WHEEL BRAKE FIRE

COCKPIT OR CABIN FIRE/SMOKE

ELECTRICAL FIRE/SMOKE

ELECTRICAL FIRE/SMOKE IN COCKPIT OR CABIN

Cockpit Overhead Circuit Breaker Panel (Partial)

Bus Load Distribution

SMOKE / FUME REMOVAL

APU TAIL PIPE FIRE ON GROUND

EMERGENCIES DURING TAKE-OFF

TAKE-OFF ABORT

ENGINE FAILURE DURING TAKE-OFF ABOVE V1

ENGINE FAILURE DURING COUPLED APPROACH

ELECTRICAL FAILURES

FAILURE OF BOTH GENERATORS

EMERGENCY BUS FAILURE

ENGINE OIL PRESSURE LOW

ENGINE OIL TEMPERATURE HIGH

BLEED AIR LEAK

BLEED AIR FAILURE MODES

BLEED LINE OVERPRESSURE /OVERTEMPERATURE

DUCT TEMPERATURE HIGH

RAPID DECOMPRESSION

CABIN UNDERPRESSURIZATION

EMERGENCY DESCENT

JAMMED RUDDER

JAMMED ELEVATOR

JAMMED AILERON

FAILURE OF BOTH ENGINES

EMERGENCY LANDING (Both Engines Inoperative)

PASSENGER EVACUATION

DITCHING

PREPARATIONS

APPROACH

BEFORE TOUCHING WATER

AFTER DITCHING

EMERGENCY EXIT

LOSS OF ALL CABIN PRESSURE INDICATIONS AND CONTROL

Abnormal Procedures

LIST OF FIGURES

EICAS CAUTION, ADVISORY AND STATUS MESSAGES

EICAS Display - Primary Page

CAUTION MESSAGES

ADVISORY MESSAGES

STATUS MESSAGES

FADEC FAILURES

FADEC FAULTY MESSAGE

HOT START - GROUND

ENGINE FAILURE/FLAMEOUT DURING FLIGHT

ENGINE SLOW RESPONSE

ENGINE SHUTDOWN IN FLIGHT

AIR STARTS

Air Start Envelope (Windmilling and Starter-Assist)

WINDMILLING AIR START (IF AUTO IGNITION IS UNSUCCESSFUL)

STARTER-ASSIST AIR START AFTER COMPLETE SHUT- DOWN

SINGLE-ENGINE OPERATIONS

SINGLE-ENGINE LANDING

SINGLE-ENGINE GO-AROUND

ELECTRICAL SYSTEM FAILURES

BATTERY OVERHEAT

BATTERY DISCONNECTED

FAILURE OF ONE GENERATOR

APU GENERATOR FAILURE

EMERGENCY BUS ALTERNATE FEED

UNCOMMANDED STARTER GENERATOR ENGAGEMENT

APU SHUT-DOWN FAILURE

MAIN BATTERY DISCHARGE

EMERGENCY BATTERY DISCONNECTED

EMERGENCY BATTERY OVERHEAT

EMERGENCY BATTERY DISCHARGE

GENERATOR OVER LOAD

APU GENERATOR OVER LOAD

ENGINE/NACELLE ANTI-ICE SYSTEM FAILURE

ENVIRONMENTAL CONTROL SYSTEM FAILURES

CABIN OVERPRESSURIZATION

UNPRESSURIZED DISPATCH AND FLIGHT

AIR DATA COMPUTER FAILURES

BOTH ADC 1 & 2 INOPERATIVE

DE-ICING SYSTEM FAILURE

FLIGHT CONTROL SYSTEM FAILURES

ELEVATOR CONTROL FAILURES

AILERON CONTROL FAILURE

HORIZONTAL STABILIZER TRIM FAILURE

INADVERTENT GROUND / FLIGHT AIR BRAKES DEPLOYMENT IN FLIGHT

SLATS/FLAPS FAIL TO MOVE

JAMMED HORIZONTAL STABILIZER

SLATS, KRUEGER OR FLAPS FAILURES

FUEL SYSTEM

ABNORMAL FUEL TANK TRANSFER

FUEL JETTISON

WING FUEL UNBALANCE

FUEL BOOST JET PUMP FAILURE

FUEL PRESSURE LOW

FUEL LEVEL LOW

FQMC FAILURE

ABNORMAL FUEL TANK TEMPERATURE

FUEL FILTER CLOGGED

OIL SYSTEM FAILURES

ENGINE CHIP DETECTOR

OIL FILTER CLOGGED

ENGINE VIBRATION

THRUST REVERSER FAILURE

THRUST REVERSER READY LIGHT IN FLIGHT

MAIN HYDRAULIC SYSTEM FAILURES

FAILURE OF ONE HYDRAULIC PUMP

FAILURE OF COMPLETE MAIN HYDRAULIC SYSTEMS

HYDRAULIC SYSTEM OVER HEAT

LANDING GEAR SYSTEM FAILURES

EMERGENCY LANDING GEAR EXTENSION

LANDING GEAR DOES NOT LOCK UP

LANDING GEAR DOES NOT LOCK DOWN

LANDING GEAR FAILURE TO RETRACT

LANDING WITH ABNORMAL LANDING GEAR CONDITIONS

PREPARATION FOR LANDING WITH ABNORMAL GEAR CONDITION

LANDING WITH NOSE GEAR UNSAFE OR RETRACTED, BOTH MAIN GEAR DOWN & LOCKED

LANDING WITH NOSE AND ONE MAIN LANDING GEAR DOWN AND LOCKED, OPPOSITE MAIN GEAR UNSAFE OR RETRACTED