TABLE OF CONTENTS ELECTRONIC DISPLAY SYSTEM. Page. 7-i

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1 Chapter 7: Electronic Display ystem TABLE OF COTET Page Introduction...7- Aural and Visual Warning ystem...7- Display...7- ystems ynoptics tatus Page Bleed/Anti-Ice ynoptic Page Air Conditioning ynoptic Page...7- Hydraulic ynoptic Page AC Electrical ynoptic Page DC Electrical ynoptic Page Fuel ynoptic Page...7- Flight Controls ynoptic Page...7- Description...7- Electronic Display ystem...7- Crew Alerting ystem...7- Master Warning/Master Caution Lights Warning/Caution Messages Advisory/tatus Messages...7- Message crolling Aurals Alphabetical List of Voice Messages...7- Aural Warning Test...7- Aural Warning Panel...7- Inhibits...7- Takeoff Configuration Warnings...7- Landing Configuration Warning...7- tall Warning Reversion Control Panel Reversion Control...7- Reversion Control...7- ADC Reversion...7- IR Reversion Control Panel ystems ELECT Control ystems ELECT Flight Data Recorder Central Aircraft Information and Maintenance ystem (CAIM) Messages ummary Electronic Flight Instruments...7- EFI etwork Description Pitot-tatic ystem i

2 Pitot-tatic chematic Air Data ystem Primary Flight Instruments Primary Flight Display Airspeed Tape Altitude Tape Radio Altitude Attitude Director Indicator (ADI) Vertical peed Indicator (VI) PFD Control Panel MIIMUM Knob PFD (HI) BARO ET Knob Multifunction Display (MFD) Map Format Plan Format MFD Control Panel Traffic Collision Avoidance ystem (TCA) Button Map/Plan Button Menu Button Terrain (TERR) Button avaids/airports (AV/APT) Button ormal Procedures (ORM) Waypoint Listing ORM - Disclaimer ORM - Before tart Abnormal Procedures (AB) Button Emergency Procedures tandby Attitude Indicator tandby Altimeter/Airspeed Indicator tandby Magnetic Compass Clock Time etting tandby Airspeed/Altitude/Altimeter (if installed) PFD Comparison Monitor Annunciations ystem Integration Electronic Display ystem Messages EM Circuit Protection ii

3 IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT 4 KOP KKLM LUF KHJ KABC KDEF.5M ET 5 9. KDVT : 5. M W. 5 ETE+ WX KKLM AT -5 T5. % KDEF KHJ TAT -4 85% FL8 TA 4 TAB 4 4 PD 45 LX TERR IHIB I TART.5 FF (PPH) OIL TEMP OIL PRE TART.5 I 457ED EAR mb/hpa ALT 5 IA FEET 4 KOT I H CKPT ( C) FWD AFT CAB ALT CABI ( C) CABI ( C) P CAB RATE LD ELEV OXYE % OUTFLOW VALVE OPE OPE % % RPM OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O BEARI RA9.8M+ TA 4. 5M -4 ET WX LX -4 KDEF MA KABC - KHJ 4 4 KKLM KHJ KDEF + KKLM FL8 - LUF +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT ITRODUCTIO The following chapter introduces the BD 7 Electronic Display ystem. The first part of this chapter covers the aural and visual warning system whereas the second part covers the electronic flight instrument system. AURAL AD VIUAL WARI YTEM The aural and visual warning system provides indications to warn of potentially unsafe operating conditions or airplane configurations, system malfunctions, and non-normal situations. Indications can be generated by the following: Crew alerting subsystem within the Engine Indication and Crew Alerting ystem () Enhanced round Proximity Warning ystem (EPW) Weather Radar (WX) system Traffic alert and Collision Avoidance ystem (TCA) Altitude alert portion of the Air Data Computer (ADC) tick shaker portion of the tall Protection ystem (P) provides the crew with the necessary displays for airplane engine control and monitoring, control surface monitoring, and all major subsystem synoptic displays. During normal operation the engine and control surface information is displayed on the Display Unit (DU) and the system synoptic information is displayed on the YTEM display (DU4). DU DU DU DU 4 DU 5 DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 PFD MFD TRU 5 5 FM CRZ EPR T/O O TAKEOFF PARK/EMER BRAKE O YC D D D OUT ITT YC O O 575O U TRIM 5 5 AIL TOTAL FUEL (LB) 455O LWD RWD 4OO OOOO 4OO D 5O TAB L RUDDER R BARO YTEM 5 :.5L FM 5 5 MFD M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M PFD 8 X_7_ 7-

4 displays: Primary engine parameters econdary engine parameters Fuel quantities Landing gear position Flaps/slats/spoilers positions urface trim indication Crew Alerting ystem (CA) messages YTEM provides synoptic displays of: Bleed/Anti-Ice Air Conditioning Hydraulics AC Electrical DC Electrical Fuel Flight Controls tatus 7-

5 DIPLAY.5.54 CRZ EPR L E FLAMEOUT FUEL LO QTY.5 FUEL IMBALACE.54 YD OFF < FUEL XFER O LD MAUAL ARM PARK/EMER BRAKE O Crew Alerting ystem Window 4 message lines with ear/lats/flaps popup displayed. I TART O T/O YC 789 ITT YC FF (PPH) OIL TEMP OIL PRE TOTAL FUEL (LB) 45OO 4OO OOOO 4OO OO 7. TART O D D D OUT I U 7. D TAB EAR TRIM LWD L AIL RUDDER O RWD R lats/flaps, poilers, and ear Position Pop-Up The pop-up display will be removed from the primary page (in flight only) seconds after the gear and flaps indicate up, and no predetermined malfunctions exist, or Flight spoilers out. The pop-up display will appear with flap selection greater than zero degrees, gear selected down and/or if any predetermined malfunctions exist. TRIM Indications for Aileron, Rudder, and tabilizer trim. Aft tank not applicable to lobal 5 OTE: will automatically be displayed when the airplane is powered up (BATT MATER O). Crew Alerting ystem Window 4 message lines with ear/lats/flaps Pop-up not displayed. Engine Indicating Indications of EPR,, ITT,, Fuel Flow, Oil temperature and Pressure CRZ EPR T/O YC 789 L E FLAMEOUT FUEL LO QTY.5 FUEL IMBALACE.54 YD OFF < FUEL XFER O LD MAUAL ARM PARK/EMER BRAKE O Fuel Indications of total fuel quantity and individual tank quantity. Aft tank not applicable to lobal 5 I TART O 5 8 ITT YC FF (PPH) OIL TEMP OIL PRE TART O 5 8 TOTAL FUEL (LB) 45OO 4OO OOOO 4OO OO I U 7. D TAB TRIM LWD L AIL RUDDER RWD R X_7_ 7-

