Remove the ground items that protect the parked aircraft and establish the developer's preflight state.

1. Confirm wheel chocks are initially in place and position external power if you intend to use it.
2. Remove protective covers and blanking caps, including engine, propeller and pitot/static protection as applicable in the simulation.
3. Confirm the tail support and safety equipment are accounted for before departure.
4. Use the EFB or avatar-mode interactions to manage ground equipment and doors.

Work around both wings, engines, fuselage and empennage before entering the cockpit.

1. Check each wing's flap, aileron/trim tab, filler cap, navigation/landing light, stall vane and tank vent.
2. At each engine/nacelle, check fuel drains, cowling security, air inlet/inertial separator, propeller/spinner, oil-cooler inlet, landing gear/brake area, pump vents and defueling/cross-feed drain areas.
3. At the nose, check antennas, anti-collision light, pitot tubes, avionics doors, windshield wipers, nose gear/tire/doors and taxi light.
4. At the aft fuselage and empennage, check antennas/lights, both static ports, hydraulic-reservoir level, control surfaces and trim tabs.

The product contains passenger and cargo variants, so use the branch that matches the loaded model.

1. Passenger configuration: check oxygen pressure, emergency equipment and exits; check toilet condition if fitted and baggage-compartment attachment.
2. Cargo configuration: confirm the front-right emergency exit area is clear, the cargo arresting net is attached and the load is tied down.
3. Confirm doors are appropriate for the selected model: the EMB-110P uses one rear-left main door, while P1/P2 variants provide two left-side doors with cargo/passenger differences.

Establish the developer checklist's initial cockpit configuration and test the principal warning systems.

1. Review the flight logbook, check tabs and circuit breakers, set the parking brake and remove gust locks.
2. Set weather radar OFF, propeller synchronizer OFF, landing gear selector DOWN and air-conditioning master OFF.
3. Set power levers MIN, propeller levers MAX RPM and fuel-condition levers FUEL CUT-OFF.
4. Set trim tabs neutral/green band; check oxygen/full-face mask equipment if installed.
5. Apply battery or external power, check voltages, test static/pitot heat, leave inertial separation OFF and verify the gyros are ready.
6. Verify shut-off valves OPEN, perform both engine fire tests, check fuel quantity/totalizer and test the multiple alarm panel.

Use the EFB/performance tools and source-backed aircraft data when preparing the simulator flight.

1. Keep takeoff weight at or below 6,010 kg, landing weight at or below 5,700 kg and zero-fuel weight at or below 4,496 kg.
2. The published usable fuel capacity is 1,381 kg and the published range with maximum payload is 1,058 NM.
3. Use the product EFB performance page to check takeoff and landing distance for the actual weight, flap setting, inertial-separation state and weather.
4. Remember the published service ceiling is 21,000 ft and VMO is 230 KIAS.
5. Respect 180 KIAS for 25% flap and 148 KIAS for full flap; the gear operating/extended limits are 148/146 KIAS respectively.

Secure the aircraft and establish electrical, hydraulic and fuel-system configuration before cranking.

1. Confirm exterior and cabin/cockpit inspections complete; remove and stow wheel chocks and tail support.
2. Close the doors, adjust seats/pedals/belts and keep the parking brake SET.
3. Select BATTERY or EXTERNAL POWER, set the rotating anti-collision light and navigation lights ON, and set interior lights as required.
4. For a passenger configuration, set cabin signs ON.
5. Switch both inverters ON, set the fuel totalizer, switch the hydraulic booster pump ON and close the clear-vision windows.
6. Cycle auxiliary fuel pumps ON then AUTO and switch the main fuel pumps ON.

Use the NextGen checklist sequence for the first engine with battery or external power.

1. Switch the selected engine ignition ON.
2. Momentarily select START and release the starter switch.
3. Verify a positive oil-pressure indication while the engine accelerates.
4. At approximately 12% Ng, move the corresponding fuel-condition lever to LO IDLE.
5. Monitor ITT during the start.
6. After approximately 45% Ng, switch ignition OFF.
7. Confirm oil pressure is at least 40 psi, check hydraulic pressure, then set the fuel-condition lever and air conditioning as required.
8. Switch the corresponding generator ON and check the ammeter.

Repeat the defined start sequence for the remaining engine and confirm its electrical/hydraulic indications.

1. Switch the second engine ignition ON and momentarily select START.
2. Confirm positive oil pressure, then move its fuel-condition lever to LO IDLE at approximately 12% Ng.
3. Monitor ITT and switch ignition OFF after approximately 45% Ng.
4. Check oil and hydraulic pressure.
5. Set the fuel-condition lever and air conditioning as required.
6. Switch the corresponding generator ON and verify the ammeter indication.

The developer checklist provides a short start-interruption recovery action.

1. Move the affected fuel-condition lever to FUEL CUT-OFF.
2. Select starter INTERRUPTION.
3. Do not continue the normal start sequence until the simulated condition has been resolved.

Once both engines are stable, place the electrical, heating, avionics and cabin systems into taxi configuration.

1. Return the battery master to BATTERY and confirm both generators ON.
2. Check voltage/current indications and battery temperature.
3. Set static/pitot heat and Px heat as required.
4. Set radios as required, weather radar STBY and transponder STBY.
5. Set air conditioning as required.

Make the initial rolling checks before continuing toward the runway.

