Global 5000 Flight Crew Operating Manual (Volume 2)

BOMBARDIER GLOBAL 5000 · Pilot's Operating Handbook

Free account — keep the POHs & checklists you reference in one place.

Overview

This document is the Flight Crew Operating Manual for the Bombardier Global 5000, detailing the aircraft's central display system and crew alerting messages. It covers the functionalities of the Engine Indication and Crew Alerting System (EICAS), including aural and visual warnings, and the display of critical aircraft information.

The EICAS provides critical engine and system monitoring displays.
Crew alerting messages are categorized into warnings, cautions, advisories, and status messages.
The central display system integrates data from multiple aircraft systems for crew use.
EICAS displays up to 24 messages, with a pop-up for Gear/Slats/Flaps.
Warning messages require immediate crew action and are prioritized in the display.
Caution messages indicate the need for crew awareness and may require action.
Advisory messages inform the crew of non-critical issues without an aural alert.
Status messages serve as reminders for non-normal pilot selections.

Document

Source

Originally published by com.br. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at com.br

Report a problem or request removal

Document details

Type: Pilot's Operating Handbook
Year: 2005
File size: 1.7 MB
Publisher: com.br
Language: en

About this document

What is the Global 5000 Flight Crew Operating Manual (Volume 2)?

The Global 5000 Flight Crew Operating Manual (Volume 2) is a pilot's operating handbook for the BOMBARDIER GLOBAL 5000, dated 2005.

Where does the Global 5000 Flight Crew Operating Manual (Volume 2) come from?

This copy of the Global 5000 Flight Crew Operating Manual (Volume 2) was originally published by com.br and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Global 5000 Flight Crew Operating Manual (Volume 2) published?

The Global 5000 Flight Crew Operating Manual (Volume 2) — the BOMBARDIER GLOBAL 5000 pilot's operating handbook on file — is dated 2005.

Documentation completeness

2/7

Most owners only have the POH. Here's the essential set for the BOMBARDIER GLOBAL 5000.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins on file
Type Certificate (TCDS)

More BOMBARDIER GLOBAL 5000manuals & documents

In this document

General

The aural and visual warning system provides indications for unsafe operating conditions, system malfunctions, and non-normal situations, utilizing various subsystems.

Central Display System

The central display system offers displays for aircraft control, navigation, and engine monitoring, transmitting data through a dual-channel system.

Crew Alerting Messages

EICAS monitors systems and displays crew alerting messages categorized by urgency, with warnings requiring immediate action and advisories indicating non-critical issues.

EICAS Display

The EICAS display unit shows primary engine parameters, fuel quantities, and system statuses, with a maximum of 24 messages displayed.

Message Prioritization

Messages are prioritized in the EICAS display, with warnings at the top, followed by cautions, advisories, and status messages.

Aural Alerts

Different aural alerts accompany warning and caution messages, with warnings triggering a unique tone or triple chime.

Safety notes

Warning messages cannot be removed until the failure is rectified.
Caution messages can be paged and scrolled from view but require crew awareness.
Advisory messages flash for 5 seconds before becoming steady.
Status messages do not have an aural alert and can be scrolled from view.

Full document text

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 03−10−17 Aural Warning Panel 03−10−18 Inhibits 03−10−18 Central Aircraft Information and Maintenance System (CAIMS) 03−10−21 Flight Data Recorder 03−10−23 Stall Warning 03−10−23 Take-off Configuration Warnings 03−10−24 Landing Configuration Warning 03−10−25 EICAS Display 03−10−26 Systems Display (STAT Page) 03−10−27 Reversion Control Panel 03−10−28 PFD Reversion Control 03−10−29 PFD Reversion 03−10−30 EICAS Reversion Control 03−10−31 EICAS Reversion 03−10−32 SG Reversion Control 03−10−33 SG Reversion 03−10−34 EICAS Control Panel 03−10−37 Systems Reversion Control 03−10−38 Message Scrolling 03−10−40 Systems Synoptics 03−10−41 STAT Page 03−10−41 Bleed/Anti-Ice Synoptic Page 03−10−42 Air Conditioning Synoptic Page 03−10−43 Hydraulic Synoptic Page 03−10−44 AC Electrical Synoptic Page 03−10−45 DC Electrical Synoptic Page 03−10−46 Fuel Synoptic Page 03−10−47 AURAL AND VISUAL WARNINGS TABLE OF CONTENTS CHAPTER 3 03−00−1 Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−00−1 Page TABLE OF CONTENTS DESCRIPTION Flight Controls Synoptic Page 03−10−48 Aural and Visual Warning EICAS Messages 03−10−49 EMS CIRCUIT PROTECTION CB − Ind/Record System 03−20−1 CB − CAIMS System 03−20−2 AURAL AND VISUAL WARNINGS TABLE OF CONTENTS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−00−2 Page GENERAL 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 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, control surface monitoring and all major sub-system synoptic displays. During normal operation, the engine and control surface information is displayed on the EICAS display unit (DU3) and the system synoptic information is displayed on the SYSTEMS display (DU4). GF0310_001 DU 1 DU 2 DU 3 DU 4 DU 5 DU 6 PFD 1 MFD 1 EICAS SYSTEMS MFD 2 PFD 2 VS 2000 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 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 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−1 CENTRAL DISPLAY SYSTEM The central display system provides crew with displays for aircraft control, navigation, engine control and monitoring and systems synoptic. Other systems information provided for display are WX display, 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, with both channels updating data at the same time. The ASCB is the principal communications network interconnecting the system components. Data traffic flow on the ASCB is managed by 3 bus controllers (one bus controller in each IAC). Only one bus 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). The SGs process data from various sources and output the data to the 6 DUs. The FWC compares sensor input data, verifies all critical display data and displays warning, caution, advisory and status messages 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 Autothrottle AFCS AFCS AFCS AURAL AND VISUAL WARNINGS

