Section 2 Expanded Flashcards

1
Q

*2. Hydraulic panel Set

A

a. AUX pump switch - OFF
b. Antiskid switch - ON
c. Engine pump switches - ON
d. Suction boost pump switches - OFF

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2
Q
  1. Fire extinguisher Checked, secured
A
Security of mounting
The nozzle is unobstructed 
The pull-pin is in place
Lock wire seal is in place
Pressure gage registers in the green zone (125 +/- 50 PSIG)
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3
Q

*8. Air conditioning panel

A

a. Air conditioning master switch - OFF
b. Cargo compartment and flight station/flight deck shutoff switches - NORM/NORMAL
c. Cargo compartment and flight station/flight deck temperature controls - OFF/NORMAL
d. Flight station airflow switch (some airplanes) - NORMAL
e. Under floor heating heat switch - OFF
f. Under floor heating fan switch (some airplanes) - OFF
g. Emergency depressurization switch NORMAL, safetied

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4
Q

*9. Anti-icing panel

A

a. NESA window switches - OFF
b. Nacelle preheat switches - OFF
c. Propeller and engine anti-icing master switch - OFF
d. Pitot heat switches - OFF
e. Engine inlet air duct anti-icing switches - OFF
f. Propeller ice control switches - OFF
g. Anti-icing wing and anti-icing empennage switches - OFF

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5
Q

*10. Bleed air switches

A

a. Bleed air divider valve switch - NORMAL

c. Engine bleed air switches - OFF

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6
Q

*11. Fuel panel Set

A

a. Dump pump switches - OFF
b. Dump valve switches - NORM/NORMAL, Safetied
c. Fuel boost pump switches - OFF
d. All crossfeed and bypass valve switches - CLOSED

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7
Q

*1. Electrical panel Set

A
Note: Ensure external electrical power is OFF prior to performing electrical panel checks.
a. INS battery charge switch - OFF
b. Generator switches - OFF\OFF/RESET
c. Generator disconnect switches - OFF, safetied
d. AC bus tie switch - OFF
e. Inverter switch(es) - OFF
f. INS battery bus voltage - Checked
Note: INS battery bus 1/2 volt lower than INS battery
g. INS battery voltage - Checked
h. Airplane battery voltage - Checked
i. DC power switch - BAT
j. DC bus tie switch - TIED
k. Volts and frequency - Checked
l. External AC power switch - EXT AC PWR
m. DC loadmeters - Checked
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8
Q

*4 Fire handles and overheat test panel

A

a. Fire handles
b. Turbine overheat test
c. Engine fire test
d. Nacelle overheat warning test
e. Anti-ice overheat circuit test

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9
Q

*5. SCNS (dual INU only)

A

Note: IFF must be in STBY
a. SCNS switch - ON
b. INU switches - ON
c. IDCU and SCNS control panel brightness - As required
d. Present position - Entered, verified
e. INS modes - ALIGN
Press Nav, INIT, INS ALIGN, COMMAND MODE 1 and 2, VERIFY

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10
Q

*8. APU

A

a. Clear APU (with GC)
b. Bleed air valve switch - CLOSED
c. Control switch - START RUN
d. APU on speed

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11
Q

APU generator

A

Note: Check volts and freqs after placing APU generator ON
a. Essential DC bus voltage - Checked
b. INS battery bud - Checked
Note: 1/2v lower than ESS DC
c. INS battery - Checked
d. INS battery charge switch - ON, checked, OFF
Note: INS battery voltage should increase then decrease

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12
Q

*10. AC bus tie switch Checked

A

a. MAIN AC OFF light - Illuminated
b. AC BUS TIE SW ON light - Extinguished
c. AC bus tie switch - ON
d. MAIN AC OFF light - Extinguished
e. AC BUS TIE SW ON light - Illuminated

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13
Q

*14. Bleed air system Checked

A

a. All propellers - Clear (with GC)
b. Bleed air divider valve switch - CLOSED
c. APU bleed air valve switch - OPEN
d. Engine bleed air switches - OVRD
e. Bleed air divider valve switch - OPEN (while monitoring bleed air manifold pressure)
f. System pressure - Checked
g. APU bleed air valve switch - CLOSED
h. System pressure leakage - Checked
i. Engine bleed air switches - OFF
j. APU - As required

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14
Q

*17. Standby attitude indicator Checked

A

a. Unlock and uncage the gyro and observe that the warning flag is out of view and that the indication is completely stabilized within 3 minutes
b. Place standby attitude switch to the INS BUS position and observe that the warning flag remains out of view.
c. Adjust caging knob to obtain desired outcome h presentation
d. Place standby attitude indicator switch to OFF, and observe the warning flag appears
e. Standby attitude indicator gyro - Caged and locked

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15
Q
  1. Crew entrance door Checked
A

a. Door handle - check hooks for over center travel
b. Rotating shaft - Check alignment, no excessive movement
c. Closure - Movement, fit
d. Seal, rope, telescopic arm - General condition

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16
Q

*1. Crew entrance area Checked

A

a. Close the door and visually check that the hooks contact the eyebolts and the over centering linkage contacts the stops
b. Crew door master door warning light shutoff switch - ON, safetied
c. Radio and equipment rack - Checked

17
Q
  1. Exterior Inspection Completed
A

a. Nose landing gear pin - Removed
b. Pitot covers - Removed
c. Dust excluders - Removed
d. Ground wires - Removed
e. Landing gear doors - Closed, secured
f. Access panels - Closed, secured

18
Q
  1. Air conditioning panel Set
A

a. Air conditioning master switch - OFF
b. Cargo compartment and flight station shutoff switches - NORM
c. Cargo compartment and flight station temperature controls - OFF, NORMAL
d. Underfloor heating heat switch - OFF
e. Underfloor heating fan switch - OFF
f. Emergency depressurization switch - NORMAL

19
Q
  1. APU panel
A

a. Control switch - STOP

b. Bleed air valve switch - CLOSE

20
Q
  1. Anti-icing panel Set
A

a. NESA windshield switches - OFF
b. Nacelle preheat switches - OFF
c. Prop and engine anti-icing master switch - AUTO
d. Pitot heat switches - OFF
e. Engine inlet air duct anti-icing switches -OFF
f. Propeller ice control switches - OFF
g. Anti-icing wing and anti-icing empennage switches - OFF

21
Q
  1. Fuel panel Set
A

a. Dump valve switches - NORM, safetied
b. Dump pump switches - OFF, safetied/OFF
c. No. 2 (or No. 3 on airplanes with Main AC bus tie switch) main tank BOOST OUMP switch - ON
d. All other fuel BOOST OUMP switches - OFF
e. Main tank crossfeed and crossfeed separation switches - OPEN
f. Bypass switches - CLOSED

22
Q
  1. Electrical panel - Set
A

a. Engine generator switches - ON
b. Main AC BUS TIE switch - ON
c. DC power switch - BAT/BATTERY
d. DC BUS TIE switch - TIED
e. External power - EXT AC or DC PWR (as required)