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A reads text to speech;
411 Cards in this Set
- Front
- Back
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#1 and #2 Engine Fire EXTG Handle with fire
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Illuminates when fire is detected.
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#1 and #2 Engine Fire EXTG Handle: PULL
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Closes the associated engine bleed air, fuel,and hydraulic shutoff valves. The under speed logic will eventually open the generator line contactor as the engine decelerates.
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#1 and #2 Engine Fire EXTG Handle: ROTATE
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Discharges the associated fire extinguisher bottle into the associated engine.
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#1 and #2 WINDSHIELD WIPER Controls HI
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Windshield wipers operate at high speed.
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#1 and #2 WINDSHIELD WIPER Controls LOW
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Windshield wipers operate at low speed.
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#1 and #2 WINDSHIELD WIPER Controls OFF
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Stops wind shield wipers in the stowed position.
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#1 and #2 WINDSHIELD WIPER Controls TIMER
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Provides eight-second intermittent operation.
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A valid Fire Dectection AURAL WARNING
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FIRE BELL/TRIPLE CHIME
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A valid Fire Dectection EICAS
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ENG 1 FIRE ENG 2 FIRE APU FIRE CARGO FWD SMOKE CARGO AFT SMOKE
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A valid Fire Dectection GLARESHIELD PANEL/EICAS
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Master Warning Lights illuminated FIRE icon on engine 1 and 2 ITT gauges
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A valid Fire Dectection Overhead Panel
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Engine 1 and 2 fire EXTG handles illuminate FWD and AFT CARGO SMOKE pushbuttons illuminate APU fire extinguisher pushbutton illuminates Red bar in APU EMER STOP pushbutton illuminates
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AC BUS TIE source priority
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APU, GPU, the IDG
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AC BUS TIES Selector Knob: 1 OPEN
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Opens the Bus Tie Contactor (BTC) 1, segregating AC BUS 1 from the AC BUS TIE
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AC BUS TIES Selector Knob: 2 OPEN
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Opens the Bus Tie Contactor (BTC) 2, segregating AC BUS 2 from the AC BUS TIE
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AC BUS TIES Selector Knob: AUTO
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This position allows automatic operation of the BTCs according to system logic
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AC PUMP 1 and 2: AUTO
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Allows automatic operation of the the associated AC PUMP ATSL
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AC PUMP 1 and 2: OFF
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Deactivates the associated AC PUMP
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AC PUMP 1 and 2: ON
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Activates the associated AC PUMP
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AC PUMP System Logic
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AC PUMP will activate automatically when the fuel pressure is demanded and ejector output is insufficient and for XFEED ops. With AC power on the ground, AC PUMP 2 will run for APU Start and to feed the APU
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ADS Button
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Momentary action pushbutton. Manually reverts the ADS source. When ADS source reversion is selected, a white striped bar illuminates in the button.
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AILERON DISCONNECT Handle PULL
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Disconnects the aileron control system. The Captain will control his/her on-side aileron, MFS panel 5L/R with artificial feel. The First Officer will control his/her on-side aileron, MFS panel 4L/R with no artificial feel. MFS panel 3L/ R is locked out for both pilots. The system cannot be reset in flight. Disconnection can be confirmed by a cyan AILERON DISC EICAS message.
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Allowable takeoff positions
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1, 2, 3, or 4.
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Alphanumeric Buttons
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Enter alphanumeric inputs. Space key (SP) is used to insert a space. A toggle plus/minus key inserts the corresponding symbol.
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ALRT RST Button
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Cancels a fault indication.
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ALT Button
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Activates or deactivates the altitude hold function.
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ALT SEL Knob
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Selects the desired altitude in 100' increments.
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ALT SEL Knob Clockwise rotation
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Increases the altitude target.
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ALT SEL Knob Counter clockwise rotation
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Decreases the altitude target.
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Alternate Gear Extension Lever (Two Position)
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When pulled releases all hydraulic fluid from the landing gear lines and releases all landing gear uplocks.
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Alternate Gear Extension Lever Unlock Pushbutton
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When pressed releases the handle from the fully actuated position.
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Amber LED next to DISC position on IDG Knob
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Indicates which IDG to disconnect. Will illuminate in association with the IDG1(2) OIL caution EICAS, and will extinguish after the IDG is disconnected
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An engine bleed leak
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Will cause the illumination of an amber striped bar in the upper half of the associated engine bleed button.
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ANNUNCIATORS TEST Button
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The striped bars and caption indications in all main panel, overhead panel, and control pediestal pushbuttons illuminate when pressed, allowing verification of lamp integrity. The EMRG/PRKG BRAKE light, Master Warning and Master Caution, and GPU pushbutton light and fire test light are not illuminated.
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AP Button
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Commands autopilot engagement or disengagement.
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AP/TRIM DISCONNECT BUTTON (Momentary Action)
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Primary means to disengage the autopilot and cancel the autopilot disconnect alert. Disables both HS-ACE channels as long as the button remains pressed.
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APP Button
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Activates or deactivates the approach mode of the AFCS to intercept an ILS or BC. For an ILS, the Autopilot Approach
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APU (Guarded)
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Momentary action pushbutton. Closes the APU fuel shutoff valve and discharges the APU fire extinguisher bottle. The light will illuminate when the APU EMER STOP button has been pushed in when an APU fire has been detected, or 60 seconds after an APU fire has been detected and no pilot action has occurred. If no fire is detected, one push will arm and discharge the fire bottle.
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APU BLEED Button PUSH IN
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Allows the AMS to automatically configure the position of the APU bleed valve.
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APU BLEED Button PUSH OUT
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Manually closes the APU bleed valve.
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APU bleed leak
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An APU bleed leak will cause the illumination of
an amber striped bar in the upper half of the APU BLEED button. |
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APU GEN Button: IN
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The position allows the APU generator to connect to the AC BUS TIE, automatically according to the source priority
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APU GEN Button: OUT
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Opens the APU generator contactor and isolates the APU generator from the AC BUS TIE. The APU generator is tripped off line and de-excited.
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APU Shutdown Process
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The process involves a one minute cool down. During the cool down APU pneumatics are removed as soon as the MASTER rotary knob is positioned to OFF. If the APU generator is the only source of AC power during the cool down, then APU electrical power will still be available during the one minute cool down period. If there is any other source of AC power on the aircraft when the MASTER rotary knob is moved to OFF, then APU electrical power is removed right away. During any portion of the one minute cool down, the MASTER rotary knob can be moved from OFF back to ON and the APU will continue running.
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AT Button (GROUND)
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Arms the autothrottle system.
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AT BUTTON (IN FLIGHT)
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Engages or disengages the autothrottle system.
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AT DISC Buttons
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Disconnects the autothrottles and cancels the autothrottle aural alert.
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ATTND CALL Button
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Pressing the button sounds a chime in the passenger cabin and illuminates a green light on the FA rainbows
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AUD Button (13X)
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Related channel is available for reception. When selected a green light will illuminate in the button. Multiple channels may be selected for reception. When an AUD channel is selected the LCD will display the selected channel to allow volume adjustment. After 10 seconds the LCD display will revert to the selected MIC channel. To deselect an AUD channel press the associated AUD twice in succession.