6 YTEM YOPTIC To view YTEM synoptic displays, select the appropriate button on the control panel. TATU PAE CKPT/CABI Temperature Indications of cockpit, forward, and Aft Cabin selected (cyan) and actual (green) temperature. OXYE Indication of oxygen quantity. OUTFLOW VALVE Indication of outflow valves position (manual mode only). BRAKE TEMP Indication of brake temperatures. CKPT ( C) CABI ( C) CABI ( C) 9 OXYE 9% AFT OUTFLOW VALVE OPE OPE % % OIL QTY (QT). E. APU 5. RE. APU DOOR. RPM ET 5 BRAKE TEMP CAB ALT P CAB RATE. CAB ALT, P and CAB RATE Indications of cabin altitude, cabin differential pressure and cabin rate of climb. Cabin rate shown in manual only. OIL QTY Indication of engine, APU and reservoir oil quantity. APU Indication of APU RPM and ET. Indication of APU door position if failed in other than commanded position. DOOR Indication of passenger entry door, overwing emergency exit, baggage door and service doors. BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_ OTE TAT page will automatically be displayed when airplane is powered up (BATT MATER O). 7-4

7 BLEED/ATI-ICE YOPTIC PAE BLEED / ATI-ICE LP HP PI AIR COD L R PI LP HP APU BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_4 7-5

8 AIR CODITIOI YOPTIC PAE AIR CODITIOI CKPT C FWD C AFT C C C C C C C TRIM AIR C 5 C L PACK RAM AIR R PACK BLEED BLEED BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X 5 7-

9 HYDRAULIC YOPTIC PAE C HYDRAULIC 8 C C % % % B A RAT B B A IBD BRAKE 5 PI OUTBD BRAKE ORM A 5 PI RUD L ELEV L AIL FLT PLR D PLR L REVERER 5 PI RUD L ELEV R L AIL R D PLR EAR OE TEER PARK/ EMER BRAKE 5 PI RUD ELEV R AIL R FLT PLR EAR REVERER R BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_ 7-7

10 AC ELECTRICAL YOPTIC PAE AC ELECTRICAL AC E BU AC BU AC BU 4 AC BU AC BU 5 5 V KVA 5 V KVA 5V KVA 4HZ 5 V KVA 5 5 V KVA E E E E E 4 APU BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_7 7-8

11 DC ELECTRICAL YOPTIC PAE AC BU FEEDER DC ELECTRICAL AC BU FEEDER AC E BU AC BU FEEDER TRU 8V 5A E TRU 8V 5A E TRU 8V 5A TRU 8V 5A DC E BU DC BU DC BU BATT BU AV BATT DIR BU DC EMER BU APU BATT DIR BU 4V A 5V A AV BATT C APU BATT C BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_8 7-9

12 FUEL YOPTIC PAE (lobal 5 ee Appendix ) TOTAL FUEL 455OLB AUX 5O5OLB P FUEL 5OLB P P 5O5OLB FUEL UED P AUX OLB P P P O C O C P P P APU C LO PRE OOLB C LO PRE BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_9 7-

13 FLIHT COTROL YOPTIC PAE FLIHT COTROL LAT OUT FLAP O AIL ELEV ELEV AIL RUDDER BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_ 7-

14 DECRIPTIO The Electronic Display ystem (ED) provides the crew with displays for aircraft control, navigation, engine control and monitoring and system synoptics. Other systems information displayed are WX, TCA, EPW, and the Lightning ensor ystem (L). Data is transmitted from aircraft systems to 4 dual channel Data Acquisition Units (DAU) through the Avionics tandard Communication Bus (ACB) to Integrated Avionics Computers (IAC), and finally to the Display Units (DU). The 4 dual channel DAUs operate with one channel active and the other channel on standby, with both channels updating data at the same time. The ACB is the principal communications network interconnecting the system components. Data traffic flow on the ACB is managed by bus controllers (one bus controller in each IAC). Only one bus controller is in control at a time with the other in standby status. The three IACs each contain a ymbol enerator () and a Fault Warning Computer (FWC). The s process data from various sources and output the data to the DUs. The FWC compares sensor input data, verifies all critical display data and displays Warning, Caution, Advisory and tatus messages as applicable. DU DU DU DU 4 DU 5 DU IAC IAC IAC FWC FWC FWC ACB CH A DAU CH B CH A DAU CH B CH A DAU CH B DAU 4 CH A CH B X_7_ AIRPLAE DATA 7-

15 The IACs perform the following functions: IAC IAC IAC EFI,, FWC, CAIM EFI,, FWC, CAIM EFI,, FWC, CAIM Tone/Aural generator LAERTRACK (if installed) Tone/Aural generator Flight Management ystem FM (if installed) Flight Management ystem Autothrottle AFC Autothrottle AFC CREW ALERTI YTEM The crew alerting system portion of continually monitors all airplane systems. If an operationally significant fault occurs on a system, displays a crew alerting message on the display unit. In addition to the display messages, some crew alerts are also indicated by aural tones, voice advisories, MATER WARI and MATER CAUTIO lights. All crew alerting system messages are divided into one of four categories and in the following priority: Warning messages: RED Caution messages: AMBER Advisory messages: CYA tatus messages: WHITE Red warning messages are generated when immediate recognition and corrective or compensatory action is required. They are the most urgent type of crew alerts. They always appear at the top of the message stack on the display. All warning messages cause the MATER WARI lights on the glareshield to flash and generate an aural alert of a triple-chime. pecific warnings are also accompanied by a voice message. Once acknowledged, by pressing the warning light, the light will extinguish and the system will re-arm to indicate any additional warning messages. Failure to re-arm the system will mean that any subsequent CA Warning Message will not be announced by the triple chime and Master Warning lights, however, related voice messages will remain valid. OTE The tall Warning ystem is not part of the MATER WARI light system. The approach of an aerodynamic stall will be indicated by a separate warning indication. 7-

16 BRT BRT ROLL EL ROLL EL RAD RAD BR V/L FM BR BARO HI BR V/L FM BR BARO HI I I Hpa Hpa FD FD FM FM D FLC AV BAK VAV ALT I MA BC APR D FLC AV BAK VAV ALT I MA BC APR UP UP V V AP YD CPL AP YD CPL FD FD RAD RAD BR V/L FM BR BARO HI BR V/L FM BR BARO HI I I Hpa Hpa ROLL EL ROLL EL MATER WARI/MATER CAUTIO LIHT Two MATER WARI switch/lights come on flashing when any warning message occurs. The lights remain on as long as the warning exists. Pushing either MATER WARI switch/light extinguishes both MATER WARI lights for the duration of that warning and resets the lights for future warnings. HUD DIM OFF ROLL PLR PLT ROLL PLT COT MATER WARI/CAUTIO WARI CAUTIO MIIMUM AV RC BARO ET PUH TD CR PD T ALT CR C H PUH DCT PUH CH PUH YC P PUH DCT MIIMUM AV RC BARO ET PUH TD MATER WARI/CAUTIO WARI CAUTIO ROLL PLR CPLT ROLL CPLT COT MATER WARI/CAUTIO MATER WARI/CAUTIO WARI CAUTIO WARI CAUTIO X_7_ Pushing the MATER WARI also silences the related aural warnings except for the following cases: Configuration warnings ear horn Two MATER CAUTIO switch/lights flash when any caution occurs. Pushing either MATER CAUTIO switch/light extinguishes both MATER CAUTIO lights for the duration of that caution and resets the lights for future cautions. HUD DIM OFF ROLL PLR PLT ROLL PLT COT MATER WARI/CAUTIO WARI CAUTIO MIIMUM AV RC BARO ET PUH TD CR PD T ALT CR C H PUH DCT PUH CH PUH YC P PUH DCT MIIMUM AV RC BARO ET PUH TD MATER WARI/CAUTIO WARI CAUTIO ROLL PLR CPLT ROLL CPLT COT MATER WARI/CAUTIO MATER WARI/CAUTIO WARI CAUTIO WARI CAUTIO X_7_ Certain aural alerts/voice messages are not part of MATER WARI/MATER CAUTIO light alerting system. The following aural alerts/voice messages will not trigger a MATER WARI/MATER CAUTIO light: - tall warnings - Trim clacker - EPW/TCA (voice and aurals) - Autopilot disconnect cavalry charge - Overspeed continuous horn (A-Chord) - ear horn 7-4

