Manual Deletion
If you prefer not to run the script and would rather delete the folders manually, you can find them here: `%USERPROFILE%\AppData\Local\Packages\Microsoft.FlightSimulator_8wekyb3d8bbwe\LocalState\packages` or `%USERPROFILE%\AppData\Roaming\Microsoft Flight Simulator\Packages` Delete all folders starting with `fss-aircraft-e`.
FLIGHT DECK
EMERGENCY EQUIPMENT
ENGINE
INGITION A / B
FUEL FLOW
OIL PRESS
IGNITION A / B OUT
TIMER
START 1 / 2
at 7% N2
at 20% N2
within 10 SECONDS
at 50% N2
2 MIN WARMUP
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## Step 2
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1. Open **NAV IDENT** and verify the loaded navdata cycle against the current date.
2. If navdata is out of date, follow the [Navdata Updater](https://docs.flightsim-studio.com/e-jet-series/special-features/electronic-flight-bag/navdata-updater) process (**EFB → Settings → Navdata**, or the desktop fallback).
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## Step 3
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1. If your SimBrief username or userid is stored, import the latest route from **ACT RTE**.
2. Use **DLK FPL** (LSK 3L) or **SEND** (LSK 4L) after origin, destination, and **FLIGHT ID** match your OFP.
3. See SimBrief Import.
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## Step 4
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1. Verify the imported waypoints on the datalink flight-plan list.
2. **ACTIVATE** (or **APPLY ACTIVE**) to load the route into the active plan.
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## Step 5
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1. On **ACT RTE**, select **DEPARTURE>** (LSK 6R) to open departure procedures.
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## Step 6
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1. Open runway selection for the departure airport.
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## Step 7
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1. Select the planned departure runway.
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## Step 8
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1. Select the planned SID.
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## Step 9
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1. Confirm the selected departure procedure.
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## Step 10
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1. **INSERT/APPLY** the departure procedure into the **MOD** flight plan.
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## Step 11
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1. Review the **MOD ACTIVE FPL**.
2. **ACTIVATE** (LSK 6R) to make the departure procedure active.
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## Step 12
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1. Return to **ACT RTE** and select **ARRIVAL>** (LSK 6R).
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## Step 13
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1. Open runway selection for the arrival airport.
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## Step 14
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1. Select the planned arrival runway.
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## Step 15
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1. Select the planned approach procedure.
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## Step 16
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1. If you do not use an approach transition, skip directly to **STAR** selection.
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## Step 18
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1. Select the planned STAR.
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## Step 19
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1. Confirm the selected arrival procedure.
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## Step 20
{% columns %}
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1. **INSERT/APPLY** the arrival procedure into the **MOD** flight plan.
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## Step 21
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1. Review the **MOD ACTIVE FPL**.
2. **ACTIVATE** (LSK 6R).
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## Step 23
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1. Press **FPL** and scan the active flight plan for discontinuities (`>>DISCONTINUITY<<`).
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## Step 24
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1. Use **NEXT** to walk through all flight-plan pages and check legs and constraints.
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## Step 26
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1. If a discontinuity remains (example on page 3/7), type the missing waypoint in the scratchpad (e.g. **PEVOS**).
2. Press the left LSK next to the discontinuity (dashed line) to insert the waypoint.
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## Step 28
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1. Press **DEL** to put `*DELETE*` in the scratchpad.
2. Delete the discontinuity dashes on the flight-plan page.
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## Step 29
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1. Review the **MOD** flight plan.
2. **ACTIVATE** (LSK 6R).
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## Step 30
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1. Press **PERF** and select **PERF INIT** (LSK 1L).
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## Step 31
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1. On **PERF INIT 1/3**, select **SEND REQST** to pull performance data from your SimBrief OFP.
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## Step 32
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1. Press **NEXT** to **PERF INIT 2/3**.
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## Step 34
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1. Enter **TO CG** from the EFB manifest (e.g. type `23.0` on the keypad).
2. Transfer the scratchpad value with the **TO CG** line-select key (LSK 5L).
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{% endcolumns %}
## Step 35
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1. Press **NEXT** to **PERF INIT 3/3**.
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## Step 36
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1. Press **CONFIRM INIT>** (LSK 6R, inverse white) to confirm performance initialization.
2. Without this step the vertical profile is **not** calculated — see PERF.
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## Step 37
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1. Select **PERF DATA>** (LSK 6R) to review the performance summary.
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## Step 38
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1. Select **TAKEOFF>** from the performance workflow prompts.
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## Step 39
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1. Enter **V1**, **VR**, **V2**, and **VFS** from the EFB manifest / loadsheet.
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## Step 40
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1. Preflight MCDU setup complete — you are ready for departure.
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# Overhead Panel
# ELECTRICAL - AC
### IDG 1 and IDG 2 SELECTOR KNOBS
**AUTO:** This position closes the IDG contactor, connecting the IDG to the respective AC BUS. When an engine starts, the IDG will automatically come on line, powering the respective AC BUS. The previous power source is disconnected from that AC BUS.
**OFF:** Opens the IDG contactor, isolating the IDG from the respective AC BUS. IDG is tripped off-line and de-excited.
**DISC:** Must be held in this position for one second to mechanically disconnect the IDG. After disconnect the flight crew cannot reconnect the IDG.
Source Priority for the AC BUS 1 and 2: Respective IDG (Onside), APU Generator (Inside), Ground Power Unit (Outside), Opposite IDG (Cross-side).
### APU GENERATOR BUTTON
**PUSH IN:** Automatically connects the APU generator to the AC BUS TIE, according to the source priority.
**PUSH OUT:** Opens the APU generator contactor and isolates the APU generator from the AC BUS TIE.
### IDG OIL INDICATOR
* Illuminates for high oil temperature or low oil pressure (HOTLOP) indicating which IDG must be disconnected.
* LED will be OFF after IDG disconnection.
* Associated with an EICAS message.
### AC BUS TIES SELECTOR KNOB
**TWO OPEN:** Opens the Bus Tie Contactor 1, segregating AC BUS 1 from AC BUS 2
**AUTO:** This position controls the operation of the BTCs, according to system logic. If one of the AC power sources fails, both AC electrical networks are automatically connected by BTCs.
**ONE OPEN:** Opens the BUS TIE Contactor 2, segregating AC BUS 2 from AC BUS 1.
### GROUND POWER UNIT (GPU) BUTTON
**PUSH IN:** Connects the AC GPU to the AC BUS TIE, according to source priority (AVAIL -> IN USE).
**PUSH OUT**: Isolates the AC GPU from the AC BUS TIE (IN USE -> AVAIL).
**AVAIL:** AC GPU is connected and AC power quality requirements (voltage/amperage/frequency) are within limits.
**IN USE:** AC GPU is powering the airplane.
{% hint style="info" %}
Before disconnecting the AC GPU the push button must be pushed out. The AC GPU has to be pushed out for the next connection.
{% endhint %}
# ELECTRICAL - DC
### TRU 1 and TRU 2 TOGGLE
**AUTO:** Automatic operation of the electrical system. Connects TRU 1 (2) to the respective DC bus
**OFF:** Isolates TRU 1(2) from the respective DC bus
### TRU ESS SWITCH
**AUTO:** Automatic operation of the electrical system. Connects TRU ESS to the ESS BUS 3
**OFF:** TRU ESS is isolated from ESS BUS 3
NOTE: DC GPU supplies power to only APU START BUS. It does not charge the batteries.
### BATT 1 SELECTOR KNOB
**ON:** Connects Battery 1 to DC ESS BUS 1
**OFF:** Power is only supplied to HOT BATT BUS 1
**HOT BATT BUS 1 powers:** Engine 1A and 2A fire extinguisher, engine fuel shutoff valve 1, hydraulic system shutoff valve 1, engine 1 oil level indication, Courtesy/Service lights fwd, DC ceiling lights.
### BATT 2 SELECTOR KNOB
**AUTO:** Connects Battery 2 to DC ESS BUS 2. Allows Battery 2 to power the APU START BUS during APU start.
**OFF:** Power is only supplied to the HOT BATT BUS 2
**HOT BATT BUS 2 powers:** Engine 1B and 2B fire extinguisher, engine fuel shutoff valve 2, hydraulic system shutoff valve 2, engine 2 oil level indication, refueling panel, Water and Waste controller, and CMC.
NOTES:
* Supply essential loads for 10 minutes.
* On ground if powered only by batteries for more than 5 minutes a horn will sound.
* Wait to turn the batteries off when leaving the aircraft until the APU off and APU FUEL SOV CLSD EICAS messages are displayed (approx.. 80 seconds).
### DC BUS TIES
**AUTO:** Allows automatic operation of the electrical system.
**OFF:** DC bus ties open.
# COCKPIT LIGHTS
### MAIN PNL KNOB
**OFF:** Turns the lights off.
**BRT:** Lights full bright.
### OVHD PNL KNOB
**OFF:** Turns the lights off.
**BRT:** Lights full bright.
### PEDESTAL KNOB
**OFF:** Button/window indications remain illuminated to full bright as a default operations configuration. All other lights turned off (backlighting).
**BRT:** Lights full bright.
### ANNUNCIATOR TEST BUTTON (Momentary position)
* Illuminates the white/amber striped bars and caption indications verifying the lamp integrity.
* Does NOT check parking brake ON light, AC GPU Button, or Fire indications.
### DOME SWITCH
**ON:** Turns 2 cockpit dome lights ON.
**OFF:** Turns 2 cockpit dome lights OFF.
# ENGINE FIRE HANDLE
### ENGINE FIRE HANDLE
**PULL:** Closes the associated engine bleed air, fuel and hydraulic shutoff valves, and crossbleed valve.
**ROTATE (left or right):** Discharges the A (left) or B(right) fire extinguisher bottle into the associated engine.
Engine Fire Indication:
* Engine Fire handle illuminates
* EICAS displays ENG (1) (2) FIRE message
* Master Warning triple chime and fire bell
* FIRE displayed on the respective engine ITT gauge
* Master Warning lights on glareshield illuminate
# FUEL
### XFEED SELECTOR KNOB
**LOW 1:** Opens the crossfeed valve and automatically activates AC PUMP2, supplying fuel to both engines from the right wing tank.