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AUTOBRAKE APPLICATION LOGIC LANDING MODE
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Condition-ARMED, Selector Knob Position-LO, MED or HI, WOW Indication-On the ground, Wheel Speed-Above 60 knots, Brake Control System-No faults, Brake Pedal Position-Not pressed, Thrust Levers Position-Idle or below
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AUTOBRAKE APPLICATION LOGIC REJECTED TAKEOFF MODE
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Condition-ARMED, Selector Knob Position-RTO, WOW Indication-On the ground, Wheel Speed-Above 60 knots, Brake Control System-No faults, Brake Pedal Position-Not pressed, Thrust Levers Position-Idle or below
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AUTOBRAKE ARMING LOGIC LANDING MODE
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Selector Knob Position-LO, MED or HI, WOW Indication-In flight, Wheel Speed-Below 60 knots, Brake Control System-No faults, Brake Pedal Position-Not pressed, Thrust Levers Position-Any
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AUTOBRAKE ARMING LOGIC REJECTED TAKEOFF MODE
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Selector Knob Position-RTO, WOW Indication-On the ground, Wheel Speed-Below 60 knots, Brake Control System-No faults, Brake Pedal Position-Any, Thrust Levers Position-Idle or below
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AUTOBRAKE DISARMING LOGIC LANDING MODE
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Selector Knob Position-OFF or RTO, WOW Indication-NA, Brake Control System-Faults detected, Brake Pedal Position-Pressed, Thrust Levers Position-Above Idle while Autobrake is being applied
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AUTOBRAKE DISARMING LOGIC REJECTED TAKEOFF MODE
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Selector Knob Position-OFF, LO, MED or HI, WOW Indication-In flight, Brake Control System-Faults detected below 60 knots of Wheel Speed, Brake Pedal Position-Pressed while Autobrake is being applied, Thrust Levers Position-Above Idle while Autobrake is being applied
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AUTOBRAKE Selector Knob HI
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Selects the high deceleration rate.
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AUTOBRAKE Selector Knob LO
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Selects the low deceleration rate.
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AUTOBRAKE Selector Knob MED
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Selects the medium deceleration rate
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AUTOBRAKE Selector Knob OFF
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Autobrake is deactivated.
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AUTOBRAKE Selector Knob RTO
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Selects RTO deceleration rate.
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Autopilot
Minimum engagement height on go-around |
400 ft AGL
Applies to manually-flown go-around |
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Autopilot
Minimum engagement height on takeoff |
Acceleration altitude
Use of the auto pilot in TO mode is prohibited |
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Autopilot
Minimum use height - non precesion approach |
MDA
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Autopilot
Minimum use height - precesion approach |
50 ft below DH(A)
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Autopilot
Minimum use height - visual approach |
500 ft AGL
Applies to all visual approaches with no instrument backup |
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Autopilot disconnect warning
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Multiple pushes of the AP button will not cancel the autopilot disconnect warning. The autopilot disconnect warning can only be cancelled by pushing the yoke AP/TRIM DISC button.
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BANK Button
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Selects or deselects the bank limiting function of the AFCS. A white arc will appear on the bank indicator of the PFD when bank limiting is engaged. Bank limiting is available in HDG mode only.
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BARO Knob
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Allows manual setting of the altimeter.
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BARO SET Knob (INNER)
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Sets barometric altimeter correction. Pushing this control knob sets barometric correction to standard.
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BARO SET Knob (OUTER) HPa
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Sets the altitude in hectopascals.
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BARO SET Knob (OUTER) IN
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Sets the altimeter in inches of mercury.
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BATT 1 Selector Knob: OFF
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The battery supplies power to HOT BATT BUS 1 only
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BATT 1 Selector Knob: ON
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The battery is connected to the DC ESS BUS 1
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BATT 2 Selector Knob: AUTO
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This position connects BATT 2 to either the DC ESS BUS 2 or the APU START BUS automatically, ATSL
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BATT 2 Selector Knob: OFF
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The battery supplies power to HOT BATT BUS 2 only
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BKUP VOL Switch NORM (PUSH IN)
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Normal operation mode.
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BKUP VOL Switch NORM BKUP (PUSH OUT)
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Selected when the ACP fails or both digital audio busses fail. The CAPT will be connected to COMM1 only and the FO will be connected to COMM2 only.
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BLEED 1 and BLEED 2 Buttons PUSH IN
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Allows the AMS to automatically configure the position of the associated engine bleed valve.
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BLEED 1 and BLEED 2 Buttons PUSH OUT
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Manually closes the associated engine bleed valve.
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BRG Buttons CIRCLE
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Displays #1 RMI bearing pointer information on the PFD. The display can be toggled to view VOR 1, FMS 1, or OFF.
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BRG Buttons DIAMOND
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Displays #2 RMI bearing pointer information on the PFD. The display can be toggled to view VOR 2, FMS 2, or OFF.
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Brightness Adjustment Buttons
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Adjusts brightness.
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Brightness Cell
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Automatically adjusts the instrument brightness according to the ambient lighting.
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BRT/DIM Switch
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Controls display brightness.
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CAB ALT Selector Knob
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Rotary knob is only active when the pressurization MODE knob is selected to MAN.
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CAB ALT Selector Knob DOWN
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Manually closes the OFV.
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CAB ALT Selector Knob STOP (Spring Loaded)
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Normal operation position.
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CAB ALT Selector Knob UP
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Manually opens the OFV.
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Cabin Altitube HI
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Oxygen Masks...........................ON, 100%
Crew Communications..............Establish |
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CABIN IFE Button (GUARDED)
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Controls the power supply to the LiveTV system and the XM Satellite Digital Radio. A striped bar illuminates in the button when selected off.
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CABN Button
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Enables cabin crew interphone communications via the hotmic.
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CABN Button CABIN TO COCKPIT
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When the In-flight crewmember presses the PILOT button on the flight attendant panel a single chime will be heard in the cockpit and the CABN button green light will flash quickly. When the pilot presses the CABN button the green light will illuminate steady green.
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CABN Button COCKPIT TO CABIN
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Sounds a single chime in the cabin and illuminates the steady green light on the flight attendant rainbow lights panel. The ACP LCD will read CABN CALL. The green light in the CABN button will flash slowly. When the In-flight crewmember lifts the cabin handset and selects PILOT, a single chime will sound in the cockpit and the green light in the CABN button will flash quickly. Pressing the CABN button again will connect the cockpit and cabin and the green light will illuminate steady.
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CAGE Button
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Resets attitude to zero, eliminating accumulated drift when the button is pressed for more than two seconds. Not operational during the initialization mode and must be used with wings leveled on stabilized flight conditions. When pressed, an amber CAGE flag is displayed on the upper right corner of the IESS.
