulic systems are pressured and? -
answer Hydraulic reservoir temperature is at or above +10 degrees C, or H-PBIT
timer is at 0 HOURS regardless of temperature

On the post flight external inspection you notice fluid leaking from the nose wheel gear
assembly. Which hydraulic system would you expect to be the source of this leek? -
answer System 2

If Hydraulic Pump 3A fails during taxi out to the runway, will Hydraulic Pump 3B
automatically turn on? - answer No

In system 3, what pump is the primary hydraulic pump? - answer 3A

Where would you look to check the hydraulic reservoir temperature, pressure, and
quantity? - answer Hydraulic Synoptic page on the MFD

T/F In the event of a total loss of hydraulic systems 1 and 2 the only way to stop the
aircraft is with reverse thrust? - answer False

The PBE (Protective Breathing Equipment) provides oxygen by? - answer Pulling the
mask apart with two hands, which activates each of the oxygen cylinders, providing 15
minutes of oxygen

T/F When cleaning the oxygen mask is it acceptable to use alcohol wipes on the lens
and rubber parts of the mask? - answer False

, Halon Fire Extinguishers can be used for what Class of fires? - answer Class A, B, C
fires

T/F in the case of an emergency evacuation the PIC must make every effort to preserve
aircraft documents and maintenance records - answer True

In the case of partial slide deployment what action should be taken? - answer Stop
immediately and notify maintenance

Should the cockpit door become inaccessible, how can the flight crew evacuate the
aircraft? - answer Out the Direct View (DV) window using the escape rope

During an Emergency descent the crew oxygen mask provides? - answer Sufficient
oxygen for all crew members, 98 minutes in Normal at 10,000 ft, and 22 minutes in
100%

Water Fire Extinguishers can be used for? - answer Class A fires

According to the SOPM, how can you identify if the flashlight is sufficiently charged? -
answer Flashing red LED every 3-8 seconds

If the humidity indicator on the PBE is showing Blue - answer This is normal

T/F During the origination flow with the APU running, the pilot presses and holds the
Fire Extinguisher TEST button for more than 10 seconds. Will the APU turn off? -
answer True. White when pressed, Red when a fire is detected

At FL350 you experience an IDG failure, after completing the appropriate QRH, you
elect to start the APU. What altitude must you descend to in order to start the APU? -
answer FL300

T/F The APU will automatically shut down for a fire inflight - answer False

What is the maximum altitude the APU can be started at? - answer FL330

While starting the APU, the APU master switch is first rotated "ON". Prior to rotating the
APU master switch to "START" what should be verified? - answer EICAS must be
energized for a minimum of 30 seconds, no APU FAIL messages displayed on EICAS,
and the APU indication on the EICAS changes from off to the APU

When powering down the APU, using the leaving the airplane checklist, what indication
are you looking for prior to switching Battery 1 and 2 to OFF? - answer Wait until
APU indicates "OFF" and there is an APU Fuel shutoff valve EICAS message within 80
seconds

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