17 WARI/CAUTIO MEAE Warning messages cannot be removed from view unless the applicable failure has been rectified. If the failure is rectified, messages which appeared below the deleted message will move up one line. When a new fault occurs, the new message will move to the top of the stack. MATER WARI/CAUTIO WARI CAUTIO L E FIRE Aural Triple Chime LEFT EIE FIRE X_7_4 lareshield Display Amber caution messages are generated when immediate crew awareness is required and subsequent crew action will be required. Caution messages appear immediately below the warnings messages in the message stack on the display. All cautions cause the MATER CAUTIO lights on the glareshield to flash and have an aural alert consisting of a single chime. Once acknowledged by pressing the CAUTIO Light, the flashing stops and the system is re-armed to indicate any further caution messages. Failure to re-arm the system will mean that any subsequent CA Caution Message will not be announced by the single chime and Master Caution lights. MATER WARI/CAUTIO WARI CAUTIO L E FLAMEOUT Aural ingle Chime X_7_5 lareshield Display Caution messages can be paged and scrolled from view using the CROLL knob on the control panel. If a new abnormal situation occurs, the corresponding caution message will flash and the remaining messages will remain steady. The new message will be displayed at the top of the stack. To view all of the non-displayed messages, turn the CROLL knob on the control panel. croll Knob BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT Control Panel YTEM ELECT X_7_ 7-5

18 ADVIORY/TATU MEAE Cyan advisory messages are generated when crew awareness is required and subsequent crew action may be required. Advisory messages appear immediately below the caution message in the message stack on the display. When a new advisory message appears, it will flash for 5 seconds then remain steady. There is no aural alert for advisory messages. L REVERER FAULT X_7_7 Display Advisory messages can be paged and scrolled from view using the CROLL knob on the control panel. To view all of the non-displayed messages, turn the CROLL knob on the control panel. White status messages are generated to indicate non-normal pilot selections and are reminders to the crew. They are set in the message stack below the advisories. There is no aural alert for status messages. L E OV CLD X_7_8 Display 7-

19 tatus messages can be scrolled from view using the CROLL knob on the control panel. To view all of the non-displayed messages, turn the CROLL knob on the control panel. The message window displays up to 4 messages with the ear/lats/flaps pop-up icon displayed. With the ear/lats/flaps pop-up icon not displayed, the window can display up to 4 messages. I TART O CRZ EPR T/O YC 789 ITT YC FF (PPH) OIL TEMP OIL PRE TOTAL FUEL (LB) 45OO 4OO OOOO 4OO OO L E FLAMEOUT FUEL LO QTY.5 FUEL IMBALACE.54 YD OFF < FUEL XFER O LD MAUAL ARM PARK/EMER BRAKE O 7. TART O D D D OUT I U 7. D TAB EAR TRIM LWD L AIL RUDDER O RWD R I TART T/O YC 789 ITT YC FF (PPH) OIL TEMP OIL PRE TOTAL FUEL (LB) 45OO 4OO OOOO 4OO OO L E FLAMEOUT FUEL LO QTY.5 FUEL IMBALACE.54 YD OFF < FUEL XFER O LD MAUAL ARM PARK/EMER BRAKE O CRZ EPR messages 4 messages ear/ lats/ Flaps Pop-Up Icon O TART O 5 8 I U 7. D TAB TRIM LWD L AIL RUDDER RWD R X_7_9 If there are non-displayed messages above the top of the display or below the bottom of the display, xxx messages xxx symbols will appear at the bottom of the message window. The number of non-displayed messages will be indicated beside the or arrows. If there are no more messages, an ED symbol will appear below the last message. The color of the status line corresponds to the highest level of messages not displayed. Warning messages cannot be scrolled from view, they will remain at the top of the message stack. 7. CRZ EPR T/O YC 7. HYD LO PRE HYD LO PRE HYD LO PRE ICE DETECTOR FAIL AC BU FAIL L REVERER ULKD W TEERI FAIL LATERAL MODE OFF MATCH TRIM FAIL MACH TRIM FAIL MEAE EAR D D D 7. CRZ EPR T/O YC MACH TRIM FAIL R OIL PRE R FADEC FAIL PITCH DIC FAULT R OIL FILTER 7. IAC WOW IOP R E BLEED OFF TRIM AIR OFF 457ED O MEAE O EAR D D D X_7_ MEAE ED O MEAE O 7-7

20 MEAE CROLLI I TART O 7. T/O YC 789 ITT YC FF (PPH) TART O 789 I U L PACK FAIL LATERAL MODE OFF MACH TRIM FAIL AFC PFD IR REV AFC TBY ADC FAIL AFT EQUIP BAY DOOR R PACK FAIL HYD LO PRE HYD LO PRE HYD LO PRE ICE DETECTOR FAIL ACB FAIL BLEED COFI FAIL DAU FAIL ELEC Y FAULT O MEAE TRIM BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD TAT CROLL YTEM ELECT CROLL Knob Used to scroll messages out of view and/or display nondisplayed messages. Warning messages cannot be scrolled out of view. Turning CROLL knob clockwise will scroll messages up Turning CROLL knob counterclockwise will scroll messages down. CROLL OTE: Each click of the CROLL knob will move the message stack, one line up or down. I TART O 7. T/O YC 789 ITT YC FF (PPH) TART O 789 I U R PACK FAIL HYD LO PRE HYD LO PRE HYD LO PRE ICE DETECTOR FAIL ACB FAIL BLEED COFI FAIL DAU FAIL ELEC Y FAULT AT IR MICOMP AUTOBRAKE FAIL TAB CH OFF TRIM AIR OFF DAU B ELECTED PARK BRAKE O ED TRIM X_7_ 7-8

