AURAL AND VISUAL WARNINGS TABLE OF CONTENTS CHAPTER 3 · 2012. 6. 27. · mach trim fail 14...

DESCRIPTION

General 03−10−1

Central Display System 03−10−2

Crew Alerting Messages 03−10−3

Master Warning/Master Caution Lights 03−10−12

Aurals 03−10−13

Aural Warning Test 03−10−19

Aural Warning Panel 03−10−20

Inhibits 03−10−20

Central Aircraft Information and Maintenance System (CAIMS) 03−10−23

Flight Data Recorder 03−10−25

Stall Warning 03−10−25

Take-off Configuration Warnings 03−10−26

Landing Configuration Warning 03−10−27

EICAS Display 03−10−28

Systems Display (STAT Page) 03−10−29

Reversion Control Panel 03−10−30

PFD Reversion Control 03−10−31

PFD Reversion 03−10−32

EICAS Reversion Control 03−10−33

EICAS Reversion 03−10−34

SG Reversion Control 03−10−35

SG Reversion 03−10−36

EICAS Control Panel 03−10−39

Systems Reversion Control 03−10−40

Message Scrolling 03−10−42

Systems Synoptics 03−10−43STAT Page 03−10−43Bleed/Anti-Ice Synoptic Page 03−10−44Air Conditioning Synoptic Page 03−10−45Hydraulic Synoptic Page 03−10−46AC Electrical Synoptic Page 03−10−47DC Electrical Synoptic Page 03−10−48Fuel Synoptic Page 03−10−49

AURAL AND VISUAL WARNINGS

TABLE OF CONTENTS

CHAPTER 3

03−00−1

REV 41, Jul 08, 2004 Flight Crew Operating Manual

CSP 700−6

Volume 203−00−1

Page

TABLE OF CONTENTS

DESCRIPTIONFlight Controls Synoptic Page 03−10−50

Aural and Visual Warning EICAS Messages 03−10−51

EMS CIRCUIT PROTECTION

CB − Ind/Record System 03−20−1

CB − CAIMS System 03−20−2


TABLE OF CONTENTS

REV 41, Jul 08, 2004Flight Crew Operating Manual

CSP 700−6

Volume 203−00−2

Page

GENERAL

The aural and visual warning system provides indications to warn of potentially unsafe operatingconditions or airplane configurations, system malfunctions, and non-normal situations. Indicationscan be generated by the following:

• Crew alerting sub-system within the Engine Indication and Crew Alerting System (EICAS).• Enhanced Ground Proximity Warning System (EGPWS).• Weather Radar (WX) system.• Traffic alert and Collision Avoidance System (TCAS).• Altitude alert portion of the Air Data Computer (ADC).• Stick shaker portion of the Stall Protection System (SPS).

EICAS provides crew with the necessary displays for airplane engine control and monitoring, controlsurface monitoring and all major sub-system synoptic displays. During normal operation, the engineand control surface information is displayed on the EICAS display unit (DU3) and the systemsynoptic information is displayed on the SYSTEMS display (DU4).

GF

0310

_001

DU 1 DU 2 DU 3 DU 4 DU 5 DU 6

PFD 1 MFD 1 EICAS SYSTEMS MFD 2 PFD 2

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3

VAPP VNAVASELAP1HDG 10400

29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4

TOTALFUEL(LBS) 41550

1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2

N2FF (PPH)OIL TEMPOIL PRESS

93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT

OIL QTY (QTS)ENGAPURES

RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

EICAS provides display of:

• Primary engine parameters• Fuel quantities• Flaps/slats/spoilers positions• Crew Alerting System (CAS) messages

• Secondary engine parameters• Landing gear position• Surface trim indication

SYSTEMS provides synoptics display of:

• Bleed/Anti-Ice Air• Hydraulics• DC Electrical• Flight Controls

• Air Conditioning• AC Electrical• Fuel• Status



CSP 700−6

Volume 203−10−1

CENTRAL DISPLAY SYSTEM

The central display system provides crew with displays for aircraft control, navigation, engine controland monitoring and systems synoptic. Other systems information provided for display are WXdisplay, TCAS, EGPWS and Lightning Sensor System (LSS) display.

Airplane data is transmitted from airplane systems to 4 dual channel, Data Acquisition Units (DAU),through the Avionics Standard Communication Bus (ASCB), to 3 Integrated Avionics Computers(IAC), to the Display Units (DU).

The 4 dual channel DAUs operate with one channel active and the other channel on standby, withboth channels updating data at the same time.

The ASCB is the principal communications network interconnecting the system components. Datatraffic flow on the ASCB is managed by 3 bus controllers (one bus controller in each IAC). Only onebus controller is in control at a time, with the other 2 in standby status.

The three IACs, each contain a Symbol Generator (SG) and a Fault Warning Computer (FWC). TheSGs process data from various sources and output the data to the 6 DUs. The FWC comparessensor input data, verifies all critical display data and displays warning, caution, advisory and statusmessages as applicable.


The IACs perform the following functions:

IAC 1 IAC 2 IAC 3

EFIS, EICAS, FWC, CAIMS EFIS, EICAS, FWC, CAIMS EFIS, EICAS, FWC, CAIMS

Tone/Aural generator Tone/Aural generator LASERTRACK (if installed)

Flight Management System Flight Management System FMS 3 (if installed)

Autothrottle Autothrottle

AFCS AFCS



CSP 700−6

Volume 203−10−2

CREW ALERTING MESSAGES

The crew alerting system portion of EICAS continually monitors all airplane systems. If anoperationally significant fault occurs on a system, EICAS displays a crew alerting message on theEICAS display unit. In addition to the display messages, some crew alerts are also indicated by auraltones, voice advisories, MASTER WARNING and MASTER CAUTION lights.

All crew alerting system messages are divided into one of four categories and in the following priority:

Warning messages are generated when immediate recognition and corrective orcompensatory action is required. They are the most urgent type of crew alerts. They alwaysappear at the top of the message stack on the EICAS primary display. All warnings cause theMASTER WARNING lights on the glareshield to flash and have an aural alert consisting of aunique tone or a triple chime plus a voice advisory. Once acknowledged flashing stops.

L ENG FIRE

Glareshield EICAS Display Aural

"LEFT ENGINE FIRE"Triple Chime

MASTERWARNING/CAUTION

WARNING

CAUTION

Warning messages cannot be removed from view, unless the applicable failure has beenrectified. If a failure is rectified, messages which appeared below the deleted message, willmove up one line. When a new fault occurs, the new message will move to the top of the stack.Caution messages are generated when immediate crew awareness is required andsubsequent crew action will be required. Caution messages appear immediately below thewarnings in the message stack on the EICAS display. All cautions cause the MASTERCAUTION lights on the glareshield to flash and have an aural alert consisting of a singlechime. Once acknowledged flashing stops .

L ENG SHUTDOWN

Glareshield EICAS Display Aural

Single Chime

GF

0310

_005


WARNING

CAUTION

Caution messages can be paged and scrolled from view, using SCROLL knob on EICAScontrol panel. If a new abnormal situation occurs, the corresponding caution message will flashand the remaining messages will remain steady. To view all of the non-displayed messages,turn SCROLL knob on the EICAS control panel. If a new message is posted, it will bedisplayed at the top of the stack.

EICAS Control Panel

Scroll Knob



CSP 700−6

Volume 203−10−3

CREW ALERTING MESSAGES (CONT'D)Advisory messages are generated when crew awareness is required and subsequent crewaction may be required. Advisory messages appear immediately below the cautions in themessage stack on the EICAS display. When a new advisory message appears, it will flash for5 seconds, then steady. There is no aural alert for advisory messages.

GF

0310

_007

L REVERSER FAULT

EICAS Display

Advisory messages can be paged and scrolled from view, using SCROLL knob on EICAScontrol panel. To view all of the non-displayed messages, turn SCROLL knob on the EICAScontrol panel.

Status messages are generated to indicate non-normal pilot selections and are reminders tothe crew. They are set in the message stack below the advisories. There is no aural alert forstatus messages.

GF

0310

_008

L ENG SOV CLSD

EICAS Display

Status messages can be scrolled from view, using SCROLL knob on EICAS control panel.To view all of the non-displayed messages, turn SCROLL knob on the EICAS control panel.

The EICAS message window displays up to 14 messages with the Gear/Slats/Flaps pop updisplayed. With the Gear/Slats/Flaps pop up not displayed, the window can display up to24 messages.

GF

0310

_009

TOTALFUEL(LBS)

789789

N1

CRZEPR

73.373.3

1.651.65

NU TRIMSFF (PPH)OIL TEMPOIL PRESS

93.45750 115 81

ITT

1460041550

10000 2350

14600 ND STAB RUDDERNL

LWD RWD

NR

1.541.54

7.5

GEAR

OUT

30

DN 789789

N1

CRZEPR

73.373.3

1.651.65


93.45750 115 81

93.45750 115 81

ITT

1.541.54

7.2

93.45750 115 81

DN DN

TOTALFUEL(LBS)

NU TRIMS

1460041550

10000 2350

14600 ND STAB RUDDERNL

LWD RWD

NR

14 Messages

Gear/Slats/Flaps Pop Up

24 Messages

N2



CSP 700−6

Volume 203−10−4

CREW ALERTING MESSAGES (CONT'D)

If there are non-displayed messages above the top of the display or below the bottom of the displayXXX↑ messages ↓XXX symbols will appear at the bottom of message window. The number ofnon-displayed messages will be indicated beside the ↑ or ↓ x arrows. If there are no more messages,END symbol will appear below last message. The colour of the status line corresponds to the highestlevel of messages not displayed. Warning messages are not part of the colour logic.