**OFF:** Closes the crossfeed valve.
**LOW 2**: Opens the crossfeed valve and automatically activates AC PUMP 1, supplying fuel to both engines from the left wing tank.
Note: Setting AC PUMP 1 or 2 selector knob to any position different than AUTO overrides fuel crossfeed pumps command.
### DC PUMP SELECTOR KNOB
**OFF:** Deactivates the DC fuel pump.
**AUTO:** Automatically operates the DC fuel pump according to the system’s logic.
**ON:** Activates the DC fuel pump.
### AC PUMP SELECTOR KNOBS
**OFF:** Deactivates the associated AC fuel pump.
**AUTO:** Automatically operates the associated AC fuel pump according to the system’s logic.
**ON:** Activates the associated AC fuel pump.
# PASSENGER SIGNS
### EMER LT SELECTOR KNOB
OFF: Prevents all emergency lights from illuminating if electrical power is turned off or fails.
ARMED: Automatically illuminates all emergency lights if the airplane loses electrical power or if airplane electrical power is turned off.
ON: Turns on all emergency lights.
### ATTND CALL BUTTON (Momentary Position)
**PUSH:** Single hi/lo tone chime in passenger cabin.
### STERILE SWITCH
**ON:** Illuminates the sterile rainbow light in the cabin.
**OFF:** Turns off the sterile rainbow light in the cabin.
### NO ELEC DEVICES / NO SMKG SWITCH
**ON:** Illuminates the respective signs.
**OFF:** Turns off the respective signs.
### FSTN BELTS SWITCH
**ON:** Illuminates the FASTEN SEAT BELTS signs.
**OFF:** Turns off the FASTEN SEAT BELTS signs.
# FIRE EXTINGUISHER
### FWD/AFT CARGO FIRE DETECTION/EXTINGUISHER BUTTON (Guarded)
Button illuminates if smoke is detected in the respective cargo compartment.
### FIRE DETECTION SYSTEM TEST BUTTON (Momentary position)
* Tests the engine fire, APU fire, and cargo smoke detection systems
* Press and hold the test button for a minimum of 3 seconds, but not more than 10 seconds if the APU is running or it will automatically shutdown the APU.
* Ventilation outflow valve closes – only when bleed air is being provided by the engines or the APU
### APU FIRE EXTINGUISHER BUTTON (Guarded)
* Illuminates in the event of a fire when APU EMER STOP button is pressed.
* Illumination turns OFF when the fire input from the APU fire detectors disappears.
* APU FIRE EXTINGUISHER button pressed:
* Discharges the APU fire bottle.
* Shuts down the APU through the APU FADEC
* Closes the APU fuel shutoff valve (SOV)
# APU CONTROL
### APU SELECTOR KNOB
**OFF:** Normal shutdown is initiated. Pneumatic power is removed immediately, electric power is removed at the end of a 1-minute cooldown. Rotating the knob back to ON during shutdown cancels the shutdown sequence.
**ON:** Normal position when running.
**START (Momentary position):** Initiates the APU start cycle.
Note: APU electrical and pneumatic are available 3 seconds after reaching 95% rpm.
### APU EMERGENCY STOP BUTTON
**PUSH IN:** Closes the APU shutoff valve, shutting the APU down without a cool down period. White bar illuminates in the lower half of the button.
**PUSH OUT:** Normal Position.
{% hint style="info" %}
Red striped bar in the top half of the button illuminates in the event of an APU fire. When pushed in a white striped bar illuminates and the APU FIRE EXTINGUISHER button illuminates.
{% endhint %}
APU Fuel Supply:
* DC power only the DC fuel pump provides fuel to the APU.
* AC power available with engines off, the fuel is provided by the AC fuel pump 2.
* Right engine running fuel is supplied by the ejector fuel pump from the right wing tank.
* Fuel normally supplied from the right or left fuel tank through the crossfeed valve.
# WINDSHIELD WIPER
### WINDSHIELD WIPER
**TIMER:** Intermittent operation
**OFF:** Windshield wiper stops in the stowed position
**LOW:** Operates at a low speed
**HI:** Operates in a high speed
# EXTERNAL LIGHTS
### NAV SWITCH
**ON:** Nav lights on
**OFF:** Nav lights off
### STROBE SWITCH
**ON:** Strobe lights on
**OFF:** Strobe lights off
### RED BCN SWITCH
**ON:** Red beacon on
**OFF:** Red beacon off
### LOGO SWITCH
**ON:** Logo lights on
**OFF:** Logo lights off
### TAXI LIGHT SWITCHES
**ON:** Respective taxi light on
**OFF:** Respective taxi light off
### INSP SWITCH
**ON:** Wing inspection lights on
**OFF:** Wing inspection lights off
### LANDING LIGHT SWITCHES
**ON:** Respective landing light on
**OFF:** Respective landing light off
# HYDRAULIC
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### ENG PUMP SHUTOFF BUTTON
**PUSH IN:** Closes the hydraulic shutoff valve (SOV), isolating the respective engine driven pump (EDP) from the associated hydraulic system.
**PUSH OUT:** Normal position.
### ELECTRIC HYDRAULIC PUMP SELECTOR KNOB
**OFF:** Turns the respective pump off.
**AUTO:** Back-up for the respective EDP.
In flight: Activates in case of
* EDP or engine fail, or
* Flaps selected > 0.
On ground: Activates in case of flaps selected >0, and
* TL set to takeoff thrust, or
* Groundspeed > 50 kts.
**ON:** Pump operates continuously, overriding system logic.
Note: ELEC PUMP 2 in AUTO: If engine 1 running and parking brake released pump turns on (Single engine taxi logic).
### PTU (POWER TRANSFER UNIT) KNOB
**OFF:** PTU is turned off.
**AUTO:** Allows the PTU to operate automatically, according to hydraulic system logic.
**ON:** Operates continuously, overriding system logic.
### HYDRAULIC SYSTEM 3 SELECTOR KNOBS
**OFF:** Turns the respective electrical pump off.
**ON:** Turns the respective electrical pump on. 3B overrides system logic.
**AUTO (3B):** Turns 3B on automatically if AC Electric Pump 3A fails.
{% hint style="info" %}
The PTU does not work on the ground.
{% endhint %}
Note: HYDRAULIC SYSTEM 3A pump is powered by the AC ESS BUS (Electrical Emergency).
# PRESSURIZATION
### CABIN ALT SELECTOR KNOB
**DOWN (Momentary action):** Closes the outflow valve manually.
**STOP:** Normal position.
**UP (Momentary action):** Opens the outflow valve manually.
### MODE SELECTOR KNOB
**MAN:** Manual control of the outflow valve. No automatic cabin depressurization on the ground after landing.
**AUTO:** Automatic operation, changes between the different pressurization modes.
**LFE CTRL:** Allows manual input of the landing field elevation. Pressurization remains in automatic CPCS control. FMS-derived LFE is shown in green. Manually selected LFE is shown with a cyan **M** in front of the altitude readout.
{% hint style="info" %}
If no destination airport is in the FMS, LFE defaults to 0 ft until you set it manually in LFE CTRL.
{% endhint %}
### DUMP BUTTON
**PUSH IN:** CPCS system operates automatically
**PUSH OUT:** Returns the system to normal operation.
Note: Not available in manual mode. If pushed in while in manual mode both recirculation fans and packs are turned off.
### LFE SELECTOR KNOB
**DOWN (Momentary action):** Decreases LFE in 100 ft increments.
**STOP:** Normal position.
**UP (Momentary position):** Increases the LFE in 100 ft increments.
Note: Only works when the MODE selector knob is in LFE CTRL.
# ICE PROTECTION
### WINDSHIELD HEATING (1) (2) BUTTON
**PUSH IN:** activates the respective windshield heating system. Only operates if there are at least 2 AC electrical sources. If only single AC power source is available only the left windshield heat is powered.
**PUSH OUT:** Deactivates the respective windshield heating system.
### ICE PROTECTION ENGINE (1) (2) BUTTON
**PUSH IN:** Automatic operation. Engine cowls are heated with high stage bleed from the respective engine.
**PUSH OUT:** Deactivates the respective engine anti-ice system.
### WING ICE PROTECTION BUTTON
**PUSH IN:** Automatic operation. Allows wing anti-ice protection to operate according to the ice protection mode selector setting or MCDU setting. If 1 bleed air or one engine fails, xbleed valve automatically opens and uses opposite bleed for both wings.
**PUSH OUT:** Deactivates the wing anti-ice system.
### ICE PROTECTION MODE SELECTOR KNOB
**AUTO:** If an icing condition is detected during flight, the ice detectors command the wing and engine anti-ice valves to open and remain activated for 2 minutes after the icing condition is no longer detected.
* For taxi out and takeoff, anti-icing operation must be set in the MCDU.
* For taxi in, mode selector knob must be selected to ON if icing is anticipated or encountered.
**ON:**
* Inflight: Overrides system logic, activating the anti-ice system
* Ground: Activates the anti-ice on the ground.
* Engine anti-ice whenever an engine is running
* Wing anti-ice at wheel speed above 40kts
### ICE PROTECTION TEST SELECTOR KNOB
**OFF:** Spring-loaded position. Normal position.
Wing anti-ice system tests itself during flight 10min after takeoff or at 10.000ft AGL, whichever occurs first.
* EICAS message A-I WING VLV OPEN will be displayed
# AIR COND / PNEUMATIC
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### RECIRC BUTTON
**PUSH IN:** Allows automatic operation by the AMS. Turns on both recirculation fans, according to system logic.
**PUSH OUT:** Turns off both recirculation fans.
### PACK (1) (2) BUTTON
**PUSH IN:** Allows automatic operation by the AMS. Opens the respective pack flow control valve.
**PUSH OUT:** Manually closes the respective pack flow control valve.
NOTE: During first engine start, Emergency Ram Air Valve Built-In Test (BIT) commands PACK 1 OFF.
### BLEED (1) (2) BUTTON
**PUSH IN:** Allows automatic operation by the AMS. Commands the respective engine bleed valves, according to system logic.