Show full text

Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−2 CREW ALERTING MESSAGES The crew alerting system portion of EICAS continually monitors all airplane systems. If an operationally significant fault occurs on a system, EICAS displays a crew alerting message on the EICAS display unit. In addition to the display messages, some crew alerts are also indicated by aural tones, 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 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 EICAS primary display. All warnings cause the MASTER WARNING lights on the glareshield to flash and have an aural alert consisting of a unique 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 MASTER WARNING/CAUTION WARNING CAUTION Warning messages cannot be removed from view, unless the applicable failure has been rectified. If a 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. Caution messages are generated when immediate crew awareness is required and subsequent crew action will be required. Caution messages appear immediately below the warnings in the message stack on the EICAS display. All cautions cause the MASTER CAUTION lights on the glareshield to flash and have an aural alert consisting of a single chime. Once acknowledged flashing stops . L ENG SHUTDOWN Glareshield EICAS Display Aural Single Chime GF0310_005 MASTER WARNING/CAUTION WARNING CAUTION Caution messages can be paged and scrolled from view, using SCROLL knob on EICAS control panel. If a new abnormal situation occurs, the corresponding caution message will flash and 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 be displayed at the top of the stack. EICAS Control Panel Scroll Knob AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−3 CREW ALERTING MESSAGES (CONT'D) Advisory messages are generated when crew awareness is required and subsequent crew action may be required. Advisory messages appear immediately below the cautions in the message stack on the EICAS display. When a new advisory message appears, it will flash for 5 seconds, then steady. There is no aural alert for advisory messages. GF0310_007 L REVERSER FAULT EICAS Display Advisory messages can be paged and 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. 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. GF0310_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 up displayed. With the Gear/Slats/Flaps pop up not displayed, the window can display up to 24 messages. FGF0310_003 TOTALFUEL(LBS) 789 789 N1 CRZ EPR 73.3 73.3 1.65 1.65 NU TRIMS FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 ITT 14600 41550 10000 14600 ND STAB RUDDER NL LWD RWD NR 1.54 1.54 7.5 GEAR OUT 30 DN 789 789 N1 CRZ EPR 73.3 73.3 1.65 1.65 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 ITT 1.54 1.54 7.2 93.4 5750 115 81 DN DN TOTALFUEL(LBS) NU TRIMS 14600 41550 10000 14600 ND STAB RUDDER NL LWD RWD NR 14 Messages Gear/Slats/ Flaps Pop Up 24 Messages N2 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−4 CREW ALERTING MESSAGES (CONT'D) If there are non-displayed messages above the top of the display or below the bottom of the display XXX↑ messages ↓XXX symbols will appear at the bottom of message window. The number of non-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 highest level of messages not displayed. Warning messages are not part of the colour logic. GF0310_010 789 789 ITT 789 789 AC BUS 1 FAIL LATERAL MODE OFF L REVERSER UNLKD MACH TRIM FAIL 14 MESSAGES 6 NW STEERING FAIL MACH TRIM FAIL 789 789 ITT PITCH DISC FAULT R OIL FILTER R ENG BLEED OFF TRIM AIR OFF IAC 1 WOW INOP R OIL LO PRESS R FADEC FAIL N1 END 10 MESSAGES 0 14 MESSAGES 6 10 MESSAGES 0 END AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−5 CREW ALERTING MESSAGES (CONT'D) FGF0310_007 APU FIRE APU OVERSPEED 5 APU OVERTEMP 5 BRAKE OVHT 15 CABIN ALT 2 CABIN DELTA P 2 CHECK PFD 11 CONFIG AIL TRIM 10 CONFIG RUD TRIM 10 CONFIG SLAT/FLAP 10 CONFIG SPOILERS 10 CONFIG STAB TRIM 10 DUAL ENGINE OUT 18 EMER PWR ONLY 7 GEAR 15 L ENG FIRE 9 L OIL LO PRESS 18 L REVERSER UNLKD 18 MLG BAY OVHT 9 NORM BRAKE FAIL 15 PARK/EMER BRAKE ON 15 R ENG FIRE 9 R OIL LO PRESS 18 R REVERSER UNLKD 18 SMOKE AFT LAV 9 SMOKE AVIONICS BAY 9 SMOKE BAGGAGE 9 SMOKE FWD LAV SMOKE CABIN SMOKE CLOSET SMOKE CLOSET FWD SMOKE CLOSET AFT WING A/ICE OVHT EICAS WARNING MESSAGES Chapt. Ref. NOTE A 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 9 9 9 9 9 14 AV RACK OVHT 2 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−6 CREW ALERTING MESSAGES (CONT'D) AC BUS 1 FAIL 7 AC BUS 2 FAIL 7 AC BUS 3 FAIL AC BUS 4 FAIL AC ESS BUS FAIL ADC 1 MSCMP 11 ADC 2 MISCMP ADC 3 MISCMP AFCS ENGAGE INVAL ALL ADC MISCMP ALL IRS MISCMP AP TRIM IS LWD AP TRIM IS RWD AP TRIM IS ND AP TRIM IS NU AP PITCH TRIM FAIL APU BATT FAIL APU BLEED SYS FAIL APU DOOR FAIL APU EGT SENSORS APU FIRE FAIL APU FUEL SOV APU GEN OVERHEAT APU GEN OVLD APU OIL HI TEMP APU OIL LO PRESS APU REVERSE FLOW ASCB FAIL A/T NOT IN HOLD AUTOBRAKE FAIL AUTO PRESS FAIL AV BATT FAIL BATT BUS FAIL BATT MASTER OFF BRAKE 50% DGRADED CABIN ALT CARGO DOOR CAT 2 INVALID CB TRIP AC FEED CB TRIP DC FEED CHECK DU 1 CHECK DU 2 CHECK DU 3 CHECK DU 4 CHECK DU 5 CHECK DU 6 CPLT BRAKE FAULT CTR FUEL XFER FAIL DC BUS 1 FAIL DC BUS 2 FAIL DC EMER BUS FAIL Chapt. Ref. EICAS CAUTION MESSAGES DOOR SYS FAIL ELT TRANSMITTIG EMER DEPRESS