AURAL AND VISUAL WARNINGS TABLE OF CONTENTS CHAPTER 3 · 2012. 6. 27. · mach trim fail 14...
Transcript of 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
AURAL AND VISUAL WARNINGS
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
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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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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.
DU 1 DU 2 DU 3 DU 4 DU 5 DU 6
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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
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MASTERWARNING/CAUTION
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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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
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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
N2FF (PPH)OIL TEMPOIL PRESS
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
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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
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_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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−5
CREW ALERTING MESSAGES (CONT'D)
GF
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_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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−6
CREW ALERTING MESSAGES (CONT'D)
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
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_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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−7
CREW ALERTING MESSAGES (CONT'D)
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−8
CREW ALERTING MESSAGES (CONT'D)
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
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_014
FUEL XFER ON
XFER VALVE OPENXFER VALVE OPEN
FUEL XFER ON
77771111111111114412121244725597755599111111111818181818272
7721515
27312
333333337773
718187777
101111910101017171712121212121212
157777101717
112131313131313
11
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−9
CREW ALERTING MESSAGES (CONT'D)
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−10
CREW ALERTING MESSAGES (CONT'D)
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
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FUEL XFER ON FUEL XFER ON
2
710
7772
171677
1212
15777710101717
17
2121414181891818121291822221214
2
161522
121291822221214
161010
2
1414121212
2212
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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.
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MASTERWARNING/CAUTION
WARNINGROLL SPLRS
PLT CONT
ROLLSELPLT
ROLL
MASTERWARNING/CAUTION
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.
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MASTERWARNING/CAUTION
ROLL SPLRS
PLT CONT
ROLLSELPLT
ROLL
MASTERWARNING/CAUTION
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
AURAL AND VISUAL WARNINGS
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−13
AURALS (CONT'D)
VOICE MESSAGE − ALPHABETICAL
W = Warning
SYS = System
Voice Message Type ChapterRef.
EICAS/ PFD INDICATION
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−14
AURALS (CONT'D)
VOICE MESSAGE − ALPHABETICAL
W = Warning
SYS = System
Voice Message Type ChapterRef.
EICAS/ PFD INDICATION
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−15
AURALS (CONT'D)
VOICE MESSAGE − ALPHABETICAL
W = Warning
SYS = System
Voice Message Type ChapterRef.
EICAS/ PFD INDICATION
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:
VOICE MESSAGE − ALPHABETICAL
W = Warning
SYS = System
Voice Message Type ChapterRef.
EICAS/ PFD INDICATION
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−16
AURALS (CONT'D)
VOICE MESSAGE − ALPHABETICAL
W = Warning
SYS = System
Voice Message Type ChapterRef.
EICAS/ PFD INDICATION
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−17
AURALS (CONT'D)
VOICE MESSAGE − ALPHABETICAL
W = Warning
SYS = System
Voice Message Type ChapterRef.
EICAS/ PFD INDICATION
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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).
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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”.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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.
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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.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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
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• DATA UPLOAD/DOWNLOAD switch and PRINT MAINT REPORT switch (on airplanes withSB 700-45-001 incorporated) (located on bulkhead behind pilot).
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−23
CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS) (CONT'D)
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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).
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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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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).
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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.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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Volume 203−10−27
EICAS DISPLAY
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TOTALFUEL(LBS) 41550
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
TOTALFUEL(LBS) 41550
1.541.54
73.373.3
789789
14600 1460010000 2350 ND
STAB
NU
RUDDERNL
LWD RWD
NR
TRIMS
7.2
N2FF (PPH)OIL TEMPOIL PRESS
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.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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
OIL QTY (QTS)ENGAPURES
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.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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.
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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.
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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
VAPP VNAVASELAP1HDG 10400
29.92 INH23.4NM
SRP
BARO9500
10500
10000
HDG 330
3
1300
1000
S
N
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
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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.
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
NDSTAB
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−33
EICAS REVERSION
GF
0310
_031
ALTN 1 − EICAS displayed on DU4.
ALTN 2 − EICAS displayed on DU2.
ALTN 3 − EICAS displayed on DU5.