GF

0310

_010

789789

ITT

789789

AC BUS 1 FAIL

LATERAL MODE OFF

L REVERSER UNLKD

MACH TRIM FAIL

14 MESSAGES 6

NW STEERING FAIL

MACH TRIM FAIL789789

ITT

PITCH DISC FAULTR OIL FILTER

R ENG BLEED OFFTRIM AIR OFF

IAC 1 WOW INOP

R OIL LO PRESSR FADEC FAILN1

END

10 MESSAGES 0

14 MESSAGES 6 10 MESSAGES 0

END



CSP 700−6

Volume 203−10−5


GF

0310

_011

APU FIREAPU OVERSPEED 5APU OVERTEMP 5

BRAKE OVHT 9

CABIN ALT 2CABIN DELTA P 2CHECK PFD 11CONFIG AIL TRIM 10CONFIG RUD TRIM 10CONFIG SLAT/FLAP 10CONFIG SPOILERS 10CONFIG STAB TRIM 10

DUAL ENGINE OUT 18

EMER PWR ONLY 7

GEAR 15

L ENG FIRE 9L OIL LO PRESS 18L REVERSER UNLKD 18

MLG BAY OVHT 9

NORM BRAKE FAIL 15

PARK/EMER BRAKE ON 15

R ENG FIRE 9R OIL LO PRESS 18R REVERSER UNLKD 18

SMOKE AFT LAV 9SMOKE AVIONICS BAY 9SMOKE BAGGAGE 9SMOKE FWD LAVSMOKE CABINSMOKE CLOSETSMOKE CLOSET FWDSMOKE CLOSET AFT

WING A/ICE OVHT

EICAS WARNING MESSAGES

Chapt. Ref.

NOTEA single message or a combined message can be displayed on a message line, up to a maximum of 18 characters.Example: L REVERSER UNLKD or R REVERSER UNLKD or L−R REVERSER UNLKD

9

99999

9



CSP 700−6

Volume 203−10−6


AC BUS 1 FAIL 7 AC BUS 2 FAIL 7AC BUS 3 FAILAC BUS 4 FAILAC ESS BUS FAILADC 1 MSCMP 11ADC 2 MISCMPADC 3 MISCMPAFCS ENGAGE INVALAFT XFER FAILAFT XFER OFF SCHEDALL ADC MISCMPALL IRS MISCMPAP TRIM IS LWDAP TRIM IS RWDAP TRIM IS NDAP TRIM IS NUAP PITCH TRIM FAILAPU BATT FAILAPU BLEED SYS FAILAPU DOOR FAILAPU EGT SENSORSAPU FIRE FAILAPU FUEL SOVAPU GEN OVERHEATAPU GEN OVLDAPU OIL HI TEMPAPU OIL LO PRESSAPU REVERSE FLOWASCB FAILA/T NOT IN HOLDAUTOBRAKE FAILAUTO PRESS FAILAV BATT FAIL

BATT BUS FAILBATT MASTER OFFBRAKE 50% DGRADED

CABIN ALTCARGO DOORCAT 2 INVALIDCB TRIP AC FEEDCB TRIP DC FEEDCHECK DU 1CHECK DU 2CHECK DU 3CHECK DU 4CHECK DU 5CHECK DU 6CPLT BRAKE FAULTCTR FUEL XFER FAIL

DC BUS 1 FAILDC BUS 2 FAILDC EMER BUS FAIL

Chapt. Ref.EICAS CAUTION MESSAGESDC ESS BUS FAIL 7DISP CTRLS FAILDOOR SYS FAIL

ELT TRANSMITTIGEMER DEPRESSEMER LIGHTS OFFELEVATOR SPLIT

FIRE BTL1 LO PRESSFIRE BTL2 LO PRESSFLAP FAILFLT SPOILERS FAILFLT SPLR DEPLOYEDFUEL COMPUTR FAILFUEL IMBALANCEFUEL LO QTYFUEL TEMP SENSOR FUEL UNIT MISMATCH

GEAR DISAGREEGEAR SYS FAILGEN 1 OVLDGEN 2 OVLDGEN 3 OVLDGEN 4 OVLDGND LIFT DUMP

HUD FAILHUD MISCOMPAREHYD 1 HI TEMPHYD 2 HI TEMPHYD 3 HI TEMPHYD 1 LO PRESSHYD 2 LO PRESSHYD 3 LO PRESSHYD 1 LO QTYHYD 2 LO QTYHYD 3 LO QTYHYD 3 OVERFILLEDHYD RAT PUMP FAIL

IAC 1 OVHTIAC 2 OVHTIAC 3 OVHTICE ICE DETECTOR FAILINBD BRK LO PRESSIRS 1 MSCMPIRS 2 MSCMPIRS 3 MSCMPIRS 1 OVHTIRS 2 OVHTIRS 3 OVHTIRS 1 SET HDGIRS 2 SET HDGIRS 3 SET HDG

Chapt. Ref.

NOTEA single message or a combined message can be displayed on a message line, up to a maximum of 18 characters.

GF

0310

_012

Example: DU 1 FAN or DU 2 FAN or DU 3 FAN or DU 1−2−3 FAN

FUEL XFER ON FUEL XFER ONFUEL XFER FAIL FUEL XFER FAIL

777

1111412121111444447255957755211181527

7715

2117773333331512

777

3

16

1

62

10

99101010121212121212121212

1515777710

11111313131313131313131313

333141415111111111111111111



CSP 700−6

Volume 203−10−7


EICAS CAUTION MESSAGES

Chapt. Ref.Chapt. Ref.

LARGE SERV DOORSL AOA HEAT FAILL BLEED LEAKL BLEED SYS FAILL COWL A/ICE FAILL EMER EXITL ENG FIRE FAILL ENG FLAMEOUTL ENG FUEL LO TEMPL ENG FUEL SOVL ENGINE OVHTL ENG OVERSPEDL ENG SAV FAILL FADEC FAILL FADEC N1 CTLL FADEC OVHTL FUEL FILTERL FUEL LO PRESSL FUEL RECIRC FAILL HYD SOV FAILL INBD BRAKE FAILL MAIN GEAR DOORL OIL LO QTYL OUTBD BRAKE FAILL PACK AUTO FAILL PACK FAILL PACK TEMPL PRI FUEL PUMPSL REVERSER FAILL REV LOCK FAILL START ABORTEDL THROTTLE FAILL WINDOW HEAT FAILL WING A/ICE FAILL WING FULLL WSHLD HEAT FAIL

MACH TRIM FAILMLG BAY OVHT FAIL

NOSE DOORNOSE STEER FAIL

OUTBD BRK LO PRESSOXYGEN LO QTY

Chapt. Ref.

PARK/EMER BRAKE ONPASSENGER DOORPITOT 1 HT FAILPITOT 2 HT FAILPITOT 3 HT FAILPLT BRAKE FAULT

RAT GEN FAILR AOA HEAT FAILR BLEED LEAKR BLEED SYS FAILR COWL A/ICE FAILR EMER EXITR ENG FIRE FAILR ENG FLAMEOUTR ENG FUEL LO TEMPR ENG FUEL SOVR ENGINE OVHTR ENG OVERSPEDR ENG SAV FAILR FADEC FAILR FADEC N1 CTLR FADEC OVHTR FUEL FILTERR FUEL LO PRESSR FUEL RECIRC FAILR HYD SOV FAILR INBD BRAKE FAILR MAIN GEAR DOORR OIL LO QTYR OUTBD BRAKE FAILR PACK AUTO FAILR PACK FAILR PACK TEMPR PRI FUEL PUMPSR REVERSER FAILR REV LOCK FAILR START ABORTEDR THROTTLE FAILR WINDOW HEAT FAILR WING A/ICE FAILR WING FULLR WSHLD HEAT FAILROLL SELECTROLL SPOILERS FAILRUD AUTHORITY HIGHRUD AUTHORITY LOWRUD LIMITER FAIL

Note:A single message or a combined message can be displayed on a message line, up to a maximum of 18 characters.Example: L HYD SOV FAIL or R HYD SOV FAIL or L−R HYD SOV FAIL

SG 1 FAILSG 2 FAILSG 3 FAILSLAT − FLAP FAILSLAT−FLAP FAULTSMALL SERV DOORSSMOKE AFT LAV FAILSMOKE AV BAY FAILSMOKE BAGGAGE FAILSMOKE CABIN FAILSMOKE CLOSET FAILSMOKE CLO FWD FAILSMOKE CLO AFT FAILSMOKE FWD LAV FAILSPLR LEVER FAILSTAB TRIMSTALL PROTECT FAILSTBY PITOT HT FAIL

TRIM AIR FAILTRIM AIR LEAK

UNCOMMANDED BRAKEWING A/ICE LO HEATWING A/ICE LEAKWING FUEL HI TEMPWING FUEL LO TEMPWING TO CTR LEAKWOW FAIL

XBLEED FAIL

YD 1 FAILYD 2 FAILYD OFF

GF

0310

_013

115222191818181818181818181818121315151815222121818181814141214

109

1515

158

15114141415

7152221918181818181818181818181213151518152221218181818141412141010101010

333101019999999910101014

22

15141412121215

2

444



CSP 700−6

Volume 203−10−8


AC BUS 1 XFER FAULTAC BUS 2 XFER FAULTAC BUS 3 XFER FAULTAC BUS 4 XFER FAULTADC 1 FAILADC 2 FAILADC 3 FAILADC 1 DEGRADEDADC 2 DEGRADEDADC 3 DEGRADEDAFCS 1 FAILAFCS 2 FAILAFT R/D VALVE OPENAFT XFER FAULTAFT XFER OFF SCHEDAP 1 FAILAP 2 FAILAPU BATT CHGR FAILAPU BLEED DISABLEDAPU FADEC FAILAPU FAULTAPU FIRE FAULTAPU GEN FAILAPU IN BITEAPU NOT AVAILABLEAPU OIL LO QTYAPU SHUTDOWNAPU SQUIB 1 FAILAPU SQUIB 2 FAILASCB FAULTASCB CTLR 1 FAILASCB CTLR 2 FAILASCB CTLR 3 FAILAT 1 FAILAT 2 FAILAT ADC MISCMPAT IRS MISCMPATS ENVELOPE AUTO PRESS FAULTAV BATT CHGR FAILAVIONIC FAN FAIL