EMER LIGHTS OFF ELEVATOR SPLIT FIRE BTL1 LO PRESS FIRE BTL2 LO PRESS FLAP FAIL FLT SPOILERS FAIL FLT SPLR DEPLOYED FUEL COMPUTR FAIL FUEL IMBALANCE FUEL LO QTY FUEL TEMP SENSOR FUEL UNIT MISMATCH GEAR DISAGREE GEAR SYS FAIL GEN 1 OVLD GEN 2 OVLD GEN 3 OVLD GEN 4 OVLD GND LIFT DUMP HUD FAIL HUD MISCOMPARE HYD 1 HI TEMP HYD 2 HI TEMP HYD 3 HI TEMP HYD 1 LO PRESS HYD 2 LO PRESS HYD 3 LO PRESS HYD 1 LO QTY HYD 2 LO QTY HYD 3 LO QTY HYD 3 OVERFILLED HYD RAT PUMP FAIL IAC 1 OVHT IAC 2 OVHT IAC 3 OVHT ICE ICE DETECTOR FAIL INBD BRK LO PRESS IRS 1 MSCMP IRS 2 MSCMP IRS 3 MSCMP IRS 1 OVHT IRS 2 OVHT IRS 3 OVHT IRS 1 SET HDG IRS 2 SET HDG IRS 3 SET HDG Chapt. Ref. NOTE A single message or a combined message can be displayed on a message line, up to a maximum of 18 characters. FGF0310_008 Example: DU 1 FAN or DU 2 FAN or DU 3 FAN or DU 1−2−3 FAN 7 7 7 11 11 4 11 11 4 4 4 4 4 7 2 5 5 9 12 7 7 5 5 5 11 18 15 2 7 7 7 15 2 1 17 7 7 3 3 3 3 3 3 15 12 7 7 7 16 1 6 2 10 9 9 10 10 10 12 12 12 12 12 15 15 7 7 7 7 10 11 11 13 13 13 13 13 13 13 13 13 13 13 3 3 3 14 14 15 11 11 11 11 11 11 11 11 11 ASCB CTRL 3 FAIL 11 ASCB CTRL 2 FAIL 11 ASCB CTRL 1 FAIL 11 AV FANS FAIL 2 CTR TANK FULL 12 DC ESS BUS FAIL 7 DISP CTRLS FAIL 11 EVS FAIL EVS HEAT FAIL EVS HEAT OVHT 11 11 11 Chapt. Ref. FUEL XFER ON FUEL XFER ON FUEL XFER FAIL FUEL XFER FAIL 12 12 12 12 INT CABIN DOOR 1 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−7 CREW ALERTING MESSAGES (CONT'D) EICAS CAUTION MESSAGES Chapt. Ref. Chapt. Ref. LARGE SERV DOORS L AOA HEAT FAIL L BLEED LEAK L BLEED SYS FAIL L COWL A/ICE FAIL L EMER EXIT L ENG FIRE FAIL L ENG FLAMEOUT L ENG FUEL LO TEMP L ENG FUEL SOV L ENG OVHT L ENG OVERSPED L ENG SAV FAIL L FADEC FAIL L FADEC N1 CTL L FADEC OVHT L FUEL FILTER L FUEL LO PRESS L FUEL RECIRC FAIL L HYD SOV FAIL L INBD BRAKE FAIL L MAIN GEAR DOOR L OIL LO QTY L OUTBD BRAKE FAIL L PACK AUTO FAIL L PACK FAIL L PACK TEMP L PRI FUEL PUMPS L REVERSER FAIL L REV LOCK FAIL L START ABORTED L THROTTLE FAIL L WINDOW HEAT FAIL L WING A/ICE FAIL L WING FULL L WSHLD HEAT FAIL MACH TRIM FAIL MLG BAY OVHT FAIL NOSE DOOR NOSE STEER FAIL OUTBD BRK LO PRESS OXYGEN LO QTY Chapt. Ref. PARK/EMER BRAKE ON PASSENGER DOOR PITOT 1 HT FAIL PITOT 2 HT FAIL PITOT 3 HT FAIL PLT BRAKE FAULT RAT GEN FAIL R AOA HEAT FAIL R BLEED LEAK R BLEED SYS FAIL R COWL A/ICE FAIL R EMER EXIT R ENG FIRE FAIL R ENG FLAMEOUT R ENG FUEL LO TEMP R ENG FUEL SOV R ENG OVHT R ENG OVERSPED R ENG SAV FAIL R FADEC FAIL R FADEC N1 CTL R FADEC OVHT R FUEL FILTER R FUEL LO PRESS R FUEL RECIRC FAIL R HYD SOV FAIL R INBD BRAKE FAIL R MAIN GEAR DOOR R OIL LO QTY R OUTBD BRAKE FAIL R PACK AUTO FAIL R PACK FAIL R PACK TEMP R PRI FUEL PUMPS R REVERSER FAIL R REV LOCK FAIL R START ABORTED R THROTTLE FAIL R WINDOW HEAT FAIL R WING A/ICE FAIL R WING FULL R WSHLD HEAT FAIL ROLL SELECT ROLL SPOILERS FAIL RUD AUTHORITY HIGH RUD AUTHORITY LOW RUD 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 FAIL SG 2 FAIL SG 3 FAIL SLAT−FLAP FAIL SLAT−FLAP FAULT SMALL SERV DOORS SMOKE AFT LAV FAIL SMOKE AV BAY FAIL SMOKE BAGGAGE FAIL SMOKE CABIN FAIL SMOKE CLOSET FAIL SMOKE CLO FWD FAIL SMOKE CLO AFT FAIL SMOKE FWD LAV FAIL SPLR LEVER FAIL STAB TRIM STALL PROTECT FAIL STBY PITOT HT FAIL TRIM AIR FAIL TRIM AIR LEAK UNCOMMANDED BRAKE WING A/ICE LO HEAT WING A/ICE LEAK WING FUEL HI TEMP WING FUEL LO TEMP WING TO CTR LEAK WOW FAIL XBLEED FAIL YD 1 FAIL YD 2 FAIL YD OFF GF0310_013a 1 14 2 2 14 1 9 18 18 18 18 18 18 18 18 18 18 18 12 13 15 15 18 15 2 2 2 12 18 18 18 18 14 14 12 14 10 9 15 15 15 8 15 1 14 14 14 15 7 14 2 2 14 1 9 18 18 18 18 18 18 18 18 18 18 18 12 13 15 15 18 15 2 2 2 12 18 18 18 18 14 14 12 14 10 10 10 10 10 3 3 3 10 10 1 9 9 9 9 9 9 9 9 10 10 10 14 2 2 15 14 14 12 12 12 15 2 4 4 4 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−8 CREW ALERTING MESSAGES (CONT'D) AC BUS 1 XFER FAULT AC BUS 2 XFER FAULT AC BUS 3 XFER FAULT AC BUS 4 XFER FAULT ADC 1 FAIL ADC 2 FAIL ADC 3 FAIL ADC 1 DEGRADED ADC 2 DEGRADED ADC 3 DEGRADED AFCS 1 FAIL AFCS 2 FAIL AP 1 FAIL AP 2 FAIL APU BATT CHGR FAIL APU BLEED DISABLED APU FADEC FAIL APU FAULT APU FIRE FAULT APU GEN FAIL APU IN BITE APU NOT AVAILABLE APU OIL LO QTY APU SHUTDOWN APU SQUIB 1 FAIL APU SQUIB 2 FAIL ASCB FAULT ASCB CTLR 1 FAULT ASCB CTLR 2 FAULT ASCB CTLR 3 FAULT AT 1 FAIL AT 2 FAIL AT ADC MISCMP AT IRS MISCMP ATS ENVELOPE AUTO PRESS FAULT AV BATT CHGR FAIL AVIONIC FAN FAIL BATT BUS XFER FAULT BATT EMER PWR ON BLEED MISCONFIG BRAKE FAULT BRAKE TEMP CAB ALT LEVEL HI CB TRIP CHECKLIST MISMATCH CTR XFER FAULT EICAS ADVISORY MESSAGES Chapt. Ref. DAU 1A FAIL DAU 1B FAIL DAU 2A FAIL DAU 2B FAIL DAU 3A FAIL DAU 3B FAIL DAU 4A FAIL DAU 4B FAIL DC BUS 1 XFER FAULT DC BUS 2 XFER FAULT DC ESS XFER FAULT DU 1−2−3−4−5−6 FAN ELEC SYS FAULT ENG SYNC FAIL ENG SYNC LIMIT ESS TRU 1 FAIL ESS TRU 2 FAIL EXT AC PWR AVAIL EXT DC PWR AVAIL FCU FAULT FDR ACCEL FAIL FDR FAIL FIRE SYS FAULT FLAP DRIVE OVHT FLAP HALFSPD FLT SPOILERS FAULT FMS 1 FAIL FMS 2 FAIL FMS 3 FAIL FUEL COMPUTR FAULT FUEL QTY DEGRADED FUEL RECIRC ON GEAR SYS FAULT GEN 1 FAIL GEN 2 FAIL GEN 3 FAIL GEN 4 FAIL GND LIFT DUMP GND PROX FAIL GPWS SYSTEM FAIL HUD FAN FAIL HUD MISALIGN HYD EDP 1A FAIL HYD EDP 2A FAIL HYD PUMP 3A FAIL HYD PUMP 1B FAIL HYD PUMP 2B FAIL HYD PUMP 3B FAIL Chapt. Ref. NOTE A 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 