1. Release the parking brake and test the wheel brakes promptly.
2. Check flight instruments for sensible indications during movement.
3. Check the beta lights and weather radar, then leave the radar in STBY.

Finish the EMB-110 taxi/run-up items before the dedicated before-takeoff flow.

1. Check fuel cross-feed operation and return cross-feed OFF.
2. Check fuel pumps and leave them in the required operating state.
3. Move both fuel-condition levers to HI IDLE.
4. Move the propeller levers to FEATHER twice as the developer checklist directs.
5. Test the autopilot and leave it OFF.
6. Check/set the trim tabs.

Complete the full developer before-takeoff setup before entering the runway.

1. Use cockpit lights at night and set inertial separation as required.
2. Select 25% flaps and confirm the flap-position indication.
3. Check flight controls and set all trim tabs for takeoff.
4. Verify takeoff data and complete the takeoff briefing.
5. Switch strobe, landing and taxi lights ON.
6. Set flight instruments/radios for departure, weather radar as required and transponder ON.
7. Set air conditioning OFF or VENT.
8. Check the annunciator panel, confirm fuel-condition levers HI IDLE, parking brake released, auto-feather SET and pressures/temperatures normal.

Begin the developer's after-takeoff cleanup once safely airborne.

1. Retract the landing gear after a positive climb is established.
2. Retract flaps to 0% and confirm the indicator.
3. Continue into the climb configuration without leaving takeoff settings in place longer than needed.

Transition from takeoff to the developer's normal climb configuration.

1. Set propeller levers to approximately 91% Nh.
2. Set power levers for climb.
3. Set air conditioning as required.
4. Switch landing and taxi lights OFF and cockpit lights OFF when no longer needed.
5. Set inertial separation as required.
6. Switch auto-feather OFF and propeller synchronizer ON.
7. Switch the hydraulic booster pump OFF.
8. Check engine instruments; set passenger signs and oxygen as required.

Use the developer's propeller and power configuration while respecting torque.

1. Set propeller levers to approximately 83% Nh while observing the maximum torque limit.
2. Set power levers for the desired cruise.
3. Set passenger signs and autopilot as required.

The developer cruise checklist explicitly calls for Px heat when outside air temperature is below 5°C.

1. When OAT is below 5°C, switch Px heat ON.
2. Continue to configure the other ice-protection/inertial-separation systems according to the simulated conditions and developer controls.

Move the passenger, lighting, oxygen, heating and performance setup into the developer's approach state.

1. For passenger operations, switch cabin signs ON.
2. Reset altimeters as required and switch cockpit lights ON at night.
3. Close the oxygen valve if installed.
4. Set Px heat as required and switch landing lights ON.
5. Check landing data and complete the approach briefing.

Configure propellers, flaps, auto-feather, hydraulics and landing gear before final approach.

1. Set propeller levers to approximately 91% Nh initially and cross-check the altimeters.
2. Select 25% flaps and confirm the flap-position indicator.
3. Switch propeller synchronizer OFF and set auto-feather.
4. Move propeller levers to MAX RPM as the checklist sequence reaches the landing configuration.
5. Switch the hydraulic booster pump ON and check hydraulic pressure.
6. Lower the landing gear and confirm three green indications.
7. Set weather radar as required.

Complete the final flap, inlet, cabin and autopilot configuration for landing.

1. Select 100% flaps and confirm the flap-position indicator.
2. Set inertial separation as required.
3. Set air conditioning OFF or VENT.
4. Disengage the autopilot above the applicable critical altitude or decision height.

Go-around is a normal manoeuvre in the supplied checklist, not an RFoV abnormal/emergency procedure.

1. In flight: set propeller levers MAX RPM and advance power levers to the takeoff-power limit.
2. Select 25% flaps and confirm the indication.
3. Retract the landing gear after a positive climb is established.
4. If initiating the manoeuvre on the ground, set elevator trim into the green band, select 25% flaps, set propellers MAX RPM and advance to takeoff power.

Return lighting, radar, transponder, flaps and protection systems to the developer's taxi-in configuration.

1. Switch strobe lights OFF and set landing/taxi lights as required.
2. Set inertial separation as required and auto-feather OFF.
3. Switch weather radar OFF and set the transponder STBY or OFF.
4. Retract flaps to 0%.
5. Set air conditioning and fuel-condition levers as required.
6. Set trim tabs for taxi/parking.

Stabilise the aircraft on stand and place the engine controls in the developer's shutdown starting state.

1. Check ITT is below 650°C before shutdown.
2. Set the parking brake.
3. Move both power levers to MIN.
4. Set propeller levers to FEATHER or MIN RPM.
5. Switch the air-conditioning master OFF.

Complete the developer's engine, fuel, hydraulic and electrical shutdown sequence.

1. Move both fuel-condition levers to FUEL CUT-OFF.
2. Switch the remaining operational switches OFF and switch the hydraulic booster pump OFF.
3. After Ng reaches 0%, switch the fuel pumps OFF.
4. Return propeller levers to MAX RPM.
5. Switch panel/interior lights and both generators OFF.
6. Set the battery master to BATTERY or EXTERNAL POWER as required for the remaining ground state.
7. Wait until both propellers are fully stopped before opening doors.

Finish the developer's post-flight ground-security items.

1. Keep the parking brake SET and put wheel chocks in place.
2. Make the required flight-logbook entries.
3. Install the protective covers and blanking caps.
4. Close and secure the aircraft doors.