**PUSH OUT:** Manually closes the engine bleed valves.
### CKPT TEMPERATURE SELECTOR
Controls cockpit temperature relative to the knob position.
### PAX CABIN TEMPERATURE SELECTOR
Controls passenger cabin temperature relative to the knob position.
**ATTND position:** Enables the flight attendant panel(s) to control the cabin temperature. An “ENABLED” led turns on in the flight attendant panel(s) indicating they have control of the temperature.
### XBLEED BUTTON
**PUSH IN:** Allows automatic operation by the AMS. This position opens the cross-bleed valve, according to system logic.
**PUSH OUT**: Manually closes the cross-bleed valve.
### BLEED APU BUTTON
**PUSH IN:** Allows automatic operation by the AMS. Commands the APU bleed valve, according to system logic.
**PUSH OUT:** Closes the APU bleed valve.
# PASSENGER OXYGEN
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### MASK DEPLOY SELECTOR KNOB
OFF: Disables automatic deployment of passenger oxygen masks.
AUTO: Automatically deployed when the cabin altitude is between 14.000ft to 14.750ft.
OVRD: Deploys the passenger oxygen masks regardless of cabin altitude.
### MASKS DEPLOYED LIGHT
An ON light illuminates, indicating that the passenger and flight attendant oxygen masks have been deployed.
When the passenger masks doors are commanded open the FASTEN SEAT BELT and the NO SMOKING signs turn on regardless of the switch position.
# GND PROX TERR INHIB AND EMERG/PRKG BRAKE
#### GND PROX TERR INHIB BUTTON
* When pushed in, inhibits EGPWS and thus avoids unwanted terrain alerts in airports not covered by EGPWS database.
#### EMERG/PRKG BRAKE LIGHT
* ON: Illuminates when the emergency/parking brake is actuated and there is hydraulic pressure on the brake line.
# Main Panel
# Primary Flight Display (PFD)
# SPEEDS
### SELECTED AIRSPEED READOUT
Displays speed/mach values.
**MAGENTA:** Automatically set by the FMS
**CYAN:** Manually entered by the flight crew.
### V2 SPEED (2)
Takeoff safety speed
### VR SPEED (R)
Takeoff rotation speed
### V1 SPEED (1)
Takeoff decision speed
**AIRSPEED TRANSITION:** Airspeed transitions automatically between IAS and Mach and vice versa at approximately 29.000 ft.
### VSPEED Bugs
Preview mode displays in the lower portion of the airspeed tape. VSPEEDS are entered in the MCDU. When no valid VSPEED data is available and the aircraft is on the ground cyan dashes are displayed.
### AIRSPEED ROLLING DIGITS
**GREEN:** Normal range.
**AMBER** Airspeed trend vector is reaching the VMO/MMO or it is at amber low speed awareness tape or the actual airspeed is at amber low speed awareness tape.
**RED INVERSE VIDEO:** Airspeed trend vector or actual airspeed is at red low speed awareness tape or at VMO/MMO barber pole.
### LOW SPEED AWARENESS (LSA) TAPE
Indicates the margin to the stick shaker speed. It rises from the bottom of the speed tape and has two colored ranges.
### SELECTED MACH READOUT
Displays speed/mach values.
**MAGENTA:** Automatically set by the FMS.
**CYAN:** Manually entered by the flight crew.
### SELECTED AIRSPEED BUG
**MAGENTA:** Displayed at the FMS airspeed target when an FMS mode is valid.
**CYAN:** Displayed at the Manual mode airspeed target.
### MACH AIRSPEED DIGITAL DISPLAY
Mach digital display of the current airspeed is displayed followed by an “M” label.
### VMO/MMO BARBER POLE
Displayed when the VMO/MMO is within the viewable range and covers speeds at or above VMO/MMO.
### VAC SPEED (AC)
Approach climb speed
### VF SPEED (F)
Flap retraction speed
### VAP SPEED (AP)
Approach speed
### VRF SPEED (RF)
Reference speed
### GREEN DOT
Provides a margin of 1.3g over stick shaker speed. Does account for ice, however it is invalid above FL200 with the ice EICAS message displayed.
### VFS SPEED (FS)
Takeoff final segment speed.
# FLIGHT MODE ANNUNCIATORS (FMA)
### AUTOTHROTTLE ANNUNCIATIONS ON FMA
**Left Column:**
* The AT mode annunciations displayed on the Flight Mode Annunciation display (FMA) are:
* Top row indicates autothrottle engagement mode
* Bottom row indicates autothrottle armed mode
**Right Column:**
* Depicts whether the Autothrottle is engaged or disengaged.
### AUTOPILOT ENGAGE (AP/TCS) ANNUNCIATOR
### AUTOPILOT/AUTOTHROTTLE SOURCE SELECTION
PFD source that currently supplies the references (primary NAV source and selected airspeed reference) for FGCS autothrottle or flight director operation. It is controlled by the SRC button the Glareshield Panel.
### APPROACH STATUS INDICATION
Approach armed status is white, left of the source selector. Approach engaged status is green, right of the source selector.
| Annunciator | Color | Meaning |
| --------------- | ------------- | ------------------------------------------------------ |
| **APPR 1** | White / Green | CAT I capable — armed / engaged |
| **APPR 1 ONLY** | White / Amber | CAT I is the only available approach mode |
| **APPR 2** | White / Green | CAT II capable — armed / engaged |
| **APPR 2 ONLY** | White / Amber | CAT II armed/engaged and it is the only available mode |
| **AUTOLAND 1** | White / Green | Autoland 1 (Cat IIIa) armed / engaged |
| **AUTOLAND 2** | White / Green | Autoland 2 (Cat IIIb) armed / engaged — E170 only |
| **NO AUTOLAND** | Red | Autopilot still engaged after AUTOLAND 1/2 was lost |
| **L/VNAV** | White | FMS LNAV/VNAV approach armed |
| **LPV** | White | LPV approach armed |
Armed modes flash reverse video for 5 seconds, then remain steady.
**CAT I (APPR 1)**
* Minimums set to **BARO** (DA).
* LOC and GS armed or active.
* Engages when LOC and GS are active and radio altitude is below 1,500 ft (or RA invalid).
* Disconnect AP before 200 ft AGL on a CAT I approach.
**CAT II (APPR 2)**
Armed when all of the following are met:
* Both PFDs set minimums to **RA** (and the same RA value).
* Both NAV receivers on the ILS frequency and course.
* Dual valid NAV / independent IRS and air data (no relevant miscompares).
* LOC and GS armed or active.
* Steep approach not armed or engaged.
* Radio altitude not below 800 ft (capability freeze).
* Airplane is approach-2 capable (valid RA, dual PFDs, etc.).
If APPR 2 is not capable, **APPR 2 NOT AVAIL** is posted on CAS.
**AUTOLAND**
Autoland is an option, enabled on the MCDU **OPR CONFIG** page.
* **AUTOLAND 1** — E170/E175/E190/E195.
* **AUTOLAND 2** — E170 only, and autobrake must be armed.
Typical extra requirements versus APPR 2: autoland option ON, autopilot engaged, yaw damper on, independent NAV sources on each side.
If autoland was engaged and the configuration is lost, **NO AUTOLAND** is shown in red.
{% hint style="info" %}
AUTOLAND 1/2 is approach-status logic on the FMA. It is not a substitute for a real-world Cat III autoland qualification.
{% endhint %}
### AUTOPILOT
* Autopilot disengagement:
* Either AP/TRIM DISC button is pushed.
* AP button on the Glareshield Panel is pushed
* Any manual pitch trim is activated
* Stick shaker activated
* Windshear escape guidance is activated
* A pilot input contrary to the autopilot is made on the controls.
* Autopilot will remain engaged in the event of an engine failure.
* Default Modes for the autopilot are: ROLL and FPA.
### LATERAL FLIGHT DIRECTOR MODES
### VERTICAL FLIGHT DIRECTOR MODES
**Default Modes:**
* Roll Hold (ROLL) is the default lateral mode (roll hold, wings level, and heading hold).
* When the autopilot is engaged without any modes being selected, ROLL is automatically engaged.
* When a vertical mode is selected without a lateral mode, the default ROLL mode is activated. The mode is displayed above the attitude indicator on the PFD
* Flight Path Angle (FPA) mode is the default vertical mode.
Magenta FMS modes (**FLCH**, **PTH**, **ASEL**, **ALT**, **GP**) are shown when VNAV is active. Automatic **OVSP** is shown when overspeed protection is active. **GA** is shown during go-around.
### WINDSHEAR
* Activated between 10 ft and 1.500 ft radio altitude.
* “WSHEAR” label displays on the PFD
* Windshear Caution: Increasing headwind and up drafts. Amber flag and aural alert “CAUTION, WINDSHEAR”.
* Windshear Warning: Decreasing headwind (or increasing tailwind) and down drafts. Red flag and aural alert “WINDSHEAR, WINDSHEAR, WINDSHEAR”.
* Autopilot automatically disconnects when windshear guidance is activated.
* Windshear alerting will last until 1.500 ft AGL or clear of windshear.
* Windshear alerting system will not function if both radar altimeters and/or EGPWS is inoperative.
### FLIGHT DIRECTOR GUIDANCE CUE IN TAKEOFF MODE
* Magenta vertical and horizontal bar.
* Displayed when the TO flight director mode is active.
* Takeoff guidance crossbars maintain extended runway centerline and pitch attitude based on appropriate configuration.
# ALTITUDES
### SELECTED ALTITUDE DIGITAL READOUT
* Displays altitude rounded to 100 ft.
* Displays cyan dashes on ground power-up.
* Altitude alerter sounds when the aircraft is within 1.000 ft of selected altitude.
* After altitude capture, when the aircraft departs more than 200ft from the selected altitude, altitude alerter sounds.
### METRIC SELECTED ALTITUDE READOUT
* Alternately displayed or removed by the PUSH FT-M switch that is integral on the ALT knob.
* An M indicates meters with a resolution of 50 meters.
### ALTITUDE ROLLING DIGITS DISPLAY
* Actual altitude rolled to a resolution of 1 foot but labeled every 20 feet.
* For negative altitudes a (-) is displayed in the place of the thousands digit.
* The ten-thousands, thousands and hundreds digits are taller.