21 AURAL Aurals and tones that call attention to warnings and cautions. AURAL/TOE IDICATIO CHAPTER REFERECE C-chord ( second) Altitude alert Chapter 7, Electronic Display ystem Cavalry Charge Caution (ingle chime) Autopilot disconnect Tone that precedes an aircraft system caution message Chapter, Automatic Flight Control ystem Chapters through 7 Clacker Excessive stabilizer movement Chapter, Flight Controls Landing ear Horn Double C-chord Horn Continuous (A-chord) Landing gear not down-and-locked for landing VAV vertical track alert Overspeed warning Chapter 4, Landing ear Chapter, Automatic Flight Control ystem Chapter, Automatic Flight Control ystem Chapter, Flight Controls tick haker tall Chapter, Flight Controls Warning (Triple chime) Whoop-Whoop Tone that precedes an aircraft system warning message and/or voice advisory EPW mode or (excessive descent rate or excessive closure rate) (if installed) Chapters through 7 EPW, Chapter, avigation 7-9

22 ALPHABETICAL LIT OF VOICE MEAE VOICE MEAE - ALPHABETICAL W = WARI Y = YTEM /PFD IDICATIO VOICE MEAE TYPE CH.REF Adjust Vertical peed, Adjust Y TCA - Reduce vertical speed APU FIRE W 9 APU FIRE Bank Angle Y EPW - Excessive bank angle on final approach CABI ALTITUDE W CABI ALT/Cabin altitude >9 feet Clear of Conflict Y Climb, Climb Y TCA - Encounter has ended and separation increasing TCA - Indicates climb, put AC symbol in green box Climb, Crossing, Climb Climb, Crossing, Climb Climb, Climb, ow Climb, Climb, ow Descent, Crossing, Descent Descent, Crossing, Descent Y Y Y TCA - Indicates climb, put AC symbol in green box TCA - Following a descent advisory, a reversal of vertical speed is necessary to provide adequate separation TCA - Descent, the airplane flightpath will cross intruder s altitude Descend, Descend Y TCA - Descent, put AC symbol in green box Descend, Descend, ow Descend, Descend, ow Y TCA - Following a climb advisory, a reversal of vertical speed is necessary to provide adequate separation Don t ink Y EPW - ink after takeoff EAR BAY OVERHEAT W 9 ML BAY OVHT/Main wheel well overheat lideslope Y EPW - Excessive deviation below glideslope Increase Climb Increase Climb Y TCA - Increase climb, put AC symbol in green box Increase Descent Increase Descent Y TCA - Increase descent, put AC symbol in green box LEFT EIE FIRE W 9 L E FIRE Minimums Y At minimum altitude selected on PFD Monitor Vertical peed Y TCA - Monitor vertical speed to keep AC symbol out of red prohibited areas 7-

23 VOICE MEAE - ALPHABETICAL W = WARI Y = YTEM /PFD IDICATIO VOICE MEAE TYPE CH.REF O TAKEOFF W 7 & COFI AIL TRIM COFI LAT/FLAP COFI TAB TRIM COFI RUD TRIM COFI POILER PARK BRAKE O Pull Up Y EPW - Corrective action after excessive descent rate during approach Maintain Vertical peed, Maintain Y TCA: tay in green box Maintain Vertical peed, Crossing Maintain Y TCA: tay in green box RIHT EIE FIRE W 9 R E FIRE elcal Y ELCAL HF, ELCAL VHF, ELCAL VHF, ELCAL VHF ink Rate Y EPW - Excessive descent rate during approach MOKE W 9 lobal Express lobal 5 MOKE AVIOIC BAY MOKE AVIOIC BAY MOKE CABI MOKE AV RACK MOKE BAAE MOKE BAAE MOKE FWD LAV MOKE CLOET MOKE AFT LAV MOKE FWD LAV MOKE CLOET MOKE AFT LAV Terrain, Terrain Y EPW - Excessive terrain closure Too Low Flap Y EPW - Insufficient flap, low altitude Too Low ear Y EPW - ear up, low altitude Too Low Terrain Y EPW - Terrain closure low altitude Traffic, Traffic Y TCA - Conduct visual search for intruder Windshear, Windshear Y EPW - WIDHR (decreasing performance) 5,, 5, Y EPW - Descending altitude callouts 7-

24 AURAL WARI TET Most aural alerts are exercised as part of their own system test. For all other aural alerts, an AURAL WARI TET can be initiated via the Electrical Management ystem Control Display Unit (EM CDU) located on the pilot s and copilot s side panel. There are two warning test selections provided to test the Integrated Avionics Computer (IAC and IAC ). Activation Key TET COTROL / FIRE TET TET TALL TET OFF AURAL WARI TET OFF AURAL WARI TET OFF LAMP TET OFF LAMP TET OFF M TET COTROL / FIRE TET OFF TALL TET OFF AURAL WARI TET OFF AURAL WARI TET OFF LAMP TET OFF LAMP TET OFF M CIRCUIT BREAKER TAT Y BU PREV PAE EXT PAE CTL YTEM TET BRT BU EMER COT CIRCUIT BREAKER TAT Y BU PREV PAE EXT PAE CTL YTEM TET BRT BU EMER COT X_7_ OTE: TET is initiated by pressing activation key and can be terminated by pressing activation key again. Test duration is seconds. OTE TET is initiated by pressing activation key and can be terminated by pressing activation key again. The test sequences through each tone and/or voice message in the following priority order: AURAL WARI TET aural or AURAL WARI TET TALL (stall shaker active) Continuous tone (overspeed) Triple Chime tone (any warning) O TAKEOFF LEFT EIE FIRE RIHT EIE FIRE APU FIRE MOKE CABI ALTITUDE EAR BAY OVERHEAT LEFT REVERER ULOCKED RIHT REVERER ULOCKED ORMAL BRAKE FAIL ingle Chime (any caution) 7-

25 EAR ingle Cavalry Charge tone (autopilot disengage) AUTOTHROTTLE aural C-chord tone (altitude alert - capture) Double C-chord (vertical track alert) Trim clacker (trim in motion) MIIMUM ELCAL AURAL WARI PAEL The aural warning panel, located on the overhead panel, is used to disable the tone/ aural generators located in IAC and IAC. Aurals for EPW and TCA will not be inhibited by muting the IACs. AURAL WARI IAC IAC MUTED MUTED PUH TO MUTE X_7_ IAC and IAC PUH TO MUTE witches Used to disable respective tone/aural generator located in respective IACs. IHIBIT During takeoff and landing, the IAC fault warning computer will process inhibit logic to minimize spurious or distracting messages. Warnings and status messages are not inhibited except for CABI ALT and APU OVERTEMP (T/O only), ORMAL BRAKE FAIL, BRAKE OVHT, CABI DELTA-P. During takeoff, the caution and advisory messages are inhibited when: Weight On Wheels; and Indicated airspeed transitions from less than 8 knots to greater than or equal to 8 knots The caution and advisory messages inhibit is removed: 5 seconds after Weight Off Wheels; or Pressure Altitude is greater than or equal to takeoff altitude +4 feet; or Indicated airspeed is less than 5 knots; or 7-

