FEB 2006 Lights and Switches Guide

Embraer 190 Lights and Switches Guide

Revised august 1, 2007This guide is to be used for training purposes only. This guide in no way supercedes or replaces information published in offi cial documentation.

Please forward all suggestions and corrections to Jim Miner at [email protected]. Please note the page number and error, as well as a suggested correction.

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Numeric Table of ContentsCOCKPIT LIgHTS Panel ......................................5DVDR CONTROL PaNeL ......................................5eLeCTRIC Panel....................................................6aC POWeR ............................................................6DC POWeR ............................................................7FUeL Panel ............................................................7PaSSeNgeR SIgNS Panel ...................................8FIRe eXTINgUISHeR Panel .................................8aPU CONTROL Panel .........................................10eXTeRNaL LIgHT Panel ..................................... 11HYDRaULIC System Panel.................................. 11PReSSURIZaTION Panel ....................................12ICe PROTeCTION Panel .....................................13aIRCOND/PNeUMaTIC Panel .............................14PaSSeNgeR OXYgeN Panel .............................15WINDSHIeLD WIPeR Panel ................................15gP aFCS Controls ................................................17Vertical guidance Controls ...................................18Lateral guidance Controls ....................................19SPeeD and MODe Controls ................................19

Display Controller Panel .......................................20glareshield Lights Control Panel ..........................21Primary Flight Display (PFD) ................................22ReVeRSIONaRY PaNeL .....................................22Multi Function Display (MFD) ...............................23IeSS .....................................................................24aUTOBRaKe Panel .............................................24gND PROX TeRR INHIB Pushbutton/ eMeRg/PRKgBRaKe Light ..............................................25engine Indication and Crew alerting System Display (eICaS) ................................................................26Clock/Chronometer Display ..................................26Landing gear Panel..............................................27eLT Panel .............................................................27gND PROX g/S INHIB and Lg WRN INHIB Panel .28WaTeR Panel and aDS PROBeS Panel .............28MaSTeR CaUT and WaRN Pushbuttons ............28FLIgHT CONTROLS MODe and STaLL WaRNINg Panel ....................................................................31POWeRPLaNT and IgNITION Panel ..................31

Multifunction Control Display Unit (MCDU) ..........32T/O CONFIg Button and eICaS FULL Button .....33Cursor Control Device (CCD) ...............................33Speedbrake Lever ................................................34Thrust Levers........................................................34RaT MaNUaL DePLOY Handle ...........................35gND PROX FLaP OVRD Switch .........................35eMeRg/PRKNg BRaKe Handle .........................35audio Control Panel (aCP) ...................................36SLaT/FLaP Lever .................................................38TRIM Panel...........................................................38COCKPIT DOOR CONTROL Panel .....................39IFe/CSS POWeR Panel .......................................40Printer ...................................................................40Pa Button ..............................................................41Disconnect Handles..............................................41alternate gear extension Compartment ..............42Heads Up guidance Display .................................43HgS Menu ............................................................43Yoke ......................................................................44Tiller ......................................................................45

Alphabetic Table of ContentsaC POWeR ............................................................6aIRCOND/PNeUMaTIC Panel .............................14alternate gear extension Compartment ..............42aPU CONTROL Panel .........................................10audio Control Panel (aCP) ...................................36aUTOBRaKe Panel .............................................24Clock/Chronometer Display ..................................26COCKPIT DOOR CONTROL Panel .....................39COCKPIT LIgHTS Panel ......................................5Cursor Control Device (CCD) ...............................33DC POWeR ............................................................7Disconnect Handles..............................................41Display Controller Panel .......................................20DVDR CONTROL PaNeL ......................................5eLeCTRIC Panel....................................................6eLT Panel .............................................................27eMeRg/PRKNg BRaKe Handle .........................35engine Indication and Crew alerting System Display (eICaS) ................................................................26eXTeRNaL LIgHT Panel ..................................... 11

FIRe eXTINgUISHeR Panel .................................8FLIgHT CONTROLS MODe and STaLL WaRNINg Panel ....................................................................31FUeL Panel ............................................................7glareshield Lights Control Panel ..........................21gND PROX FLaP OVRD Switch .........................35gND PROX g/S INHIB and Lg WRN INHIB Panel .28gND PROX TeRR INHIB Pushbutton/ eMeRg/PRKgBRaKe Light ..............................................25gP aFCS Controls ................................................17Heads Up guidance Display .................................43HgS Menu ............................................................43HYDRaULIC System Panel.................................. 11ICe PROTeCTION Panel .....................................13IeSS .....................................................................24IFe/CSS POWeR Panel .......................................40Landing gear Panel..............................................27Lateral guidance Controls ....................................19MaSTeR CaUT and WaRN Pushbuttons ............28Multifunction Control Display Unit (MCDU) ..........32

Multi Function Display (MFD) ...............................23Pa Button ..............................................................41PaSSeNgeR OXYgeN Panel .............................15PaSSeNgeR SIgNS Panel ...................................8POWeRPLaNT and IgNITION Panel ..................31PReSSURIZaTION Panel ....................................12Primary Flight Display (PFD) ................................22Printer ...................................................................40RaT MaNUaL DePLOY Handle ...........................35ReVeRSIONaRY PaNeL .....................................22SLaT/FLaP Lever .................................................38SPeeD and MODe Controls ................................19Speedbrake Lever ................................................34Thrust Levers........................................................34Tiller ......................................................................45T/O CONFIg Button and eICaS FULL Button .....33TRIM Panel...........................................................38Vertical guidance Controls ...................................18WaTeR Panel and aDS PROBeS Panel .............28WINDSHIeLD WIPeR Panel ................................15Yoke ......................................................................44

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Embraer 190 Lights and Switches Guide

OVeRHeaD PaNeLS

MaIN PaNeLS

PeDeSTaL PaNeLSPeDeSTaL PaNeLS

e190 PaNeLS

Page 4OVeRHeaD PaNeL

DVDR CONTROL

FIRe PROTeCTION

WINDSHIeLD WIPeR

aIR COND/PNeUMaTIC

PaSSeNgeROXYgeN

PReSSURIZaTION

eXTeRNaL LIgHTINg

eLeCTRICaC/DC POWeR

COCKPIT LIgHTS

FUeL

PaSSeNgeR SIgNS

ICe PROTeCTIONaPU CONTROL

HYDRaULIC

PReSSURIZaTION

eXTeRNaL LIgHTINg

WINDSHIeLD WIPeRWINDSHIeLD WIPeR

PaSSeNgeR SIgNS

Overhead PanelCOCKPIT LIgHTS Panel .................................................................................. 5DVDR CONTROL PaNeL .................................................................................. 5eLeCTRIC Panel................................................................................................ 6aC POWeR ........................................................................................................ 6DC POWeR ........................................................................................................ 7FUeL Panel ........................................................................................................ 7PaSSeNgeR SIgNS Panel ............................................................................... 8

FIRe eXTINgUISHeR Panel ............................................................................. 8aPU CONTROL Panel ..................................................................................... 10eXTeRNaL LIgHT Panel ................................................................................. 10HYDRaULIC System Panel...............................................................................11PReSSURIZaTION Panel ................................................................................ 12ICe PROTeCTION Panel ................................................................................. 13aIRCOND/PNeUMaTIC Panel ........................................................................ 14PaSSeNgeR OXYgeN Panel ......................................................................... 15WINDSHIeLD WIPeR Panel ............................................................................ 15


DVDR CONTROL PANEL

1. CVR ERASEallows CVR data to be erased when the aircraft is on the ground with the parking brake set.

2. DVDR TESTCommands a self test of DVDR 1 and DVDR 2. a failure is indicated by a CVR aFT(FWD) FaIL advisory message on the eICaS.

3. HEADPHONE Jackallows a headset to be inserted to monitor the composite audio output of the DVDR unit during tests and normal operations.