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Cargo smoke detected IN FLIGHT
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A single button push will discharge the HIGH rate bottle. 60 seconds later the LOW rate bottle will discharge automattically.
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Cargo smoke detected ON GROUND
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A single button push will discharge the HIGH rate bottle. Automatic discharge of the LOW rate bottle is inhibited on the ground. However, a second button push will discharge the LOW rate bottle.
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CARGO SMOKE FWD and AFT Buttons
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Momentary action pushbutton. Illuminates when the high rate bottle is armed.
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Cargo smoke not detected IN FLIGHT
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A single button push will arm the HIGH rate bottle. A second button push will discharge the HIGH rate bottle. 60 seconds later the LOW rate bottle will discharge.
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Cargo smoke not detected ON GROUND
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A single button push will arm the HIGH rate bottle. A second push will discharge the HIGH rate bottle. A third button push will discharge the LOW rate bottle.
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CHR Button
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Starts/stops the chronometer.
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CHRONO
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It has three functions; START-STOP-RESET. The timer appears on the upper right corner of the PFD HSI.
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CKPT Temperature Control Knob
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Controls cockpit temperature according to the knob position.
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Clock/Chronometer Display
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Displays chronometer, time/date and elapsed time. If no GPS signal is detected, the clock will display dashes and only the positions INT and SET on the GPS/INT/SET selector will be available. The chronometer display is blanked in the non-operating mode.
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CLR
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Clears alphanumeric entries or messages in the scratchpad.
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COCKPIT DOOR CONTROL INHIB Pushbutton (MOMENTARY ACTION)
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Pushing this button will lock the door for 500 seconds if emergency access is requested. When pushed a white bar will illuminate in the button. If emergency access is requested and INHIB is not selected within 30 seconds the door will unlock.
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COCKPIT DOOR CONTROL LOCK Pushbutton (GUARDED)
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Locks and unlocks the door. A white bar in the switch illuminates when unlock is selected (push in). Deactivates the inhibition control. Resets the buzzer alarm and EMERG CALL command. Resets the green LED on the flight attendant access panel.
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Cockpit/Cabin Smoke/Fumes
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Oxygen Masks...........................ON, EMER, then 100%
Crew Communications..............Establish |
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CONTROL WHEEL COMMUNICATIONS SWITCH HOT
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Allows INPH communications over the HOT mic.
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CONTROL WHEEL COMMUNICATIONS SWITCH OFF
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Allows only audio reception.
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CONTROL WHEEL COMMUNICATIONS SWITCH PTT (momentary)
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Allows VHF transmissions as well as PA announcements.
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CSS Button (GUARDED)
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Controls power to the Cabin Surveillance System. A striped bar illuminates in the button when selected off.
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CVR ERASE
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Allows CVR data to be erased when the aircraft is on the ground with the parking break set
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DATE/SET Button
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Allows time setting when the GPS/INT/SET selector is in the SET position. Repeated pressing of the SET button causes the selector to cycle between minute, hour, year, month, and day. The desired digits flash and the setting is obtained by rotating the DATE/SET button. Allows the date to be displayed on the associated indicator when the GPS/INT/SET selector is set to GPS or INT.
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DC BSU TIES Toggle Switch: AUTO
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This postion allows automatic operation of the DC TIE contactors (1 DCTC/2ETCs) according to system logic
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DC BUS TIES Toggle Switch: OFF
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Opens all the DC TIE contactors
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DC PUMP System Logic
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DC PUMP will activate for APU start if AC power is not available. The DC PUMP is not a backup for the AC PUMP
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DC PUMP: AUTO
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Allows automatic operation of the DC PUMP ATSL
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DC PUMP: OFF
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Deactivates the DC flue pump
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DC PUMP: ON
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Activates the DC fuel pump
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DEL
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Works together with line select buttons in order to delete waypoints and other items displayed. This button is inhibited when a message is displayed in the scratchpad.
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Design maneuvering speed
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Full application of any single flight control surface in a single direction as well as maneuvers that involve angles of attack near stall, must be confined to speeds below
240 KIAS |
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DISPLAYS Knob AUTO
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Allows automatic reversion of the MFD in case of display failure.
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DISPLAYS Knob EICAS
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Forces the associated MFD to display as an EICAS.
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DISPLAYS Knob MFD
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Forces the associated MFD to display as an MFD.
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DISPLAYS Knob PFD
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Forces the associated MFD to display as a PFD.
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DOME Light Switch
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Turns on/off the two cockpit dome lights. Batteries must be ON/AUTO to have dome lights on.
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Dry Windshield
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Windshield wipers will not operate on a dry windshield.
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DUMP Button (Guarded)
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When pushed in a white striped bar will illuminate in thebutton. With the pressurization mode in MAN or AUTO pushing this button in will turn off both sets of air conditioning packs and recirculation fans. Additionally, in AUTO only, the outflow valve will modulate to raise the cabin to 12400' at 2000' fpm. Once the cabin has been dumped to 12400' natural leak will raise the cabin higher. If a cabin dump has been commenced, it can be cancelled by reselecting the button to its normal (out) position. NOTE: Selecting the DUMP button in while in MAN mode will stil command the PACK's and RECIRC FAN's to shutdown.
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DVDR TEST
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Commands a self test of DVDR 1 and DVDR 2. A failure message is indicated by a CVR AFT (FWD) FAIL advisory message ont he EICAS
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EICAS FULL Button PUSH IN
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Full EICAS information is presented and auto declutter is inhibited. A white striped bar illuminates in the button.
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EICAS FULL Button PUSH OUT
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Enables the automatic EICAS de-clutter logic.
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ELAPSED TIME SELECTOR AUTO
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(Spring loaded neutral) Automatically starts the chronometer on liftoff.
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ELAPSED TIME SELECTOR RST
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Resets the elapsed time if WOW is present.
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Electrical Override Switch GEAR DOWN
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Bypasses the landing gear lever and extends
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Electrical Override Switch NORMAL
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The landing gear lever performs landing gear extension and retraction.
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ELEVATOR DISCONNECT Handle PULL
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Disconnects the elevator control system. Each pilot will control their on-side elevator. The system cannot be reset in flight. Disconnection can be confirmed by a cyan ELEVATOR DISC EICAS message.
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EMER Button
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Interphone communication with the cabin is enabled over the hot-mic.
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EMER Button CABIN TO COCKPIT
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When the In-flight crewmember presses the EMER call button from the flight attendant panel, a triple HI/LO chime is sounded in the cockpit. The green light in the EMER button will be flashing quickly. When the pilot pushes the EMER button the green light will be solid green indicating that a connection has been made.
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EMER Button COCKPIT TO CABIN
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Initiates a triple HI/LO chime in the cabin and illuminates the flashing red light on the flight attendant rainbow lights panel. EMER CALL will be seen in the LCD on the ACP. When pushed the green light inside the button flashes slowly. When the In-flight Crewmember picks up the cabin handset and selects EMER PILOT the green light will flash quickly and a single chime will be heard in the cockpit. The cockpit crew must push the EMER button again to establish communication. The light in the EMER button will now be solid green. When the In-flight crewmember hangs up the handset the connection will be broken.
