Startup (DCS A-10C v1.1.0.8+)
Initiate electrical power 1. Right console Electrical Panel BATTERY switch: PWR (up position)
@Night: Turn on Flood Light
2. Right console Electrical Panel INVERTER switch: STBY (up position)
Electrical power running
Test caution and
warning systems,
activate oxygen supply
1. Test cockpit indication lights
Left console Auxiliary Lighting (AUX LTG) Panel press and hold LAMP TEST button
2. Test fuel indicator
Front dash press and hold TEST IND button
Both needles point to ~3000 lbs, digital totalizer readout: ~5900 lbs
3. Right console Oxygen Regulator Panel Oxygen SUPPLY switch: ON
Oxygen flow indicated in the FLOW window
4. Test the oxygen remaining indicator: Hold OXY IND TEST (Oxygen Indicator Test) button
OXY LOW caution light flashing when indication < 0,5l
Power the radios Left console
1. VHF/AM Frequency Mode Dial: TR (left position)
2. VHF/FM Frequency Mode Dial: TR (left position)
3. UHF Radio Function Dial: MAIN (up position)
Initiate engine start
sequence
1. Close canopy to minimize the noise
Right console Cano y Control Switch: Right click and hold (LCTRL+C)
2. Provide power to boost pumps of left/right wing tanks and left/right fuselage tanks
Left console Fuel System Control Panel
Boost Pum s Left Wing switch: ON (up position)
Boost Pum s Right Wing switch: ON (up position)
Boost Pum s Main Fuselage Left switch: ON (up position)
Boost Pum s Main Fuselage Right switch: ON (up position)
3. Start APU: Left console APU switch: START (up position)
Monitor front dash EMI Panel APU EGT and RPM gauges
→ Wait until APU EPM @100%!
4. Right console Electrical Panel APU GEN (Generator) switch: PWR (up position)
APU generator powers aircraft and relieves battery drain
5. Right console Electrical Panel
Left AC Generator Power: PWR (up position)
Right AC Generator Power: PWR (up position)
Request startup from
ATC
1. Tune VHF-AM radio to ATC frequency
2. Broadcast on VHF-AM: HOTAS Mic Switch FORWARD (LALT+NUM+)
3. Main ATCs... (F5) <AIRFIELD> (FX) Request startup (F3)
Crank up left engine 1. Left throttle from OFF to IDLE (RALT+POS1)
2. Monitor EMI panel
APU GEN caution light starts flashing once left engine is at ~50% core fan RPM
APU GEN no longer providing power to the aircraft systems and can be switched off:
Right console Electrical Panel APU GEN switch: OFF
Core fan RPM stabilizes at ~60%
Left Hydraulic system pressure normalizes between 2800 and 3350 PSI
Crank up right engine 1. Right throttle from OFF to IDLE (RCTRL+POS1)
2. Monitor EMI panel
Core fan RPM stabilizes at ~60%
Right Hydraulic system pressure normalizes between 2800 and 3350 PSI
Flight controls check Check
•stick/rudder input: rudder left (Y) / rudder right (X)
•speedbrakes: extract (LCTRL+B) / retract (LSHIFT+B)
•flaps: extract (F) / retract (LSHIFT+F)
Turn off APU Left console Throttle Panel APU switch: OFF
Power up CDU and EGI
Systems
1. Right console CDU ower switch: ON (up position)
2. Right console EGI ower switch: ON (up position)
automated BIT begins