4. Selector SwitchFWD: enables the test tone of DVDR 1 to be heard when a headset is plugged in to the headphone jack.AFT: enables the test tone of DVDR 2 to be heard when a headset is plugged in to the headphone jack.

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DVDR Control Panel

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COCKPIT LIGHTS Panel

1. MAIN PNL KnobTurns on/off and sets the lighting brightness of the guidance Panel and Instrument Panel background lighting.

2. OVHD PNL KnobTurns on/off and sets the brightness of the overhead panel’s background lighting. Rotating the knob to the OFF position will illuminate all annunciator lights to full bright.

3. PEDESTAL KnobTurns on/off and sets pedestal lighting brightness.

4. DOME Light SwitchTurns on/off the two cockpit dome lights. Batteries must be ON/aUTO to have dome lights on.

5. ANNUNCIATORS TEST ButtonThe striped bars and caption indications in all main panel, overhead panel, and control pedestal pushbuttons illuminate when pressed, allowing verifi cation of lamp integrity. Only the

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COCKPIT LIgHTS PanelEMRG/PRKG BRAKE light, GPU pushbutton light, and fi re test lights are not illuminated.


DISC: Must be held in this position for one second to mechanically disconnect the IDg. The IDg cannot be reconnected in fl ight.NOTE 1: Normal aC BUS source priority is on-side IDg, aC BUS TIe, off-side IDg.NOTE 2: The illumination of an amber LeD next to the DISC position of the IDg 1 or IDg 2 rotary knob indicates to the pilot which IDg to disconnect. This LeD will illuminate in association with the IDg 1(2) OIL caution eICaS, and will extinguish after the IDg is disconnected.

2. AC BUS TIES Selector Knob 1 OPEN: Opens the Bus Tie Contactor (BTC) 1, segregating aC BUS 1 from the aC BUS TIe.AUTO: This position allows automatic operation of the BTC’s according to system logic. 2 OPEN: Opens the Bus Tie Contactor (BTC) 2, segregating aC BUS 2 from tthe aC BUS TIe.NOTE: aC BUS TIe source priority is aPU, gPU, then IDg.

3. GPU ButtonPUSH IN: Connects the aC gPU to the aC BUS TIe, according to the source priority.PUSH OUT: Isolates the aC gPU from the aC BUS TIe.NOTE: aVaIL Light: aVaIL will illuminate with the button pushed in or out when the aC gPU is connected to the aircraft, but is not powering the aC BUS TIe. IN USe Light: IN USe will only illuminate when the button is pushed in, and the aC gPU is powering the aC BUS TIe.

4. APU GEN ButtonPUSH IN: This position allows the aPU generator to connect to the aC BUS TIe, automatically according to the source priority.PUSH OUT: 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.

ELECTRIC Panel

AC POWER

1. IDG 1 and IDG 2 Selector Knob AUTO: This position allows the IDg contactor to close, connecting the IDg to the respective aC BUS automatically, according to system logic.OFF: Opens the IDg contactor isolating the IDg from the respective aC BUS.

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eLeCTRIC Panel


DC POWER

5. TRU ESS Toggle SwitchAUTO: This position allows automatic connection of the TRU eSS to the eSS BUS 3.OFF: Isolates the TRU eSS from the eSS BUS 3.

6. TRU 1 and TRU 2 Toggle SwitchAUTO: This position allows automatic connection of the TRU to the respective DC BUS. OFF: Isolates the TRU from the respective DC BUS.

7. BATT 1 Selector Knob ON: The battery is connected to the DC eSS BUS 1.OFF: The battery supplies power to HOT BaTT BUS 1 only.

8. DC BUS TIES Toggle SwitchAUTO: This position allows automatic operation of the DC TIe contactors (1 DCTC/2eTC’s), according to system logic. OFF: Opens all DC TIe contactors.

9. BATT 2 Selector Knob AUTO: This position connects BaTT 2 to either the DC eSS BUS 2 or the aPU STaRT BUS automatically, according to system logic. OFF: The battery supplies power to HOT BaTT BUS 2 only.

2. DC PUMPOFF: Deactivates the DC fuel pump.AUTO: allows automatic operation of the DC PUMP in accordance with system logic.ON: activates the DC fuel pump.NOTE: The DC PUMP will activate for aPU start if aC power is not available. The DC PUMP is not a backup for the aC PUMP.

3. AC PUMP 1 and AC PUMP 2OFF: Deactivates the associated aC PUMP.AUTO: allows automatic operation of the associated aC PUMP in accordance with system logic. ON: activates the associated aC PUMP.NOTE: The aC PUMP will activate automatically when fuel pressure is demanded and ejector output is insuffi cient (engine start or ejector pump failure), and for XFeeD operations.

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FUeL Panel

FUEL Panel

1. XFEED Selector KnobLOW 1: Opens the cross feed valve, and activates aC PUMP 2 to supply fuel to both engines from the right wing tank.OFF: Closes the crossfeed valve.LOW 2: Opens the cross feed valve, and activates aC PUMP 1 to supply fuel to both engines from the left wing tank.


PASSENGER SIGNS Panel

1. EMER LT Selector KnobOFF: Disables automatic operation of the emergency lights. The lights can still be turned on from the FWD or aFT aTTeNDaNT panel.ARMED: automatically illuminates all emergency lights if DC BUS 1 loses power or if the airplane electrical power is turned off. ON: Turns on all emergency lights regardless of the position of the eMeRgeNCY LIgHT switch on the FWD and aFT aTTeNDaNT panels.

2. ATTND CALL Button Pressing this button sounds a chime in passenger cabin, and illuminates the green light on the Flight attendant rainbow.

3. FSTN BELTS Toggle SwitchON: Illuminates the FaSTeN BeLTS signs. Turning the switch ON sounds a single low tone chime in the cabin, lavatories, and galleys.OFF: Turns off the FaSTeN SeaT BeLTS signs. Turning the switch OFF sounds a single low tone chime in the cabin.

PaSSeNgeR SIgNS Panel

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NOTE: The Fasten Seat Belts sign will automatically illuminate when masks are commanded to deploy.

4. NO SMKG Toggle SwitchON: Illuminates the NO SMOKINg signs. Turning the switch ON sounds a single low tone chime in the cabin.OFF: Turns off the NO SMOKINg signs. Turning the switch OFF sounds a single low tone chime in the cabin.NOTE: The No Smoking sign will automatically illuminate when the oxygen masks are commanded to deploy.

5. STERILE Toggle SwitchON: Illuminates the amber sterile light on the fl ight attendant rainbow. Turning the switch ON sounds a single high tone chime in the cabin.OFF: Turns off the amber sterile light on the fl ight attendant rainbow.

FIRE EXTINGUISHER Panel

1. #1 and #2 Engine Fire EXTG Handle: Illuminates when fi re is detected.PULL: 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.ROTATE (left (A) or right (B)): Discharges the associated fi re extinguisher bottle into the associated engine.

2. APU (Guarded)Momentary action pushbutton.Closes the aPU fuel shutoff valve and discharges the aPU fi re extinguisher bottle. The light will illuminate when the aPU eMeR STOP button has been pushed in when an aPU fi re has been detected, or 60 seconds after an APU fi re has been detected and no pilot action has occurred. If no fi re is detected, one push will arm and discharge the fi re bottle.


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FIRe eXTINgUISHeR Panel

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NOTE: The aircraft must not be left unattended with the aPU running because the APU fi re bottle will not automatically discharge in the event of a fi re.

3. CARGO SMOKE FWD and AFT Buttons (GUARDED)Momentary action pushbutton. Illuminates when the high rate bottle is armed. The table below describes the operation:

SMOKE DETECTED SMOKE NOT DETECTED

IN FLIGHT: a single button push will discharge the HIgH rate bottle. 60 seconds later the LOW rate bottle will discharge automattically.