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EMER LT Selector Knob: ARMED
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Automatically illuminates all emergency lights if DC BUS 1 loses power or if the airplane electrical power is turned off
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EMER LT Selector Knob: OFF
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Disables automatic operation of the emergency lights, The lights can still be turned on from the FWD or AFT ATTENDANT panel
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EMER LT Selector Knob: ON
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Turns on all emergency lights regarless of the postion of the EMERGENCY LIGHT switch on the FWD and AFT ATTENDANT panel
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EMER STOP Button In case of fire
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The upper half of the button illuminates red. When pushed in, a white striped bar illuminates on the lower half of the button.
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EMER STOP Button PUSH IN
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Closes the APU fuel shutoff valve, shutting down the APU without a one minute cool down. Selection of this button will illuminate a white stripe in the lower half of the APU EMER STOP button.
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EMER STOP Button PUSH OUT
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Normal position, with the fuel shut off valve open.
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EMERG/PRKGBRAKE Light
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The word "ON" illuminates when the EMERG/PRKGBRAKE is actuated. Illumination of the light indicates that sufficient hydraulic pressure is available to maintain brake pressure.
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EMERG/PRKNG BRAKE Handle
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Actuates the emergency/parking brake. The handle will lock when pulled up to the fully actuated position. To release the handle from the fully actuated position, the button must be pressed.
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Engaging the autopilot when no FD mode is active
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Causes FPA mode to become the active vertical mode, and the FD guidance cue to come into view.
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Engine and wing anti-ice system
On the Ground |
The MCDU T/O DATASET MENU must be set to REF A/I ALL when the OAT is 10 degrees C or less and:
1. Icing conditions exist, or 2. The ceiling is less than 1,700 feet |
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ENGINE ICE PROTECTION Button Ground
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Engine anti-ice is selected ON from the MCDU, TRS INDEX, TO DATA SET MENU, REF A/I LSK.
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ENGINE ICE PROTECTION Button In-Flight
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Operation is automatic through the AMS.
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ENGINE ICE PROTECTION Button PUSH IN
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Allows automatic operation of the associated engine anti-ice system.
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ENGINE ICE PROTECTION Button PUSH OUT
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Deactivates the associated engine anti-ice system.
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Engine shutdown
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Following high thrust operation such as maximum reverse thrust during landing, the engine will be operated at or near idle for two (2) minutes before shutdown to thermally stabilize the engines hot section. Taxi time at or near idle can be included in this period.
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Engine warm-up
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After the engine has been started, operate at or near idle for at least two (2) minutes before selecting high thrust. Taxi time at or near idle can be included in the warm-up period
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Enter Keys
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Used to select soft keys or menu options.
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FAULT Button
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Illuminates when senses no paper or printer door open. Illuminates in conjunction with test button in case of self-test failure.
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FD Button
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Removes the FD cue from the associated PFD when the AP is not engaged, but does not turn off the FD system. If theAP is engaged the FD cue cannot be removed from the PFD that is on the same side as the AFCS source.
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Fire Detection System TEST Button
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Momentary action button. Tests the engine and APU fire detection systems, and the forward and aft cargo compartment smoke detection systems. Prior to performing a FIRE TEST confirm that there are no FIRE DET FAIL, FIREX FAIL, FIREX ARM, or BTL DISCH messages on the EICAS.
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Flap Override Switch (GUARDED)
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Inhibits triggering of flap alerts in case of landings where flap configuration is other than 5 or FULL.
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Flap position 1
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230 KIAS
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Flap position 2
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215 KIAS
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Flap position 3
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200 KIAS
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Flap position 4
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180 KIAS
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Flap position 5
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180 KIAS
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Flap position full
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165 KIAS
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FLCH Button
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FLCH will initiate a climb or descent based on the current aircraft altitude vs. the altitude selected.
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FLCH Button For altitude changes less than 2000'
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The thrust levers will modulate somewhere between TOGA and IDLE. The TRS mode for all climbs and descents will be CLB. In FLCH pitch is commanded to maintain airspeed.
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FLCH Button If the AT system is engaged
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A climb will be made with the thrust levers at TOGA and descents will be made with the thrust levers at IDLE.
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FLIGHT CONTROLS MODE Buttons (GUARDED) PUSH IN
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Selects DIRECT MODE for the associated flight control. A white bar will illuminate in the push button. NOTE: In DIRECT Mode high level functions are lost.
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FLIGHT CONTROLS MODE Buttons (GUARDED) PUSH OUT
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Returns the associated flight control to NORMAL MODE.
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FMS Button
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Selects FMS as the navigation source, and displays a magenta needle on the PFD HSI. The FMS source can be toggled between on side and cross side navigation information.
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Format location buttons
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Places the cursor on the associated display.
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FPA Button
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Activates or deactivates the Flight Path Angle mode. This is the basic vertical mode.
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FPA SEL Knob
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Manually selects the desired Flight Path Angle if FPA is the active vertical mode. If FPA is not the active mode and FPR is selected on the Display Control Panel, this knob adjusts the position of the flight path reference line.
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FPR Button
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Selects or deselects the display of a cyan flight path reference line on the PFD. The FPA SEL knob can be rotated to change the value of this line +/- 9.9 degrees.
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FSTN BELTS Toggle Switch: OFF
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Turns off the FASTEN BELTS signs. Sounds a single high-low chime
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FSTN BELTS Toggle Switch: ON
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Illuminates the FASTEN BELTS signs. Sound a single high-low chime
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Fuel Crossfeed operations
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The XFEED Selector must be set to OFF during takeoff and landing
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Function Keys CB
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Displays the circuit breaker page.
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Function Keys DLK
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ACARS functions.
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Function Keys FPL
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Displays the flight plan page.
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Function Keys MENU
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Displays the menu page.
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Function Keys NAV
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Displays the navigation page.
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Function Keys PERF
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Displays the performance page.
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Function Keys PROG
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Displays the progress page.
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Function Keys RADIO
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Displays the radio page.
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Function Keys RTE
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Display the route page.
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Function Keys TRS
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Thrust rating select
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GND PROX G/S INHIB Button
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Momentary pushbutton annunciator used to manually cancel glideslope alerts. Illuminates when pressed any time below 2000 ft RADAR altitude and will automatically reset (light off) by climbing above 2000 ft RADAR altitude or descending below 30 ft. RADAR altitude.
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GND PROX TERR INHIB Pushbutton
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When pressed, inhibits EGPWS and thus avoids unwanted terrain alerts in airports not covered by EGPWS database.
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GPS/INT/SET Selector GPS
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Synchronizes with UTC and DATE from GPS.
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GPS/INT/SET Selector INT
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Displays information from the internal clock.
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GPS/INT/SET Selector SET
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Sets the clock modes.
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GPU AVAIL Light
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Illuminates when the button is pushed in or out when the AC GPU is connected, but not powering the AC BUS TIE.