FGF0310_009 FUEL XFER ON XFER VALVE OPEN XFER VALVE OPEN FUEL XFER ON 7 7 7 7 11 11 11 11 11 11 4 4 4 4 7 5 5 5 9 7 5 5 5 5 9 9 11 11 11 11 18 18 18 18 18 2 7 2 7 7 2 15 15 2 7 3 12 3 3 3 3 3 3 3 3 7 7 7 3 7 18 18 7 7 7 7 10 4 4 9 10 10 10 17 17 17 12 12 12 12 12 12 12 15 7 7 7 7 10 17 17 11 13 13 13 13 13 13 11 AV FANS FAIL AV RACK FAN FAIL 2 2 EVS DEFOG FAULT 11 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−9 CREW ALERTING MESSAGES (CONT'D) RECIRC FAN FAIL REVRSION CTLR FAIL R AUX FUEL PUMP R BLEED FAULT R COWL A/ICE FAULT R ENG FIRE FAULT R ENG SQUIB 1 FAIL R ENG SQUIB 2 FAIL R FADEC FAULT R FUEL FILTER R OIL FILTER R PACK FAULT R PRI FUEL PUMP R POBE MON FAIL R R/D VALVE OPEN R REVERSER FAULT R REV LOCK FAULT RUD AUTHORITY SAFE RUD LIMITER FAULT SAFETY VALVE OPEN SELCAL HF 1 SELCAL HF 2 SELCAL VHF 1 SELCAL VHF 2 SELCAL VHF 3 SET LDG ELEV SHAKER 1 FAIL SHAKER 2 FAIL SLAT DRIVE OVHT SLAT HALFSPD SLAT/FLAP BIT SLAT−FLAP HALFSPD SPLRS/STAB IN TEST STAB CH 1 FAIL STAB CH 2 FAIL STALL WARN ADVANCE STALL WARN BASIC TAT 1 FAIL TAT 2 FAIL TAT 3 FAIL TAT HT 1 FAIL TAT HT 2 FAIL TAT HT 3 FAIL TERR FAIL TRIM AIR FAULT TRU 1 FAIL TRU 2 FAIL WINDSHEAR FAIL WINDMILL ENVELOPE WING A/ICE FAULT WING A/ICE SENSOR WOW FAULT XFEED VALVE FAIL YD HEAT 1 FAIL YD HEAT 2 FAIL YD NOT CENTERED Chapt. Ref. EICAS ADVISORY MESSAGES IAC 1 AURAL FAIL IAC 2 AURAL FAIL IAC 1 INVALID IAC 2 INVALID IAC 3 INVALID IAC 1 MEM FULL IAC 2 MEM FULL IAC 3 MEM FULL IAC 1 WOW INOP IAC 2 WOW INOP IAC 3 WOW INOP IAC CONFIG MISMTCH ICE ICE DETECTOR FAULT IRS 1 AUX FAIL IRS 2 AUX FAIL IRS 3 AUX FAIL IRS 1 FAIL IRS 2 FAIL IRS 3 FAIL IRS 1 NO ALIGN IRS 2 NO ALIGN IRS 3 NO ALIGN IRS 1 AUX PWR IRS 2 AUX PWR IRS 3 AUX PWR L AUX FUEL PUMP L BLEED FAULT L COWL A/ICE FAULT L ENG FIRE FAULT L ENG SQUIB 1 FAIL L ENG SQUIB 2 FAIL L FADEC FAULT L FUEL FILTER L OIL FILTER L PACK FAULT L PRI FUEL PUMP L PROBE MON FAIL L R/D VALVE OPEN L REVERSER FAULT L REV LOCK FAULT LTRK FAIL MACH XDUCER FAIL MAN PRESS FAULT MFD CTLR 1 FAIL MFD CTLR 2 FAIL MLG BAY OVHT FAULT NAV LIGHTS FAIL NO TAKEOFF OIL RES LO QTY OUTFLOW VLV 1 FAIL OUTFLOW VLV 2 FAIL PASSENGER OXY ON PITCH DISC FAULT PITCH FEEL FAULT Chapt. Ref. NOTE A 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 GF0310_015a 3 3 3 3 3 3 3 3 15 15 15 3 14 14 11 11 11 11 11 11 11 11 11 11 11 11 12 2 14 9 9 9 18 18 18 2 12 14 12 18 18 17 10 2 3 3 9 16 10 18 2 2 8 10 10 2 3 12 2 14 9 9 9 18 18 18 2 12 14 12 18 18 10 10 2 6 6 6 6 6 2 10 10 10 10 10 10 10 10 10 10 10 14 14 14 14 14 14 17 2 7 7 17 18 14 14 15 12 4 4 4 RAM AIR FAIL RAT GEN ON 2 7 SPLRS/STAB BIT 10 MACH XDUCER FAULT 10 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−10 CREW ALERTING MESSAGES (CONT'D) PARK/EMER BRAKE ON PLT ROLL SPLRS RAT GEN OFF RAM AIR ON RECIRC FAN OFF R AUX PUMPS OFF R COWL A/ICE AUTO R COWL A/ICE ON R ENG BLEED ON R ENG BLEED OFF R ENG SOVS CLSD R ENG SHUTDOWN R FADEC NI CTL Chapt. Ref. AC BUS1 MAN OFF AC BUS 2 MAN OFF AC BUS 3 MAN OFF AC BUS 4 MAN OFF APU BLEED OFF APU BLEED ON APU FUEL SOV CLSD APU GEN OFF APU SOVS CLSD AUTOBRAKE HI AUTOBRAKE LOW AUTOBRAKE MED Chapt. Ref. HUD ON HYD PUMP 1B OFF HYD PUMP 1B ON HYD PUMP 2B OFF HYD PUMP 2B ON HYD PUMP 3A OFF HYD PUMP 3B OFF HYD 3B ON HIGH PRESS RATE IAC 1 AURAL MUTE IAIC 2 AURAL MUTE IRS 1 IN ATT IRS 2 IN ATT Chapt. Ref. EICAS STATUS MESSAGES 7 7 7 7 5 5 12 7 9 15 15 15 11 13 13 13 13 13 13 13 2 3 3 11 11 15 10 7 2 2 12 14 14 18 18 9 18 18 R FUEL SOV CLSD R FUEL RECIRC ON R HYD SOV CLSD R IGNITION ON R PACK HIGH FLOW R PACK LOW FLOW R PACK MAN TEMP R PACK OFF R PRI PUMPS OFF R WSHLD HEAT OFF SEAT BELTS SIGN ON STAB CH 1 OFF STAB CH 2 OFF TRIM AIR OFF WING A/ICE AUTO WING A/ICE ON WING FUEL XFER OFF WING XBLEED FROM L WING XBLEED FROM R XBLEED CLOSED XBLEED OPEN XFEED VALVE OPEN AUX PRESS ON BATT BUS MAN OFF CPLT ROLL SPLRS DC BUS 1 MAN OFF DC BUS 2 MAN OFF DC ESS BUS MAN OFF DITCHING ON EGPWS TERR OFF EMER LIGHTS ON EXT AC PWR ON EXT DC PWR ON GEAR HORN MUTED GEN 1 OFF GEN 2 OFF GEN 3 OFF GEN 4 OFF GLD MANUAL ARM GND LIFT DUMP OFF GPWS FLAP OVRD GPWS G/S MUTED IRS 3 IN ATT LDG ELEV MAN L AUX PUMP OFF L COWL A/ICE AUTO L COWL A/ICE ON L ENG BLEED ON L ENG BLEED OFF L ENG SOVS CLSD L ENG SHUTDOWN L FADEC NI CTL L FUEL SOV CLSD L FUEL RECIRC ON L HYD SOV CLSD L IGNITION ON L PACK HIGH FLOW L PACK LOW FLOW L PACK MAN TEMP L PACK OFF L PRI PUMPS OFF L WSHLD HEAT OFF MAN PRESS CONTROL NO SMKG SIGN ON NOSE STEER OFF OUTFLOW VLV 1 CLSD OUTFLOW VLV 2 CLSD NOTE A 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 FGF0310_010 FUEL XFER ON FUEL XFER ON 2 7 10 7 7 7 2 17 16 7 7 12 12 15 7 7 7 7 10 10 17 17 11 2 12 14 14 18 18 9 18 18 12 12 9 18 2 2 2 2 12 14 2 16 15 2 2 12 12 9 18 2 2 2 2 12 14 16 10 10 2 14 14 12 14 14 2 2 12 EVS ON EVS CAL 11 11 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−11 MASTER WARNING/MASTER CAUTION LIGHTS Two MASTER WARNING switch/lights come on flashing when any warning occurs. Pushing either MASTER WARNING switch/light extinguishes both MASTER WARNING lights for the duration of that warning and resets the lights for future warnings. FGF0310_004 MASTER WARNING/CAUTION WARNING ROLL SPLRS CPLT CONT ROLL SEL CPLT ROLL RAD BARO MINIMUMS NAV SCR BARO SET PUSH STD HPa IN RAD BARO MINIMUMS NAV SCR BARO SET PUSH STD HPa IN SPD PUSH CHG MAN FMS CRS 1 PUSH DCT HDG PUSH SYNC DN UP ALT CRS 2 