IN FLIGHT: 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.

SMOKE DETECTED SMOKE NOT DETECTED

ON GROUND: 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.

ON GROUND: 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.

NOTE: In fl ight or on ground, with no smoke detected, if either cargo smoke fi re extinguisher button is pushed inadvertently, push the test button to cancel or wait two minutes for the system to reset automatically.

4. Fire Detection System TEST ButtonMomentary action button. Tests the engine and aPU fi re detection systems, and the forward and aft cargo compartment smoke detection systems. Prior to performing a FIRE TEST confi rm that there are no FIRE DET FAIL, FIREX FaIL, FIReX aRM, or BTL DISCH messages on the eICaS. a valid test is indicated by the following lights/messages:

AURAL WARNING FIRe BeLL/TRIPLe CHIMe

Overhead Panel (6)

Engine 1 and 2 fi re EXTG handles illuminate

FWD and aFT CaRgO SMOKe pushbuttons illuminate

APU fi re extinguisher pushbutton illuminates

Red bar in aPU eMeR STOP pushbutton illuminates

EICAS (5)

eNg 1 FIRe

eNg 2 FIRe

aPU FIRe

CaRgO FWD SMOKe

CaRgO aFT SMOKe

GLARESHIELD PANEL/EICAS (4)

Master Warning Lights illuminated

FIRe icon on engine 1 and 2 ITT gauges


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eXTeRNaL LIgHT PanelAPU CONTROL Panel

1. MASTER KnobOFF: Normal position when the aPU is not running. ON: Normal position when the aPU is running.START: (Momentary action) Initiates the aPU start cycle.NOTE 1: Moving this knob from ON to OFF starts the aPU shutdown process. 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.NOTE 2: 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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aPU CONTROL Panel2. EMER STOP Button (Guarded)

PUSH IN: 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. PUSH OUT: Normal position, with the fuel shut off valve open.NOTE: In case of fi re, the upper half of the button illuminates red. When pushed in, a white striped bar illuminates on the lower half of the button.NOTE: The aircraft must not be left unattended with the aPU running because the APU fi re bottle will not automatically discharge in the event of a fi re.


HYDRAULIC System Panel

1. PTU SwitchOFF: Turns the PTU off.

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HYDRaULIC System Panel

AUTO: During takeoff or landing with the fl aps 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. ON: The PTU operates continuously.

2. SYS 1 and SYS 2 ENG PUMP SHUTOFF Buttons (Guarded)Momentary action pushbuttons.PUSH IN: Closes the hydraulic shutoff valve (SOV), isolating the respective eDP from the associated hydraulic system.PUSH OUT: Normal position. Hydraulic SOV open.

3. SYS 1 and SYS 2 ELEC PUMP Selector KnobsOFF: Turns the associated electrical pump off.AUTO: On Ground: SYS 1 and SYS 2 will run automatically for takeoff when the fl aps 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.

In Flight: SYS 1 and SYS 2 will operate automatically with the failure of its associated EDP, or when fl aps are not at zero.

ON: Operates the electrical pump continuously.

4. SYS 3 ELEC PUMP A Selector KnobOFF: Turns the electrical pump off.ON: Operates the electrical pump continuously.

5. SYS 3 ELEC PUMP B Selector KnobOFF: Turns the electrical pump off.AUTO: In fl ight, the pump will turn on when SYS 3A ELEC PUMP fails.ON: Operates SYS 3 B pump continuously.

EXTERNAL LIGHT Panel

1. NAV, STROBE and RED BCN SwitchesTurns on/off the associated light.

2. INSP Light SwitchTurns on/off the inspection lights.

3. LANDING Light SwitchesTurns on/off the associated landing light.

4. TAXI Light SwitchesTurns on/off the taxi lights.

5. LOGO Light SwitchTurns on/off the logo lights.


PRESSURIZATION Panel

1. Pressurization MODE Selector KnobMAN: Allows manual control of the outfl ow valve (OFV). AUTO: Allows automatic operation of the pressurization system.LFE CTRL: Allows manual input of landing fi eld 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.

2. DUMP Button (Guarded): When pushed in a white striped bar will illuminate in the button. 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 outfl ow 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

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14PReSSURIZaTION Panel

button to its normal (out) position.NOTE: Selecting the DUMP button in while in MaN mode will still command the PaCK’s and ReCIRC FaN’s to shutdown.

3. CAB ALT Selector KnobRotary knob is only active when the pressurization MODE knob is selected to MaN. DOWN: Manually closes the OFV.STOP (Spring Loaded): Normal operation position.UP: Manually opens the OFV.

4. LFE KnobManual input of the LFe is only possible when the pressurization MODE knob is selected to LFE.DOWN: Decreases the LFe in 100’ increments. If held longer than 5 seconds the LFe will decrease in 500’ increments. STOP (Spring Loaded): Normal operation position.UP: Raises the LFe in 100’ increments. If held longer than 5 seconds the LFe will increase in 500’ increments.

ICe PROTeCTION Panel 1

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ICE PROTECTION Panel

1. WINDSHIELD HEATING BUTTON 1 and 2PUSH IN: allows automatic operation of the associated windshield heating system.PUSH OUT: Deactivates the associated windshield heating system.NOTE: On the ground 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).NOTE: In flight 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.

2. WING ICE PROTECTION ButtonPUSH IN: allows automatic operation of the wing anti-ice system. Ground: Wing anti ice is selected ON from the MCDU, TRS INDeX, TO DaTa SeT MeNU, ReF a/I LSK.In-flight: Operation is automatic through the aMS.PUSH OUT: Deactivates the wing anti-ice system.

3. ENGINE ICE PROTECTION ButtonPUSH IN: allows automatic operation of the associated engine anti-ice system. Ground: engine anti-ice is selected ON from the MCDU, TRS INDeX, TO DaTa SeT MeNU, ReF a/I LSK. In-Flight: Operation is automatic through the aMS.PUSH OUT: Deactivates the associated engine anti-ice system.

4. ICE PROTECTION MODE Selector KnobAUTO: allows automatic operation of the wing and engine anti-ice systems.

ON: Overrides the system logic inflight, activating the anti-ice system regardless of icing condition.

5. ICE PROTECTION TEST KnobENG: Provides a test for the engine anti-ice system.OFF: Spring-loaded position.WING: Provides a test for the wing anti-ice system.NOTE: Operation of this switch will be a function of Technical Operations.

TO DaTaSeT

MeNU

MODe SeLeCTOR

KNOB

ICe CONDITION

eNgINe a/I aCTIVIaTION

WINg a/I aCTIVaTION

eICaS CaUTION MeSSage

OFF aUTO NOT DeTeCTeD

(N/a) (N/a) (N/a)

DeTeCTeD ON: 1700’ agL or 2 min after liftoff

OFF: 5 min after ice condition no longer

detected

ON: 1700’ agL or 2 min after liftoff


detected

(N/a)

ON NOT DeTeCTeD

ON: engine Running

OFF: engine shutdown

ON: LiftoffOFF: Touchdown

eNg ReF a/I DISag

DeTeCTeD ON: engine Running


ON: LiftoffOFF: Touchdown

eNg ReF a/I DISag

aLL aUTO NOT DeTeCTeD

ON: engine Running

OFF: 1700’ agL or 5 min after liftoff

ON: Wheel speed > 40kts

OFF: 1700’agL or 5 min after liftoff

(N/a)



detected



detected

(N/a)

ON NOT DeTeCTeD

ON: engine Running



OFF: Touchdown

(N/a)


OFF: engine Shutdown

ON: Wheel Speed > 40kts

OFF: Touchdown

(N/a)


3. RECIRC ButtonPUSH IN: allows for automatic operation of the ReCIRC fans through the aMS.PUSH OUT: Turns off both ReCIRC fans.NOTE: 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.