* Altitudes above 0 but less than 10.000 ft have a green/black hashed box symbol that replaces the ten-thousands digit.
### METRIC ALTITUDE DISPLAY
* Alternately displayed or removed from display by the PUSH FT-M switch that is integral to the ALT knob.
* Current altitude in meters is displayed to a resolution of 5 meters. An M indicates meters.
### SELECTED ALTITUDE BUG
* Corresponds to the altitude value set in the altitude alert select digital display.
* When the selected altitude is off the displayed range, half of the bug remains on the top or bottom of the scale to indicate the direction to the selected altitude.
### ALTITUDE TREND VECTOR
* White thermometer starting at the altitude reference line and extends to the altitude the aircraft is at in 6 seconds, based on current vertical speed.
### ALTITUDE TAPE
* White tick marks are at 100-foot increments, except the white chevrons are at the 500-foot increments.
* When barometric altitude status or BARO correction data is invalid, altitude data is removed and a X is placed over the entire altitude tape area.
### BAROMETRIC ALTITUDE BOX
* Value is adjusted with BARO SET knob on the guidance panel.
* When the PUSH STD button on the BARO SET knob is pushed the altimeter setting window changes to STD and the correction is set to 29.92 inHg or 1013 hPa.
### SELECTED VERTICAL SPEED READOUT and BUG
* Displayed when VS is the active vertical flight director mode.
* Vertical speed is manually entered by using the VS wheel when the FGCS is in VS mode.
* Cyan filled bug is displayed on the vertical speed scale and is positioned at the selected vertical speed readout value.
* Cyan arrows above or below the display indicate the aircraft must climb or descend to attain the target vertical speed.
### VERTICAL SPEED SCALE
* Green pointer indicates the vertical speed on the scale.
* When pressure altitude data is invalid, display shows X
### VERTICAL SPEED DIGITAL READOUT
* Displays digital vertical speed.
* If TCAS RA is active, vertical speed readout is removed.
* At vertical speeds greater than +- 9.900 FPM, when the pressure altitude data received is invalid or when the altitude rate data is invalid the readout displays ----
### AVOIDANCE ZONE
Red trapezoid indicating the pitch that should be left to prevent collision with other aircrafts.
### FLY-TO-ZONE
Green rectangle indicating the pitch that should be followed to prevent collision with other aircrafts.
### RADIO ALTITUDE READOUT
* Only displayed when radio altitude is valid and less than 2.500 ft.
* RALT 1 is displayed on PFD 1, and RALT 2 is displayed on PFD 2.
* When one radio altimeter is invalid, the system automatically selects the other radio altimeter. Both displays turn amber and a CAS message is posted for the non-valid radio altitude system.
* When a miscompare occurs between system 1 and 2, an RA source data miscompare annunciator is displayed above the digital readout box (RA).
* When the radio altitude is invalid in both RA systems, the radio altitude readout is removed and is displayed. Corresponding CAS message is posted indicating both radio altitude systems have failed (-RA-).
### SELECTED MINIMUM RA/BARO ALTITUDE READOUT and BUG
* Set using the MINIMUMS rotary knob when BARO is selected on the MINIMUMS RA/BARO select switch.
* If additional counterclockwise clicks occur after the display reads 0 it will display OFF. After 5 seconds display is removed from view.
* Selected BARO altitude bug (with a horizontal L that sticks out from the left edge of the altitude tape).
* When barometric altitude is equal to or less than the approach minimums set value the bug and MIN annunciator turn amber.
* BARO minimum bug has priority over the trend vector.
# MARKER BEACONS
### MARKER BEACONS
Located in the upper right corner:
# FLIGHT PATH / ATTITUDE INDICATIONS
### FLIGHT PATH VECTOR (FPV)
* Consists of a green aircraft symbol that indicates the current flight path angle in reference to the horizon line.
* FPV turns red when TCAS RA is active and the FPV is in the Avoidance Zone.
* FPV is removed when excessive pitch is exceeded.
### FLIGHT PATH VECTOR SPEED ERROR TAPE
* Green tape that rises or descends from the left wing of the FPA symbol.
* Represents the difference between the selected airspeed and the current airspeed.
* Down indicates current airspeed is less than the selected airspeed, and up indicates more.
### FLIGHT PATH VECTOR ACCELERATION POINTER
* Displayed when FD is selected and gives an analog indication of acceleration and deceleration rate along the flight path.
* Moves up for increasing values of flight path acceleration and moves down for decreasing values of flight path acceleration.
### ATTITUDE REFERENCE AIRCRAFT SYMBOL
* Aircraft symbol is centered and always points to the top of the display. The background rotates around it.
* Displayed at all times and is used with the pitch tape to reflect aircraft pitch and roll attitude in relation to the horizon line.
### HORIZON LINE
* Based on the current aircraft pitch and roll attitude.
* When the horizon line and the attitude reference aircraft symbol are overlaid, the aircraft is in a level pitch attitude.
### FLIGHT DIRECTOR GUIDANCE CUE
* Displayed as a magenta diamond with short wings.
* Fits within the flight path vector symbol.
* If pitch or roll command data is invalid, the flight director guidance cue is removed.
Flight Director automatically displays:
* TOGA button actuation
* Autopilot is activated
* Windshear detection
### PITCH LIMIT INDICATOR (PLI)
The PLI is a pitch-based cue between stick-shaker angle of attack and current airplane angle of attack. It is shown on the PFD attitude display.
**DISPLAY LOGIC**
* Airplane airborne.
* Radio altitude greater than 200 ft.
* Calibrated airspeed at or below 1.2 Vs (low-speed / high-AOA regime).
**COLORS**
* **Green** — more than 5° remaining to stick shaker.
* **Amber** — 5° or less remaining to stick shaker.
* **Red** — stick shaker is active.
The PLI is removed above the speed/AOA gate and below 200 ft RA.
###  ### ROLL SCALE * Tick marks are located every 10 degrees up to 30 degrees. * Inverted triangles are displayed at 0 and 45 degrees of roll. ### ROLL POINTER AND SLIP/SKID INDICATION * The triangle is the roll pointer. * Bottom half of the roll pointer is used as a slip/skid indicator. * Lower portion of the triangle moves left or right to show the slip or skid condition  ### LOW BANK LIMIT ARC * Helps the pilot to fly with low bank angles during turns.  ### FLIGHT PATH ANGLE (FPA) * Indicates the current flight path in reference to the horizon line * Cyan color. # HORIZONTAL SITUATION INDICATOR (HSI)  ### HORIZONTAL SITUATION INDICATOR (HSI) DISPLAYS AND ANNUNCIATORS * Heading display on the HSI has 3 selectable modes: Full compass, Arc, and Map mode. * Modes are selected by pushing the HSI button. ### FULL COMPASS MODE * Displayed on initialization. * 360-degree compass view * Present heading is indicated by a fixed lubber  line at the top of the heading scale with a digital heading readout directly above the lubber line. ### ARC MODE * 90 degrees of compass view. * Weather is displayed when the WX button is pushed. * When the heading bug goes beyond the display range is displayed and shows the shortest direction to the heading select bug. ### MAP MODE * 90 degrees of compass view. * Weather is displayed when the WX button is pushed. * Flight plans are displayed * Cannot be used for preview mode.  ### SELECTED HEADING DIGITAL READOUT AND BUG * Displays the digital value for the aircraft selected heading. * Cyan heading select bug is positioned by rotating the HDG SEL knob. * Pushing the PUSH SYNC button on the HDG SEL knob synchronizes the heading bug and readout to the current aircraft heading. * When the aircraft selected heading (or the referenced aircraft heading) is invalid, the bug is removed, and digital readout is replaced with   ### DRIFT ANGLE BUG * Represented by an inverted solid white triangle displayed on the outside edge of the heading scale. * The difference between the aircraft heading and the aircraft ground track is the drift angle. * The drift angle bug is placed on the edge of the heading scale and aligned to the drift angle with respect to the lubber line. * When the drift angle is 0 degrees, the drift bug fits inside the heading bracket notch.  ### PRIMARY NAV SOURCE ANNUNCIATOR * Selected using the **V/L** or **FMS** buttons. * The **V/L**(VOR/LOC) button selects the available SRN (short-range navigation) source, displayed in green. * The associated annunciators are  * The **FMS**button selects FMS as the source, displayed in magenta. * With dual FMS systems installed the identifier will show  * When both sides have the same NAV source selected, digital readout for all information turns amber. ### PRIMARY NAV DISTANCE IDENTIFIER * Displays the NAV source station identifier. * The next magenta TO waypoint identifier is displayed. ### PRIMARY NAV DISTANCE READOUT * Distances of 100 NM or more, the digits are displayed with 1 NM resolution * Distances of less than 100 NM, the digits are displayed with 0.1 NM resolution ### PRIMARY NAV ESTIMATED TIME ENROUTE * Time is always displayed in minutes.  ### HEADING SOURCE ANNUNCIATORS * Selected by the IRS reversion buttons. * Not displayed when the on-side IRS source and magnetic heading are selected.  ### COURSE SELECT/DESIRED TRACK POINTER AND READOUT * Green for VOR and LOC navigation and the label is  * When VOR or LOC is selected, the track pointer is positioned by turning the CRS knob. * When the PUSH DIR button in the center of the CRS knob is pushed, the course select value is set to the course that minimizes the lateral deviation. * Magenta for FMS navigation and the label is  * Value of the desired track is supplied by the FMS. * Course deviation bar moves laterally and shows lateral deviation. * If both sides have the same navigation source selected the pointer, deviation bar, and digital readout turn amber.  ### TO/FROM INDICATOR * Magenta for FMS, Green for VOR or LOC. Turns amber if both sides are selected to the same source. * Pointer indicates the aircraft is flying to or away from the selected navigation source. * For a TO indication the triangle is located above the nose of the aircraft symbol. * The FROM indication is a triangle pointer on the tail of the aircraft symbol.  ### COURSE DEVIATION INDICATOR (CDI) AND LATERAL DEVIATION SCALE * Only displayed when a navigation source is active. * Deviation bar moves left or right to show the deviation from the selected NAV source. * When the back course mode is selected, or when tuned to a localizer frequency and the selected course is more than 100 degrees from the aircraft heading, the course deviation automatically reverses to properly sense deviation with respect to the course centerline. * When lateral deviation data is invalid, the CDI is removed and  is displayed in the CDI scale area.  ### BEARING POINTERS * Source is either VOR, ADF, or FMS. * Source is selected using the buttons on the guidance panel.  ### GROUNDSPEED * Displayed in the upper left corner of the HIS just below the airspeed tape. * When the IRS is invalid the digits are replaced with   ### DME SOURCE ANNUNCIATOR * DME source is selected by pushing the V/L button. * DME source annunciation reflects the short-range navigation source selection. * VOR1/LOC1 displays  VOR2/LOC2 displays  * When primary NAV source is FMS, the last selected VOR/LOC is used for the DME distance display. * When the same source is used, the DME data is displayed in amber. ### DME STATION IDENTIFIER, DISTANCE, AND TTG READOUT * DME source station identifier is displayed directly below the DME source annunciator. * Distance to go to the waypoint identified by the DME station identifier is shown in nautical miles. * TTG to the waypoint identified by the DME station identifier is shown in minutes. * When DME is in DME hold mode  is displayed in the front of the distance readout.  ###
# LATERAL/VERTICAL DEVIATION INDICATION \  ### ADI LATERAL DEVIATION * Magenta diamond for FMS deviation. Green trapezoid pointer used for LOC. * When both are displayed during PREV mode the FMS pointer overwrites the LOC pointer when both are at the same point. In PREV mode the trapezoid is displayed in cyan. * When a valid deviation is not available a X is depicted.  ### VERTICAL DEVIATION SCALE AND POINTER * Pointer is controlled by the selected primary navigation source (PNS). * Vertical deviation scale is displayed when: * Localizer (LOC) is selected as the PNS. * FMS is selected as the PNS, and the FMS commands the VNAV vertical scale in view. * ILS LOC deviation pointer is a green trapezoid. VNAV FMS is a magenta hollow diamond. * When glideslope data is invalid or when the vertical deviation scale is commanded into view by the FMS and a valid deviation is not available a X is depicted. * Preview vertical deviation is displayed when LOC is the PREV source. * LOC and FMS deviation are displayed the same way as the lateral deviation. # VERTICAL NAVIGATION (VNAV) ### VNAV ALTITUDE WAYPOINT CONSTRAINT READOUT * Displays an active waypoint constraint altitude automatically honored by the FMS prior to arrival at the preselected altitude.  ### VNAV TARGET ALTITUDE BUG * Displayed when a VNAV target altitude is valid and the FMS is the primary NAV source. ### VERTICAL TRACK ALERT (VTA) Magenta **VTA** on the PFD (above the vertical deviation scale). Flashes reverse video for 5 seconds, then remains steady. A VTA is issued when: * Within 1,000 ft of capturing an altitude constraint that is not the altitude preselect. * In cruise, 1 minute before TOD. * 1 minute before resuming a climb or descent from a constrained waypoint. * 1 minute before a step climb (cruise). An aural VTA is also issued. ### TOC / TOD ON THE MAP When FMS is the map source, **TOC** and **TOD** are shown on the MFD flight-plan overlay as altitude transition points on the vertical profile. # WIND DISPLAY / TIMER ### WIND DISPLAY 
**Cartesian:** Indicates the magnitude and direction of the wind as X and Y components. **Polar:** Digital readout for wind speed and arrow vector for direction.
### ELAPSED TIMER 
* Located in the top right corner of the HSI. * Displays time in hours and minutes (HH:MM) or minutes and seconds (MM:SS). * Controlled by the CHRONO button on the control yoke. **1st push:** Displays readout with the readout counting up from 00:00. **2nd push:** Pauses readout. **3rd push:** Resets the readout back to 00:00 and pauses. **4th push:** restarts the count. * Display is removed after 30 seconds in pause or reset. # FMS MODE ANNUNCIATORS 
* Displays the active and applicable FMS mode annunciators. * Located to the right of the HIS compass below the DME distance display. * RNP is displayed when FMS is the primary navigation source. * RNP values are determined in the priority order as follows: * Manual entry by pilot. * Default based on Phase of Flight: * Approach 0.3 * Terminal 1.00 * En route 2.00 * Oceanic/Remote 2.00 # COM / NAV  ### PFD RADIO CURSOR BOX * When the PFD is selected using the CCD, a cyan box is placed around the last selected radio frequency. The font size of the frequency digits and the radio source identifier become larger. * Defaults to the original grey outline and the font decreases in size when mouse cursor is leaving the corresponding box. * MCDU menu page can change COM1 to COM2 and NAV1 to NAV2 and vice versa. {% hint style="info" %} CCD is not simulated. Instead functionality is being provided by mouse over and clicking on the corresponding PFD areas. {% endhint %}  ### EXCHANGE PROMT * Indicates the green active frequency data is exchanged with the white standby frequency when the CCD ENTER button pushed. {% hint style="info" %} CCD is not simulated. Instead you can click on the cyan icon to swap frequencies. {% endhint %} ### ADJUST PROMT * Indicates the frequency is changed using the CCD rotary knobs.  {% hint style="info" %} CCD is not simulated. Instead you can use your mouse wheel to change standby frequency when hovering over it with the mouse. {% endhint %} ### COM FREQUENCY AND IDENTIFIER DISPLAY * White COM source identifier annunciator. * Green COM active frequency. * White COM standby frequency. ### NAV FREQUENCY AND IDENTIFIER DISPLAY * White NAV source identifier annunciator * Green active frequency when manually tuned or magenta when auto tuned. * White NAV standby frequency. # DISPLAYS \  ### FMS PLAN DISPLAY * Map data is oriented to the current aircraft heading (up). * FMS flight plan is displayed when: * HIS MAP mode has been selected. * Current leg and next waypoint (the TO waypoint) are displayed in magenta. All other legs and waypoints are white. ### LATERAL DEVIATION DISPLAY * Lateral deviation is displayed below the aircraft symbol at the bottom of the display. * Consists of a digital readout and either in the color of the primary navigation source, indicating deviation to the left or right.  ### WEATHER DISPLAY * Weather is displayed when the WX button on the PFD display controller is pushed. * Each PFD displays independently selected weather information. ### WEATHER RADAR SECTOR * Display sector is indicated by tick marks on the half range ring positioned at +-60. * In sector scan mode (SECT is selected), tick marks are located at +-30. ### WEATHER RADAR ANNUNCIATORS * Displayed to the left of the NAV radio box in the lower right area below the HSI. * Displays the specific weather mode.  ### PREVIEW MODE * When FMS is the primary navigation source and preview is selected, course, lateral deviation and vertical deviation are displayed. * The previewed navigation source automatically transitions to the primary navigation source when captured by the flight director (FD)/automatic flight control system (AFCS), FMS data is removed. * Only available in full compass or arc mode. ### PREVIEW NAVIGATION SOURCE * Preview NAV source is annunciated in cyan to the right of the primary NAV source. * Available annunciations are:  ### PREVIEW COURSE POINTER, DEVIATION BAR, AND DIGITAL READOUT * Cyan course arrow and deviation bar displayed at the same time as the primary NAV source DTK pointer and deviation bar. * Changed by turning the on-side CRS select knob when PREV is displayed. * TO/FROM pointer is a smaller cyan arrowhead that is displayed at the top (TO) or bottom (FROM) of the deviation bar. * With PREV displayed and no station information is present the TO/FROM pointer is removed. # Multifunction Display (MFD) # GENERAL ### TITLE MENU BUTTONS (HOT KEYS) * Each have menus to control and show the associated MFD display pages. * Controlled using the Cursor Control Device (CCD) ### PRIMARY NAV SOURCE, TO WAYPOINT IDENTIFIER, DISTANCE AND TIME DISPLAY * Displays the primary NAV source on the top row, TO waypoint next row down, Distance readout below and the bottom line contains the time-to-go readout. ### WIND DISPLAY, POLAR OR CARTESIAN * Polar wind display shows a single vector, Cartesian displays two vector arrows. ### FLIGHT INFORMATION DISPLAY * Displays Static Air Temperature (SAT), Total Air Temperature (TAT), and True Airspeed (TAS). * Use SAT when ATC asks for OAT. * Performance manuals are predicated upon SAT. ### DME DISPLAY * Displays DME source, Station Identifier on the middle row, and distance readout on the bottom row. * If DME Hold is active an amber  is displayed to the left of the distance readout. ### PROGRESS DISPLAY  * Displays waypoint name, destination, distance-to-go, ETA/ETE, and fuel remaining based on calculations received from the FMS. ### VERTICAL SCALE TAPE * Used as an altitude reference for the pilot. ### FMS SOURCE INDICATOR * Displays the primary navigation source. ### SELECTED ALTITUDE INDICATOR * Shows the selected altitude set by the altitude select knob. ### HALF- AND FULL-RANGE INDICATORS * Vertical scaling ranges are selected based on the horizontal half-range currently shown. * When range is controllable it is displayed in cyan. When the range is not controllable it is displayed in white. ### AIRCRAFT TRAJECTORY LINE * Shows the vector trend of the aircraft in the vertical axis based on the current flight path angle. ### WAYPOINT DISPLAYS * Contains a waypoint symbol, waypoint identifier, waypoint altitude, and when required a hold annunciator. ### VERTICAL TRACK LINES * Connect continuous waypoints in the flight plan. ### ALTITUDE PROFILE POINTS * Shows the relative location of specific altitude transition points on the vertical flight plan (i.e. TOC, TOD). ### AIRCRAFT SYMBOL * Gives a horizontal and vertical reference point for downpath waypoints.  ### **EPGWS** * Only displayed in the Map format. * Selected by checking the terrain button on the Map dropdown menu. * Solid Red: Warning Terrain (Approximately 30 seconds from impact). * Solid Yellow: Caution Terrain (Approximately 60 seconds from impact).   ### **MAP AND PLAN DIFFERENCES CHART** | **Function** | **Map Mode** | **Plan Mode** | | ---------------------------------------- | ------------------------------------ | -------------------------------------------------------------------- | | Display orientation | Heading, Up | North-Up | | View | Looking at Map from nose of aircraft | Looking at Map relative to North-Up | | Nonmoving reference at center of display |