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GPU Button: IN
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Connects the AC GPU to the AC BUS TIE, according to source priority
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GPU Button: OUT
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Isolates the AC GPU from the AC BUS TIE
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GPU IN USE Light
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Illuminates when the button is pressed in and the AC GPU is powering the AC BUS TIE
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HDG Button
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Selects or deselects HDG as the lateral navigation mode.
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HDG SEL Knob
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Manually selects the desired heading. Pressing the center of the knob will center the heading bug to the current heading.
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HDPH Button
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Allows audio to be heard over the headphone. When selected the green light illuminates.
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HEADPHONE Jack
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Allows a headset to be inserted to monitor the composite audio output of the DVDR unit during test and normal operations
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HEATER Button PUSH IN
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Activates the ADS probes heater. A white striped bar illuminates.
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HEATER BUTTON PUSH OUT
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The ADS probes heater works in AUTO mode.
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HSI Button
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Toggles the HSI view on the PFD between full compass rose, arc and arc with map.
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Hydraulics, Brakes and Landing Gear
Temperature Limitation |
Do not takeoff with brake temperature indicators in the amber range
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ICE PROTECTION MODE Selector Knob AUTO
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Allows automatic operation of the wing and engine anti-ice systems.
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ICE PROTECTION MODE Selector Knob ON
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Overrides the system logic inflight, activating the anti-ice system regardless of icing condition.
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ICE PROTECTION TEST Knob ENG
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Provides a test for the engine anti-ice system.
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ICE PROTECTION TEST Knob OFF
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Spring-loaded position.
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ICE PROTECTION TEST Knob WING
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Provides a test for the wing anti-ice system.
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ID Button
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Activates a filter that eliminates voice on VOR and ADF audio so the identification can be heard.
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IDG 1 and IDG 2 Selector Knob: AUTO
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This position allows the IDG contactor to close connecting the IDG to the respective AC BUS automatically, according to system logic
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IDG 1 and IDG 2 Selector Knob: DISC
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Must be held in this position for one second to manually disconnect the IDG. The IDG cannot be reconnected in flight.
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IDG 1 and IDG 2 Selector Knob: OFF
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Opens the IDG contactor isolating the IDG from the respective AC BUS
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If ALT was the active vertical mode
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The altitude to be held synchronizes to the altitude existing at the moment of button release, but the selected altitude readout does not change.
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If both the windshield wiper knobs are selected to LOW/HI
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They will sync to the Captains (#1) controller.
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If FLCH or GS was the active vertical mode
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control returns to that mode.
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If VS or FPA were the active vertical modes
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The selected VS or FPA synchronizes to the VS or FPA existing at the moment of button release.
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IFE RACK Button (GUARDED)
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Controls power to the LiveTV System, the CSS, XM Satellite Radio system, and Wireless Aircraft Data Link (WADL). Controls power to the PA buffer, rack fan, and flow switch. Power to smoke detection and ventilation systems is not turned off by pressing this switch. A striped bar illuminates in the button when selected off.
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IGNITION Selector Knob AUTO
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FADEC automatically controls the ignition system, depending on engine requirements.
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IGNITION Selector Knob OFF
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Deactivates the ignition system on the ground. When dry motoring on the ground there is no fuel flow. The FADEC disregards the OFF position in flight.
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IGNITION Selector Knob OVRD
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Directs FADEC to continuously activate both igniters.
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ILS Button
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Selects or deselects the display of ILS 1 LOC and GS deviation indications on the IESS. ILS 1 will be annunciated in the upper left corner of the IESS. In case of a failure, a red cross replaces the annunciation.
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Inadvertant press of cargo smoke bottom with no smoke
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NOTE: In flight or on ground, with no smoke detected, if either cargo smoke fire extinguisher button is pushed inadvertently, push the test button to cancel or wait two minutes for the system to reset automatically.
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Inboard button
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is the EICAS.
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INPH Button
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Enables interphone audio. When selected the green light illuminates.
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IRS Button
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Momentary action pushbutton. Reverts the IRS source. When IRS source reversion is selected, a white striped bar illuminates in the button.
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Items decluttered from EICAS
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Oil pressure. Oil temperature. Engine vibration. Slat position. Flap position. Speed brake position. Landing gear position (if AUTOBRAKES are OFF) Pitch trim green band.
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Jammed Control Column - Pitch
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ELEVATOR DISCONNECT Handle...................PULL
Working Pitch Control.........................................Identify and Assign PF |
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Jammed Control Wheel - Roll
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AILERON DISCONNECT Handle...................PULL
Working Roll Control........................................Identify and Assign PF |
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Landing mode WOW
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The WOW must indicate the airplane is on the ground for more than 2 seconds to allow autobrake application.
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LFE Knob DOWN
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Decreases the LFE in 100' increments. If held longer than 5 seconds the LFE will decrease in 500' increments.
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LFE Knob Manual input of the LFE
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Only possible when the pressurization MODE knob is selected to LFE.
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LFE Knob STOP (Spring Loaded)
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Normal operation position.
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LFE Knob UP
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Raises the LFE in 100' increments. If held longer than 5 seconds the LFE will increase in 500' increments.
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LG WRN INHIB Button
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Pressing the button will inhibit the landing gear warning in the event of a dual radio altimeter failure. When pressed a white striped bar will illuminate inside the button. The light will extinguish allowing a new warning when the thrust levers are advanced. NOTE: If FLAP 5 or FULL is selected with the gear up the warning cannot be cancelled.
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Line Select Keys (LSK)
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Data is selected to a line from the scratchpad or vice-versa. On the radio pages only, if a single white triangle is displayed, a sub-menu will be available to view when the LSK is pushed twice. The first push will bring the cursor box to the LSK selected, and the second push will open the submenu.
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Liquid Crystal Display (LCD)
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Displays the selected audio channel and digital volume information.
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LOW PPR Button
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Illuminates when the printer senses the last remaining 10 feet of paper on the paper supply roll
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MAIN PNL Knob
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Turns on/off and sets the lighting brightness of the Guidance Panel and Instrument panel background lighting
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Mask Deployment
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Fasten Seat Belts and No Smoking signs will automatically illuminate when masks are commanded to deploy
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MASKS DEPLOY Knob AUTO
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Enables automatic deployment of passenger oxygen masks when cabin pressure altitude is above 14000 ft.
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MASKS DEPLOY Knob OFF
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Disables automatic deployment of passenger oxygen masks.
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MASKS DEPLOY Knob OVRD
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Deploys the passenger oxygen masks regardless of cabin altitude.
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MASKS DEPLOYED Indicator
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An ON light illuminates, indicating that the passenger and flight attendant oxygen masks have been commanded to deploy.
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MASTER Knob OFF
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Normal position when the APU is not running.
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MASTER Knob ON
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Normal position when the APU is running. APU FADEC faults that command automatic shutdown of the APU will command shutdown in 10 seconds after the fault is detected.
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Max 90 crosswind component (including gusts) for Cat II approaches or takeoffs and landings from contaminated runways.