BATT BUS XFER FAULTBATT EMER PWR ONBLEED MISCONFIGBRAKE FAULTBRAKE TEMP

CAB ALT LEVEL HICB TRIPCHECKLIST MISMATCHCTR XFER FAULT

EICAS ADVISORY MESSAGES

Chapt. Ref.DAU 1A FAILDAU 1B FAILDAU 2A FAILDAU 2B FAILDAU 3A FAILDAU 3B FAILDAU 4A FAILDAU 4B FAILDC BUS 1 XFER FAULTDC BUS 2 XFER FAULTDC ESS XFER FAULTDU 1−2−3−4−5−6 FAN

ELEC SYS FAULTENG SYNC FAILENG SYNC LIMITESS TRU 1 FAILESS TRU 2 FAILEXT AC PWR AVAILEXT DC PWR AVAIL

FCU FAULTFDR ACCEL FAIL FDR FAILFIRE SYS FAULTFLAP DRIVE OVHTFLAP HALFSPDFLT SPOILERS FAULTFMS 1 FAILFMS 2 FAILFMS 3 FAILFUEL COMPUTR FAULTFUEL QTY DEGRADEDFUEL RECIRC ON

GEAR SYS FAULTGEN 1 FAILGEN 2 FAILGEN 3 FAILGEN 4 FAILGND LIFT DUMPGND PROX FAILGPWS SYSTEM FAIL

HUD FAN FAILHUD MISALIGNHUMIDIFIER FAILHYD EDP 1A FAILHYD EDP 2A FAILHYD PUMP 3A FAILHYD PUMP 1B FAILHYD PUMP 2B FAILHYD PUMP 3B FAIL

Chapt. Ref.

NOTEA single message or a combined message can be displayed on a message line, up to a maximum of 18 characters.Example: AFCS 1 FAIL or AFCS 2 FAIL or AFCS 1−2 FAIL

GF

0310

_014

FUEL XFER ON

XFER VALVE OPENXFER VALVE OPEN

FUEL XFER ON

77771111111111114412121244725597755599111111111818181818272

7721515

27312

333333337773

718187777

101111910101017171712121212121212

157777101717

112131313131313

11



CSP 700−6

Volume 203−10−9


RAM AIR FAILRAT GEN ONRECIRC FAN FAILREVRSION CTLR FAILR AUX FUEL PUMP R BLEED FAULTR COWL A/ICE FAULTR ENG FIRE FAULTR ENG SQUIB 1 FAILR ENG SQUIB 2 FAILR FADEC FAULTR FUEL FILTERR OIL FILTERR PACK FAULTR PRI FUELPUMPR POBE MON FAILR R/D VALVE OPENR REVERSER FAULTR REV LOCK FAULTRUD AUTHORITY SAFERUD LIMITER FAULT

SAFETY VALVE OPENSELCAL HF 1SELCAL HF 2SELCAL VHF 1SELCAL VHF 2SELCAL VHF 3SET LDG ELEVSHAKER 1 FAILSHAKER 2 FAILSLAT DRIVE OVHTSLAT HALFSPDSLAT/FLAP BITSLAT/FLAP HALFSPDSPLRS/STAB IN TESTSTAB CH 1 FAILSTAB CH 2 FAILSTALL WARN ADVANCESTALL WARN BASIC

TAT 1 FAIL TAT 2 FAIL TAT 3 FAILTAT HT 1 FAIL TAT HT 2 FAIL TAT HT 3 FAILTERR FAIL TRIM AIR FAULTTRU 1 FAILTRU 2 FAIL

WINDSHEAR FAILWINDMILL ENVELOPEWING A/ICE FAULTWING A/ICE SENSORWOW FAULT

XFEED VALVE FAIL

YD HEAT 1 FAILYD HEAT 2 FAILYD NOT CENTERED

Chapt. Ref.

EICAS ADVISORY

MESSAGES

IAC 1 AURAL FAILIAC 2 AURAL FAILIAC 1 INVALIDIAC 2 INVALIDIAC 3 INVALIDIAC 1 MEM FULLIAC 2 MEM FULLIAC 3 MEM FULLIAC 1 WOW INOPIAC 2 WOW INOPIAC 3 WOW INOPIAC CONFIG MISMTCHICEICE DETECTOR FAULTIRS 1 AUX FAILIRS 2 AUX FAILIRS 3 AUX FAILIRS 1 FAILIRS 2 FAILIRS 3 FAILIRS 1 NO ALIGNIRS 2 NO ALIGNIRS 3 NO ALIGNIRS 1 AUX PWRIRS 2 AUX PWRIRS 3 AUX PWR

L AUX FUEL PUMPL BLEED FAULTL COWL A/ICE FAULTL ENG FIRE FAULTL ENG SQUIB 1 FAILL ENG SQUIB 2 FAILL FADEC FAULTL FUEL FILTERL OIL FILTERL PACK FAULTL PRI FUELPUMPL PROBE MON FAILL R/D VALVE OPENL REVERSER FAULTL REV LOCK FAULTLTRK FAIL

MACH XDUCER FAULTMAN PRESS FAULTMFD CTLR 1 FAILMFD CTLR 2 FAILMLG BAY OVHT FAULT

NAV LIGHTS FAILNO TAKEOFF

OIL RES LO QTYOUTFLOW VLV 1 FAILOUTFLOW VLV 2 FAIL

PASSENGER OXY ONPITCH DISC FAULT PITCH FEEL FAULT

Chapt. Ref.

NOTEA single message or a combined message can be displayed on a message line, up to a maximum of 18 characters.Example: MFD CTLR 1 FAIL or MFD CTLR 2 FAIL or MFD 1−2 CTLR FAIL G

F03

10_0

15

33111111111111151515111414111111111111111111111111

122149991818182121412181817

102111115

163

1822

81010

272312214999181818212141218181010

26666621010101010101010101010

14141414141417277

1818141415

12

444



CSP 700−6

Volume 203−10−10


PARK/EMER BRAKE ONPLT ROLL SPLRS

RAT GEN OFFRAM AIR ONRECIRC FAN OFFR AUX PUMPS OFFR COWL A/ICE AUTOR COWL A/ICE ONR ENG BLEED ONR ENG BLEED OFFR ENG SOVS CLSDR ENG SHUTDOWNR FADEC NI CTL

Chapt. Ref.AC BUS1 MAN OFF AC BUS 2 MAN OFFAC BUS 3 MAN OFFAC BUS 4 MAN OFFAFT FUEL XFER OFFAFT FUEL XFER ONAPU BLEED OFFAPU BLEED ONAPU FUEL SOV CLSDAPU GEN OFFAPU SOVS CLSDAUTOBRAKE HIAUTOBRAKE LOWAUTOBRAKE MED

Chapt. Ref.HUD ONHYD PUMP 1B OFFHYD PUMP 1B ONHYD PUMP 2B OFFHYD PUMP 2B ONHYD PUMP 3A OFFHYD PUMP 3B OFFHYD 3B ONHIGH PRESS RATE

IAC 1 AURAL MUTEIAIC 2 AURAL MUTEIRS 1 IN ATTIRS 2 IN ATT

Chapt. Ref.

EICAS STATUS MESSAGES

77771212551279151515

11131313131313132

3311717

1510

722121414181891818

R FUEL SOV CLSDR FUEL RECIRC ONR HYD SOV CLSDR IGNITION ONR PACK HIGH FLOWR PACK LOW FLOW R PACK MAN TEMPR PACK OFFR PRI PUMPS OFFR WSHLD HEAT OFF

SEAT BELTS SIGN ONSTAB CH 1 OFFSTAB CH 2 OFF

TRIM AIR OFF

WING A/ICE AUTOWING A/ICE ONWING FUEL XFER OFFWING XBLEED FROM LWING XBLEED FROM R

XBLEED CLOSEDXBLEED OPENXFEED VALVE OPEN

AUX PRESS ON

BATT BUS MAN OFF

CPLT ROLL SPLRS

DC BUS 1 MAN OFFDC BUS 2 MAN OFFDC ESS BUS MAN OFFDITCHING ON

EGPWS TERR OFF EMER LIGHTS ONEXT AC PWR ONEXT DC PWR ON

GEAR HORN MUTEDGEN 1 OFFGEN 2 OFFGEN 3 OFFGEN 4 OFFGLD MANUAL ARMGND LIFT DUMP OFFGPWS FLAP OVRDGPWS G/S MUTED

IRS 3 IN ATT

LDG ELEV MANL AUX PUMP OFFL COWL A/ICE AUTOL COWL A/ICE ONL ENG BLEED ONL ENG BLEED OFFL ENG SOVS CLSDL ENG SHUTDOWNL FADEC NI CTLL FUEL SOV CLSDL FUEL RECIRC ONL HYD SOV CLSDL IGNITION ONL PACK HIGH FLOWL PACK LOW FLOWL PACK MAN TEMPL PACK OFFL PRI PUMPS OFFL WSHLD HEAT OFF

MAN PRESS CONTROL

NO SMKG SIGN ONNOSE STEER OFFOUTFLOW VLV 1 CLSDOUTFLOW VLV 2 CLSD

NOTEA single message or a combined message can be displayed on a message line, up to a maximum of 18 characters.Example: L IGNITION ON or R IGNITION ON or L−R IGNITION ON

GF

0310

_016

FUEL XFER ON FUEL XFER ON

2

710

7772

171677

1212

15777710101717

17

2121414181891818121291822221214

2

161522

121291822221214

161010

2

1414121212

2212



CSP 700−6

Volume 203−10−11

MASTER WARNING/MASTER CAUTION LIGHTS

Two MASTER WARNING switch/lights come on flashing when any warning occurs. Pushing eitherMASTER WARNING switch/light extinguishes both MASTER WARNING lights for the duration of thatwarning and resets the lights for future warnings.