26 Takeoff inhibit has been active for consecutive seconds During landing, the caution and advisory messages are inhibited when: Landing gear down; and Radio altitude from feet to less than or equal to feet The caution and advisory message inhibit is removed: 5 seconds after air to ground transition; or Radio altitude greater than feet; or Indicated airspeed less than 5 knots The following caution messages are OT inhibited during takeoff and/or landing. AIRPLAE YTEM CAUTIO MEAE ADVIORY MEAE AFC Air Conditioning Pressurization Aural and Visual Warnings Electrical Power Doors and Exits Flight Controls Hydraulic Power Ice and Rain Protection Instruments AP TRIM is U (D) (Ldg only) AP TRIM LWD - RWD (Ldg only) YD - FAIL YD OFF EMER DEPRE L-R PACK FAIL CHECK DU () () (4) (5) () () () FAIL BATT MATER OFF CARO DOOR LARE ERV DOOR R EMER EXIT PAEER DOOR MALL ERV DOOR ELEVATOR PLIT FLT PLR DEPLOYED FLT POILER FAIL D LIFT DUMP ROLL ELECT ROLL POILER FAIL RUD AUTHORITY LOW LAT-FLAP FAIL TAB TRIM TALL PROTECT FAIL HYD () () LO PRE HYD RAT PUMP FAIL (Ldg only) ICE ADC () () MICMP ALL ADC MICMP YD OT CETERED (TO only) BATT EMER PWR O RAT E O (Ldg only) FLT POILER FAULT D LIFT DUMP O TAKEOFF (TO only) RUD AUTHORITY AFE HAKER () FAIL LAT-FLAP BIT LAT-FLAP HALFPD TALL WAR ADVACE ADC () () FAIL 7-4

27 AIRPLAE YTEM CAUTIO MEAE ADVIORY MEAE Landing ear Lighting avigation Power Plant BRAKE 5% DERADED CPLT BRAKE FAULT EAR DIAREE IBD BRK LO PRE L (R) IBD BRAKE FAIL L (R) OUTBD BRAKE FAIL OE TEER FAIL OUTBD BRK LO PRE PARK/EMER BRAKE O (Ldg only) PLT BRAKE FAULT UCOMMADED BRAKE EMER LIHT OFF ALL IR MICMP A/T OT I HOLD (TO only) L (R) FADEC CTL L (R) FUEL FILTER L (R) REV LOCK FAIL L (R) REVERER FAIL (Ldg only) BRAKE TEMP (TO only) EAR Y FAULT O TAKEOFF (TO only) A/T - FAIL 7-5

28 TAKEOFF COFIURATIO WARI Takeoff configuration warnings are armed when the airplane is on the ground and both engines are accelerated towards takeoff thrust (throttle position ). A voice warning, warning message, and both MATER WARI lights come on for any of the following: CODITIO VOICE MEAE MEAE Aileron trim outside of takeoff range O TAKEOFF COFI AIL TRIM Parking brake on during takeoff O TAKEOFF PARK BRAKE O Rudder trim outside of takeoff range O TAKEOFF COFI RUD TRIM Flaps not in takeoff position O TAKEOFF COFI LAT/FLAP poilers not in takeoff position O TAKEOFF COFI POILER Horizontal stabilizer outside of takeoff range ( green band ) O TAKEOFF COFI TAB TRIM All configuration warning indications are canceled when the configuration error is corrected, or the airplane is airborne, or either thrust lever is retarded. A O TAKEOFF CA Advisory message will indicate a configuration error prior to the throttles being advanced towards takeoff. LADI COFIURATIO WARI The EAR aural will sound if any gear is not down and locked and: The radio altitude is less than, feet AL and the descent rate is more than 4 feet per minute; or The radio altitude is less than 5 feet AL and either throttle is below 5º throttle lever angle and the flap position is º The radio altitude is less than 5 AL and both throttles are below 5º throttle lever angle and the flap position is not at º OTE The EAR aural can not be muted during any of these conditions. The Too Low ear (EPW) aural warning is heard if any landing gear is not down and locked with the radio altitude less than 5 feet AL and the indicated airspeed at less than 9 knots. 7-

29 If neither radio altimeter is valid, the EAR aural will sound if any gear is not down and locked and the airplane is below,5 feet. The landing gear horn may be muted by pressing the mute horn switch/light on the landing gear control panel. With both thrust levers at IDLE, (less than three degrees throttle lever angle) the horn cannot be muted. TALL WARI Warning of an impending stall is provided by independent stall protection systems. Both systems are energized in flight and deactivated on the ground through air/ground logic. The flight displays indicate airplane approach to stall speed by low speed cues (red band) on the primary flight displays (PFDs) airspeed tape. tall warnings are provided by an aural TALL, a TALL icon appears on the PFD and vibration of both control columns. If the airplane angle-of-attack continues to increase to the point of an aerodynamic stall, the stick pusher pushes the control column forward. For more information refer to Chapter FLIHT COTROL. 7-7

30 IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4 KDEF MA KABC - KHJ 4 4 KKLM KHJ KDEF + KKLM FL8 - LUF +9 FL BELOW TCA TET.5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB I.5.5 I O TAKEOFF PARK/EMER BRAKE O ED EAR mb/hpa ALT 5 IA FEET 4 KOT I H CKPT ( C) OXYE FWD CABI ( C) % OUTFLOW VALVE OPE OPE % % RPM AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4 KDEF MA KABC - KHJ 4 4 KKLM KHJ KDEF + KKLM FL8 - LUF +9 FL BELOW TCA TET.5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT REVERIO COTROL PAEL The reversion panel located on the pedestal can be used to revert the display to alternate display units, and to revert IRs, ADCs, and s. DU DU DU DU 4 DU 5 DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 5 :.5L FM CRZ EPR T/O YC D D D OUT ITT YC TART TART O O FF (PPH) 575O U TRIM 5 OIL TEMP 5 AIL 8 OIL PRE 8 7. TOTAL FUEL (LB) 455O LWD RWD 4OO OOOO 4OO D 5O TAB L RUDDER R BARO :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 PFD MFD YTEM MFD PFD PFD and PFD Reversion Knobs ORM PFD displayed on DU, PFD displayed on DU ALT PFD displayed on DU, PFD displayed on DU 5 ORM ALT ALT ORM ALT ALT ALT ORM Knob Used to revert display to alternate display units. PFD PFD IR and ADC Pushbuttons Used to revert IR and ADCs. PFD PFD IR ADC ADC IR ORM ALT ORM ALT ORM ALT X_7_4,, Knobs Used to revert applicable symbol generators to specific displays. 7-8

31 IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT I.5.5 I O TAKEOFF PARK/EMER BRAKE O ED EAR mb/hpa ALT 5 IA FEET 4 KOT I H CKPT ( C) OXYE FWD CABI ( C) % OUTFLOW VALVE OPE OPE % % RPM AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT PFD REVERIO DU DU 5 THRUT AP AEL ATT VAPP VAV ADC 4.54 CRZ EPR THRUT AP AEL ATT VAPP VAV ADC M FM DTK LOC 4 5 M 8 7. T/O YC 789 ITT YC D D D OUT TART TART O O FF (PPH) 575O U TRIM 5 OIL TEMP 5 AIL 8 OIL PRE 8 7. TOTAL FUEL (LB) 455O LWD RWD 4OO OOOO 4OO D 5O TAB L RUDDER R BARO M FM DTK LOC 4 5 M 8 PFD and PFD Reversion Knobs ALT PFD displayed on DU, PFD displayed on DU 5 ORM ALT ALT ORM ALT ALT ALT ORM PFD PFD PFD PFD IR ADC ADC IR ORM ALT ORM ALT ORM ALT X_7_5 7-9