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15 kts
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Max 90 degree crosswind component, takeoff and landin
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28 kts sustained with gusts up to 35 kts
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Max takeoff and landing tailwind component
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10 kts
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Maximum airspeed for windshield wiper operation
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250 KIAS
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Maximum gear extended speed (Vle)
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265 KIAS
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Maximum gear extension speed (Vlo Extension)
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265 KIAS
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Maximum gear retraction speed (Vlo Rectaction)
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235 KIAS
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Maximum landing weight (MLW)
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97,000 lbs
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Maximum takeoff weight (MTOW)
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114,200 lbs
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Maximum taxi and ramp weight
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114,550 lbs
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MIC Button (6X)
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Related channel is available for transmission and reception. A green light will illuminate in the associated MIC and AUD button. Only one MIC button may be selected at a time. To deselect a MIC channel either select a new channel, or press the lighted MIC button twice in succession.
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MIC/MASK Switch AUTO (PUSHED IN)
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Automatically turns on the mask microphone when the oxygen mask is removed from its cabinet, or is tested.
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MIC/MASK Switch MASK (PUSHED OUT)
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Turns on the oxygen mask microphone. This function is used if the AUTO mode does not work. Oxygen mask stowage box doors must be closed and the TEST/RESET button selected in order to enable the hand mic or headset boom microphone after using the oxygen mask.
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Middle button
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is the MFD.
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Min Knob BARO
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Allows for auto call outs based on the barometric altimeter. This position is used for all CAT I ILS and nonprecission approaches.
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MINIMUMS Knob (INNER)
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Adjusts up or down the selected approach minimums. The value will be displayed on the PFD.Rotation counterclockwise beyond 0 will turn the display and auto callouts OFF.
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MINIMUMS Knob (OUTER)
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Sets the approach minimums for all nonprecision and precision approaches.
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Mins Knob RA
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Allows for auto callouts based on the RADAR altimeter. This position is used only for CAT II and CAT III ILS approaches.
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Multifunction Control Display Unit (MCDU) General
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The MCDU allows FMS control, radio tuning, PFD radio tuning display setup, manual engine rating selection, engine takeoff data set and avionics display setup and test.
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NAV Button
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Selects or deselects VOR/LOC or LNAV as the lateral navigation mode.
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NEXT
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Selects the next page.
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NO SMKG Toggle Switch: OFF
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Turns off the NO SMOKING signs. Sounds a single high-low chime
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NO SMKG Toggle Switch: ON
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Illuminates the NO SMOKING signs. Sounds a single high-low chime
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Normal AC BUS source priority
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on-side IDG, AC BUS TIE, off-side IDG
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Normal landing positions
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5 or FULL.
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Normal Start Sequence Display/Observe at 7% N2
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IGN A or B - Displayed
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Normal Start Sequence Display/Observe at light-of (within 5 seconds after fuel flow)
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ITT - Increasing
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Normal Start Sequence Display/Observe at start
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N2 - Increasing
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Normal Start Sequence Display/Observe at ≈ 20% N2 and ITT LEss than 120˚ C
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n1 - Increasing and Fuel Flow - Increasing
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Normal Start Sequence Display/Observe at ≈ 50% N2
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IGN A or B - Extinguishes and Oil Pressure - Positive Indication
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Nosewheel Steering Runaway
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STEER DISC Switch............................PRESS
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Notes on ADS
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NOTE 1: ADS source flag is displayed on the PFD. NOTE 2: Reversion to ADS 3 is automatic. NOTE 3: Reversions that will place both pilots on the same ADS source must be done manually.
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Notes on IRS
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NOTE 1: IRS source flag is displayed on the PFD. NOTE 2: IRS reversion must be performed manually.
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Notes on Speedbrake lever
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The speedbrake lever does not move for autoretraction, or for ground spoiler deployment. The speedbrake lever is inhibited on the ground.
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Outboard button
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is the PFD
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OVHD PNL Knob
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Turnus on/off and sets the brightness of the overhead panel's background lighting. Rotating to OFF illuminates all annunciator lights to full bright
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PA Button
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The MIC portion allows transmission to the cabin. The AUD portion allows the flight crew to monitor PA transmissions.
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PACK 1 and PACK 2 Buttons PUSH IN
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Allows for automatic operation by the AMS. This position opens the associated pack valve, according to system logic.
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PACK 1 and PACK 2 Buttons PUSH OUT
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Manually closes the associated pack valve.
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PACK 1 and PACK 2 Notes
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Will be automatically commanded OFF when the DUMP button is selected IN, smoke is detected in the recirculation bay, the thrust levers are set to MAX, or during takeoff with REF ECS OFF and APU BLEED unavailable.
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PAX CABIN Temperature Control Knob
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Controls passenger cabin temperature according to the knob position.
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PEDESTAL Knob
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Turns on/off and sets the pedestal lighting brightness
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PITCH BACKUP SW
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Actuates the pitch trim through the back-up channel. Operation of the switch while the autopilot is engaged causes the autopilot to disengage.
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Pitch trim priority
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backup trim, Captain trim, First Officer trim, and the autopilot trim.
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PITCH TRIM SWITCH (SPRING-LOADED TO NEUTRAL)
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Trims the airplane when the autopilot is not engaged. Captain's pitch trim switch actuation has priority over the first officer's.
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Pneumatic bleed source priority
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Is on side bleed, off side bleed, and then APU bleed.
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Positioning the thrust lever between the thrust control quadrant
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detents selects intermediate thrust settings.
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Powerplant starter limits
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First Start
90 seconds ON (ground) 10 seconds OFF 120 seconds ON (in flight) 10 seconds OFF |
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PPR ADV Button
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Continuously advances paper while pushbutton is depressed.
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Pressing and holding the TCS button causes
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(If A/P is engaged), disengagement of the A/P servos, allowing manual aircraft maneuvering. Synchronization of the FD guidance cue to the FPV.
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Pressing the center of the ALT SEL knob
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Will activate or deactivate the metric presentation of current altitude and preselected altitude on the PFD. This selection does not remove the display of current altitude and preselected altitude in feet from the PFD.
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Pressurization MODE Selector Knob AUTO
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Allows automatic operation of the pressurization system.
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Pressurization MODE Selector Knob LFE CTRL
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Allows manual input of landing field elevation. This function is used when the FMS is inoperative, or when landing at an airport not in the FMS database. Other automatic functions of the pressurization system remain operative.
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Pressurization MODE Selector Knob MAN
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Allows manual control of the outflow valve (OFV).
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PREV
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Selects the previous page.
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PREV Button
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Selects or deselects the display of lateral and vertical deviation information from the tuned VOR/ILS/LOC frequency while FMS is the active navigation source. A blue needle depicts the PREV information. Toggling the PREV button alternates the display of on side or cross side navigation information. For a LOC/BC or ILS, if APPR mode is armed, the previewed navigation source will become the primary navigation source when captured. The PREV needle will not change to amber when cross side information is displayed.
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Printer OFF Button
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Turns the printer off and on.