Aircraft ref. = waypoint
Map ref. = aircraft
NO
Doors & emergency lights (6)
**DOOR CRG AFT OPEN** Shown when the indicated door is open while an engine is running or the aircraft is airborne. **DOOR CRG FWD OPEN** Shown when the indicated door is open while an engine is running or the aircraft is airborne. **DOOR PAX AFT OPEN** Shown when the indicated door is open while an engine is running or the aircraft is airborne. **DOOR PAX FWD OPEN** Shown when the indicated door is open while an engine is running or the aircraft is airborne. **DOOR SERV AFT OPEN** Shown when the indicated door is open while an engine is running or the aircraft is airborne. **DOOR SERV FWD OPEN** Shown when the indicated door is open while an engine is running or the aircraft is airborne.Fire protection (5)
**APU FIRE** Shown from the fire test panel or fire detection logic. **CARGO AFT SMOKE** Shown from the fire test panel or fire detection logic. **CARGO FWD SMOKE** Shown from the fire test panel or fire detection logic. **ENG 1 FIRE** Shown from the fire test panel or fire detection logic. **ENG 2 FIRE** Shown from the fire test panel or fire detection logic.Electrical (3)
**BATT 1-2 OFF** Warning when both main batteries are switched off while the aircraft needs electrical power. **BATT DISCHARGING** Shown when the indicated battery is discharging. **ELEC EMERGENCY** Shown when the electrical system is in emergency configuration.Air conditioning & pressurization (1)
**CABIN ALTITUDE HI** Warning when cabin altitude exceeds the CPCS high-altitude threshold.Fuel (1)
**FUEL 2 LO LEVEL** Shown when fuel quantity in the indicated tank is low.Doors & emergency lights (2)
**EMER LT NOT ARMED** Shown when the simulator detects: emer lt not armed. **EMER LT ON** Shown when the simulator detects: emer lt on.Electrical (19)
**AC BUS 1 OFF** Shown when ac bus 1 off is detected by the monitored system. **AC BUS 2 OFF** Shown when ac bus 2 off is detected by the monitored system. **BATT 1 DISCHARGING** Shown when the indicated battery is discharging. **BATT 1 OFF** Shown when batt 1 off is detected by the monitored system. **BATT 2 DISCHARGING** Shown when the indicated battery is discharging. **BATT 2 OFF** Shown when batt 2 off is detected by the monitored system. **DC BUS 1 OFF** Shown when dc bus 1 off is detected by the monitored system. **DC BUS 2 OFF** Shown when dc bus 2 off is detected by the monitored system. **DC ESS BUS 1 OFF** Shown when dc ess bus 1 off is detected by the monitored system. **DC ESS BUS 2 OFF** Shown when dc ess bus 2 off is detected by the monitored system. **DC ESS BUS 3 OFF** Shown when dc ess bus 3 off is detected by the monitored system. **GPU CONNECTED** Shown when external GPU power is connected to the aircraft. **IDG 1 OFF BUS** Shown when idg 1 off bus is detected by the monitored system. **IDG 1 OIL** Shown when the simulator detects: idg 1 oil. **IDG 2 OFF BUS** Shown when idg 2 off bus is detected by the monitored system. **IDG 2 OIL** Shown when the simulator detects: idg 2 oil. **TRU 1 FAIL** Shown when tru 1 fail is detected. **TRU 2 FAIL** Shown when tru 2 fail is detected. **TRU ESS FAIL** Shown when tru ess fail is detected.Engines & takeoff dataset (6)
**ENG 1 OIL LO LEVEL** Shown when engine oil quantity is below about 2 quarts. **ENG 2 OIL LO LEVEL** Shown when engine oil quantity is below about 2 quarts. **ENG NO TAKEOFF DATA** Caution on the ground when takeoff data is incomplete or inconsistent: V-speeds, flap setting, thrust rating, temperature, flex data, or FADEC/MCDU dataset agreement. Suppressed during takeoff (80 kt to 400 ft AGL) and for 120 s after landing. Also suppressed when flaps are up. **ENG REF A-I DISAG** Caution when REF A/I in the T/O DATASET MENU does not match the overhead ice protection configuration (OFF, ENG, or ALL) while below 1,700 ft RA and not in landing mode. Clears above 1,700 ft RA or 120 s after takeoff. **ENG REF ECS DISAG** Caution when REF ECS in the MCDU T/O DATASET MENU (TRS → TO DATASET) does not match the actual bleed configuration used for FADEC takeoff N1. The MCDU setting is ON or OFF; the aircraft is treated as ECS ON only when both packs are on, both engine bleeds are open, no APU bleed is supplying the manifold, and Pack 1 is not held off by the emergency ram air valve built-in test. Active below 1,700 ft radio altitude, not in landing mode, with both engines running. Clears when the mismatch ends or 120 s after takeoff. First flight of the day (ERAV BIT): on the first engine start of each UTC flight day the emergency ram air valve runs a \~90 s built-in test and holds Pack 1 off. With REF ECS ON, this caution can appear until the test completes. Spawn in turnaround mode in EFB Settings → Aircraft skips the ERAV BIT on that spawn. Engines on + APU bleed on: with both engines running and APU bleed open, bleed air comes from the APU (FADEC ECS OFF) even if packs stay on. REF ECS ON then disagrees. Close APU bleed or set REF ECS OFF. REF ECS does not command the packs; it is the takeoff N1 assumption. See AIR COND / PNEUMATIC and SYSTEMS/ECS (MFD). **ENG TLA NOT TOGA** Caution when thrust levers are not in the TOGA detent by 60 kt during takeoff.Air conditioning & pressurization (1)
**CABIN DIFF PRESS FAIL** Caution when cabin differential pressure exceeds the CPCS limit.APU (3)
**APU ALTITUDE EXCEED** Shown when the simulator detects: apu altitude exceed. **APU FAULT** Shown when apu fault is detected. **APU GEN OFF BUS** Shown when apu gen off bus is detected by the monitored system.Fuel (1)
**FUEL IMBALANCE** Caution when fuel quantity imbalance between wing tanks exceeds the monitored limit.Hydraulics (3)
**HYD 1 LO PRESS** Shown for low hydraulic pressure or quantity in the indicated system. **HYD 2 LO PRESS** Shown for low hydraulic pressure or quantity in the indicated system. **HYD 3 LO PRESS** Shown for low hydraulic pressure or quantity in the indicated system.Ice & rain protection (1)
**A-I LO CAPACITY** Shown for anti-ice valve or mode: a-i lo capacity.Flight controls & autoflight (1)
**FLT CTRL BIT EXPIRED** Caution when the flight control built-in test has expired; cycle power to reset.Flight instruments & surveillance (1)
**XPDR 1 IN STBY** Shown when the simulator detects: xpdr 1 in stby.Air conditioning & pressurization (6)
**BLEED 1 OFF** Shown when bleed 1 off is detected by the monitored system. **BLEED 2 OFF** Shown when bleed 2 off is detected by the monitored system. **LAND FIELD ELEV** Advisory when the landing field elevation entered in pressurization does not match the destination elevation in the FMS. **PACK 1 OFF** Shown when pack 1 off is detected by the monitored system. **PACK 2 OFF** Shown when pack 2 off is detected by the monitored system. **XBLEED SW OFF** Shown when xbleed sw off is detected by the monitored system.Fuel (1)
**FUEL EQUAL XFEED OPEN** Shown when the simulator detects: fuel equal xfeed open.Hydraulics (6)
**HYD 1 LO QTY** Shown for low hydraulic pressure or quantity in the indicated system. **HYD 2 LO QTY** Shown for low hydraulic pressure or quantity in the indicated system. **HYD 3 LO QTY** Shown for low hydraulic pressure or quantity in the indicated system. **HYD 3 PUMP A NOT ON** Shown when hyd 3 pump a not on. **HYD PTU NOT AUTO** Shown when hyd ptu not auto. **HYD PUMP NOT AUTO** Shown when hyd pump not auto.Ice & rain protection (4)
**A-I MODE NOT AUTO** Shown when a-i mode not auto. **A-I SWITCH OFF** Shown when a-i switch off is detected by the monitored system. **ICE CONDITION** Shown for ice protection: ice condition. **STALL PROT ICE SPEED** Shown for ice protection: stall prot ice speed.Flight controls & autoflight (4)
**SHAKER 1 FAIL** Shown when shaker 1 fail is detected. **SHAKER 2 FAIL** Shown when shaker 2 fail is detected. **SPDBRK LEVER DISAG** Advisory when the speedbrake lever position disagrees with the commanded speedbrake surface position. **YD OFF** Shown when yd off is detected by the monitored system.Landing gear & brakes (2)
**BRK LH FAULT** Shown when brk lh fault is detected. **BRK RH FAULT** Shown when brk rh fault is detected.Flight instruments & surveillance (1)
**IRS ALIGNING** Advisory while the IRS is aligning after power-up.Oxygen (1)
**PAX OXY SW NOT AUTO** Shown when pax oxy sw not auto.Engines & takeoff dataset (4)
**ENG 1 TLA NOT IDLE** Status when engine 1 start or shutdown is attempted while the left thrust lever is not at idle. **ENG 2 TLA NOT IDLE** Status when engine 2 start or shutdown is attempted while the right thrust lever is not at idle. **ENG TDS REF A-I ALL** Status reminder that REF A/I in the takeoff dataset is ALL (wing and nacelle anti-ice). **ENG TDS REF A-I ENG** Status reminder that REF A/I in the takeoff dataset is ENG (nacelle anti-ice only).Air conditioning & pressurization (1)
**BLEED APU VLV OPEN** Status when the APU is running, APU bleed is selected on the overhead, and the APU bleed valve is open.APU (1)
**APU SHUTTING DOWN** Shown when the simulator detects: apu shutting down.Hydraulics (2)
**HYD 1 SOV CLOSED** Shown when the simulator detects: hyd 1 sov closed. **HYD 2 SOV CLOSED** Shown when the simulator detects: hyd 2 sov closed.Ice & rain protection (3)
**A-I ENG 1 VLV OPEN** Shown for anti-ice valve or mode: a-i eng 1 vlv open. **A-I ENG 2 VLV OPEN** Shown for anti-ice valve or mode: a-i eng 2 vlv open. **A-I WING VLV OPEN** Shown for anti-ice valve or mode: a-i wing vlv open.Flight controls & autoflight (1)
**FLT CTRL TEST IN PROG** Status while the flight control built-in test is running (about three minutes).Landing gear & brakes (1)
**STEER OFF** Shown when steer off is detected by the monitored system.
### AUTOBRAKE EICAS INDICATION
* Autobrake status is shown on EICAS in the LG/AUTOBRAKE box.
