• Forward airplane systems
• The #1 Engine.

• Aft airplane systems
• The #2 Engine.

• EICAS caution message.
• The digital engine readouts are replaced with dashes on the failed DAU side.

• Parking brake off 
• Flaps set for takeoff 
• Spoilers closed
• Pitch trim in green range

• Aircraft on ground
• Thrust levers retarded
• Wheel speed above 25 kts.

• Flaps 0° or 9°
• Thrust levers retarded
• Speed brake lever OPEN

• Speed brake lever OPEN with:
• Thrust levers advanced; or
• Flaps set above 9
• Speed brake lever CLOSED;
• Taxi speed faster than 25 kts.

• ROL GA mode commanding a pitch attitude of 10°; then
• ROL IAS mode commanding 170 knots; then
• ROL IAS mode commanding the blue airspeed bug if unable 170 knots.

• After initial power up
• After an unsuccessful test

• Autopilot
• Main trim switches on yoke
• Speed brake auto-trim

2.

• The electo-pneumatic outflow valve is commanded by the pressure controller 
• The pneumatic outflow valve is slaved to follow it.

No. The cabin altitude is kept at the departure airport field elevation until:

• Theoretical cabin altitude increases; or
• 15 minutes.

A red "X" over the

• Airspeed 
• Altitude
• VSI

• Blue horizon
• Red X over the Heading indicator
• ATT FAIL 
• HDG FAIL

• Amber ATT1 in the lower left corner of the FO's PFD.
• Amber MAG1 above the FO's Heading indicator.

• SG 
• ADC2 
• ATT2 
• MAG2 

• Select both (CA's and FO's) MFD reversionary knobs to EICAS 
• Determine which IC 600 is accurate.

• AHRS panel 
• Flux valve in wing

• Captain hard wired to COMM 1 and NAV 1.
• FO hard wired to COMM 2 and NAV 2.
• Observer loses radio communication.

• Cross-side NAV or FMS navigation source is selected.
• CDI display changes to yellow

• Pull the gain knob out. 
• Amber VAR flag on the PFD's and MFD's.

• 240 KIAS below 10,000 ft
• 240-270 KIAS between 10 - 12,000 ft
• 270 KIAS below 18000 ft
• .56 MACH below FL 370

• 2000 fpm above 12,000ft
• 2000-1000 fpm between 12,000-10,000 ft
• 1000 fpm below 10,000 ft

1. Select TEST/RESET
2. Then ARM.

• Operating in dead reckoning mode
• Taking off or landing within 15NM of an airport that has a runway which:
• Is less than 3,500 feet long
• Is not in the database
• No IAP

• Below 1200ft RA and Gear NOT down and locked; with
• Thrust levers retarded; or
• Flaps 45°

• Press landing gear warning cutout button; with 
• Flap lever less than 22 deg

• Thrust levers advanced; or
• Flap lever set above 22 deg; or
• Landing gear down and locked

• Fasten Seat Belts Signs illuminated
• No Smoking Signs Illuminated

40 minutes.

Note: Can be increased to 45 minutes if you shut-off PITOT 3 heat

When directed by a checklist.

Example: ELEC ESS TFR FAIL procedure

• PFDs and MFDs - dark 
• EICAS and RMUs - lit.

• BATT 1 - AUTO; and
• BACKUP button - in.

• GPU Connected
• GPU button out
• BATT 1 & 2 knobs OFF

Pulling the handle does what?

[image]

It closes the following Shut Off Valves (H.A.L.F)

• Hydraulic Pump SOV
• Bleed Air SOV
• Engine Lip Anti-ice SOV
• Fuel SOV

When this handle is pulled, what EICAS messages will you see?

[image]

• FUEL SOV CLSD
• HYDR SOV CLSD
• BLEED SOV CLSD

When will this handle illuminate?

[image]

Can you cancel the visual warning of the Fire Handle?

[image]

What do these knobs do?

[image]

What happens if the selected fuel pump fails?

[image]

What buss(es) power the fuel pumps?

[image]

Pumps A,B - Essential Buss

Pump C - DC Buss

When these knobs are in the off position?

[image]

When these knobs are in the ON position?

[image]

When this knob is in the OFF position?

[image]

When this knob is in LOW 1?

[image]

When this knob is in the LOW 2 position?

[image][image]

What does this button do?

[image]

What does this button do?

[image]

• Allows communication between FA and pilots if the normal mode fails
• Both CABIN AND CAB EMER illuminate on ICU
• Both PILOT AND EMER PILOT illuminate on FA panel

4 Total:

• 1 in each wing
• 2 in the tail

8 total:

• 2 in each wing
• 4 in the tail

• When RED BCN to ON; or
• Aircraft is airborn

What does this button do?