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PTU SWITCH AUTO
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During takeoff or landing with the flaps not at zero, the PTU will activate with a failure of ENG 2 or the ENG 2 Engine Driven Pump (EDP) to provide normal landing gear extension and retraction.
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PTU Switch OFF
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Turns the PTU off.
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PTU Switch ON
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The PTU operates continuously.
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PUSH IAS-MACH
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Toggles the speed selected on the PFD between IAS and MACH.
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Ram Air Turbine Deployment Handle
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Manually deploys the ram air turbine.
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RAMP Button
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Enables ramp interphone communications over the hot mic.
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RAMP Button COCKPIT TO RAMP
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When RAMP is pushed the green light in the button will flash. When the ramp crewmember engages their headset the green light will be steady illuminated. The ACP LCD will read RAMP CALL.
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RAMP Button RAMP TO COCKPIT
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When a call is initiated from the ramp a single chime will be heard in the cockpit and the RAMP button will flash green. When the cockpit crewmember selects the RAMP button the green light will illuminate steady.
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RECIRC Button PUSH IN
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Allows for automatic operation of the RECIRC fans through the AMS.
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RECIRC Button PUSH OUT
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Turns off both RECIRC fans.
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RECIRC fans
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The RECIRC fans will automatically be commanded off when the DUMP Button is selected IN, smoke is detected in the recirculation bay, or when its associated pack is OFF.
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Release of the TCS button causes
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A/P servos to reengage, if A/P was engaged prior to TCS selection. FD cue to resume movement to guide toward active lateral and vertical modes. FGCS lateral mode: control returns to previously selected lateral mode. FGCS vertical mode
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Reversionary Logic CA
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ADS 1 ADS 3 ADS 2
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Reversionary Logic FO
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ADS 2 ADS 3 ADS 1
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ROLL Trim Switch
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Actuates the roll trim left or right.
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Rotating the knob to the ATTND position
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Allows cabin temperature control via the flight attendant control panel.
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RST Button
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Resets the chronometer to zero if the chronometer is stopped.
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SAT Button
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SATCOM is unavailable.
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Scratchpad
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The working area, located on the bottom line of the display. The pilot can enter data and/or verify data before line selecting the data into its proper position. Data is retained on the scratchpad throughout all mode and page changes. The scratchpad also provides advisory and alerting messages.
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SELCAL Button
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When a SELCAL is received the button will flash green, a single chime will be heard, an EICAS message will post, SELCAL will post in the ACP LCD, and the MIC and AUD button of the called channel will flash green. Holding down the SELCAL pushbutton will display the SELCAL code that has been programmed for the aircraft. The button will illuminate steady green when active for transmission.
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Selector Switch AFT
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Enables the test tone of DVDR 2 to be heard when headset is plugged into the headphone jack
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Selector Switch FWD
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Enables the test tone of DVDR 1 to be heard when headset is plugged into the headphone jack
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SHAKER CUTOUT Button PUSH IN
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Cuts out the associated yoke shaker channel.
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SHAKER CUTOUT Button PUSH OUT
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Allows normal operation of the stick shaker.
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SLAT/FLAP Selector Lever
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Selects slat/flap position. The lever must be unlatched by and lifting the trigger below the head. Intermediate positions are not enabled. Position 4 is gated.
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SPEED Selector Knob (INNER)
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Manually selects the desired airspeed. Manual speeds are displayed in cyan on the PFD.
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SPEED Selector Knob (OUTER) FMS
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The desired speed is controlled by the FMS. Changes can be entered through the MCDU. FMS speed is displayed in magenta on the PFD.
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SPEED Selector Knob (OUTER) MAN
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The desired speed is controlled manually, displayed in cyan on the PFD.
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Speedbrake Lever
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In flight, symmetrically deploys the multi-function spoilers in proportion to the speedbrake lever position. The speedbrakes will automatically retract when the thrust lever angle exceeds 60 degrees, greater than FLAP 1 is selected, or the speed drops below 180 KIAS.
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SPKR Button
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Allows audio to be heard over the speaker. Ensure this button illuminates as a part of the oxygen test. When selected the button illuminates.
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SRC Button
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Selects the Captain or First Officer AFCS side as data source. A green arrowhead on the FMA indicates the selected side.
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Stable Engine Start Parameters
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N1 22% ITT 480˚C N2 63% Fuel Flow 450 lbs/hr Oil Presure greater than 25 psi
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START
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(Momentary action) Initiates the APU start cycle.
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START/STOP Selector Knob RUN
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Normal position for engine operation.
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START/STOP Selector Knob START
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(Momentary action): Initiates the engine startsequence.
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START/STOP Selector Knob STOP
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Commands the FADEC to shut down the engine, provided the associated thrust lever is in the IDLE position.
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Status Annunciator displays the following
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APPR 2: CAT II ILS Capable APPR 1: CAT I ILS Capable APPR 1 ONLY: System logic is requesting CAT II guidance but only CAT I is capable.
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STD Button
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Sets the barometric pressure to standard atmospheric pressure.
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STEERING DISENGAGE Switch (Momentary Action)
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Disengages the nosewheel steering system.
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STERILE Toggle Switch: OFF
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Turns off the amber sterile light on the FA rainbow
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STERILE Toggle Switch: ON
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Illuminates the amber sterile light of the FA rainbow. Sounds a single high-low chime
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Switch type and notes
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The switches on both pilot yokes, the PITCH BACKUP SW trim switch, and the ROLL trim switch are split rocker type switches. If one half of a switch is actuated for more than 5 seconds that particular switch will be deactivated.
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SYS 1 and SYS 2 ELEC PUMP Selector Knobs AUTO In Flight
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SYS 1 and SYS 2 will operate automatically when low pressure is detected, or when flaps are not at zero.
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SYS 1 and SYS 2 ELEC PUMP Selector Knobs AUTO On Ground
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SYS 1 and SYS 2 will run automatically for takeoff when the flaps are not set at zero; and the thrust levers are advanced beyond 60 degrees of TLA, or the ground speed is greater than 50 kts. Additionally, the SYS 2 ELEC PUMP will run automatically for single engine taxi when ENG 1 has been started and the EMERG/PRKG BRAKE Handle has been released.
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SYS 1 and SYS 2 ELEC PUMP Selector Knobs OFF
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Turns the associated electrical pump off.
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SYS 1 and SYS 2 ELEC PUMP Selector Knobs ON
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Operates the electrical pump continuously.
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SYS 1 and SYS 2 ENG PUMP SHUTOFF Buttons PUSH IN
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Closes the hydraulic shutoff valve (SOV), isolating the respective EDP from the associated hydraulic system.
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SYS 1 and SYS 2 ENG PUMP SHUTOFF Buttons PUSH OUT
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Normal position. Hydraulic SOV open.
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SYS 1 CUTOUT Switch (GUARDED) PUSH IN
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Disables pitch trim channel 1.
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SYS 1 CUTOUT Switch (GUARDED) PUSH OUT
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Enables pitch trim channel 1.