4. PACK 1 and PACK 2 ButtonsPUSH IN: allows for automatic operation by the aMS. This position opens the associated pack valve, according to system logic.PUSH OUT: Manually closes the associated pack valve.NOTE: PaCK 1 and PaCK 2 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.

5. XBLEED ButtonPUSH IN: allows the aMS to control automatic operation of the cross bleed valve.PUSH OUT: Manually closes the cross bleed valve.

6. BLEED 1 and BLEED 2 ButtonsPUSH IN: Allows the AMS to automatically confi gure the position of the associated engine bleed valve.PUSH OUT: Manually closes the associated engine bleed valve.NOTE: an engine bleed leak will cause the illumination of an amber striped bar in the upper half of the associated engine bleed button.

7. APU BLEED ButtonPUSH IN: Allows the AMS to automatically confi gure the position of the aPU bleed valve.PUSH OUT: Manually closes the aPU bleed valve.

aIRCOND/PNeUMaTIC Panel

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AIRCOND/PNEUMATIC PanelPneumatic bleed source priority is on side bleed, off side bleed, and then aPU bleed. When the engine and aPU bleed are available simultaneously, 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.

1. CKPT Temperature Control KnobControls cockpit temperature according to the knob position.

2. PAX CABIN Temperature Control KnobControls passenger cabin temperature according to the knob position. Rotating the knob to the aTTND position allows cabin temperature control via the fl ight attendant control panel.


PASSENGER OXYGEN Panel

1. MASKS DEPLOY KnobOFF: Disables automatic deployment of passenger oxygen masks.AUTO: enables automatic deployment of passenger oxygen masks when cabin pressure altitude is above 14000 ft.OVRD: Deploys the passenger oxygen masks regardless of cabin altitude.NOTE: The NO SMKg and FSTN BeLTS will automatically illuminate when the oxygen masks are commanded to deploy.

2. MASKS DEPLOYED Indicatoran ON light illuminates, indicating that the passenger and fl ight attendant oxygen masks have been commanded to deploy.

1 2 PaSSeNgeR OXYgeN Panel1 2

WINDSHIELD WIPER Panel

#1 and #2 WINDSHIELD WIPER ControlsTIMER: Provides eight-second intermittent operation.OFF: Stops wind shield wipers in the stowed position.LOW: Windshield wipers operate at low speed.HI: Windshield wipers operate at high speed. NOTE: If both the windshield wiper knobs are selected to LOW/HI they will sync to the Captains (#1) controller. Windshield wipers will not operate on a dry windshield.

Windshield Wiper Control Panel

NOTE: an aPU bleed leak will cause the illumination of an amber striped bar in the upper half of the aPU BLeeD button.

OVeRHeaD PaNeL MaIN INSTRUMeNT PaNeL Page 16

Main Instrument PanelgP aFCS Controls ............................................................................................ 17Vertical guidance Controls ............................................................................... 18Lateral guidance Controls ................................................................................ 19SPeeD and MODe Controls ............................................................................ 19Display Controller Panel ................................................................................... 20glareshield Lights Control Panel ...................................................................... 21Primary Flight Display (PFD) ............................................................................ 22ReVeRSIONaRY PaNeL ................................................................................. 22Multi Function Display (MFD) ........................................................................... 23

IeSS ................................................................................................................. 24aUTOBRaKe Panel ......................................................................................... 24gND PROX TeRR INHIB Pushbutton/ eMeRg/PRKgBRaKe Light .............. 25engine Indication and Crew alerting System Display (eICaS)......................... 26Clock/Chronometer Display .............................................................................. 26Landing gear Panel.......................................................................................... 27eLT Panel ......................................................................................................... 27gND PROX g/S INHIB and Lg WRN INHIB Panel ......................................... 28WaTeR Panel and aDS PROBeS Panel ......................................................... 28MaSTeR CaUT and WaRN Pushbuttons ........................................................ 28

gUIDaNCe

CLOCK/CHRONOMeTeR

LaNDINg geaR CONTROLS

LaNDINg geaR WaRNINg INHIBITION BUTTON

eMeRgeNCY PaRKINg BRaKe LIgHT

LH ReVeRSIONaRY PaNeL

WaTeR DUMP aND aDS PROBeS

gLaReSHIeLD LIgHTS

MaSTeR WaRNINg/CaUTION

gROUND PROXIMITY gLIDeSLOPe

gROUND PROXIMITY TeRRaIN INHIBIT

RT ReVeRSIONaRY PaNeL

INTegRaTeD eLeCTRONICSTaNDBY SYSTeM (IeSS)

PRIMaRY FLIgHT DISPLaY

MULTI FUNCTION DISPLaY (MFD)

eNgINe INDICaTIONaND CReW aLeRTINgSYSTeM DISPLaY

aUTOBRaKe

gLaReSHIeLD LIgHTS

MaSTeR WaRNINg/CaUTION

PRIMaRY FLIgHT DISPLaY


WaTeR DUMP aND aDS PROBeS

LaNDINg geaR LH ReVeRSIONaRY PaNeL

RT ReVeRSIONaRY PaNeLgROUND PROXIMITY MULTI FUNCTION DISPLaY (MFD)

LaNDINg geaR


gROUND PROXIMITY

gROUND gROUND PROXIMITY gLIDeSLOPe

eNgINe INDICaTION

eMeRgeNCY PaRKINg LaNDINg geaR WaRNINg

eLT

Page 17MaIN INSTRUMeNT PaNeL

GP AFCS Controls

1. FD ButtonRemoves the FD cue from the associated PFD when the aP is not engaged, but does not turn off the FD system. If the aP is engaged the FD cue cannot be removed from the PFD that is on the same side as the aFCS source.NOTE: When the FD cue is selected OFF by pressing the FD button, 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.

2. AP ButtonCommands autopilot engagement or disengagement.NOTE: 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.

3. AT Button(gROUND) arms the autothrottle system.(IN FLIgHT) engages or disengages the autothrottle system.NOTE: The autothrottle disconnect warning can only be

gP aFCS Controls

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4 5

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4 555

cancelled by pushing one of the thrust lever mounted aT DISC buttons.

4. YD Buttonengages or disengages the Yaw Damper/Turn Coordination function.NOTE: The YD defaults to ON at system power up. It is also automatically turned ON when the aP is engaged.

5. SRC ButtonSelects the Captain or First Offi cer AFCS side as data source. a green arrowhead on the FMa indicates the selected side.


Vertical guidance Controls

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7

84 6 8

Vertical Guidance Controls

1. FLCH ButtonFLCH will initiate a climb or descent based on the current aircraft altitude vs. the altitude selected. If the aT system is engaged a climb will be made with the thrust levers at TOga and descents will be made with the thrust levers at IDLe. For altitude changes less than 2000’, 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.

2. VNAV Buttonactivates or deactivates vertical navigation. VNaV vertical modes will appear magenta in the FMa.

3. ALT Buttonactivates or deactivates the altitude hold function.

4. ALT SEL KnobSelects the desired altitude in 100’ increments.

Clockwise rotation: increases the altitude target.Counter clockwise rotation: decreases the altitude target.NOTE: Pressing the center of the aLT SeL knob 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.

5. FPA Buttonactivates or deactivates the Flight Path angle mode. This is the basic vertical mode.NOTE: engaging the autopilot when no FD mode is active causes FPa mode to become the active vertical mode, and the FD guidance cue to come into view.

6. FPA SEL KnobManually 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 fl ight path reference line.The fl ight path angle is limited to 9.9 degrees nose up or nose down.

7. VS Buttonactivates or deactivates the VS mode.

8. VS Thumb Wheel The thumb wheel selector manually selects the desired vertical speed if VS is the active vertical mode.