GF

0310

_017


WARNINGROLL SPLRS

PLT CONT

ROLLSELPLT

ROLL


WARNINGROLL SPLRS

CPLT CONT

ROLLSEL

CPLTROLL

RAD BAROMINIMUMS NAV SCR BARO SET

PUSH STD

HPaIN RAD BAROMINIMUMS NAV SCR BARO SET

PUSH STD

HPaINSPD

PUSH CHG

MANFMSCRS 1

PUSH DCT

HDG

PUSH SYNC

DN

UP

ALT CRS 2

PUSH DCT

CAUTION CAUTION

WARNING

CAUTION

WARNING

CAUTION

Pushing the MASTER WARNING also silences the aural warnings except for the following cases:

• Stall warnings• EGPWS/TCAS (voices and aurals)• Overspeed Continuous Horn (A-chord)• Trim clacker• Autopilot disconnect cavalry charge

• Configuration warnings• Gear Horn• Autothrottle disconnect• Windshear warning

Two MASTER CAUTION switch/lights come on flashing when any caution occurs. Pushing eitherMASTER CAUTION switch/light extinguishes both MASTER CAUTION lights for the duration of thatcaution and resets the lights for future cautions.

GF

0310

_018


ROLL SPLRS

PLT CONT

ROLLSELPLT

ROLL


ROLL SPLRS

CPLT CONT

ROLLSEL

CPLTROLL

RAD BAROMINIMUMS NAV SCR BARO SET

PUSH STD

HPaIN RAD BAROMINIMUMS NAV SCR BARO SET

PUSH STD

HPaINSPD

PUSH CHG

MANFMSCRS 1

PUSH DCT

HDG

PUSH SYNC

DN

UP

ALT CRS 2

PUSH DCT

CAUTION

WARNING

CAUTION

WARNING

WARNING

CAUTION

WARNING

CAUTION

Pushing the MASTER CAUTION will not silence the following:

• EGPWS and TCAS voice alerts • Altitude alert (C-chord) aural


REV 52, Nov 10, 2006Flight Crew Operating Manual

CSP 700−6

Volume 203−10−12

AURALS

Aurals and tones that call attention to warnings and cautions.

Aural/Tone Indication Chapter Reference

C-chord (1 second) Altitude alert Chapter 11, Flight Instruments

Cavalry Charge Autopilot disconnect Chapter 4, Automatic FlightControl System

Caution (Single chime) Tone that precedes an aircraftsystem caution message

Chapters 2 through 18

Clacker Excessive stabilizer movement Chapter 10, Flight Controls

Double C-chord VNAV vertical track alert Chapter 4, Automatic FlightControl System

Horn Continuous (A-chord) Overspeed warning Chapter 4, Automatic FlightControl System Chapter 10,Flight Controls

Stick Shaker Stall Chapter 10, Flight Controls

Voice Voice aural warnings Chapters 2 through 18

Warning (Triple chime) Tone that precedes an aircraftsystem warning message and/orvoice advisory

Chapters 2 through 18

Whoop − Whoop EGPWS mode 1 or 2 (excessivedescent rate or excessive closurerate) (if installed)

EGPWS, Chapter 17, Navigation

Voice Messages

(Airplanes 9002, 9005 to 9066 not incorporating SB 700-34-013, Traffic Alert and CollisionAvoidance System − Change 7 Software Upgrade)

The following is an alphabetical list of Voice messages:

VOICE MESSAGE − ALPHABETICAL

W = Warning

SYS = System

Voice Message Type ChapterRef.

EICAS/ PFD INDICATION

Approaching Decision Height(DH)

SYS 17 Approaching DH selected on PFD

Approaching Minimums SYS 17 Approaching minimum altitude selected onPFD

APU FIRE W 5 APU FIRE

Bank Angle SYS 17 EGPWS − Excessive bank angle on finalapproach

CABIN ALTITUDE W 2 CABIN ALT / Cabin altitude >9000 feet



CSP 700−6

Volume 203−10−13

AURALS (CONT'D)


W = Warning

SYS = System



Caution Obstacle SYS 17 EGPWS − An obstacle threat has beendetected.

Caution Terrain SYS 17 EGPWS − A terrain threat has beendetected.

Cavalry Charge SYS 4 Autopilot disconnect

Clear of Conflict SYS 17 TCAS − Encounter has ended andseparation increasing

Climb, Climb, Climb SYS 17 TCAS − Indicates a climb command.Displays a green fly-to Pitch Target Zone(PTZ) and a red Pitch Avoidance Zone (PAZ)on both PFD ADIs

Climb, Climb, Now SYS 17 TCAS − Following a descent command, aclimb is necessary to provide adequateseparation

Climb, Crossing Climb SYS 17 TCAS − Indicates a climb command.Displays a green fly-to PTZ and a red PAZon both PFD ADIs. Aircraft flight path willcross intruder’s altitude

Decision Height SYS 11 At DH selected on PFD

Descend, Crossing, Descend SYS 17 TCAS − Indicates a descend command.Displays a green fly-to PTZ and a red PAZon both PFD ADIs. Aircraft flight path willcross intruder’s altitude

Descend, Descend, Descend SYS 17 TCAS − Indicates a descend command.Displays a green fly-to PTZ and a red PAZon both PFD ADIs

Descend, Descend, Now SYS 17 TCAS − Following a climb command, adescent is necessary to provide adequateseparation

Don’t Sink SYS 17 EGPWS − Sink after take-off

Gear, Gear SYS 15 Gear not all fully down and locked during anattempted landing

GEAR BAY OVERHEAT W 9 MLG BAY OVHT / Main wheel well overheat

Glideslope SYS 17 EGPWS − Excessive deviation belowglideslope

Increase Climb SYS 17 TCAS − PTZ command increases to increaseclimb rate



CSP 700−6

Volume 203−10−14

AURALS (CONT'D)


W = Warning

SYS = System



Increase Descent SYS 17 TCAS − PTZ command decreases toincrease descent rate

LEFT ENGINE FIRE W 9 L ENG FIRE

Minimums SYS 17 At minimum altitude selected on PFD

Monitor Vertical Speed SYS 17 TCAS − Monitor pitch attitude to keep pitchattitude inside PTZ and away from PAZ

NO TAKEOFF W 10&15

CONFIG AIL TRIMCONFIG RUD TRIMCONFIG SLATS/FLAPSCONFIG SPOILERSCONFIG STAB TRIMPARK BRAKE ON

Obstacle, Obstacle SYS 17 EGPWS − Excessive obstacle closure

Pull Up SYS 17 EGPWS − Corrective action after excessivedescent rate during approach

Reduce Climb SYS 17 TCAS − PTZ command decreases todecrease climb rate

Reduce Descent SYS 17 TCAS − PTZ command increases todecrease descent rate

RIGHT ENGINE FIRE W 9 R ENG FIRE

Selcal SYS 6 SELCAL HF, SELCAL VHF 1, SELCALVHF 2, SELCAL VHF 3 (On airplanes withSB 700-23-002 incorprated)

Sink Rate SYS 17 EGPWS − Excessive descent rate duringapproach

SMOKE W 9 SMOKE BAGGAGESMOKE FWD LAVSMOKE AFT LAVSMOKE CLOSETSMOKE AVIONICS BAY

Terrain, Terrain SYS 17 EGPWS − Excessive terrain closure

Too Low Flap SYS 17 EGPWS − Insufficient flap, low altitude

Too Low Gear SYS 17 EGPWS − Gear up, low altitude

Too Low Obstacle SYS 17 EGPWS − Obstacle closure low altitude

Too Low Terrain SYS 17 EGPWS − Terrain closure low altitude



CSP 700−6

Volume 203−10−15

AURALS (CONT'D)


W = Warning

SYS = System



Traffic, Traffic SYS 17 TCAS − Conduct visual search for intruder

Windshear,Windshear SYS 17 EGPWS − WINDSHR (decreasingperformance)

500, 100, 50, 30 SYS 17 EGPWS − Descending altitude callouts

Voice Messages

(Airplanes 9067 and subsequent and airplanes 9002, 9005 to 9066 incorporating SB 700-34-013,Traffic Alert and Collision Avoidance System − Change 7 Software Upgrade)

The following is an alphabetical list of Voice messages:


W = Warning

SYS = System



Adjust Vertical Speed, Adjust SYS 17 TCAS − Monitor vertical speed to keepaircraft inside PTZ and away from PAZ.

Approaching Decision Height(DH)

SYS 17 Approaching DH selected on PFD

Approaching Minimums SYS 17 Approaching minimum altitude selected onPFD

APU FIRE W 5 APU FIRE

Bank Angle SYS 17 EGPWS − Excessive bank angle on finalapproach

CABIN ALTITUDE W 2 CABIN ALT / Cabin altitude >9000 feet

Caution Obstacle SYS 17 EGPWS − An obstacle threat has beendetected.

Caution Terrain SYS 17 EGPWS − A terrain threat has beendetected.

Cavalry Charge SYS 4 Autopilot disconnect

Clear of Conflict SYS 17 TCAS − Encounter has ended andseparation increasing

Climb − Climb SYS 17 TCAS − Indicates a climb command.Displays a green fly-to PTZ and a red PAZon both PFD ADIs



CSP 700−6

Volume 203−10−16

AURALS (CONT'D)


W = Warning

SYS = System



Climb, Climb Now! −Climb, Climb Now!

SYS 17 TCAS − Following a descent command, aclimb is necessary to provide adequateseparation

Climb, Crossing Climb −Climb, Crossing Climb

SYS 17 TCAS − Indicates a climb command.Displays a green fly-to PTZ and a red PAZon both PFD ADIs. Aircraft flight path willcross intruder’s altitude

Decision Height SYS 11 At DH selected on PFD

Descend, Crossing Descend −Descend, Crossing Descend

SYS 17 TCAS − Indicates a descend command.Displays a green fly-to PTZ and a red PAZon both PFD ADIs. Aircraft flight path willcross intruder’s altitude

Descend − Descend SYS 17 TCAS − Indicates a descend command.Displays a green fly-to PTZ and a red PAZon both PFD ADIs

Descend, Descend Now! −Descend, Descend Now!