32 IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4 KDEF MA KABC - KHJ 4 4 KKLM KHJ KDEF + KKLM FL8 - LUF +9 FL BELOW TCA TET.5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB I.5.5 I O TAKEOFF PARK/EMER BRAKE O ED EAR mb/hpa ALT 5 IA FEET 4 KOT I H CKPT ( C) OXYE FWD CABI ( C) % OUTFLOW VALVE OPE OPE % % RPM AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4 KDEF MA KABC - KHJ 4 4 KKLM KHJ KDEF + KKLM FL8 - LUF +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT REVERIO COTROL DU DU DU 4 DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 5 :.5L FM 5 5 TART O CRZ EPR T/O YC 789 ITT YC FF (PPH) OIL TEMP OIL PRE TOTAL FUEL (LB) 455O 4OO OOOO 4OO 5O D D D OUT TART O U 5 8 D TAB 7. TRIM LWD L AIL RUDDER O RWD R BARO :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 Reversion Knob ORM displayed on DU ALT displayed on DU 4 ALT displayed on DU ALT displayed on DU 5 ORM ALT ALT ORM ALT ALT ALT ORM PFD PFD PFD PFD IR ADC ADC IR ORM ALT ORM ALT ORM ALT X_7_ 7-

33 IA VOR ADF IA VOR ADF IA VOR ADF AT F ATT LE F T W AT F ATT LE F T W AT F ATT LE F T W RAD RAD RAD VTA E LOC VTA E LOC VTA E LOC ALT ALT ALT I O BEARI RA 9. 8M + TA4.5M-4 ET WX LX -4 O BEARI RA 9. 8M + TA4.5M-4 ET WX LX.5-4 KDEF MA KABC - KHJ 4 4 KDEF MA KABC - KHJ KKLM KHJ I KDEF + KKLM KHJ KDEF KKLM FL8 - LUF +9 FL BELOW TCA TET.5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB O TAKEOFF PARK/EMER BRAKE O ED + KKLM FL8 EAR - LUF +9 FL BELOW TCA TET.5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB mb/hpa mb/hpa mb/hpa ALT 5 IA FEET 4 KOT ALT 5 IA FEET 4 KOT ALT 5 IA FEET 4 KOT I H 9 9 I H 9 9 I H I CKPT ( C) OXYE CKPT ( C) OXYE.5 FWD CABI ( C) % OUTFLOW VALVE OPE OPE % % RPM FWD CABI ( C) % AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP OUTFLOW VALVE OPE OPE % % RPM.5 I AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O TAKEOFF PARK/EMER BRAKE O ED EAR O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX I -4 O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4.5 KDEF MA KABC - KHJ 4 4 KDEF MA KABC - KHJ KKLM KHJ KDEF + KKLM KHJ I KDEF KKLM FL8 + KKLM FL8 - LUF - LUF +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB O TAKEOFF PARK/EMER BRAKE O ED EAR IA VOR ADF IA VOR ADF IA VOR ADF AT F ATT LE F T W AT F ATT LE F T W AT F ATT LE F T W RAD RAD RAD VTA E LOC VTA E LOC VTA E LOC ALT ALT ALT REVERIO DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 5 :.5L FM 5 5 BARO TART O CRZ EPR T/O YC 789 ITT YC FF (PPH) OIL TEMP OIL PRE TOTAL FUEL (LB) 455O 4OO OOOO 4OO 5O D D D OUT TART O U 5 8 D TAB 7. TRIM LWD L AIL RUDDER O RWD R 5 :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 ALT displayed on DU 4 ALT ORM ALT ALT DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M CRZ EPR T/O YC 789 ITT YC D D D OUT TART TART O O FF (PPH) 575O U TRIM 5 OIL TEMP 5 AIL 8 OIL PRE 8 7. TOTAL FUEL (LB) 455O LWD RWD 4OO OOOO 4OO D 5O TAB L RUDDER R BARO :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 ALT displayed on DU ALT ORM ALT ALT DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 5 :.5L FM 5 5 BARO CRZ EPR T/O YC 789 ITT YC D D D OUT TART TART O O FF (PPH) 575O U TRIM 5 OIL TEMP 5 AIL 8 OIL PRE 8 7. TOTAL FUEL (LB) 455O LWD RWD 4OO OOOO 4OO D 5O TAB L RUDDER R M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 ALT displayed on DU 5 ALT ORM ALT ALT X_7_7 7-

34 REVERIO COTROL ORM ALT ALT ORM ALT ALT ALT ORM PFD PFD PFD PFD IR ADC ADC IR ORM ALT ORM ALT ORM ALT X_7_8,, Reversion Knobs ORM drives DU and DU ORM drives DU5 and DU ORM drives DU and DU4 7-

35 IA VOR ADF AT F ATT LE F T W RAD VTA E 5 ALT LOC KOP KKLM LUF KHJ KABC KDEF. 5M ET 5 9. KDVT : 5. M W. 5 ETE+ WX KKLM AT -5 T5. % KDEF KHJ TAT -4 85% FL8 TA 4 TAB 4 4 PD 45 LX TERR IHIB I TART 4OO.5 YC FF (PPH) OIL TEMP OIL PRE OOOO 5O TART 4OO.5 I ED EAR CKPT ( C) FWD AFT CAB ALT CABI ( C) CABI ( C) P CAB RATE LD ELEV OXYE % OUTFLOW VALVE OPE OPE % % RPM OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4 KDEF MA KABC - KHJ 4 4 KKLM KHJ KDEF + KKLM FL8 - LUF +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB IA VOR ADF AT F ATT LE F T W RAD VTA E 5 ALT LOC 9.9 REVERIO ORM drives DU and DU ORM drives DU5 and DU ORM drives DU and DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 TRU FM O CRZ EPR T/O ITT YC TOTAL FUEL (LB) 455O O U 5 8 D TAB O TAKEOFF PARK/EMER BRAKE O 789 D D D OUT 7. TRIM LWD L AIL RUDDER O RWD R :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 ORM ALT ORM ALT ORM ALT X_7_9 7-