Lateral guidance Controls

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34

5

2

3

Lateral Guidance Controls

1. NAV ButtonSelects or deselects VOR/LOC or LNaV as the lateral navigation mode.

2. HDG ButtonSelects or deselects HDg as the lateral navigation mode.

3. HDG SEL KnobManually selects the desired heading. Pressing the center of the knob will center the heading bug to the current heading.

4. BANK ButtonSelects 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.

5. APP Buttonactivates or deactivates the approach mode of the aFCS to intercept an ILS or BC. For an ILS, the autopilot approach Status annunciator displays the following:•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.

SPeeD and MODe Controls

SPeeD SeLeCTOR KNOBSPeeD SeLeCTOR KNOB

SPEED and MODE Controls

SPEED Selector Knob (OUTER)FMS: The desired speed is controlled by the FMS. Changes can be entered through the MCDU. FMS speed is displayed in magenta on the PFD.MAN: The desired speed is controlled manually, displayed in cyan on the PFD.SPEED Selector Knob (INNER)Manually selects the desired airspeed. Manual speeds are displayed in cyan on the PFD.PUSH IAS-MACH: Toggles the speed selected on the PFD between IaS and MaCH.


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10

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8796

12

Display Controller Panel

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10

8779666

Display Controller Panel

1. BARO SET Knob (INNER)Sets barometric altimeter correction.Pushing this control knob sets barometric correction to standard.

2. BARO SET Knob (OUTER) IN: Sets the altimeter in inches of mercury. HPa: Sets the altitude in hectopascals.

3. HSI ButtonToggles the HSI view on the PFD between full compass rose, arc and arc with map.

4. WX ButtonWhen 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.

5. FMS ButtonSelects 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.

6. BRG ButtonsCIRCLE: Displays #1 RMI bearing pointer information on the PFD. The display can be toggled to view VOR 1, FMS 1, or OFF. DIAMOND: Displays #2 RMI bearing pointer information on the PFD. The display can be toggled to view VOR 2, FMS 2, or OFF.

7. PREV ButtonSelects 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.

8. V/L ButtonSelects 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.

9. FPR ButtonSelects or deselects the display of a cyan fl ight path reference line on the PFD. The FPa SeL knob can be rotated to change the value of this line +/- 9.9 degrees.


10. MINIMUMS Knob (OUTER)Sets the approach minimums for all nonprecision and precision approaches. RA: allows for auto callouts based on the RaDaR altimeter. This position is used only for CaT II and CaT III ILS approaches.BARO: allows for auto call outs based on the barometric altimeter. This position is used for all CaT I ILS and nonprecission approaches.

11. MINIMUMS Knob (INNER)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.

glareshield Lights Control Panel

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2

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22222

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Glareshield Lights Control Panel

1. STBY/CLK KnobSets the brightness of the standby instruments/clock lighting.

2. PFD/MFD/EICAS KnobSets the brightness of the associated electronic display.

3. FLOOD/STORM KnobTurns on/off and sets the brightness of the fl ood/storm panel lighting.Provides maximum brightness for storm conditions at BRT position.

4. CHART KnobTurns on/off and sets the brightness of associated chart holder lighting.

5. PTT Buttonallows transmissions on the COMM system selected via the aCP mic buttons.


ReVeRSIONaRY PaNeL

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3

2

3

Primary Flight Display (PFD)

aUTOPILOT aPPROaCH STaTUS aNNUNCIaTORFLIgHT MODe aNNUNCIaTORaTTITUDe aND SIDeSLIPaLTITIUDeaIR SPeeD MaCHaIR SPeeD TReND VeCTOR VeRTICaL SPeeDFLIgHT PaTH aNgLeFLIgHT PaTH VeCTORTOTaL eNeRgYFLIgHT DIReCTORTCaS ReSOLUTION aDVISORYWINDSHeaRRaDIO aLTIMeTeR

HeaDINgWeaTHeR RaDaRLS/VOR/DMeRaDIO COMMUNICaTION TUNNINgRaDIO NaVIgaTION TUNNINgFMS aNNUNCIaTION/INDICaTIONWINDeLaPSeD TIMe

AVIATE

NAVIGATE AND COMMUNICATE

HeaDINgWeaTHeR RaDaRLS/VOR/DMeRaDIO COMMUNICaTION TUNNINgRaDIO NaVIgaTION TUNNINgFMS aNNUNCIaTION/INDICaTIONWINDeLaPSeD TIMe

NAVIGATE AND COMMUNICATE

aUTOPILOT aPPROaCH STaTUS aNNUNCIaTORFLIgHT MODe aNNUNCIaTORaTTITUDe aND SIDeSLIPaLTITIUDeaIR SPeeD MaCHaIR SPeeD TReND VeCTOR VeRTICaL SPeeDFLIgHT PaTH aNgLeFLIgHT PaTH VeCTORTOTaL eNeRgYFLIgHT DIReCTORTCaS ReSOLUTION aDVISORYWINDSHeaRRaDIO aLTIMeTeR

REVERSIONARY PANEL

1. DISPLAYS KnobPFD: Forces the associated MFD to display as a PFD.AUTO: allows automatic reversion of the MFD in case of display failure.MFD: Forces the associated MFD to display as an MFD.EICAS: Forces the associated MFD to display as an eICaS.

EDS AUTO REVERSION LOGIC

PFD eICaS X PFDeICaS X PFD eICaS MFD PFD

X PFD X eICaS PFD

PFD eICaS X PFD X

PFD MFD eICaS PFD X

X PFD X eICaS X

aUTO aUTO aUTO

aUTO aUTO aUTO

aUTO aUTO aUTO aUTO

2. ADS ButtonMomentary action pushbutton:Manually reverts the aDS source.

Primary Flight Display (PFD)The PFD displays information such as airspeed indicator, altitude indicator, aDI, HSI, vertical speed indicator, radio aids, autopilot, fl ight director and radio altitude data. In the event of a display failure, information will be automatically presented in the MFD.The display controller portion of the guidance panel allows the selection of PFD HSI formats, navigation sources, weather display, and bearing pointer selection.


MaPPLaNSYSTeM SYNOPTIC PageSTCaSWeaTHeR RaDaRegPWS (TeRRaIN)

Multi Function Display (MFD)

TCaS ZOOM WeaTHeR RaDaR CONTROLLeRTCaS CONTROLLeR

MaPPLaNSYSTeM SYNOPTIC PageSTCaSWeaTHeR RaDaRegPWS (TeRRaIN)

TCaS ZOOM WeaTHeR RaDaR CONTROLLeRTCaS CONTROLLeR

NAVIGATE (VNAV)

NAVIGATE

Multi Function Display (MFD)The MFD presents map and plan navigation formats and various systems synoptic formats selectable by the fl ight crew. The MFD provides redundancy to display both the PFD and eICaS formats based upon reversion. It also has the ability to display maintenance information. The MFD consists of menu softkeys, on the top and bottom of the screen, which are used to select formats and control various systems.

When aDS source reversion is selected, a white striped bar illuminates in the button. NOTE 1: ADS source fl ag is displayed on the PFD.NOTE 2: Reversion to aDS 3 is automatic.NOTE 3: Reversions that will place the both pilots on the same aDS source must be done manually.

Reversionary LogicNormal

Operation1st reversion 2nd reversion

Captain aDS 1 aDS 3 aDS 2

First Offi cer aDS 2 aDS 3 aDS 1

3. IRS ButtonMomentary action pushbutton:Reverts the IRS source.When IRS source reversion is selected, a white striped bar illuminates in the button.NOTE 1: IRS source fl ag is displayed on the PFD.NOTE 2: IRS reversion must be performed manually.