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SYS 2 CUTOUT Switch (GUARDED) PUSH IN
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Disables pitch trim channel 2.
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SYS 2 CUTOUT Switch (GUARDED) PUSH OUT
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Enables pitch trim channel 2.
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SYS 3 ELEC PUMP A Selector Knob OFF
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Turns the electrical pump off.
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SYS 3 ELEC PUMP A Selector Knob ON
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Operates the electrical pump continuously.
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SYS 3 ELEC PUMP B Selector Knob AUTO
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In flight only, the pump will turn on when low pressure is detected.
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SYS 3 ELEC PUMP B Selector Knob OFF
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Turns the electrical pump off.
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SYS 3 ELEC PUMP B Selector Knob ON
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Operates SYS 3 B pump continuously.
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T/O CONFIG Button
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Checks the takeoff configuration. The takeoff configuration checks for EMERG/PRKG BRAKE OFF, takeoff flaps set, spoilers retracted, and pitch trim in the green band.
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Takeoff with the Automatic Takeoff Thrust Control System (ATTCS)
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Not authorized in OFF position
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TEST Button
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Continually tests the buzzer while the test button is pressed, regardless of audio selection.
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TEST Button
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Illuminates all indicators followed by a printout of test results and a test pattern. TEST button indicator bar will remain lit in conjunction with the FAULT indicator to report a self test failure.
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The autothrottle disconnect warning
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Can only be cancelled by pushing one of the thrust lever mounted AT DISC buttons.
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The flight path angle limit
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9.9 degrees nose up or nose down.
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The NO SMKG and FSTN BELTS
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Will automatically illuminate when the oxygen masks are commanded to deploy.
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The YD defaults
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ON at system power up. It is also automatically turned ON when the AP is engaged.
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Thrust Levers IDLE
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Selects idle thrust settings.
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Thrust Levers MAX
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Provides the maximum thrust available.
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Thrust Levers MAX REV
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Provides maximum reverse thrust. The thrust lever must be pulled against a spring to achieve the MAX REV position. If the thrust lever is released it goes back to MIN REV position.
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Thrust Levers MIN REV
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Provides minimum reverse thrust.
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Thrust Levers TOGA
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Selects takeoff, go around, and maximum continuous thrust ratings.
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Thrust Reverser Trigger
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Pulling the thrust reverser trigger allows movement of the thrust levers aft of the IDLE stop (on the ground only).
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Tiller
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The handle must be pushed down to engage tiller steering. Turn the aircraft by rotating the handle left or right. With the handle released, nose wheel steering is accomplished through the rudder pedals.
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To prevent trim runaway situations
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All trim actuation is limited to three seconds of movement.
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TOUCH CONTROL STEERING BUTTON (TCS)
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Allows adjustment/synchronization of certain FGCS modes, and manual maneuvering of the aircraft if the autopilot is engaged.
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Touch Pad
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Used to move cursor.
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Trim Runaway
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AP/TRIM DISC Button.................................PRESS and HOLD
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TRU 1 and 2 Toggle Switch: AUTO
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This position allows automatic connection of the TRU to the respective DC BUS
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TRU 1 and 2 Toggle Switch: OFF
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Isolates the TRU from the respective DC BUS
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TRU ESS Toggle Switch: AUTO
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This position allows automatic connection of the TRU ESS to the ESS BUS 3
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TRU ESS Toggle Switch: OFF
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Isolates the TRU ESS form the ESS BUS 3
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Tuning knob
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Outer and inner knobs select value or mode in the data field enclosed by the cursor.
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Tuning Knob
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Rotating this knob selects frequencies or certain other numeric values.
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Turbulent air penetration speed (at or above 10,000 ft)
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270 KIAS / .76M
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UNLOCKED Indicator
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Illuminates ON when the door is unlocked. When access is requested an intermittent chime will sound in the cockpit and the ON light will flash on and off.
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V/L Button
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Selects VOR or LOC as the navigation source, and displays a green needle on the PFD HSI. The needle can be toggled between on side and cross side navigation information. Green represents on side navigation information, and amber represents cross side navigation information.
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VNAV Button
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Activates or deactivates vertical navigation. VNAV vertical modes will appear magenta in the FMA.
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VOL Knob
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Allows volume adjustment of any selected audio channel.
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VS Button
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Activates or deactivates the VS mode.
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VS Thumb Wheel
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The thumb wheel selector manually selects the desired vertical speed if VS is the active vertical mode.
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When does automatic declutter occur
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Automatic de-clutter of the EICAS occurs 30 seconds after gear and flap/slat retraction if all parameters are displaying normal indications.
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When the engine and APU bleed are available simultaneously
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The AMS gives priority to APU to supply bleed requirements when the following conditions are simultaneously met: the airplane is on the ground, the opposite engine bleed pressure is below the minimum for engine start, the ground speed is below 50 kts., and the cross bleed valve is operating normally.
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When the FD cue is selected OFF by pressing the FD button
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The AFCS remains in its last selected lateral, vertical, and autothrottle mode. To select the FD OFF, deselect the current autopilot vertical mode in use. This will revert the autopilot vertical mode to FPA. Next deselect FPA to turn off the FD.
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Wind shield in flight
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With only one source of AC power, power to the F/O's windshield is shed. In the event the Captain's windshield is inoperative, power will be supplied to the F/O's windshield.
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WINDSHIELD HEATING BUTTON 1 and 2 PUSH IN
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Allows automatic operation of the associated windshield heating system.
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WINDSHIELD HEATING BUTTON 1 and 2 PUSH OUT
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Deactivates the associated windshield heating system.
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Windshield on the ground
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The windshields will be heated for approximately two minutes during the PBIT. After the PBIT is complete the windshield heaters will operate normally only with two sources of AC power (excluding GPU).
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WING ICE PROTECTION Button Ground
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Wing anti ice is selected ON from the MCDU, TRS INDEX, TO DATA SET MENU, REF A/I LSK.
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WING ICE PROTECTION Button In-flight
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Operation is automatic through the AMS.
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WING ICE PROTECTION Button PUSH IN
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Allows automatic operation of the wing anti-ice system.
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WING ICE PROTECTION Button PUSH OUT
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Deactivates the wing anti-ice system.
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WX Button
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When the HSI button has been toggled to display arc with map on the PFD, the WX button turns ON/OFF the display of WX RADAR information on the PFD map. WX RADAR information can only be displayed on the PFD map when magenta needles are selected.
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XBLEED Button PUSH IN
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Allows the AMS to control automatic operation of the cross bleed valve.
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XBLEED Button PUSH OUT
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Manually closes the cross bleed valve.
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XFEED Selector Knob: Low 2
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Opens the crossfedd valve and activates AC PUMP 1 to supply fuel to both engines from the left wing tank
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XFEED Selector Knob: OFF
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Closes the crossfeed valve
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YAW Trim Switch
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Actuates the yaw trim to left or right.
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YD Button
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Engages or disengages the Yaw Damper/Turn Coordination function.
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