36 IA VOR ADF AT F ATT LE F T W RAD VTA E 5 ALT LOC KOP KKLM LUF KHJ KABC KDEF. 5M ET 5 9. KDVT : 5. M W. 5 ETE+ WX KKLM AT -5 T5. % KDEF KHJ TAT -4 85% FL8 TA 4 TAB 4 4 PD 45 LX TERR IHIB I I TART 4OO TART.5 YC FF (PPH) OIL TEMP OIL PRE OOOO 5O.5 YC FF (PPH) OIL TEMP OIL PRE TART 4OO TART 4OO OOOO 4OO 5O.5 I.5 I ED EAR ED EAR CKPT ( C) FWD AFT CAB ALT CABI ( C) CABI ( C) P CAB RATE LD ELEV OXYE % OUTFLOW VALVE OPE OPE % % RPM CKPT ( C) FWD AFT CAB ALT CABI ( C) CABI ( C) P CAB RATE LD ELEV OXYE % OUTFLOW VALVE OPE OPE % % RPM OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4-4 KDEF KDEF MA MA KABC - KABC - KHJ 4 4 KHJ 4 4 KKLM KHJ KDEF KKLM KHJ KDEF + KKLM FL8 + KKLM FL8 - LUF - LUF +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB IA VOR ADF IA VOR ADF AT F ATT LE F AT F ATT LE F T W T W RAD RAD VTA E VTA E 5 ALT LOC ALT LOC 9.9 REVERIO (Cont) FAIL O CRZ EPR T/O ITT YC TOTAL FUEL (LB) 455O O U 5 8 D TAB O TAKEOFF PARK/EMER BRAKE O 789 D D D OUT 7. TRIM LWD L AIL RUDDER O RWD R :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 ORM ALT ORM ALT ORM ALT FAIL M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 TRU FM O CRZ EPR T/O ITT YC TOTAL FUEL (LB) 455O O U 5 8 D TAB O TAKEOFF PARK/EMER BRAKE O 789 D D D OUT 7. TRIM LWD L AIL RUDDER O RWD R :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 ORM ALT ORM ALT ORM ALT X_7_ 7-4

37 IA VOR ADF AT F ATT LE F T W RAD VTA E 5 ALT LOC 9.9 I 4OO I TART TART.5 YC FF (PPH) OIL TEMP OIL PRE OOOO 5O.5 YC FF (PPH) OIL TEMP OIL PRE TART 4OO TART 4OO OOOO 4OO 5O.5 I.5 I ED EAR ED EAR CKPT ( C) FWD AFT CAB ALT CABI ( C) CABI ( C) P CAB RATE LD ELEV OXYE % OUTFLOW VALVE OPE OPE % % RPM OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4 KDEF MA KABC - KHJ 4 4 KKLM KHJ KDEF + KKLM FL8 - LUF +9 FL BELOW TCA TET.5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB IA VOR ADF AT F ATT LE F T W RAD VTA E 5 ALT LOC 9.9 REVERIO (Cont) - FAIL.54 CRZ EPR.54 O TAKEOFF PARK/EMER BRAKE O O T/O ITT YC TOTAL FUEL (LB) 455O D D D OUT O U 5 8 D TAB 7. TRIM LWD L AIL RUDDER O RWD R ORM ALT ORM ALT ORM ALT - FAIL With a dual ymbol enerator failure the remaining ymbol enerator will always drive DU, DU, DU5 and DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M O CRZ EPR T/O ITT YC TOTAL FUEL (LB) 455O O U 5 8 D TAB O TAKEOFF PARK/EMER BRAKE O 789 D D D OUT 7. TRIM LWD L AIL RUDDER O RWD R 5 :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 ORM ALT ORM ALT ORM ALT X_7_ 7-5

38 ADC REVERIO ADC witches Used to select reversion on appropriate ADC. ORM ALT PFD ALT ORM ALT ALT ALT ORM PFD PFD PFD PFD AUCIATIO IR ADC ADC IR ORM ALT ORM ALT ORM ALT PILOT ELECTED ADC Pilot s ide ormally fed as follows: ADC ifreverted then ADC if reverted then ADC COPILOT ELECTED ADC PFD OURCE AUCIATIO PFD OURCE AUCIATIO ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC ADC X_7_4 Copilot s ide ormally fed as follows: ADC if reverted then ADC if reverted then ADC 7-

39 IR REVERIO IR witches Used to select reversion on appropriate IR ORM ALT PFD ALT ORM ALT ALT ALT ORM PFD ATT PFD PFD IR ADC ADC IR PFD AUCIATIO ORM ALT ORM ALT ORM ALT Pilot s ide ormally fed as follows: IR if reverted then IR if reverted then IR Copilot s ide ormally fed as follows: IR if reverted then IR if reverted then IR PILOT ELECTED ADC COPILOT ELECTED ADC PFD OURCE AUCIATIO PFD OURCE AUCIATIO MFD OURCE AUCIATIO MFD OURCE AUCIATIO IR IR ATT ATT MA MA IR IR IR IR ATT ATT IR IR ATT ATT MA MA IR IR ATT IR IR ATT ATT IR IR ATT ATT MA MA IR IR ATT ATT IR IR ATT X_7_4 7-7

40 COTROL PAEL The control panel located on the pedestal, can be used to revert YTEM display, scroll non-displayed messages, and to display YTEM synoptic pages. BLEED Button Used to display BLEED/ATI-ICE synoptic. HYD Button Used to display HYDRAULIC synoptic. DC ELEC Button Used to display DC ELECTRICAL synoptic. FLT CTRL Button Used to display FLIHT COTROL synoptic. AIR COD Button Used to display AIR CODITIOI synoptic. AC ELEC Button Used to display AC ELECTRICAL synoptic. FUEL Button Used to display FUEL synoptic. BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_ CROLL Knob Used to scroll out of view and/or scroll into view all messages, except for warning messages TAT Button Used to display status synoptic. YTEM ELECT Knob Used to revert YTEM display to alternate displays. 7-8

41 IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT 4 KOP KKLM LUF KHJ KABC KDEF.5M ET 5 9. KDVT : 5. M W.5 ETE+ WX KKLM AT -5 T5.% KDEF KHJ TAT -4 85% FL8 TA 4 TAB 4 4 PD 45 LX TERR IHIB I.5 FF (PPH) OIL TEMP OIL PRE.5 I O TAKEOFF PARK/EMER BRAKE O ED EAR mb/hpa ALT 5 IA FEET 4 KOT I H CKPT ( C) OXYE FWD CABI ( C) % OUTFLOW VALVE OPE OPE % % RPM AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX -4 KDEF MA KABC - KHJ 4 4 KKLM KHJ KDEF + KKLM FL8 - LUF +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB IA VOR ADF AT F ATT LE F T W RAD VTA E LOC ALT YTEM ELECT COTROL DU DU DU DU 4 DU 5 DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 TRU FM CRZ EPR T/O YC D D D OUT ITT YC TART TART O O 575O U TRIM 5 5 AIL TOTAL FUEL (LB) 455O LWD RWD 4OO OOOO 4OO D 5O TAB L RUDDER R BARO :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 PFD MFD YTEM MFD PFD BLEED AIR COD HYD AC ELEC DC ELEC FUEL FLT CTRL ORM MFD MFD CROLL TAT YTEM ELECT X_7_ YTEM ELECT Knob ORM YTEM displays on DU4 MFD YTEM displayed on DU MFD YTEM displayed on DU5 7-9