IeSS

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IESS

1. Brightness Adjustment Buttonsadjusts brightness.

2. ILS ButtonSelects 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.

3. STD ButtonSets the barometric pressure to standard atmospheric pressure.

4. Brightness Cellautomatically adjusts the instrument brightness according to the ambient lighting.

aUTOBRaKe Panel

1

5. BARO Knoballows manual setting of the altimeter.

6. CAGE ButtonResets 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 fl ight conditions.When pressed, an amber CAGE fl ag is displayed on the upper right corner of the IeSS.

AUTOBRAKE Panel

1. AUTOBRAKE Selector KnobRTO: Selects RTO deceleration rate.OFF: autobrake is deactivated.LO: Selects the low deceleration rate.MED: Selects the medium deceleration rateHI: Selects the high deceleration rate.


AUTOBRAKE ARMING LOGICLaNDINg MODe ReJeCTeD TaKeOFF

MODe

Selector Knob Position LO, MeD or HI RTO

WOW Indication In fl ight On the ground

Wheel Speed Below 60 knots

Brake Control System No faults

Brake Pedal Position Not pressed any

Thrust Levers Position any Idle or below

AUTOBRAKE APPLICATION LOGICLaNDINg MODe ReJeCTeD TaKeOFF

MODe

Condition aRMeD

Selector Knob Position LO, MeD or HI 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

NOTE: For landing mode, the WOW must indicate the airplane is on the ground for more than 2 seconds to allow autobrake application.

AUTOBRAKE DISARMING LOGICLaNDINg MODe ReJeCTeD TaKeOFF

MODe

Selector Knob Position OFF or RTO OFF, LO, MeD or HI

WOW Indication - In fl ight

Brake Control System Faults detected Faults detected below 60 knots of Wheel Speed

Brake Pedal Position Pressed Pressed while autobrake is being applied

Thrust Levers Position above Idle while autobrake is being applied

gND PROX TeRR INHIB Pushbutton/ eMeRg/PRKgBRaKe Light

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GND PROX TERR INHIB Pushbutton/ EMERG/PRKGBRAKE Light

1. GND PROX TERR INHIB PushbuttonWhen pressed, inhibits egPWS and thus avoids unwanted terrain alerts in airports not covered by egPWS database.

2. EMERG/PRKGBRAKE LightThe word “ON” illuminates when the eMeRg/PRKgBRaKe is actuated. Illumination of the light indicates that suffi cient hydraulic pressure is available to maintain brake pressure.


geaRFLaPSTRIM

geaRFLaPSTRIM

eNgINe

MANAGEMENT

engine Indication and Crew alerting System Display (eICaS)

Engine Indication and Crew Alerting System Display (EICAS)

The eICaS displays engine and system parameters such as fl ap, gear, spoilers and trim positions, total fuel quantity, aPU and environmental information. The eICaS also displays warning, caution, advisory, and status messages. In case of failure in the eICaS display, its information may be presented in the MFD by appropriately setting the reversionary panel. an automatic mode de-clutters the eICaS after takeoff. De-cluttering occurs 30 seconds after landing gear and fl ap/slat retraction.

Clock/Chronometer

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Clock/Chronometer Display

1. Clock/Chonometer DisplayDisplays 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.

The following items are de-cluttered from eICaS

•Oil pressure.•Oil temperature.•Engine vibration.•Slat position.•Flap position.

•Speed brake position.•Landing gear position (if aUTOBRaKeS are OFF)•Pitch trim green band.

In normal conditions, de-clutter will be disabled when one of the above parameters is no longer in a normal indicating range, not stowed, or not up and locked. additionally, arming the aUTOBRaKe for landing will disable the de-clutter function of the eICaS.


2. DATE/SET Buttonallows 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 fl ash 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.

3. RST ButtonResets the chronometer to zero if the chronometer is stopped.

4. CHR ButtonStarts/stops the chronometer.

5. GPS/INT/SET SelectorGPS: Synchronizes with UTC and DATE from GPS.INT: Displays information from the internal clock.SET: Sets the clock modes.

6. ELAPSED TIME SELECTORAUTO: (Spring loaded neutral) automatically starts the chronometer on liftoff.RST: Resets the elapsed time if WOW is present.

Landing Gear Panel

1. DN LOCK REL ButtonMechanically releases the landing gear lever lock.

2. LANDING GEAR Lever UP: Retracts the landing gear.DOWN: extends the landing gear.

Landing gear Panel1

2

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2

ELT PanelON: activates the eLT.ARM: arms the eLT.

eLT Panel


gND PROX g/S INHIB and Lg WRN INHIB Panel

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GND PROX G/S INHIB and LG WRN INHIB Panel

1. GND PROX G/S INHIB ButtonMomentary 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.

2. LG WRN INHIB ButtonPressing 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.

WaTeR Panel and aDS PROBeS Panel1 21 2

WATER Panel and ADS PROBES Panel

1. DUMP ButtonPressing the DUMP button will command potable water drainage. When pushed a white striped bar will illuminate inside the button. Pushing the button a second time will end the dumping process, and the white striped bar will extinguish. In order to drain the potable water tank the aircraft must be airborne with the landing gear up and the drain masts heated. Complete drainage of the tank can only be confi rmed on the Aft Attendant Control Panel.

2. HEATER ButtonPUSH IN: activates the aDS probes heater. a white striped bar illuminates.PUSH OUT: The aDS probes heater works in aUTO mode.

MaSTeR CaUT and WaRN Pushbuttons

12

MASTER CAUT and WARN Pushbuttons

1. MASTER WARN Pushbutton a red light blinks inside the button when a new warning message is displayed on the eICaS. Pressing the button extinguishes the light and silences the associated aural alert (triple chime).

2. MASTER CAUT Pushbutton an amber light blinks inside the button when a new caution message is displayed on the eICaS. Pressing the button extinguishes the light and silences the associated aural alert (single chime).


INTeNTIONaLLY LeFT BLaNK

OVeRHeaD PaNeL MaIN INSTRUMeNT PaNeL Page 30CONTROL PeDeSTaL Page 30

Control PedestalFLIgHT CONTROLS MODe and STaLL WaRNINg Panel ............................. 31POWeRPLaNT and IgNITION Panel .............................................................. 31Multifunction Control Display Unit (MCDU) ...................................................... 32T/O CONFIg Button and eICaS FULL Button ................................................. 33Cursor Control Device (CCD) ........................................................................... 33Speedbrake Lever ............................................................................................ 34Thrust Levers.................................................................................................... 34RaT MaNUaL DePLOY Handle ....................................................................... 35gND PROX FLaP OVRD Switch ..................................................................... 35

eMeRg/PRKNgBRaKe Handle ...................................................................... 35audio Control Panel (aCP) ............................................................................... 36SLaT/FLaP Lever ............................................................................................. 38TRIM Panel....................................................................................................... 38COCKPIT DOOR CONTROL Panel ................................................................. 39IFe/CSS POWeR Panel ................................................................................... 40Printer ............................................................................................................... 40Pa Button .......................................................................................................... 41Disconnect Handles.......................................................................................... 41alternate gear extension Compartment .......................................................... 42

FLaP OVeRRIDe SWITCH

TaKe OFF CONFIg CHeCK BUTTON

THRUST CONTROL

eNgINe CONTROL PaNeL

aILeRON DISCONNeCTeLeVaTOR DISCONNeCT

FLIgHT CONTROL MODe/ STaLL WaRNINg PaNeLS

SPeeD BRaKe LeVeR

SLaT/FLaP SeLeCTOR LeVeR

eMeRgeNCY/PaRKINg BRaKe HaNDLe

MULTIFUNCTION CONTROL DISPLaY UNIT (MCDU)

CURSOR CONTROL DeVICe (CCD)

aUDIO CONTROL PaNeL (aCP)


MULTIFUNCTION CONTROL DISPLaY UNIT (MCDU)


eNgINe CONTROL PaNeL

DISPLaY UNIT (MCDU)

RaT MaNUaL DePLOYRaT MaNUaL DePLOY

FLaP OVeRRIDe SWITCH


TaKe OFF CONFIg CHeCK BUTTON

eICaS FULL PaNeL

THRUST CONTROL


eICaS FULL PaNeL

ReINFORCeD COCKPIT DOOR

TRIM PaNeL

PaSSeNgeR aDDReSS PTTPaSSeNgeR aDDReSS PTT

PRINTeRPRINTeR

aILeRON DISCONNeCT


PaSSeNgeR aDDReSS PTT

SLaT/FLaP SeLeCTOR LeVeR


SLaT/FLaP SeLeCTOR LeVeRSLaT/FLaP SeLeCTOR LeVeR

IFe/CSS POWeR PaNeL

Page 31CONTROL PeDeSTaL

FLIGHT CONTROLS MODE and STALL WARNING Panel

1. FLIGHT CONTROLS MODE Buttons (GUARDED)PUSH IN: Selects DIRECT MODE for the associated fl ight control. a white bar will illuminate in the push button.PUSH OUT: Returns the associated fl ight control to NORMaL MODe.