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
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
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
VAPP VNAVASELAP1HDG 10400
29.92 INH23.4NM
SRP
BARO9500
10500
10000
HDG 330
3
1300
1000
S
N
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
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
VAPP VNAVASELAP1HDG 10400
29.92 INH23.4NM
SRP
BARO9500
10500
10000
HDG 330
3
1300
1000
S
N
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
VAPP VNAVASELAP1HDG 10400
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
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
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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
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
VAPP VNAVASELAP1HDG 10400
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
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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
VAPP VNAVASELAP1HDG 10400
29.92 INH23.4NM
SRP
BARO9500
10500
10000
HDG 330
3
1300
1000
S
N
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
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
VAPP VNAVASELAP1HDG 10400
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
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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
SCROLL SYSTEM SELECT
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
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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
VAPP VNAVASELAP1HDG 10400
29.92 INH23.4NM
SRP
BARO9500
10500
10000
HDG 330
3
1300
1000
S
N
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
VAPP VNAVASELAP1HDG 10400
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
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
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
VAPP VNAVASELAP1HDG 10400
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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
SCROLL SYSTEM SELECT
789789
N1
ITT
789789
N1
ITT
EICAS
SCROLL
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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
SCROLL SYSTEM SELECT
OIL QTY (QTS)ENGAPURES
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−43
SYSTEMS SYNOPTICS (CONT'D)Bleed/Anti-Ice Synoptic Page
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EICAS
SCROLL SYSTEM SELECT
LP
HP
L R
APU
HP
LP
CONDAIR
BLEED/ANTI−ICE
40PSI
40PSI
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−44
SYSTEMS SYNOPTICS (CONT'D)Air Conditioning Synoptic Page
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EICAS
SCROLL SYSTEM SELECT
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−45
SYSTEMS SYNOPTICS (CONT'D)Hydraulic Synoptic Page
GF
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EICAS
SCROLL SYSTEM SELECT
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 %
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−46
SYSTEMS SYNOPTICS (CONT'D)AC Electrical Synoptic Page
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EICAS
SCROLL SYSTEM SELECT
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−47
SYSTEMS SYNOPTICS (CONT'D)DC Electrical Synoptic Page
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EICAS
SCROLL SYSTEM SELECT
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−48
SYSTEMS SYNOPTICS (CONT'D)Fuel Synoptic Page
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EICAS
SCROLL SYSTEM SELECT
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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−49
SYSTEMS SYNOPTICS (CONT'D)Flight Controls Synoptic Page
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EICAS
SCROLL SYSTEM SELECT
FLIGHT CONTROLS
SLAT OUT
FLAP 30
AIL
ELEV
RUDDER
AIL
ELEV
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
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.
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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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
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.
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AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−52
AURAL AND VISUAL WARNING EICAS MESSAGES (CONT'D)
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.
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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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−53
AURAL AND VISUAL WARNING EICAS MESSAGES (CONT'D)
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.
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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
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−54
AURAL AND VISUAL WARNING EICAS MESSAGES (CONT'D)
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.
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AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−10−55
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−10−56
THIS PAGE INTENTIONALLY LEFT BLANK
CB - IND/RECORD SYSTEM
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STAT SYS BUS PREV CNTL TESTPAGE
NEXTPAGE
EMERCNTL
BUS
CIRCUIT BREAKER − SYSTEM 2/2
SYSTEMCIRCUIT BREAKER
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
2/5CB − IND/RECORD SYSTEM
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
4/5CB − IND/RECORD SYSTEM
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
5/5CB − IND/RECORD SYSTEM
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
AURAL AND VISUAL WARNINGS
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 203−20−1
CB - CAIMS SYSTEM
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CAIMS PMAT LAPTOP
1/1CB − CAIMS SYSTEM
DC 1
CKPT PRINTER DC 1
IN
IN
STAT SYS BUS PREV CNTL TESTPAGE
NEXTPAGE
EMERCNTL
BUS
CIRCUIT BREAKER − SYSTEM 1/2
SYSTEMCIRCUIT BREAKER
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
AURAL AND VISUAL WARNINGS
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 203−20−2