SYS 17 TCAS − Following a climb command, adescent is necessary to provide adequateseparation

Don’t Sink SYS 17 EGPWS − Sink after take-off

Gear Bay Overheat W 9 MLG BAY OVHT / Main wheel well overheat

Gear, Gear SYS 15 Gear not all fully down and locked during anattempted landing

Glideslope SYS 17 EGPWS − Excessive deviation belowglideslope

Increase Climb − Increase Climb SYS 17 TCAS − PTZ command increases to increaseclimb rate

Increase Descent − IncreaseDescent

SYS 17 TCAS − PTZ command decreases toincrease descent rate

LEFT ENGINE FIRE W 9 L ENG FIRE

Maintain Vertical Speed,Crossing Maintain

SYS 17 TCAS − Monitor pitch attitude to keep pitchattitude inside PTZ and away from PAZ.Aircraft flight path will cross intruder’s altitude

Maintain Vertical SpeedMaintain

SYS 17 TCAS − Monitor pitch attitude to keep pitchattitude inside PTZ and away from PAZ

Minimums SYS 17 At minimum altitude selected on PFD

Monitor Vertical Speed −Monitor Vertical Speed

SYS 17 TCAS − Monitor pitch attitude to keep pitchattitude inside PTZ and away from PAZ



CSP 700−6

Volume 203−10−17

AURALS (CONT'D)


W = Warning

SYS = System



NO TAKEOFF W 10&15

CONFIG AIL TRIMCONFIG RUD TRIMCONFIG SLATS/FLAPSCONFIG SPOILERSCONFIG STAB TRIMPARK BRAKE ON

Obstacle, Obstacle SYS 17 EGPWS − Excessive obstacle closure

Pull Up SYS 17 EGPWS − Corrective action after excessivedescent rate during approach

RIGHT ENGINE FIRE W 9 R ENG FIRE

Selcal SYS 6 SELCAL HF, SELCAL VHF 1, SELCALVHF 2, SELCAL VHF 3

Sink Rate SYS 17 EGPWS − Excessive descent rate duringapproach

SMOKE W 9 SMOKE BAGGAGESMOKE FWD LAVSMOKE AFT LAVSMOKE CLOSETSMOKE AVIONICS BAY

Terrain, Terrain SYS 17 EGPWS − Excessive terrain closure

Too Low Flap SYS 17 EGPWS − Insufficient flap, low altitude

Too Low Gear SYS 17 EGPWS − Gear up, low altitude

Too Low Obstacle SYS 17 Obstacle closure low altitude

Too Low Terrain SYS 17 EGPWS − Terrain closure low altitude

Traffic, Traffic SYS 17 TCAS − Conduct visual search for intruder

Windshear, Windshear SYS 17 EGPWS − WINDSHR (decreasingperformance)

500, 100, 50, 30 SYS 17 EGPWS − Descending altitude callouts



CSP 700−6

Volume 203−10−18

AURAL WARNING TEST

Most aural alerts are exercised as part of their own system test. For all other aural alerts, an AURALWARN TEST can be initiated via the Electrical Management System (EMS) Display Unit (DU)located on the pilot’s and copilot’s side panel. There are two warning test selections provided to testIntegrated Avionics Computer (IAC 1 and IAC 2).

GF

0310

_019

STAT SYS BUS PREV CNTL TESTPAGE

NEXTPAGE

EMERCNTL

BUS

STBY

SYSTEMCIRCUIT BREAKER

CIRCUIT BREAKER − SYSTEM 1/2

FIRE TEST

STALL TEST

AURAL WARNING TEST 1

LAMP TEST 1

LAMP TEST 2

OFF

NOTE: TEST is initiated by pressing activation key and canbe terminated by pressing activation key again.

OFF

OFF

OFF

OFF

AURAL WARNING TEST 2 TEST

Activation Key

BRT

The test sequences through each tone and/or voice message in the following priority order:

• “AURAL WARNING TEST 1”or “AURAL WARNING TEST 2”.• “STALL” (stall shaker active).• Continuous Tone (overspeed).• Triple Chime tone (any warning).• “NO TAKE-OFF”.• “LEFT ENGINE FIRE”.• “RIGHT ENGINE FIRE”.• “APU FIRE”.• “SMOKE”.• “CABIN ALTITUDE”.• “GEAR BAY OVERHEAT”.• “LEFT REVERSER UNLOCKED”.• “RIGHT REVERSER UNLOCKED”.• “NORMAL BRAKE FAIL”l.• Single Chime (any caution).• “GEAR”.• Single Cavalry Charge tone (autopilot disengage).• “AUTOTHROTTLE”.• “ALTITUDE” (altitude alert − departure).• C-chord tone (altitude alert − capture).• Double C-chord tone (vertical track alert).• Single Chime.• Trim clacker (trim in motion).• “MINIMUMS, MINIMUMS” (DH and MDA).• “SELCAL, SELCAL”.



CSP 700−6

Volume 203−10−19

AURAL WARNING PANEL

The aural warning panel, located on the overhead panel, is used to disable the tone/aural generators,located in IAC 1 and IAC 2.

GF

0310

_020

IAC1 and IAC2 PUSH TO MUTE SwitchesUsed to disable respective tone/aural generatorlocated in the respective IACs.

PUSH TO MUTE

IAC 1 IAC 2

AURAL WARNING

MUTEDMUTED

INHIBITS

During take-off and landing, the IAC fault warning computer, will process inhibit logic to minimizespurious or distracting messages. Warnings and status messages are not inhibited except forCABIN ALT and APU OVERTEMP (TO only).

During take-off, the caution and advisory messages are inhibited when:

• Weight On Wheels.• Indicated airspeed transitions from less than 80 knots to greater than or equal to 80 knots.

The caution and advisory messages’ inhibit is removed 25 seconds after:

• Weight Off Wheels.• Pressure Altitude is greater than or equal to take-off altitude +400 feet.• Indicated airspeed is less than 50 knots.• Take-off inhibit has been active for 60 consecutive seconds.

During landing, the caution and advisory messages are inhibited when:

• Landing gear down.• Radio altitude transitions from 200 feet to less than or equal to 200 feet.

The caution and advisory messages’ inhibit is removed:

• 25 seconds after air to ground transition.• Radio altitude greater than 200 feet.• Indicated airspeed less than 50 knots.



CSP 700−6

Volume 203−10−20

INHIBITS (CONT'D)

The following caution and advisory messages are NOT inhibited during take-off and/or landing.

Airplane System Caution Messages Advisory Messages

AFCS AP MISTRIM NOSE UP-DN (Ldg only)AP MISTRIM LWD-RWD (Ldg only)YD OFF

YD NOT CENTERED (TO only)

Air ConditioningPressurization

EMER DEPRESS

Aural and VisualWarnings

CHECK DU 1−2−3−4−5−6SG 1−2−3 FAIL

Electrical Power BATT MASTER OFF BATT EMER PWR ONRAT GEN ON (Ldg only)

Doors and Exits CARGO DOORLARGE SERV DOORSL−R EMER EXITPASSENGER DOORSMALL SERV DOORS

Flight Controls ELEVATOR SPLITFLT SPLR DEPLOYEDFLT SPOILERS FAILGND LIFT DUMPROLL SELECTROLL SPOILERS FAILRUD AUTHORITY LOWSLAT−FLAP FAILSTAB TRIMSTALL PROTECT FAIL

FLT SPOILERS FAULTGND LIFT DUMPNO TAKEOFF (TO only)SHAKER 1−2 FAILSLAT−FLAP HALFSPDSTALL WRN ADVANCE

Hydraulic Power HYD 1−2−3 LO PRESSHYD RAT PUMP FAIL (Ldg only)

Ice and RainProtection

ICE

Instruments ALL ADC MISCMP ADC 1−2−3 FAIL



CSP 700−6

Volume 203−10−21

INHIBITS (CONT'D)

The following caution and advisory messages are NOT inhibited during take-off and/or landing.

Airplane System Caution Messages Advisory Messages

Landing Gear BRAKE 50% DEGRADEDCPLT BRAKE FAULTGEAR DISAGREEINBD BRAKE LO PRESSL−R ANTI-SKID FAILL−R INBD BRAKE FAILL−R OUTBD BRAKE FAILNOSE STEER FAILOUTBD BRAKE LO PRESSPARK/EMER BRAKE ON (Ldg only)PLT BRAKE FAULTUNCOMMANDED BRAKE

BRAKE TEMP (TO only)GEAR SYS FAULTNO TAKEOFF (TO only)

Lighting EMER LIGHTS OFF

Navigation ALL IRS MISCMP

Power Plant A/T NOT IN HOLD (TO only)L−R FADEC N1 CTLL−R FUEL FILTERL−R REV LOCK FAILL−R REVERSER FAIL (Ldg only)L−R FUEL FILTER

A/T 1−2 FAIL



CSP 700−6

Volume 203−10−22

CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS)

The CAIMS collects diagnostic and fault data from other airplane systems. From this data, theCAIMS assembles a fault record that can be used to monitor system performance during the flight.The maintenance personnel uses CAIMS to accomplish system tests and to isolate defectivecomponents.

The CAIMS supplies fault data during all phases of airplane operation through the PortableMaintenance Access Terminal (PMAT), touch screen, located in the passenger cabin . The PMAThard-disk contains approximately 8MB of operational software files and 25MB of loadable diagnosticfiles. A CD-ROM is installed in the PMAT CD-ROM drive and contains an electronic copy of theAircraft Maintenance Manual (AMM).

The crew has the option of monitoring the PMAT display for active faults and/or may print the reporton the cockpit printer. For more information on the printer, refer to chapter 6 COMMUNICATIONS.