2. SHAKER CUTOUT ButtonPUSH IN: Cuts out the associated yoke shaker channel.PUSH OUT: allows normal operation of the stick shaker.

FLIgHT CONTROLS MODe and STaLL WaRNINg Panel

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POWERPLANT and IGNITION Panel

1. START/STOP Selector KnobSTOP: Commands the FaDeC to shut down the engine, provided the associated thrust lever is in the IDLe position.RUN: Normal position for engine operation. START: (Momentary action): Initiates the engine start sequence.

2. IGNITION Selector KnobOFF: Deactivates the ignition system on the ground. The FADEC disregards the OFF position in fl ight.AUTO: FaDeC automatically controls the ignition system, depending on engine requirements.OVRD: Directs FaDeC to continuously activate both igniters.

POWeRPLaNT and IgNITION Panel

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Multifunction Control Display Unit (MCDU)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.

1. Line Select Keys (LSK)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 fi rst push will bring the cursor box to the LSK selected, and the second push will open the submenu.

2. ScratchpadThe 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

Multifunction Control Display Unit (MCDU)

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88

6

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page changes.The scratchpad also provides advisory and alerting messages.

3. Function KeysMENU: Displays the menu page.DLK: aCaRS functions.RADIO: Displays the radio page.CB: Displays the circuit breaker page.TRS: Thrust rating select PERF: Displays the performance page.NAV: Displays the navigation page.FPL: Displays the fl ight plan page.PROG: Displays the progress page.RTE: Display the route page.

4. PREV/NEXT PREV: Selects the previous page.NEXT: Selects the next page.

5. BRT/DIM SwitchControls display brightness.

6. Tuning KnobRotating this knob selects frequencies or certain other numeric values.

7. Alphanumeric Buttonsenter alphanumeric inputs.Space key (SP) is used to insert a space.a toggle plus/minus key inserts the corresponding symbol.

8. CLR/DEL ButtonsCLR: Clears alphanumeric entries or messages in the scratchpad.DEL: 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.


1

T/O CONFIg Button eICaS FULL Button

2

T/O CONFIG Button and EICAS FULL Button

1. T/O CONFIG Button: Checks the takeoff confi guration. The takeoff confi guration checks for EMERG/PRKG BRAKE OFF, takeoff fl aps set, spoilers retracted, and pitch trim in the green band.

2. EICAS FULL ButtonPUSH IN: Full eICaS information is presented and auto declutter is inhibited. a white striped bar illuminates in the button.PUSH OUT: enables the automatic eICaS de-clutter logic.NOTE: automatic de-clutter of the eICaS occurs 30 seconds after gear and fl ap/slat retraction if all parameters are displaying normal indications. The following items are de-cluttered from the eICaS:

•Oil pressure.•Oil temperature.•Engine vibration.•Slat position.•Flap position.

•Speed brake position.•Landing gear position (if aUTOBRaKeS are OFF)

•Pitch trim green band.

Cursor Control Device (CCD)

1. Tuning knobOuter and inner knobs select value or mode in the data fi eld enclosed by the cursor.

2. Format location buttonsPlaces the cursor on the associated display.Inboard button is the eICaS. Middle button is the MFD.Outboard button is the PFD

3. Touch PadUsed to move cursor.

4. Enter KeysUsed to select soft keys or menu options.

Cursor Control Device (CCD)

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2

3

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PFD

LeFT RIgHT

MFD

eICaS

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2

PFD

MFD

eICaS

MFD

eICaSeICaSeICaSeICaS

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4 4


Thrust Levers

Thrust LeversMAX: Provides the maximum thrust available. TOGA: Selects takeoff, go around, and maximum continuous thrust ratings.IDLE: Selects idle thrust settings.MIN REV: Provides minimum reverse thrust.MAX REV: 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.NOTE: Positioning the thrust lever between the thrust control quadrant detents selects intermediate thrust settings.

Thrust Reverser TriggerPulling the thrust reverser trigger allows movement of the thrust levers aft of the IDLe stop (on the ground only).

AT DISC ButtonsDisconnects the autothrottles and cancels the autothrottle aural alert.

Thrust LeversSpeedbrake Lever

Speedbrake LeverIn fl ight, 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.NOTE: The speedbrake lever does not move for autoretraction, or for ground spoiler deployment.NOTE: The speedbrake lever is inhibited on the ground.


GND PROX FLAP OVRD Switch

Flap Override Switch (GUARDED)Inhibits triggering of flap alerts in case of landings where flap configuration is other than 5 or FULL.

gND PROX FLaP OVRD Switch

RAT MANUAL DEPLOY Handle

Ram Air Turbine Deployment HandleManually deploys the ram air turbine.

RaT MaNUaL DePLOY Handle

EMERG/PRKNG BRAKE Handle

EMERG/PRKNG BRAKE Handleactuates 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.

eMeRg/PRKNgBRaKe Handle


Audio Control Panel (ACP)

1. MIC Button (6X)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.

2. AUD Button (13X) 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.

3. SAT ButtonSaTCOM is unavailable.

4. PA ButtonThe MIC portion allows transmission to the cabin. The aUD portion allows the fl ight crew to monitor PA transmissions.

5. EMER ButtonInterphone communication with the cabin is enabled over the hot-mic.COCKPIT TO CABIN: Initiates a triple HI/LO chime in the cabin and illuminates the fl ashing red light on the fl ight attendant rainbow lights panel. eMeR CaLL will be seen in the LCD on the aCP. When pushed the green light inside the button fl ashes slowly. When the In-fl ight Crewmember picks up the cabin handset and selects eMeR PILOT the green light will fl ash 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-fl ight crewmember hangs up the handset the connection will be broken.CABIN TO COCKPIT: When the In-fl ight crewmember presses the EMER call button from the fl ight attendant panel, a triple HI/LO chime is sounded in the cockpit. The green light in the EMER button will be fl ashing quickly. When the pilot pushes the eMeR button the green light will be solid green indicating that a connection has been made.

6. RAMP Buttonenables ramp interphone communications over the hot mic.COCKPIT TO RAMP: When RaMP is pushed the green light in the button will fl ash. When the ramp crewmember engages their headset the green light will be steady illuminated. The aCP LCD will read RaMP CaLL.RAMP TO COCKPIT: When a call is initiated from the ramp a single chime will be heard in the cockpit and the RaMP button will fl ash green. When the cockpit crewmember selects the RaMP button the green light will illuminate steady.

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6

8

16

101314

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8101314

audio Control Panel (aCP)

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991111 12


7. CABN Buttonenables cabin crew interphone communications via the hot-mic.COCKPIT TO CABIN: 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.CABIN TO COCKPIT: 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.