* Indicates the autobrake is armed. 
* Green labels indicate the selected mode: 
* Indicates the data is invalid. 
# APU ### APU RPM INDICATION * Displays the APU RPM (%). * Green – normal operating range, Amber – cautionary operating range, Red – operating limit exceeded. *** ### APU EGT (EXHAUST GAS TEMPERATURE) INDICATION * Displays the APU temperature in degrees Celsius * Green – normal operating range, Amber – cautionary operating range, Red – operating limit exceeded. # CABIN ALT / LFE ### CABIN ALTITUDE INDICATION * Displays cabin altitude in feet, regardless of the operating mode. * Green – normal operating range, Amber – cautionary operating range, Red – warning operating range. *** ### CABIN RATE OF CHANGE INDICATION * Displays the cabin rate of change in fpm, regardless of the operating mode. * Green – normal operating range, Amber cautionary operating range. *** ### DIFFERENTIAL PRESSURE INDICATION * Displays the differential pressure between the cabin interior and the outside in psi, regardless of the operating mode. * Green – normal operating range, Amber cautionary operating range. *** ### LANDING FIELD ELEVATION INDICATION * Displays the landing field elevation in feet, regardless of the operating mode. * Green – FMS destination elevation (AUTO mode). * Cyan, with a cyan **M** prefix – manual LFE (MODE selector in **LFE CTRL**). * Amber dashed – invalid information, out of displayable range, or manual CPCS operation (MAN). *** ### HI FIELD INDICATION * Displays HI FIELD label whenever the Cabin Altitude is in High Altitude operation mode. # TRIM ### ROLL/PITCH/YAW SCALE * Trim position configuration is indicated by a solid green triangle. * There is a green takeoff band on the pitch trim scale, corresponding to the allowable pitch trim position for takeoff. *** ### PITCH TRIM DIGITAL READOUT * Digital indication of the horizontal stabilizer trim position in tenths of a degree increments. * Indication turns red if trim is outside green takeoff band while aircraft is in takeoff mode. # Reversionary Panel  ### DISPLAY SELECTOR KNOB **PFD:** Displays PFD information in the associated MFD. **AUTO:** Automatically reverts the MFD in case of display failure.  **MFD:** Displays MFD information in the associated MFD **EICAS:** Displays EICAS information in the associated MFD.  ### ADS SENSOR BUTTON (Momentary action) Reverts the ADS source.  When the ADS source reversion is selected, a white striped bar illuminates on the button. Associated ADS source flag is displayed on the PFD after a reversion takes place. ### IRS SENSOR BUTTON Reverts the IRS source. When IRS source reversion is selected, a white striped bar illuminates on the button. Associated IRS source flag is displayed on the PFD after a reversion takes place. # Integrated Electronic Standby System (IESS)  ### BRIGHTNESS ADJUSTMENT BUTTONS * Adjusts brightness ### AIRSPEED ROLLING DIGITS * Indicates actual calibrated airspeed. ### ILS BUTTON * Selects the display of ILS 1 deviations. ### REFERENCE BAROMETRIC PRESSURE INDICATION * Indicates the barometric pressure as set by the barometric rotary knob. ### STANDARD BUTTON * Sets the barometric pressure to standard atmospheric pressure. ### BRIGHTNESS CELL * Automatically adjusts the instrument brightness according to the ambient lighting. ### ALTITUDE INDICATION * Indicates actual altitude. * Green hashed box appears on the left side of the numeric digits when altitude is below 10.000 ft. * Minus (-) symbol appears on the left side when altitude is below sea level. ### BARO ROTARY KNOB * Adjusts the barometric setting. ### CAGE BUTTON {% hint style="info" %} CAGE is not simulated. The button is modeled; it does not reset attitude or show a CAGE flag. {% endhint %} * Resets attitude to zero, eliminating accumulated drift when the button is pressed for more than 2 seconds. * Must be used with wings levelled on stabilized flight conditions. * When pressed an amber CAGE flag is displayed on the upper right corner for the IESS.  ### ROLL INDICATION AND SLIP/SKID INDICATION * Indicates the bank angle of the airplane. * Bottom half of the triangle indicates slip or skid angle if flight is not coordinated. ### AIRPLANE SYMBOL * Reference for airplane attitude indication. ### VERTICAL SPEED * Indicates the actual vertical speed (ft/min). * Arrow indicates climb or descent. ### ILS DEVIATIONS * Green diamond indicates glide slope and localizer position. ### Vmo/Mmo BARBER POLE * Displayed when Vmo/Mmo is within the viewable range. ### METER ALTITUDE INDICATION * Indicates the actual altitude in meters. ### PITCH ANGLE SCALE * Provides a pitch angle indication between the airplane symbol and the horizon line. ### MACH NUMBER INDICATION * Displays Mach speed. ### ALIGNMENT * Takes about 90 seconds to align. IESS refresh rate can be limited on EFB **Aircraft** → **Display Refresh Rate**. # Autobrake ### AUTOBRAKE SELECTOR KNOB (ROTARY ACTION) * RTO: Selects Rejected Takeoff deceleration rate. This mode is equivalent to maximum manual braking. * OFF: Autobrake is deactivated. * LO: Selects the low deceleration rate. * MED: Selects the medium deceleration rate. * HI: Selects the high deceleration rate. ### AUTOBRAKE OPERATION * Modulates hydraulic pressure to the brakes in order to provide a constant deceleration rate corresponding to the level selected. * If reverse thrust is actuated, the autobrake system will modulate the brake pressure to maintain the deceleration rate constant to the mode selected. * Anti skid, touchdown and locked wheel protections are provided during autobrake operation. * Autobrakes will be disengaged when brake pedal pressure is applied, or the thrust lever is above idle. * Rejected Takeoff autobrakes will engage when: * Thrust levers IDLE or REV. * Wheelspeed above 60kts. * Brake pedals not pressed. * Ways to disarm the autobrakes: * Selector switch set to OFF. * Pedal braking is applied. * Brake control system failure is detected. * Either thrust lever is advanced beyond IDLE during autobrake application. # Gnd Prox Terr Inhib and EMERG/PRKG Brake ###  ### GND PROX TERR INHIB BUTTON * When pushed in, inhibits EGPWS and thus avoids unwanted terrain alerts in airports not covered by EGPWS database. *** ### EMERG/PRKG BRAKE LIGHT * **ON:** Illuminates when the emergency/parking brake is actuated and there is hydraulic pressure on the brake line. # Clock  ### DATE/SET KNOB/BUTTON * Allows time setting when GPS/INT/SET selector is in the SET position. * Repeated pressings cycles between minute, hour, year, month, and day. * Rotate the knob to select the desired digits. ### RESET BUTTON * Resets the chronometer to zero if it is stopped. * Display is blanked when the RST button is pressed and the chronometer is running. ### CHRONOMETER BUTTON * Starts/stops the chronometer. ### GPS/INT/SET SELECTOR * GPS: Synchronizes with UTC and DATE from GPS. * INT: Displays information from the internal clock. * SET: Allows date and time to be set by the DATE/SET KNOB/BUTTON. ### ELAPSED TIME SELECTOR * AUTO: automatically starts the chronometer on liftoff. * RST: Resets the elapsed time if Weight-on-Wheels (WOW) is present. ### CLOCK/CHRONOMETER DISPLAY * Displays chronometer, time/date and elapsed time. # Landing Gear  ### DOWNLOCK RELEASE BUTTON (MOMENTARY ACTION) * Manually releases the landing gear lever lock by mechanically bypassing the system protection logic. * Used when the landing gear won’t retract on takeoff and terrain is imminent. ### LANDING GEAR LEVER * UP: Retracts the landing gear. * DOWN: Extends the landing gear. # ELT and GND PROX G/S INHIB  ### EMERGENCY LOCATION TRANSMITTER (ELT) * Contains an impact switch that, when armed, turns on the ELT transmitter after crash impact. * Operates on its own battery power until the battery is exhausted. * When the ELT is active (transmitting), a light continuously flashes on the cockpit switch panel.  ### GND PROX G/S INHIB BUTTON * Used to manually cancel glideslope alerts. * Iluminates when pressed any time below 2.000ft nominal radar altitude and will be automatically reset (light off) by climbing above 2.000ft nominal or descending below 30ft. # LG WRN INHIB and ADS Probes Heater  ### LANDING GEAR WARNING INHIBITION BUTTON (GUARDED-MOMENTARY ACTION) * Inhibits the landing gear aural warning in the event of dual radio altimeter failure only if the SLAT/FLAP lever is in the 0, 1, 2, 3 or 4 position. * White striped bar when pushed will extinguish if: * Thrust levers are advanced beyond a pre-determined mid-range position. * Flap selector lever is set to 5 or full without any landing gear down and locked. ### LANDING GEAR AURAL WARNING * “LANDING GEAR” aural warning cannot be silenced in the following situations: * SLAT/FLAP lever in a landing position (5 or FULL) * Regardless of thrust lever position and radio altitude. * SLAT/FLAP lever in 0 to 4 position * Radio altitude below 700ft AGL, and * Thrust lever is set below a pre-determined mid-range position.  ### ADS PROBES HEATER BUTTON * PUSH IN: activates the ADS probes heater. * PUSH OUT: the ADS probes heater operates in AUTO mode. # Central Pedestal # Multifunction Control Display Unit (MCDU) \  Allows radio tuning, PFD radio tuning display setup, manual engine rating selection, engine takeoff data set, avionics setup, performance initialization, flight planning, and access to electronics CBs, among others. The custom FMS pages are documented in the [MCDU Guide](/e-jet-series/mcdu-guide/basics): [RTE](/e-jet-series/mcdu-guide/rte), [F-PLN](/e-jet-series/mcdu-guide/f-pln), [PERF](/e-jet-series/mcdu-guide/perf), [PROG](/e-jet-series/mcdu-guide/prog), [NAV](/e-jet-series/mcdu-guide/nav), [DATALINK](/e-jet-series/mcdu-guide/datalink), [RADIO](/e-jet-series/mcdu-guide/radio), [MENU](/e-jet-series/mcdu-guide/menu), and [TRS](/e-jet-series/mcdu-guide/trs-thrust-rating-system). # FLIGHT CONTROL MODE  ### FLIGHT CONTROL MODE BUTTONS (GUARDED) * PUSH IN: places the associated flight system into direct mode. * PUSH OUT: places the associated flight system into normal mode. # STALL WARNING # POWERPLANT \  ### START/STOP SELECTOR KNOB * **STOP:** commands the FADEC to shut down the engine, provided the associated thrust lever is in the IDLE position. * **RUN:** normal position for engine operation. * **START (momentary action):** initiates the engine start sequence. ### IGNITION SELECTOR KNOB * OFF: deactivates the ignition system. On ground, fuel flow is inhibited. FADEC disregards OFF position in flight. * AUTO: FADEC automatically controls the ignition system, depending on engine requirements. * OVRD: enables FADEC ton continuously activate both exciters whem the engine is running. # T/O CONFIG and EICAS FULL \  ### TAKEOFF CONFIG CHECK BUTTON * Checks the takeoff configuration * Flap position: Matches the FMS Takeoff page 2/2 * Parking brake: OFF. * Pitch trim: In the green band. * Spoiler panels: Not deployed. * Simulates power levers in the advanced position. * Does not check that both engines are running. {% hint style="info" %} **Button Interaction** In order to start the T/O config test you have to keep the button pressed for 3 seconds. {% endhint %}  ### EICAS FULL BUTTON * **PUSH IN:** EICAS full information presented. * **PUSH OUT:**Enables the automatic EICAS de-clutter logic. * De-clutter is disabled when the landing gear is extended and/or flap/slat is not at 0. * Automatic de-clutter occurs after landing gear retraction and flap/slad retraction, if all parameters are displaying normal indications. # Cursor Control Device (CCD)  ### TUNING KNOB * Outer and inner knobs select value or mode in the data field enclosed by the cursor. *** ### FORMAT LOCATION BUTTONS * Place cursor on associated display (PFD, MFD, or EICAS). *** ### TOUCH PAD * Used to move cursor. *** ### ENTER KEYS * Used to select soft keys. # SPEEDBRAKE / SPOILERS \  ### SPEED BRAKE LEVER * Symmetrically deploys the multi-function spoilers. All spoiler panels deploy at the same angle in response to the speed brake lever position. *** ### SPOILER SYSTEM * 5 spoiler panels each wing. 3 outboard spoilers each wing are called multifunction spoilers. * Roll Control: Deployed asymmetrically for roll augmentation by pilots control wheel. * Direct mode: Function at a default fixed gain. * Speed Brakes: Deploys all six multifunction spoiler panels symmetrically during flight by speed brake handle position. * Automatically retract: selection of slat/flap 2 or above, or airspeed below 180 KIAS, or TLA above 70 degrees. * Not available in direct mode. * Ground Spoilers: All ten spoiler panels deployed symmetrically to the fully extended position during landing roll. * Ground spoilers not available in direct mode.
# THRUST LEVER QUADRANT \ Throttle levers can be moved synchronously by using an invisible clickspot in the middle of both levers. #### AUTOTHROTTLE DISCONNECT BUTTON (A/T DISC) * Disengages the autothrottles. The PFD will dipslay GREEN BLINK AT warning after normal disconnect and AMBER BLINK AT warning after non normal disconnect **until second push** on any of the A/T glareshield or throttle disconnect switches. *** #### TAKEOFF AND GO AROUND BUTTON (TO/GA) * Selects the TO, GA, or Windshear Flight Director Modes. *** ### AUTOTHROTTLE MODES * AT sets the correct engine thrust with the synchronized N1 for its various operating modes * Normal disengagement: AT disconnect button on thrust lever, and AT button on the guidance panel. * Automatically disengaged when one of the following occurs: after airplane touchdown, thrust levers beyond the TO/GA position or reverse thrust operation during RTO. * Non Normal Disengagement: difference in TLA greater than 8 degrees, or autothrottle failure. * Autothrottle Modes: takeoff mode (TO), takeoff hold mode (HOLD), speed on thrust mode (SPDt), speed on elevator (SPDe), go-around mode (GA), retard mode (RETD), limited thrust (LIM), Override (OVRD). * **TO mode:** armed on ground by pressing the AT button on the guidance panel. Engages when thrust levers are at a high TLA. * **HOLD mode:** prevents undesired thrust lever movement during the takeoff phase. Engaged at or above 60 KIAS during the takeoff roll. * **SPDt:** Controls the selected airspeed adjusting the engine thrust by moving the thrust levers. * Vertical modes related to SPDt: FPA, VS, GS, PTH, GP, ALT, ASEL * SPDt is the active mode when the FD is turned OFF (no active modes on FMA). * **SPDe:** At maintains a fixed thrust setting, and the flight director adjusts the pitch attitude to maintain the selected airspeed. * Vertical modes related to SPDe: FLCH, OVSP, VNAV flight level change (FLCH magenta) * GA: advances the thrust levers to the TO/GA position. * **RETD:** reduces the thrust levers to idle during flare on landing. Engages below 30 ft. * LIM: Autothrottle authority is not sufficient to achieve or maintain the selected airspeed. * OVRD: AT can be overridden by moving the thrust lever in any direction without causing its disengagement. * TLA NOT TOGA will be displayed on EICAS if the thrust levers are not in the TOGA detend by 60 kts. {% hint style="info" %} **Autothrottle Disconnect** The autothrottle will be disconnected automatically if you move the throttles and the airspeed is higher than 60 kts. {% endhint %} ### THRUST LEVER DETENTS * **MAX:** provides the maximum thrust rating available for dual or single engine operation. * TO/GA: selects takeoff, maximum continuous, and go-around mode settings. * IDLE: Selects idle thrust settings. * MIN REV: provides minimum reverse thrust. * MAX REV: provides maximum reverse thrust. ### THRUST REVERSER TRIGGER * Pulling the thrust reverser trigger allows reverser activation when weight on wheels. {% hint style="info" %} Pulling the triggers is not simulated because that would interfer with physical throttle devices. However weight on wheels check is included. You can't activate reverser if the aircraft is in the air. {% endhint %} # Ram Air Turbine (RAT) ### RAM AIR TURBINE (RAT) * Handle manually deploys the Ram Air Turbine. * Deploys automatically whenever AC power sources are not powering the AC buses. * 8 seconds after deployment the RAT supplies power. Batteries power during the 8 seconds. * Requires maintenance to stow the RAT. * RAT power the AC Motor-driven Pump (ACMP 3A) for primary flight control tasks. * RAT provides a lower power output than the APU and IDGs. # GND PROX FLAP OVRD and SLAT/FLAP LEVER  ### GND PROX FLAP OVRD BUTTON * Inhibits triggering flap alerts in case of landings where flap configuration is different from normal landing flap configuration.  ### SLAT/FLAP SELECTOR LEVER * Selects slat/flap position by unlatching the lever and lifting a trigger below the head. ### SLAT/FLAP SYSTEM * Position 4 and 5 are the same slat/flap degrees. Position 4 logic is for takeoff while position 5 logic is for landing. Position 4 logic does not provide for the landing gear aural warning on landing. * Caution: Using position 4 for landing is prohibited. * Flap settings approved for takeoff are: 1, 2, and 4. * Flap settings approved for landing are: 5 and FULL. * Go-Around: * Flaps 5 select flaps 2 * Flaps FULL select flaps 4. # AUDIO CONTROL ### MICROPHONE SELECTOR BUTTONS * Related communication channel is enabled for transmission and reception. *** ### AUDIO CONTROL BUTTONS * Related audio channel is enabled for reception. * Automatically activated when a transmission channel is selected. *** ### SATCOM CONTROL BUTTON * Unavailable *** ### PASSENGER ADDRESS CONTROL BUTTON * Enables PA announcements. It deactivates the microphone selector button and in this case no radio transmission occurs since there is no VHF/HF/SATCOM microphone selection. *** ### SERVICES INTERPHONE CONTROL BUTTON * **EMER:** Enables communication with flight attendants during emergency situations. When selected a green bar flashes on the button. Once the flight attendant picks up the call the green bar flashes faster. Pressing the button again, the light becomes steady and the communication with the flight attendant is enabled. A triple HI/LO chime sounds. * **RAMP:** Enables communication with ground personnel. For an incoming call, the ramp annunciator flashes and remains steady when active. Communication through the ramp interphone remains active unless PTT or PA PTT is activated, ramp resumes when PTT or PA PTT is released. {% hint style="info" %} If you click on the RAMP button the MSFS ATC window will open so you can call ground services. {% endhint %} * **CAB:** Enables communication with flight attendants during normal situations. Works the same as EMER mode. Communication through the cabin interphone remains active unless PTT or PA PTT is activated, cabin resumes when PTT or PA PTT is released. * RAMP and CAB can be selected at the same time. *** ### MASTER VOLUME CONTROL KNOBS * Allows adjustment of the most recently selected audio.
# Cockpit Side ### OXYGEN MASK #### FLOW INDICATOR * A bright yellow star when visible indicates that oxygen is flowing. *** #### TEST/RESET BUTTON (SPRING LOADED) * Pressing this button with the mask stowed tests the oxygen mask and activates the microphone. The flow indicator star momentarily blinks and oxygen flow will be audible through audio system. * Pressing this button with the mask not stowed and the mask box door closed shuts off the oxygen flow, turns off mask’s microphone and returns the communication from the cockpit speakers to the headsets. *** #### OXY ON FLAG * This flag appears whenever oxygen is supplied to the mask.
Button to arm/disarm the steep approach mode.