42 IA VOR ADF IA VOR ADF AT F ATT LE F AT F ATT LE F T W T W RAD RAD VTA E VTA E LOC LOC ALT ALT CKPT ( C) OXYE 4 FWD CABI ( C) % OUTFLOW VALVE OPE OPE % % RPM KOP KKLM AFT CAB ALT CABI ( C) P CAB RATE LD ELEV LUF KHJ KABC KDEF.5M ET 5 9. KDVT : 5. M W.5 ETE+ WX KKLM AT -5 T5.% KDEF KHJ TAT -4 85% FL8 TA 4 TAB 4 4 PD 45 LX TERR IHIB OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP I I.5 FF (PPH) OIL TEMP OIL PRE.5 FF (PPH) OIL TEMP OIL PRE.5 I.5 I O TAKEOFF PARK/EMER BRAKE O ED EAR O TAKEOFF PARK/EMER BRAKE O ED EAR mb/hpa mb/hpa ALT 5 IA ALT 5 IA FEET FEET 4 KOT 4 KOT I H 9 9 I H CKPT ( C) OXYE CKPT ( C) OXYE FWD CABI ( C) % OUTFLOW VALVE OPE OPE % % RPM FWD CABI ( C) % AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP OUTFLOW VALVE OPE OPE % % RPM AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP O BEARI RA 9. 8M + TA 4. 5M -4 ET WX LX CKPT ( C) OXYE -4 FWD CABI ( C) % KDEF OUTFLOW VALVE OPE OPE % % RPM MA KABC - KHJ 4 4 KKLM KHJ KDEF + AFT CAB ALT CABI ( C) P CAB RATE LD ELEV OIL QTY (QT) E APU RE APU DOOR. ET BRAKE TEMP KKLM FL8 - LUF +9 FL BELOW TCA TET. 5M KDVT ETE + AT -5 TAT -4 TA 4 PD 45 TERR IHIB IA VOR ADF IA VOR ADF AT F ATT LE F AT F ATT LE F T W T W RAD RAD VTA E VTA E LOC LOC ALT ALT YTEM ELECT DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M TART O CRZ EPR T/O YC 789 ITT YC TOTAL FUEL (LB) 455O 4OO OOOO 4OO 5O D D D OUT TART O U 5 8 D TAB 7. TRIM LWD L AIL RUDDER O RWD R BARO :.5L FM M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 YTEM MFD YTEM displayed on DU ORM MFD MFD YTEM ELECT DU M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 TRU FM CRZ EPR T/O YC 789 ITT YC D D D OUT TART TART O O 575O U TRIM 5 5 AIL TOTAL FUEL (LB) 455O LWD RWD 4OO OOOO 4OO D 5O TAB L RUDDER R BARO M FM DTK LOC THRUT AP AEL ATT VAPP VAV ADC M 8 YTEM MFD YTEM displayed on DU5 ORM MFD MFD YTEM ELECT X_7_4 OTE: When YTEM ELECT is reverted to either MFD or MFD, all system synoptics can be displayed on the applicable DU. 7-4

43 FLIHT DATA RECORDER channels aircraft systems data (including altitude, airspeed, heading, acceleration, and radio communications events) to the Flight Data Recorder (FDR). DAU 4 gathers sensor data for transmission to the FDR. DAU 4 is fully self-monitoring and provides CA messages in the event of a failure. If DAU 4B channel fails, FDR information is not available. To record an additional event, in the FDR, push the PILOT EVET button on the landing gear control panel located on the pedestal. Pushing the PILOT EVET will also encode the Central Aircraft Information Maintenance ystem (CAIM). CETRAL AIRCRAFT IFORMATIO AD MAITEACE YTEM (CAIM) The CAIM collects diagnostic and fault data from other airplane systems. From this data, the CAIM assembles a fault record that can be used to monitor system performance during the flight. Maintenance personnel use CAIM to accomplish system tests and to isolate defective components. The CAIM supplies fault data during all phases of airplane operation through the Portable Maintenance Access Terminal (PMAT) touch screen located in the passenger cabin. The PMAT hard-disk contains approximately 8 MB of operational software files and 5 MB of loadable diagnostic files. A CD-ROM of the Aircraft Maintenance manual (AMM) can be installed in the PMAT CD-ROM drive. The crew has the option of monitoring the PMAT display for active faults and/or may print the report on the cockpit printer. For more information on the printer, refer to chapter 5 COMMUICATIO. The CAIM is comprised of the following components: PMAT (located in the cabin) 7-4

44 Power witch Mode / Fault Annunciation.5" Disk Drive Access Port POWER HARD DRIVE FAULT OVER TEMP AM- PORTABLE MAITEACE ACCE TERMIAL X_7_5 International Inc. International Inc. AM AM CD ROM Drive Access Port DATA UPLOAD/DOWLOAD switch and PRIT MAIT REPORT switch (located on bulkhead behind pilot) 7-4

45 PRIT MAIT REPORT CAIM PRIT MAIT REPORT witch Used to get a report of active faults from the cockpit printer. DATA UPLOAD/DOWLOAD DATA ELECTOR witch Used to select system to upload/download a copy of non-volatile data on to a.5-inch disk. DAU A DAU B DAU A DAU B DAU A DAU B DAU 4A DAU 4B IR IR IR WXR IAC IAC IAC PW ATCOM DU P P ADC ADC ADC Pilot Event Marker (located on the landing gear control panel). OE TEER ARMED LD EAR OFF HOR MUTED BTM OVHT WAR REET D LCK RELEAE UP D EVET FDR/CAIM Event Button Used to record additional data in non-volatile memory of CAIM. X_7_8 7-4

46 MEAE UMMARY OTE A single message or a combined message can be displayed on a message line, up to a maximum of 8 characters. Example: L REVERER ULKD or R REVERER ULKD or L-R REVERER ULKD. WARI MEAE (RED) CA MEAE DECRIPTIO OUD/VOICE CH. APU FIRE APU fire APU FIRE 9 APU OVERPEED Annunciated when an APU overspeed protective shutdown occurs 4 APU OVERTEMP Annunciated when an APU ET overtemperature condition occurs 4 BRAKE OVHT One or more hot brakes resulting in wheels at fuse plug release temperature during low speed portion of takeoff or landing/taxi 4 CABI ALT Excessive cabin altitude. ote: Warning level is normally set at 9 feet except when a/c takes off or lands at higher altitudes CABI ALTITUDE CABI DELTA P Excessive cabin differential pressure (positive or negative) CHECK PFD COFI AIL TRIM COFI RUD TRIM COFI LAT/FLAP COFI POILER COFI TAB TRIM DUAL EIE OUT EMER PWR OLY Data wrap-around failed on both PFDs. Both PFDs may have misleading data Displayed during T.O., aileron trim is out of the certified range (green band) Displayed during T.O., rudder is out of the certified range (green band) Flaps are not at either or during takeoff. lats are not at out during takeoff Displayed during T.O. A spoiler is deployed for uses other than roll assistance. This happens in case of proportional lift dumping, LD operation, uncommanded or MF deployment Displayed during T.O. Pitch trim is out of the certified range (green band) Double engine flameout Either of the batteries are powering the DC E Bus and BATT Bus or the RAT Line Connector (LC) is in the RAT position 7 O TAKEOFF 7/ O TAKEOFF 7/ O TAKEOFF 7/ O TAKEOFF 7/ O TAKEOFF 7/ 7-44