The CAIMS is comprised of the following components:

• PMAT (located in the cabin)

POWER HARDDRIVE

FAULT OVERTEMP

Power Switch Mode /Fault Annunciation

CD ROM Drive Access Port

3.5" Disk Drive Access Port

Active Faults page 1 / 3Current Leg # Date ACSN Time

1 30 Jul 97 278 1530

49 − 61 Controller (FADEC)Internal Fault

73 − 00 Engine Fuel and Control

77 − 00 Engine Indicating

RETURN MAIN

PREVPAGE

NEXTPAGE

SHOW DETAIL

GF

0310

_021

• DATA UPLOAD/DOWNLOAD switch and PRINT MAINT REPORT switch (on airplanes withSB 700-45-001 incorporated) (located on bulkhead behind pilot).



CSP 700−6

Volume 203−10−23

CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS) (CONT'D)

GF

0310

_022

CAIMS PRINT MAINT REPORT SWITCH(On airplanes with SB 700−45−001 incorporated)Used to get a report of active faults from the cockpit printer.

Data Selector SwitchUsed to select system toupload/download a copyof non-volatile data on toa 3.5 inch disk.

PRINT MAINTREPORT

DATAUPLOAD/DOWNLOAD

DAU 1ADAU 1B

DAU 2ADAU 2B

DAU 3A

DAU 3B

DAU 4A

DAU 4BIRS 1

IRS 2IRS 3

WX

SPARE

IAC 1IAC 2

IAC 3GPWS

SATCOM SDU

CABIN COMM

GPS 1GPS 2

ADC 1ADC 2

ADC 3

• Pilot Event Marker (located on the landing gear control panel).

GF

0310

_023

FDR/CAIMS Event ButtonUsed to store information inLine Replaceable Units(LRUs), which report to CAIMS.

Landing Gear Control Panel

NOSE STEER LDG GEAR

HORN PILOTEVENT

MUTED



CSP 700−6

Volume 203−10−24

FLIGHT DATA RECORDER

EICAS channels aircraft systems data (including altitude, airspeed, heading, acceleration and radiocommunications events) to the Flight Data Recorder (FDR). DAU 4B gathers sensor data fortransmission to the FDR.

DAU 4 is fully self-monitoring and provides CAS messages in the event of a failure. If DAU 4Bchannel fails, FDR information is not available.

To record an additional event, in the FDR push the PILOT EVENT button on landing gear controlpanel, located on the pedestal. Pushing the PILOT EVENT will also encode the Central AircraftInformation Maintenance System (CAIMS).

GF

0310

_024

Landing Gear Control Panel

FDR/CAIMSEvent Button

NOSE STEER LDG GEAR

HORN PILOTEVENT

MUTED

STALL WARNING

Warning of an impending stall is provided by independent stall protection systems. Both systems areenergized in flight and deactivated on the ground through air/ground logic. The flight displays indicateairplane approach to stall speed by low speed cues (red band) and a TBD VS indicator on theprimary flight displays (PFDs) airspeed tape.

Stall warnings are provided by an aural “STALL”, a STALL icon appears on the PFD and vibration ofboth control columns. If the airplane angle-of-attack continues to increase, a stick pusher thenpushes the control column forward to prevent further development of a stall. For more informationrefer to Chapter 10, FLIGHT CONTROLS.



CSP 700−6

Volume 203−10−25

TAKE-OFF CONFIGURATION WARNINGS

Take-off configuration warnings are armed when the airplane is on the ground and both engines areaccelerated towards take-off thrust (throttle position ≥ 30°). A voice warning, EICAS warningmessage, and both MASTER WARNING lights come on for any of the following:

Condition Voice Message EICAS Message

Aileron trim outside of take-offrange

“NO TAKEOFF” CONFIG AIL TRIM

Parking brake on during take-off “NO TAKEOFF” PARK BRAKE ON

Rudder trim outside of take-offrange

“NO TAKEOFF” CONFIG RUD TRIM

Flaps not in take-off position “NO TAKEOFF” SLATS/FLAPSLERS

Spoilers not in take-off position “NO TAKEOFF” CONFIG SPOICONFIG

Horizontal stabilizer outside oftake-off range (“green band”)

“NO TAKEOFF” CONFIG STAB TRIM

All configuration warning indications are cancelled when the configuration error is corrected, or theairplane is airborne or either thrust lever is retarded.

Note: NO TAKEOFF advisory message will appear during taxi, prior to advancing throttles.



CSP 700−6

Volume 203−10−26

LANDING CONFIGURATION WARNING

The “GEAR” aural will sound if any gear is not down and locked and the airplane is below 16,500 feetand:

• The radio altitude is less than 1,000 feet AGL and the descent rate is more than 400 feet perminute

OR• The radio altitude is less than 500 feet AGL and at least 2 minutes after ground to air transition

and both throttles are below 25° throttle lever angle (approximately CRZ thrust)

OR• The radio altitude is less than 500 feet AGL and the flaps position is 30° at any throttle position

NOTE

The “GEAR” aural can not be muted during any of these conditions.

The “Too low gear” (EGPWS) aural warning is heard if any landing gear is not down and locked withthe radio altitude less than 500 feet AGL and the indicated airspeed at less than 190 knots.

If neither radio altimeter is valid, the “GEAR” aural will sound if any gear is not down and locked andthe airplane is below 16,500 feet and landing flaps selected or either thrust lever at idle and:

• 2 minutes after ground to air transition and airspeed less than 191 knots with flaps at 0°.

OR• 2 minutes after ground to air transition and the airspeed is less than 165 knots.

OR

NOTE

The landing gear horn may be muted (press muted horn switch/light onlanding gear control panel) with one thrust lever at IDLE and airplanebelow 16,500 feet and any landing gear not in the down and lockedposition and conditions A or B not satisfied.



CSP 700−6

Volume 203−10−27

EICAS DISPLAY

GF

0310

_025


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS N2FF (PPH)OIL TEMPOIL PRESS

93.45750 115 81

93.45750 115 81

EPR

N1

ITT

AIL

GEAR

OUT

30

DN DNDN

1.651.65

7.2

RWD


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD RWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

EPR

N1

ITT

AIL

1.651.65

Crew Alerting System Window14 message lines with Gear/Slats/Flapspop up displayed.

Slats/Flaps, Spoilers and Gear Position Pop UpThe pop up display will be removed from theprimary page (in flight only) 30 seconds afterthe gear and flaps indicate up, ans nopredetermined malfunctions exist, or flightspoilers out.

The pop up display will appear with flap selectiongreater than zero degrees, gear selected downand/or if any predetermined malfunctions exist.

TrimsIndications for Aileron, Rudder and Stabilizer Trim.For more information see Chapter 10, FLIGHTCONTROLS.

NOTEEICAS will automatically be displayed whenairplane is powered up (BATT MASTER ON)

Crew Alerting System Window24 message lines with Gear/Slats/Flapspop up not displayed.

Engine IndicatingIndications of EPR, N1, ITT, N2, FF,OIL TEMP and OIL PRESSURE. For moreinformation see Chapter 18, POWER PLANT.

FuelIndications of total fuel quantity andindividual tank quantity. For moreinformation see Chapter 12, FUEL.



CSP 700−6

Volume 203−10−28

SYSTEMS DISPLAY (STAT PAGE)

NOTESYSTEM display will automatically be displayed when airplane is powered up (BATT MASTER ON). G

F03

10_0

26


RPM EGT

BRAKE TEMP

10.4

90

13% 13%

400100

0303 03 03

4.55.0

10.4

OXYGEN

OPEN OPEN

OUTFLOW VALVES00

1 2

1 2

2

APU

%

1

CKPT (°C) AFTCABIN (°C)CABIN (°C)

FWD

20

1300

0.0020

CAB ALT

CAB RATE

P2319 21 22

CKPT/CABIN TemperatureIndications of cockpit, cabin forward andcabin aft temperature. For more information

CAB ALT, P and CAB RATEIndications of cabin altitude, cabin differentialand cabin rate of climb. For more information

see Chapter 2, AIR CONDITIONINGAND PRESSURIZATION.

see Chapter 2, AIR CONDITIONINGAND PRESSURIZATION.

OXYGENIndications of oxygenquantity. For moreinformation seeChapter 8, EMERGENCYEQUIPMENT.

OUTFLOW VALVESIndications of outflowvalves position (manualmode only). For moreinformation see Chapter 2,AIR CONDITIONING

BRAKE TEMPIndications of braketemperatures. For moreinformation seeChapter 15, LANDINGGEAR.

AND PRESSURIZATION.

OIL QTYIndications of engine, APUand reservoir oil quantity.For more information seeChapter 5, APU, andChapter 18, POWERPLANT.

APUIndications of APU doorposition (failure modeonly), APU RPM and EGT.For more information seeChapter 5, AUXILIARYPOWER UNIT.

DOORSIndications of passenger entrydoor, overwing emergency exitbaggage door and aft equipmentbay door. For more informationsee Chapter 1, AIRPLANEGENERAL.



CSP 700−6

Volume 203−10−29

REVERSION CONTROL PANEL

The reversion panel, located on the pedestal, can be used to revert the EICAS display to alternatedisplay units, to revert IRS and ADCs and to revert SGs.

GF

0310

_027

PFD1 and PFD2 KnobsUsed to revert PFD 1 and PFD 2displays to alternate display units.

EICAS KnobUsed to revert EICAS displayto alternate display units.

IRS and ADC KnobsUsed to revert IRS and ADCs.For more information seeChapter 11, FLIGHTINSTRUMENTS.

SG1, SG2, SG3, KnobsUsed to revert applicable symbolgenerators to specific displays.



VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

NORMALTN

PFD1

NORMALTN1

EICAS

NORMALTN

PFD2

ALTN2ALTN3

PFD1 PFD2

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2

IRS IRSADC ADC



CSP 700−6

Volume 203−10−30

PFD REVERSION CONTROL

GF

0310

_028

PFD1 and PFD2 Reversion Knobs

ALTN − PFD 1 displayed on DU2, PFD 2 displayed on DU5.NORM − PFD 1 displayed on DU1, PFD 2 displayed on DU6.



VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

NORMALTN

PFD1

NORMALTN1

EICAS

NORMALTN

PFD2

ALTN2ALTN3

PFD1 PFD2

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2

IRS IRSADC ADC



CSP 700−6

Volume 203−10−31

PFD REVERSION

GF

0310

_029

ALTN − PFD 1 displayed on DU2, PFD 2 displayed on DU5.

DU 2 DU 5

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

NORMALTN

PFD1

NORMALTN1

EICAS

NORMALTN

PFD2

ALTN2ALTN3



CSP 700−6

Volume 203−10−32

EICAS REVERSION CONTROL

GF

0310

_030

EICAS Reversion KnobNORM − EICAS displayed on DU3.ALTN 1 − EICAS displayed on DU4.ALTN 2 − EICAS displayed on DU2.ALTN 3 − EICAS displayed on DU5.



VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350

NDSTAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

NORMALTN

PFD1

NORMALTN1

EICAS

NORMALTN

PFD2

ALTN2ALTN3

PFD1 PFD2

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2

IRS IRSADC ADC



CSP 700−6

Volume 203−10−33

EICAS REVERSION

GF

0310

_031

ALTN 1 − EICAS displayed on DU4.



DU 4

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4

TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT

RWD

DU 2

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

NORMALTN1

EICAS

ALTN2ALTN3

DU 5

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

NORMALTN1

EICAS

ALTN2ALTN3

NORMALTN1

EICAS

ALTN2ALTN3



CSP 700−6

Volume 203−10−34

SG REVERSION CONTROL

SG1, SG2, SG3 Reversion Knobs

− SG2 drives DU5 and DU6 as well as DU3.

GF

0310

_032

− SG2 drives DU5 and DU6. − SG3 drives DU3 and DU4.

SG3 drives DU1 and DU2 as well as DU4. − SG1 drives DU1 and DU2 as well as DU4.

SG3 drives DU5 and DU6 as well as DU3. − SG1 drives DU1, DU2 as well as DU4.

SG2 drives DU3, DU5 and DU6.

SG1 NORM − SG1 drives DU1 and DU2.SG2 NORMSG3 NORM

SG1 ALTN

SG2 ALTN

SG3 ALTN

NORMALTN

PFD1

NORMALTN1

EICAS

NORMALTN

PFD2

ALTN2ALTN3

PFD1 PFD2

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2

IRS IRSADC ADC



CSP 700−6

Volume 203−10−35

SG REVERSION

SG1 NORM − SG1 drives DU1 and DU2.

GF

0310

_033

SG2 NORM − SG2 drives DU5 and DU6.SG3 NORM − SG3 drives DU3 and DU4.

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2



CSP 700−6

Volume 203−10−36

SG REVERSION (CONT'D)

SG1 ALTN − SG2 drives DU3, DU5 and DU6.− SG3 drives DU1, DU2 and DU4.

GF

0310

_034

SG 1 FAILIf SG 1 FAIL select

SG2 ALTN − SG1 drives DU1, DU2 and DU4.− SG3 drives DU3, DU5 and DU6.SG 2 FAIL

If SG 2 FAIL select

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2



CSP 700−6

Volume 203−10−37

SG REVERSION (CONT'D)

SG3 ALTN − SG1 drives DU1, DU2 and DU4.− SG2 drives DU3, DU5 and DU6.

GF

0310

_035

SG 3 FAILIf SG 3 FAIL select

SG2 drives DU1, DU3, DU5 and DU6.SG 1−2 FAIL

If SG 1−3 FAIL −SG1 drives DU1, DU3, DU5 and DU6.If SG 2−3 FAIL −SG3 drives DU1, DU3, DU5 and DU6.If SG 1−2 FAIL −

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2

NORMALTN

SG1

NORMALTN

SG3

NORMALTN

SG2

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT

RWD

TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

4

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES



CSP 700−6

Volume 203−10−38

EICAS CONTROL PANEL

The EICAS control panel, located on the pedestal, can be used to revert SYSTEMS display, scrollnon-displayed messages and to display SYSTEMS synoptic pages.

BLEED ButtonHYD Button

AIR COND ButtonAC ELEC Button

DC ELEC Button FLT CTRL Button

FUEL Button

EICAS SCROLL Knob

STAT Button

SYSTEMS SELECT Knob

GF

0310

_036

EICAS

SCROLL SYSTEM SELECT

Used to displayBLEED/ANTI-ICEsynoptic.

HYDRAULICUsed to display

synoptic.

Used to displayAIR CONDITIONINGsynoptic.

Used to displayAC ELECTRICALsynoptic.

Used to displayFUEL synoptic.

Used to displayDC ELECTRICALsynoptic.

Used to displayFLIGHT CONTROLSsynoptic.

Used to revert SYSTEMSdisplay to alternate displays.

Used to displaystatus synoptic.

Used to scroll out of view and/orscroll into view all messages,except for warning messages.



CSP 700−6

Volume 203−10−39

SYSTEMS REVERSION CONTROL

GF

0310

_037

SYSTEM SELECT KnobCENTER − SYSTEM displayed on DU4.MFD1 − SYSTEM displayed on DU2.MFD2 − SYSTEM displayed on DU5.

EICAS


DU 2 DU 4 DU 5

MFD 1 SYSTEMS MFD 2

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES



CSP 700−6

Volume 203−10−40

SYSTEMS REVERSION CONTROL (CONT'D)

GF

0310

_038

NOTEAll SYSTEMS synoptics can be displayed, when SYSTEM SELECT reverted, on MFD1or MFD2, by selecting applicable button on EICAS Control Panel

MFD1 − SYSTEM displayed on DU2 and DU4.

MFD2 − SYSTEM displayed on DU5 and DU4.

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000 TOC3

KSRP

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

12.5 NMKDVT

LUF

KDVT

5

N

5

360

TERROFF

30

6

33

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

VS 2000

TOC3

KSRP180

220

210

200

170

160

150

0.88

0.856 M

190

KPHX

WX SAT

GSPD

−56TATTAS

−40234345

LX

HDG330

ETE 1+36

KLAX

KPHXTOC

KSRPKDVT

4000 4000

FL180

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

12.5 NMKDVT

LUF

KDVT

51300

1000

N

5

360

S

N

TERROFF

30

6

33

1856

4


1.541.54

73.373.3

789789

14600 1460010000 2350 ND

STAB

NU

RUDDERNL

LWD

NR

TRIMS

7.2


93.45750 115 81

93.45750 115 81

1.651.65

CRZEPR

SYNC

N1

ITT


RPM EGT

10.4

22

1300

85 %

0.00

20

400100

4.55.0

10.4

CKPT (5C)

OXYGEN

CAB ALT

CAB RATE

P

FWD

APU

RWD

CABIN (5C)AFT

CABIN (5C)

21

29

23

20"1300

LDG ELEV 1000

VS 2000

180

220

210

200

170

160

150

0.88

0.856 M

190

FMS1DTK 360

20

20

10

10

20

20

10

10

33

30

W

24

21 15

12

E

6

3

0

1

2

1

2

3


29.92 INH23.4NM

SRP

BARO9500

10500

10000

HDG 330

3

1300

1000

S

N

1856

40

1 2

13% 13 %

OPEN OPEN

OUTFLOW VALVES

SYSTEM SELECT

FLIGHT CONTROLS

SLAT OUT

FLAP 30

AIL

ELEV

RUDDER

AIL

ELEV

LP

HP

L R

APU

HP

LP

CONDAIR

BLEED/ANTI−ICE

40PSI

40PSI

SYSTEM SELECT



CSP 700−6

Volume 203−10−41

MESSAGE SCROLLING

EICAS SCROLL KnobUsed to scroll messages out of view and/or display non−displayed messages. Warning messages cannot be scrolled out of view.− Turning SCROLL knob clockwise will scroll messages up.− Turning SCROLL knob counter−clockwise will scroll messages down.

NOTEEach "click" of the SCROLL knob will move the message stack, one line up or down.

GF

0310

_039

ICE DETECTOR FAILASCB FAIL

HYD 1 LO PRESSHYD 2 LO PRESS

R PACK FAIL

AUTOBRAKE FAILMACH TRIM FAIL

0 MESSAGES 6

AT IRS MISCMPPARK BRAKE ON

TRIM AIR OFFSTAB CH 1 OFF

CB TRIPELEC SYS FAULT

END

HYD 3 LO PRESS

HYD 3 LO PRESS

EICAS


789789

N1

ITT

789789

N1

ITT

EICAS

SCROLL



CSP 700−6

Volume 203−10−42

SYSTEMS SYNOPTICS

To view SYSTEMS synoptic displays, select the appropriate button on the EICAS control panel.