PUSH DCT CAUTION WARNING CAUTION WARNING CAUTION MASTER WARNING/CAUTION ROLL SPLRS PLT CONT HUD BRT DIM OFF WARNING CAUTION ROLL SEL PLT ROLL 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 either MASTER CAUTION switch/light extinguishes both MASTER CAUTION lights for the duration of that caution and resets the lights for future cautions. FGF0310_005 MASTER WARNING/CAUTION ROLL SPLRS CPLT CONT ROLL SEL CPLT ROLL RAD BARO MINIMUMS NAV SCR BARO SET PUSH STD HPa IN RAD BARO MINIMUMS NAV SCR BARO SET PUSH STD HPa IN SPD PUSH CHG MAN FMS CRS 1 PUSH DCT HDG PUSH SYNC DN UP ALT CRS 2 PUSH DCT CAUTION WARNING WARNING CAUTION WARNING CAUTION MASTER WARNING/CAUTION ROLL SPLRS PLT CONT HUD BRT DIM OFF WARNING CAUTION ROLL SEL PLT ROLL Pushing the MASTER CAUTION will not silence the following: • EGPWS and TCAS voice alerts • Altitude alert (C-chord) aural • Stall warning • Overspeed continuous horn (A−Chord) • Trim clacker • Autopilot disconnect cavalry charge • Gear horn AURAL AND VISUAL WARNINGS Rev 13, NOV 10, 2006 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−12 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 Flight Control System Caution (Single chime) Tone that precedes an aircraft system caution message Chapters 2 through 18 Clacker Excessive stabilizer movement Chapter 10, Flight Controls Double C-chord VNAV vertical track alert Chapter 4, Automatic Flight Control System Horn Continuous (A-chord) Overspeed warning Chapter 4, Automatic Flight Control 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 aircraft system warning message and/or voice advisory Chapters 2 through 18 Whoop − Whoop EGPWS mode 1 or 2 (excessive descent rate or excessive closure rate) (if installed) EGPWS, Chapter 17, Navigation Voice Messages The following is an alphabetical list of Voice messages: VOICE MESSAGE − ALPHABETICAL W = Warning SYS = System Voice Message Type Chapter Ref. EICAS/ PFD INDICATION Adjust Vertical Speed, Adjust SYS 17 TCAS − Monitor vertical speed to keep aircraft 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 on PFD APU FIRE W 5 APU FIRE Bank Angle SYS 17 EGPWS − Excessive bank angle on final approach CABIN ALTITUDE W 2 CABIN ALT / Cabin altitude >9000 feet AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−13 AURALS (CONT'D) VOICE MESSAGE − ALPHABETICAL W = Warning SYS = System Voice Message Type Chapter Ref. EICAS/ PFD INDICATION Caution Obstacle SYS 17 EGPWS − An obstacle threat has been detected. Caution Terrain SYS 17 EGPWS − A terrain threat has been detected. Cavalry Charge SYS 4 Autopilot disconnect Clear of Conflict SYS 17 TCAS − Encounter has ended and separation increasing Climb − Climb SYS 17 TCAS − Indicates a climb command. Displays a green fly-to PTZ and a red PAZ on both PFD ADIs Climb, Climb Now! − Climb, Climb Now! SYS 17 TCAS − Following a descent command, a climb is necessary to provide adequate separation Climb, Crossing Climb − Climb, Crossing Climb SYS 17 TCAS − Indicates a climb command. Displays a green fly-to PTZ and a red PAZ on both PFD ADIs. Aircraft flight path will cross 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 PAZ on both PFD ADIs. Aircraft flight path will cross intruder’s altitude Descend − Descend SYS 17 TCAS − Indicates a descend command. Displays a green fly-to PTZ and a red PAZ on both PFD ADIs Descend, Descend Now! − Descend, Descend Now! SYS 17 TCAS − Following a climb command, a descent is necessary to provide adequate separation 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 an attempted landing Glideslope SYS 17 EGPWS − Excessive deviation below glideslope Increase Climb − Increase Climb SYS 17 TCAS − PTZ command increases to increase climb rate AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−14 AURALS (CONT'D) VOICE MESSAGE − ALPHABETICAL W = Warning SYS = System Voice Message Type Chapter Ref. EICAS/ PFD INDICATION Increase Descent − Increase Descent SYS 17 TCAS − PTZ command decreases to increase descent rate LEFT ENGINE FIRE W 9 L ENG FIRE Maintain Vertical Speed, Crossing Maintain SYS 17 TCAS − Monitor pitch attitude to keep pitch attitude inside PTZ and away from PAZ. Aircraft flight path will cross intruder’s altitude Maintain Vertical Speed Maintain SYS 17 TCAS − Monitor pitch attitude to keep pitch attitude 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 pitch attitude inside PTZ and away from PAZ NO TAKEOFF W 10 & 15 CONFIG AIL TRIM CONFIG RUD TRIM CONFIG SLATS/FLAPS CONFIG SPOILERS CONFIG STAB TRIM PARK BRAKE ON Obstacle, Obstacle SYS 17 EGPWS − Excessive obstacle closure Pull Up SYS 17 EGPWS − Corrective action after excessive descent rate during approach RIGHT ENGINE FIRE W 9 R ENG FIRE Selcal SYS 6 SELCAL HF, SELCAL VHF 1, SELCAL VHF 2, SELCAL VHF 3 Sink Rate SYS 17 EGPWS − Excessive descent rate during approach SMOKE W 9 SMOKE BAGGAGE SMOKE FWD LAV SMOKE AFT LAV SMOKE CLOSET SMOKE 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 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−15 AURALS (CONT'D) VOICE MESSAGE − ALPHABETICAL W = Warning SYS = System Voice Message Type Chapter Ref. EICAS/ PFD INDICATION Windshear, Windshear SYS 17 EGPWS − WINDSHR (decreasing performance) 500, 100, 50, 30 SYS 17 EGPWS − Descending altitude callouts AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−16 AURAL WARNING TEST Most aural