Section 2 Expanded Flashcards
*2. Hydraulic panel Set
a. AUX pump switch - OFF
b. Antiskid switch - ON
c. Engine pump switches - ON
d. Suction boost pump switches - OFF
- Fire extinguisher Checked, secured
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)
*8. Air conditioning panel
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
*9. Anti-icing panel
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
*10. Bleed air switches
a. Bleed air divider valve switch - NORMAL
c. Engine bleed air switches - OFF
*11. Fuel panel Set
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
*1. Electrical panel Set
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
*4 Fire handles and overheat test panel
a. Fire handles
b. Turbine overheat test
c. Engine fire test
d. Nacelle overheat warning test
e. Anti-ice overheat circuit test
*5. SCNS (dual INU only)
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
*8. APU
a. Clear APU (with GC)
b. Bleed air valve switch - CLOSED
c. Control switch - START RUN
d. APU on speed
APU generator
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
*10. AC bus tie switch Checked
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
*14. Bleed air system Checked
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
*17. Standby attitude indicator Checked
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
- Crew entrance door Checked
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
*1. Crew entrance area Checked
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
- Exterior Inspection Completed
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
- Air conditioning panel Set
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
- APU panel
a. Control switch - STOP
b. Bleed air valve switch - CLOSE
- Anti-icing panel Set
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
- Fuel panel Set
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
- Electrical panel - Set
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)