8. VOL Knoballows volume adjustment of any selected audio channel.

9. HDPH Buttonallows audio to be heard over the headphone. When selected the green light illuminates.

10. INPH Buttonenables interphone audio. When selected the green light illuminates.

11.SPKR Buttonallows audio to be heard over the speaker. ensure this button illuminates as a part of the oxygen test. When selected the button illuminates.

12. Liquid Crystal Display (LCD)Displays the selected audio channel and digital volume information.

13.MIC/MASK SwitchAUTO (PUSHED IN): automatically turns on the mask microphone when the oxygen mask is removed from its cabinet, or is tested. MASK (PUSHED OUT): 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.

14.BKUP VOL SwitchNORM (PUSH IN): Normal operation mode. BKUP (PUSH OUT): 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.

15.SELCAL ButtonWhen 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. The button will illuminate steady green when active for transmission.

16. ID ButtonActivates a filter that eliminates voice on VOR and ADF audio so the identification can be heard.


TRIM PanelPitch trim priority is backup trim, Captain trim, First Offi cer trim, and the autopilot trim. To prevent trim runaway situations all trim actuation is limited to three seconds of movement. 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.

1. ROLL Trim Switchactuates the roll trim left or right.

2. PITCH BACKUP SWactuates the pitch trim through the back-up channel.Operation of the switch while the autopilot is engaged causes the autopilot to disengage.

3. YAW Trim Switchactuates the yaw trim to left or right.

TRIM Panel

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2

SLAT/FLAP Lever

SLAT/FLAP Selector LeverSelects slat/fl ap position. The lever must be unlatched by and lifting the trigger below the head. Intermediate positions are not enabled. Position 4 is gated. allowable takeoff positions are 1, 2, 3, or 4. Normal landing positions are 5 or FULL.

LEVER POSITION SLAT POSITION FLAP POSITION DETENT/GATED

0 UP UP DeTeNT/STOP

1 MID 1 DeTeNT

2 MID 2 DeTeNT

3 MID MID DeTeNT

4 FULL MID gaTeD

5 FULL MID DeTeNT

FULL FULL FULL DeTeNT/STOP

SLaT/FLaP Lever


COCKPIT DOOR CONTROL Panel

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COCKPIT DOOR CONTROL Panel

1. LOCK Pushbutton (GUARDED)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 fl ight attendant access panel.

2. INHIB Pushbutton (MOMENTARY ACTION)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.

4. SYS 1 CUTOUT Switch (GUARDED)PUSH IN: Disables pitch trim channel 1.PUSH OUT: enables pitch trim channel 1.

5. SYS 2 CUTOUT Switch (GUARDED)PUSH IN: Disables pitch trim channel 2.PUSH OUT: enables pitch trim channel 2.

3. UNLOCKED IndicatorIlluminates ON when the door is unlocked. When access is requested an intermittent chime will sound in the cockpit and the ON light will fl ash on and off.

4. TEST ButtonContinually tests the buzzer while the test button is pressed, regardless of audio selection.


Printer

1. OFF ButtonTurns the printer off and on.

2. FAULT ButtonIlluminates when senses no paper or printer door open.Illuminates in conjunction with test button in case of self-test failure.

3. ALRT RST ButtonCancels a fault indication.

4. TEST ButtonIlluminates all indicators followed by a printout of test results and a test pattern.TeST button indicator bar will remain lit in conjunction with

Printer

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IFE/CSS POWER Panel

1. CABIN IFE Button (GUARDED)Controls the power supply to the LiveTV system and the XM Satellite Digital Radio. a striped bar illuminates in the button when selected off.

2. CSS Button (GUARDED)Controls power to the Cabin Surveillance System. a striped bar illuminates in the button when selected off.

3. IFE RACK Button (GUARDED)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 fl ow 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.

IFe/CSS POWeR Panel

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Disconnect Handles

1. ELEVATOR DISCONNECT HandlePULL: Disconnects the elevator control system. each pilot will control their on-side elevator. The system cannot be reset in fl ight. Disconnection can be confi rmed by a cyan eLeVaTOR DISC eICaS message.

2. AILERON DISCONNECT HandlePULL: Disconnects the aileron control system. The Captain will control his/her on-side aileron, MFS panel 5L/R with artifi cial feel. The First Offi cer will control his/her on-side aileron, MFS panel 4L/R with no artifi cial feel. MFS panel 3L/R is locked out for both pilots. The system cannot be reset in fl ight. Disconnection can be confi rmed by a cyan AILERON DISC eICaS message.

Disconnect Handles

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the FaULT indicator to report a self test failure.

5. LOW PPR ButtonIlluminates when the printer senses the last remaining 10 feet of paper on the paper supply roll

6. PPR ADV ButtonContinuously advances paper while pushbutton is depressed.

PA ButtonPA Button: allows voice communications to the customers regardless of the MIC selection on the aCP.

Passenger address PTT Button


Alternate Gear Extension Compartment

1. Alternate Gear Extension Lever (Two Position)When pulled releases all hydraulic fl uid from the landing gear lines and releases all landing gear uplocks.

2. Alternate Gear Extension Lever Unlock PushbuttonWhen pressed releases the handle from the fully actuated position.

3. Electrical Override SwitchNORMAL: The landing gear lever performs landing gear extension and retraction.GEAR DOWN: Bypasses the landing gear lever and extends the landing gear.alternate gear extention Compartment

EMERGENCY-EXTENSION COCKPIT-QUADRANT LEVER

alternate gear extention Compartment

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Heads Up guidance Display

aLTITUDe

aDI

HSINaVDaTa

aIRSPeeD

ROLL SCaLe

MODe aNNUNCIaTIONS

Heads Up guidance DisplayThe HgS provides an integrated display of air data, navigation, and attitude information on the combiner display. HGS display elements are comprised of symbols, fl ags, and annunciations. Selections made with the guidance Panel are displayed on the PFD and repeated on the HgS combiner.

HGS MenuThe HgS Menu is accessed through the MCDU MeNU button. Pilots give input to and operate the HgS through the lines of text and related LSK’s that follow:•RWY LENGTH• RWY ELEVATION• COMBINER MODE•HUD A3

Heads Up guidance Menu


Yoke

1. TOUCH CONTROL STEERING BUTTON (TCS)Allows adjustment/synchronization of certain FGCSmodes, and manual maneuvering of the aircraft if theautopilot is engaged.Pressing and holding the button causes:• (If A/P is engaged), disengagement of the A/P servos,allowing manual aircraft maneuvering.• Synchronization of the FD guidance cue to theFPV.Release of the button causes:• A/P servos to reengage, if A/P was engaged priorto TCS selection.• FD cue to resume movement to guide towardactive lateral and vertical modes.• FGCS lateral mode: control returns to previouslyselected lateral mode.

• FGCS vertical modeIf VS or FPa were the active vertical modes, the selected VS or FPA synchronizes to the VS or FPA existing at the moment of button release.If aLT was the active vertical mode, the altitude to be held synchronizes to the altitude existing at the moment of buttonrelease, but the selected altitude readout does not change.If FLCH or gS was the active vertical mode, control returns to that mode.

2. AP/TRIM DISCONNECT BUTTON (Momentary Action) Primary means to disengage the autopilot and cancel the autopilot disconnect alert. Disables both HS-aCe channels as long as the button remains pressed.

3. PITCH TRIM SWITCH (SPRING-LOADED TO NEUTRAL)Trims the airplane when the autopilot is not engaged.Captain’s pitch trim switch actuation has priority overthe fi rst offi cer’s.

4. CONTROL WHEEL COMMUNICATIONS SWITCHPTT (momentary): allows VHF transmissions as well asPa announcements.HOT: allows INPH communications over the HOT mic.OFF: allows only audio reception.

5. CHRONOIt has three functions; START-STOP-RESET. The timer appears on the upper right corner of the PFD HSI.

Yoke 1

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Tiller

TillerThe 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.

Documents

FEB 2006 Lights and Switches Guide