alerts are exercised as part of their own system test. For all other aural alerts, an AURAL WARN TEST can be initiated via the Electrical Management System (EMS) Control Display Unit (CDU) located on the pilot’s and copilot’s side panel. There are two warning test selections provided to test Integrated Avionics Computer (IAC 1 and IAC 2). GF0310_019 STAT SYS BUS PREV CNTL TEST PAGE NEXT PAGE EMER CNTL BUS STBY SYSTEM CIRCUIT 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 can be 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”. • 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 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−17 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. Aural for EGPWS and TCAS will not be inhibited by muting the IACs. GF0310_020 IAC1 and IAC2 PUSH TO MUTE Switches Used to disable respective tone/aural generator located in the respective IACs. PUSH TO MUTE IAC 1 IAC 2 AURAL WARNING MUTED MUTED INHIBITS During take-off 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 APU OVERTEMP (TO only), NORM BRAKE FAIL (TO only), CABIN ALT, CABIN DELTA P and BRAKE OVHT (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 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−18 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 1−2 FAIL YD OFF YD NOT CENTERED (TO only) Air Conditioning Pressurization EMER DEPRESS L−R PACK FAIL Aural and Visual Warnings CHECK DU 1−2−3−4−5−6 SG 1−2−3 FAIL Electrical Power BATT MASTER OFF BATT EMER PWR ON RAT GEN ON (Ldg only) Doors and Exits CARGO DOOR LARGE SERV DOORS L−R EMER EXIT PASSENGER DOOR SMALL SERV DOORS Flight Controls ELEVATOR SPLIT FLT SPLR DEPLOYED FLT SPOILERS FAIL GND LIFT DUMP ROLL SELECT ROLL SPOILERS FAIL RUD AUTHORITY LOW SLAT−FLAP FAIL STAB TRIM STALL PROTECT FAIL FLT SPOILERS FAULT GND LIFT DUMP NO TAKEOFF (TO only) SHAKER 1−2 FAIL SLAT−FLAP HALFSPD STALL WRN ADVANCE RUD AUTHORITY SAFE SLAT−FLAP BIT Hydraulic Power HYD 1−2−3 LO PRESS HYD RAT PUMP FAIL (Ldg only) Ice and Rain Protection ICE Instruments ADC 1−2−3 MISCMP ADC 1−2−3 FAIL AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−19 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% DEGRADED CPLT BRAKE FAULT GEAR DISAGREE INBD BRAKE LO PRESS L−R INBD BRAKE FAIL L−R OUTBD BRAKE FAIL NOSE STEER FAIL OUTBD BRAKE LO PRESS PARK/EMER BRAKE ON (Ldg only) PLT BRAKE FAULT UNCOMMANDED BRAKE BRAKE TEMP (TO only) GEAR SYS FAULT NO TAKEOFF (TO only) Lighting EMER LIGHTS OFF Navigation ALL IRS MISCMP Power Plant A/T NOT IN HOLD (TO only) L−R FADEC N1 CTL L−R REV LOCK FAIL L−R REVERSER FAIL (Ldg only) L−R FUEL FILTER A/T 1−2 FAIL AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−20 CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS) The CAIMS collects diagnostic and fault data from other airplane systems. From this data, the CAIMS 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 defective components. The CAIMS 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 8MB of operational software files and 25MB of loadable diagnostic files. A CD-ROM is installed in the PMAT CD-ROM drive and contains an electronic copy of the Aircraft Maintenance Manual (AMM). 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 6 COMMUNICATIONS. The CAIMS is comprised of the following components: • PMAT (located in the cabin) POWER HARD DRIVE FAULT OVER TEMP Power Switch Mode /Fault Annunciation CD ROM Drive Access Port 3.5" Disk Drive Access Port Active Faults page 1 / 3 Current 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 PREV PAGE NEXT PAGE SHOW DETAIL GF0310_021 • DATA UPLOAD/DOWNLOAD switch and PRINT MAINT REPORT switch (located on bulkhead behind pilot). AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−21 CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS) (CONT'D) FGF0310_006 CAIMS PRINT MAINT REPORT SWITCH Used to get a report of active faults from the cockpit printer. Data Selector Switch Used to select system to upload/download a copy of non-volatile data on to a 3.5 inch disk. PRINT MAINT REPORT DATA UPLOAD/DOWNLOAD DAU 1A DAU 1B DAU 2A DAU 2B DAU 3A DAU 3B DAU 4A DAU 4B IRS 1 IRS 2 IRS 3 WX SPARE IAC 1 IAC 2 IAC 3 GPWS SATCOM SDU CABIN COMM GPS 1 GPS 2 ADC 1 ADC 2 ADC 3 • Pilot Event Marker (located on the landing gear control panel). GF0310_023 FDR/CAIMS Event Button Used to store information in Line Replaceable Units (LRUs), which report to CAIMS. Landing Gear Control Panel NOSE STEER LDG GEAR HORN PILOT EVENT MUTED AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−22 FLIGHT DATA RECORDER EICAS channels aircraft systems data (including altitude, airspeed, heading, acceleration and radio communications events) to the Flight Data Recorder (FDR). DAU 4B gathers sensor data for transmission to the FDR. DAU 4 is fully self-monitoring and provides CAS 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 EVENT button on landing gear control panel, located on the pedestal. Pushing the PILOT EVENT will also encode the Central Aircraft Information Maintenance System (CAIMS). GF0310_024 Landing Gear Control Panel FDR/CAIMS Event Button NOSE STEER LDG GEAR HORN PILOT EVENT MUTED STALL WARNING 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) and a TBD V S indicator on the primary flight displays (PFDs) airspeed tape. Stall warnings are provided by an aural “STALL”, a