STAT Page

NOTESTAT page will automatically be displayed when airplane is powered up (BATT MASTER ON). G

F03

10_0

40

EICAS



RPM EGT

BRAKE TEMP

10.4

90

13% 13%

400100

0303 03 03

4.55.0

10.4

OXYGEN

OPEN OPEN

OUTFLOW VALVES00

1 2

1 2

2

APU

%

1

CKPT (°C) AFTCABIN (°C)CABIN (°C)

FWD

20

1300

0.0020

CAB ALT

CAB RATE

P2319 21 22



CSP 700−6

Volume 203−10−43

SYSTEMS SYNOPTICS (CONT'D)Bleed/Anti-Ice Synoptic Page

GF

0310

_041

EICAS


LP

HP

L R

APU

HP

LP

CONDAIR

BLEED/ANTI−ICE

40PSI

40PSI



CSP 700−6

Volume 203−10−44

SYSTEMS SYNOPTICS (CONT'D)Air Conditioning Synoptic Page

GF

0310

_042

EICAS


AIR CONDITIONING

BLEED BLEED

RAM AIR

19 °C 21°C 22°C

CKPT FWD AFT20°C 20°C 23°C

23 °C 23 °C 23 °C

12 °C

L PACK

AIRTRIM15 °C

R PACK



CSP 700−6

Volume 203−10−45

SYSTEMS SYNOPTICS (CONT'D)Hydraulic Synoptic Page

GF

0310

_043

EICAS


70°C 68°C 70°C

HYDRAULIC

2B3B3A1B

INBDBRAKE

2900PSI

OUTBDBRAKENORM

PSIPSI PSI295030002950

RUDELEV RAIL RFLT SPLRSGEARREVERSER R

RUDL ELEV RL AIL R

GND SPLRSGEAR

NOSE STEER

RUDL ELEV

L AILFLT SPLRS

GND SPLRSL REVERSER

PARK/EMER BRAKE

1A 2A

62 % 64 % 62 %



CSP 700−6

Volume 203−10−46

SYSTEMS SYNOPTICS (CONT'D)AC Electrical Synoptic Page

GF

0310

_044

EICAS


AC BUS 1

VKVA

11512

GEN1

GEN2

AC BUS 2

VKVA

11512

GEN3

AC BUS 3

VKVA

11512

VKVA

11515

GEN4

AC BUS 4

AC ESS BUS

GEN

VKVA

00

HZ0

APU

AC ELECTRICAL



CSP 700−6

Volume 203−10−47

SYSTEMS SYNOPTICS (CONT'D)DC Electrical Synoptic Page

GF

0310

_045

EICAS


AC BUS 2FEEDER

DC BUS 1

VA

2835

TRU 1

AC BUS 3FEEDER

DC BUS 2

VA

2835

TRU 2

AC BUS 1FEEDER

AC ESSBUS

DC ESS

VA

2835

ESSTRU 1

VA

2835

ESSTRU 1

BUS

DC EMER

BATT BUS

BUSAV BATTDIR BUS

VA

260

°C20

AVBATT

VA

240

APU BATTDIR BUS

°C20

APUBATT

DC ELECTRICAL



CSP 700−6

Volume 203−10−48

SYSTEMS SYNOPTICS (CONT'D)Fuel Synoptic Page

GF

0310

_046

EICAS


FUEL

P

P

P P

P

P

P

P

P

P

TOTAL FUEL11455 LBS

FUEL USED6150 LBS

5600 LBS5855 LBSLBS

1075 LBS

AUX AUX

°C23 °C23

°C32 °C32APU



CSP 700−6

Volume 203−10−49

SYSTEMS SYNOPTICS (CONT'D)Flight Controls Synoptic Page

GF

0310

_047

EICAS


FLIGHT CONTROLS

SLAT OUT

FLAP 30

AIL

ELEV

RUDDER

AIL

ELEV



CSP 700−6

Volume 203−10−50

AURAL AND VISUAL WARNING EICAS MESSAGES

CHECK DU 1−2−3−4−5−6Indicates that data from affected DU does not match data from sensor.Note: are CHECK PFD and CHECK DU 1−2−3−4−5−6.

SG 1 (2, 3) FAILIndicates that there is a loss of communication with affected SG, or SG is indicating a power up failure.

IAC 1 (2, 3) OVHTIndicates that IAC has overheated, resulting in possible loss of functions.

DISP CTLRS FAIL Indicates that both display controllers have failed.

GF

0310

_048

If all 6 DUs fail, the messages posted CHECK DU 1CHECK DU 2CHECK DU 3CHECK DU 4CHECK DU 5CHECK DU 6DISP CTRLS FAILIAC 1 OVHTIAC 2 OVHTIAC 3 OVHTSG 1 FAILSG 2 FAILSG 3 FAIL



CSP 700−6

Volume 203−10−51

AURAL AND VISUAL WARNING EICAS MESSAGES (CONT'D)

CHECKLIST MISMATCHDAU 1A FAILDAU 1B FAILDAU 2A FAILDAU 2B FAILDAU 3A FAILDAU 3B FAILDAU 4A FAILDAU 4B FAILDU 1 FANDU 2 FANDU 3 FANDU 4 FANDU 5 FANDU 6 FANIAC 1 AURAL FAILIAC 2 AURAL FAIL

IAC 1−2 AURAL FAIL Indicates that there is no DC power to aural warning system, or a BIT failure is being indicated and not muted.

CHECKLIST MISMATCH Indicates that checklists are not identical in all IACs (on ground only).

DAU 1A−1B−2A−2B−3A−3B−4A−4B FAIL Indicates that there is a loss of communication with the affected DAU, or DAU has failed.

DU 1−2−3−4−5−6 FANIndicates that DU has overheated, resulting in possible loss of functions.

GF

0310

_049



CSP 700−6

Volume 203−10−52


MFD CTLR 1−2 FAIL Indicates that the affected MFD controller has failed.

REVRSION CTRL FAIL Indicates that there is a loss of reversionary control functions. May not be able to revert SGs or DUs.

IAC 1−2−3 INVALID Indicates that there is invalid software configuration in IAC, or incorrect airplane ID.

IAC 1−2−3 WOW INOPIndicates that there is a loss of power up testing and function loss.IAC WOW input is inconsistent with other airplane parameters.

IAC CONFIG MISMTCH Indicates that the IACs are not configured with the same options or aircraft configuration.

GF

0310

_050

IAC CONFIG MISMTCHIAC 1 INVALIDIAC 2 INVALIDIAC 3 INVALIDIAC 1 WOW INOPIAC 2 WOW INOPIAC 3 WOW INOPMFD CTLR 1 FAILMFD CTLR 2 FAILREVRSION CTLR FAIL



CSP 700−6

Volume 203−10−53


Effectivity:

• Airplanes 9002 thru 9119 not incorporating Service Bulletin:

• SB 700−31−018, Integrated Avionics Computers (IAC) − Avionics 2001 Batch 1 IACUpgrade.

MFD CTLR 1−2 FAIL Indicates that the affected MFD controller has failed.

REVRSION CTRL FAIL Indicates that there is a loss of reversionary control functions. May not be able to revert SGs or DUs.

IAC 1−2−3 INVALID Indicates that there is invalid software configuration in IAC, or incorrect airplane ID.

IAC 1−2−3 WOW INOPIndicates that there is a loss of power up testing and function loss.IAC WOW input is inconsistent with other airplane parameters.

IAC 1−2−3 MEM FULLIndicates that affected IAC has reached its memory limit.

IAC CONFIG MISMTCH Indicates that the IACs are not configured with the same options or aircraft configuration.

GF

0310

_051

IAC CONFIG MISMTCHIAC 1 INVALIDIAC 2 INVALIDIAC 3 INVALIDIAC 1 MEM FULLIAC 2 MEM FULLIAC 3 MEM FULLIAC 1 WOW INOPIAC 2 WOW INOPIAC 3 WOW INOPMFD CTLR 1 FAILMFD CTLR 2 FAILREVRSION CTLR FAIL



CSP 700−6

Volume 203−10−54


DAU 1A SELECTEDDAU 1B SELECTEDDAU 2A SELECTEDDAU 2B SELECTEDDAU 3A SELECTEDDAU 3B SELECTEDDAU 4A SELECTEDDAU 4B SELECTEDIAC 1 AURAL MUTEIAC 2 AURAL MUTE

DAU 1A−1B−2A−2B SELECTEDIndicates that the DAU has been reverted.

IAC 1−2 AURAL MUTE Indicates that the AURAL WARNING IAC1 (2) switch has been pushed. The aural warnings for the applicable IAC (s) are disabled.

DAU 3A−3B−4A−4B SELECTEDIndicates that the DAU has been reverted.

GF

0310

_052



CSP 700−6

Volume 203−10−55



CSP 700−6

Volume 203−10−56

THIS PAGE INTENTIONALLY LEFT BLANK

CB - IND/RECORD SYSTEM

GF

0320

_001


NEXTPAGE

EMERCNTL

BUS



HYD

ICE

IND/RECORD

LDG GEAR

LIGHTS

NAV

OIL

OXYGEN

THRUST REV

ADC 1

1/5CB − IND/RECORD SYSTEM

BATT

ADC 2 DC 1

ADC 3 DC ESS

AURAL WARNING 1 BATT

AURAL WARNING 2 DC ESS

CLOCK 1 BATT

IN

IN

IN

IN

IN

IN

CLOCK 2


DC 1

CLOCK BACK UP AV BATT DCPC

CVR DC ESS

CVR ERASE DC 2

DATA LOADER DC 2

DAU 1 CH A BATT

IN

IN

IN

IN

IN

IN

DAU 1 CH B

3/5

DC 1

DAU 2 CH A BATT

DAU 2 CH B DC 2

DAU 3 CH A BATT

DAU 3 CH B DC 2

DAU 4 CH A BATT

IN

IN

IN

IN

IN

IN

DAU 4 CH B


DC 1

DU 1 DC ESS

DU 2 DC ESS

DU 3 PWR A BATT

DU 3 PWR B DC 1

DU 4 PWR A BATT

IN

IN

IN

IN

IN

IN

DU 4 PWR B


DC 2

DU 5 DC 2

DU 6 DC 2

FDR DC 2

FDR ACCELEROMETER DC 2

IN

IN

IN

IN

IN

BRT

CB − IND/RECORD SYSTEM




CSP 700−6

Volume 203−20−1

CB - CAIMS SYSTEM

GF

0320

_002

CAIMS PMAT LAPTOP

1/1CB − CAIMS SYSTEM

DC 1

CKPT PRINTER DC 1

IN

IN


NEXTPAGE

EMERCNTL

BUS



AFCS

AIR COND/PRESS

APU

BLEED

CAIMS

COMM

DOORS

ELEC

ENGINE

FIRE

FLT CONTROLS

FUEL

BRT




CSP 700−6

Volume 203−20−2

AURAL AND VISUAL WARNINGS TABLE OF CONTENTS CHAPTER 3 · 2012. 6. 27. · mach trim fail 14...

Documents

Transcript of AURAL AND VISUAL WARNINGS TABLE OF CONTENTS CHAPTER 3 · 2012. 6. 27. · mach trim fail 14...