STALL icon appears on the PFD and vibration of both control columns. If the airplane angle-of-attack continues to increase, a stick pusher then pushes the control column forward to prevent further development of a stall. For more information refer to Chapter 10, FLIGHT CONTROLS. AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−23 TAKE-OFF CONFIGURATION WARNINGS Take-off configuration warnings are armed when the airplane is on the ground and both engines are accelerated towards take-off thrust (throttle position ≥ 30°). A voice warning, EICAS warning message, and both MASTER WARNING lights come on for any of the following: Condition Voice Message EICAS Message Aileron trim outside of take-off range “NO TAKEOFF” CONFIG AIL TRIM Parking brake on during take-off “NO TAKEOFF” PARK BRAKE ON Rudder trim outside of take-off range “NO TAKEOFF” CONFIG RUD TRIM Flaps not in take-off position “NO TAKEOFF” CONFIG SLATS/FLAPS Spoilers not in take-off position “NO TAKEOFF” CONFIG SPOILERS Horizontal stabilizer outside of take-off range (“green band”) “NO TAKEOFF” CONFIG STAB TRIM All configuration warning indications are cancelled when the configuration error is corrected, or the airplane 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 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−24 LANDING CONFIGURATION WARNING The “GEAR” aural will sound if any gear is not down and locked and the airplane is below 16,500 feet and: • The radio altitude is less than 1,000 feet AGL and the descent rate is more than 400 feet per minute. OR • The radio altitude is less than 500 feet AGL and either throttle is below 25° throttle lever angle and the flap position is 30°. OR • The radio altitude is less than 500 feet AGL and both throttles are below 25° throttle angle and the flap posiion is not at 30°. 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 with the 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 and the airplane is below 16,500 feet. The landing gear horn may be muted by pressing the mute hornn swith/ 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. AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−25 EICAS DISPLAY FGF0310_001 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 ND STAB NU RUDDER NL LWD NR TRIMS N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 EPR N1 ITT AIL GEAR OUT 30 DN DN DN 1.65 1.65 7.2 RWD TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 ND STAB NU RUDDER NL LWD RWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 EPR N1 ITT AIL 1.65 1.65 Crew Alerting System Window 14 message lines with Gear/Slats/Flaps pop up displayed. Slats/Flaps, Spoilers and Gear Position Pop Up The pop up display will be removed from the primary page (in flight only) 30 seconds after the gear and flaps indicate up, ans 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. Trims Indications for Aileron, Rudder and Stabilizer Trim. For more information see Chapter 10, FLIGHT CONTROLS. NOTE EICAS will automatically be displayed when airplane is powered up (BATT MASTER ON) Crew Alerting System Window 24 message lines with Gear/Slats/Flaps pop up not displayed. Engine Indicating Indications of EPR, N1, ITT, N2, FF, OIL TEMP and OIL PRESSURE. For more information see Chapter 18, POWER PLANT. Fuel Indications of total fuel quantity and individual tank quantity. For more information see Chapter 12, FUEL. AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−26 SYSTEMS DISPLAY (STAT PAGE) NOTE SYSTEM display will automatically be displayed when airplane is powered up (BATT MASTER ON). GF0310_026a OIL QTY (QTS) ENG APU RES RPM EGT BRAKE TEMP 10.4 90 13 % 13 % 400 100 03 03 03 03 4.5 5.0 10.4 OXYGEN OPEN OPEN OUTFLOW VALVES 0 0 1 2 1 2 2 APU % 1 CKPT (°C) AFT CABIN (°C) CABIN (°C) FWD 20 1300 0.00 20 CAB ALT CAB RATE P 23 19 21 22 CKPT/CABIN Temperature Indications of cockpit, cabin forward and cabin aft temperature. For more information CAB ALT, P and CAB RATE Indications of cabin altitude, cabin differential and cabin rate of climb. For more information see Chapter 2, AIR CONDITIONING AND PRESSURIZATION. see Chapter 2, AIR CONDITIONING AND PRESSURIZATION. OXYGEN Indications of oxygen quantity. For more information see Chapter 8, EMERGENCY EQUIPMENT. OUTFLOW VALVES Indications of outflow valves position (manual mode only). For more information see Chapter 2, AIR CONDITIONING BRAKE TEMP Indications of brake temperatures. For more information see Chapter 15, LANDING GEAR. AND PRESSURIZATION. OIL QTY Indications of engine, APU and reservoir oil quantity. For more information see Chapter 5, APU, and Chapter 18, POWER PLANT. APU Indications of APU door position (failure mode only), APU RPM and EGT. For more information see Chapter 5, AUXILIARY POWER UNIT. DOORS Indications of passenger entry door, overwing emergency exit baggage door. For more information see Chapter 1, AIRPLANE GENERAL. AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−27 REVERSION CONTROL PANEL The reversion panel, located on the pedestal, can be used to revert the EICAS display to alternate display units, to revert IRS and ADCs and to revert SGs. GF0310_027 PFD1 and PFD2 Knobs Used to revert PFD 1 and PFD 2 displays to alternate display units. EICAS Knob Used to revert EICAS display to alternate display units. IRS and ADC Knobs Used to revert IRS and ADCs. For more information see Chapter 11, FLIGHT INSTRUMENTS. SG1, SG2, SG3, Knobs Used to revert applicable symbol generators 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 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES NORM ALTN PFD1 NORM ALTN1 EICAS NORM ALTN PFD2 ALTN2 ALTN3 PFD1 PFD2 NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 IRS IRS ADC ADC AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−28 PFD REVERSION CONTROL GF0310_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 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES NORM ALTN PFD1 NORM ALTN1 EICAS NORM ALTN PFD2 ALTN2 ALTN3 PFD1 PFD2 NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 IRS IRS ADC ADC AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−29 PFD REVERSION GF0310_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 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES NORM ALTN PFD1 NORM ALTN1 EICAS NORM ALTN PFD2 ALTN2 ALTN3 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−30 EICAS REVERSION CONTROL GF0310_030 EICAS Reversion Knob NORM − 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 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES NORM ALTN PFD1 NORM ALTN1 EICAS NORM ALTN PFD2 ALTN2 ALTN3 PFD1 PFD2 NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 IRS IRS ADC ADC AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−31 EICAS REVERSION GF0310_031 ALTN 1 − EICAS displayed on DU4. ALTN 2 − EICAS displayed on DU2. ALTN 3 − EICAS displayed on DU5. DU 4 VS 2000 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT RWD DU 2 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES NORM ALTN1 EICAS ALTN2 ALTN3 DU 5 VS 2000 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES NORM ALTN1 EICAS ALTN2 ALTN3 NORM ALTN1 EICAS ALTN2 ALTN3 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−32 SG REVERSION CONTROL SG1, SG2, SG3 Reversion Knobs − SG2 drives DU5 and DU6 as well as DU3. GF0310_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 NORM SG3 NORM SG1 ALTN SG2 ALTN SG3 ALTN NORM ALTN PFD1 NORM ALTN1 EICAS NORM ALTN PFD2 ALTN2 ALTN3 PFD1 PFD2 NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 IRS IRS ADC ADC AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−33 SG REVERSION SG1 NORM − SG1 drives DU1 and DU2. GF0310_033 SG2 NORM − SG2 drives DU5 and DU6. SG3 NORM − SG3 drives DU3 and DU4. VS 2000 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−34 SG REVERSION (CONT'D) SG1 ALTN − SG2 drives DU3, DU5 and DU6. − SG3 drives DU1, DU2 and DU4. GF0310_034 SG 1 FAIL If 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 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES VS 2000 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−35 SG REVERSION (CONT'D) SG3 ALTN − SG1 drives DU1, DU2 and DU4. − SG2 drives DU3, DU5 and DU6. GF0310_035 SG 3 FAIL If 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 − NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 NORM ALTN SG1 NORM ALTN SG3 NORM ALTN SG2 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT RWD TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 VS 2000 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 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 VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−36 EICAS CONTROL PANEL The EICAS control panel, located on the pedestal, can be used to revert SYSTEMS display, scroll non-displayed messages and to display SYSTEMS synoptic pages. BLEED Button HYD Button AIR COND Button AC ELEC Button DC ELEC Button FLT CTRL Button FUEL Button EICAS SCROLL Knob STAT Button SYSTEMS SELECT Knob GF0310_036 EICAS SCROLL SYSTEM SELECT Used to display BLEED/ANTI-ICE synoptic. HYDRAULIC Used to display synoptic. Used to display AIR CONDITIONING synoptic. Used to display AC ELECTRICAL synoptic. Used to display FUEL synoptic. Used to display DC ELECTRICAL synoptic. Used to display FLIGHT CONTROLS synoptic. Used to revert SYSTEMS display to alternate displays. Used to display status synoptic. Used to scroll out of view and/or scroll into view all messages, except for warning messages. AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−37 SYSTEMS REVERSION CONTROL GF0310_037a SYSTEM SELECT Knob NORM − 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 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 FMS1 DTK 360 20 2 0 10 10 20 20 10 10 33 30 W 24 21 15 12 E 6 3 0 1 2 1 2 3 VAPP VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5 NM KDVT LUF KDVT 5 1300 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 14600 10000 2350 ND STAB NU RUDDER NL LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU RES RPM EGT 10.4 22 1300 85 % 0.00 20 400 100 4.5 5.0 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 TOC 3 KSRP KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX KPHX TOC KSRP KDVT 4000 4000 FL180 12.5 NM KDVT LUF KDVT 5 N 5 360 TERR OFF 30 6 33 VS 2000 180 220 210 200 170 160 150 0.88 0.856 M 190 FMS1 DTK 360 20 2 0 10 10 20 20 10 10 33 30 W 24 21 15 12 E 6 3 0 1 2 1 2 3 VAPP VNAV ASEL AP1 HDG 104 00 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 1300 1000 S N 185 6 4 0 1 2 13% 13 % OPEN OPEN OUTFLOW VALVES AURAL AND VISUAL WARNINGS Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−10−38

All BOMBARDIER GLOBAL 5000 pilot's operating handbook