[image]

• Sends stop signal to FADEC
• Closes APU SOV in Wing
• Closes Fuel valve on APU
• Discharges APU fire bottle

What does this button do?

[image]

Tests the first detection system.

Should hear Fire bell and should see (Remember 3-4-5):

• 3 lights illuminated (2 fire handles, 1 BAGG EXTG button)
• 4 lights flashing (2 warning, 2 caution)
• 5 Messages (2 warn, 3 caution)
• APU FIRE
• ENG 1(2) FIRE
• BAGG SMOKE
• APU FIRE DET FAIL
• ENG 1(2) FIRE DET FAIL

When will this button illuminate?

[image]

What happens when this button is pushed?

[image]

• Both bottles discharged (High rate & Metered)
• Baggage compartment fans off

What happens when this knob is selected OFF?

[image]

4 things (Remember OFF has 3 letters + 1):

• Sends a stop signal to FADEC
• Closes APU FUEL SOV in Wing
• Closes Fuel valve on APU
• Indications and alarms are disabled

What happens when this knob is selected ON?

[image]

4 things (Remember ON has 2 letters x 2):

• FADEC energized
• FADEC performs self-test
• Opens APU FUEL SOV in Wing
• Enables indications and alarms for APU

What happens when this knob is selected START?

[image]

What happens when this button is pushed?

[image]

2 things:

• Sends stop request to FADEC
• Closes fuel valve on APU

What happens when this button is pushed?

[image]

3 things (Remember 3 syllables in button name):

• Sends stop request to FADEC
• Closes APU FUEL SOV in Wing
• Closes fuel valve on APU

What happens when this knob is selected OFF?

[image]

Auto-relight is disabled

* Doesn't actually turn off the ignitors

What happens when this knob is selected AUTO?

[image]

Active FADEC controls ignition (A or B)

• 1 ignitor for ground start (14% N₂)
• 2 ignitors for air start (10% N₂)
• Auto-relight (above 53% N₂)

What happens when this knob is selected ON?

[image]

• First flight of the day
• Cold engine start OR Oil < 5C
• Ext Air or XBLEED start
• Contaminated rwy AND OAT < 10C
• Moderate or greater turbulence
• Heavy precip

What happens when this knob is selected RESET?

[image]

What happens when this knob is selected ALTN?

[image]

Alternates the FADEC in control

* Switch becomes inop if held for more than 3 seconds

What happens when this knob is selected STOP?

[image]

What happens when this knob is selected RUN?

[image]

What happens when this knob is selected START?

[image]

• Initiates start cycle
• Switches FADEC from the last one that succesfully started the engine

What happens if this button is held for more than 10 seconds?

[image]

2 Spool High Bypass Turbofan

• High pressure spool
• 14 stage compressor
• 2 stage turbine
• Low pressure spool
• 1 high bypass fan
• 3 stage turbine

• Hydraulic Pump
• Electrical Generators
• ATS (Air Turbine Starter)
• PMA (Primary Magnetic Alternator)
• Oil Pump
• FPMU (Fuel Pump Metering Unit)

• FADEC receives engine inop signal; or
• Opposite engine thrust level is retarded; or
• Opposite engine does not arm within 2 seconds

• Windshear
• ATTCS inoperative
• Runway is contaminated
• Performance requires it
• Discretion of the Captain

10% - PMA powers ignition

14% - FADEC enables ignition

28% - Fuel flows

42%-48% - Possible hung start range

50% - PMA powers FADEC

53% - Start control valvle closes

57% - Ignition OFF, Generators online

64% - Ground Idle

When does Rudder SYS 1 automatically shutoff?

[image]

• Force on any pedal > 130 lbs; and
• Rudder deflected > 5^o to opposite side; and
• Both engines running (N₂ > 57%)

What does this button do?

[image]

What happens when this knob is selected OFF?

[image]

What happens when this knob is selected AUTO?

[image]

Electric Hydraulic pump turns on if:

• Hydraulic pressure falls below 1600 psi; or
• N₂ < 57%

What happens when this knob is selected ON?

[image]

• Hydraulic pressure < 1600 psi; or
• N₂ < 57%

• Gear uplocks are mechanically released
• Landing hydraulic pressure is relieved

• ICE CONDITION (blue)
• SPS/ICE SPEEDS (blue)

• ENGINE AIR INLET - When engine is running 
• WING and STAB A/I - When icing detected and wheel speed > 25 kts.

• ENGINE AIR INLET - When icing detected 
• WING and STAB A/I - When icing detected; and wheel speed >25 kts or airborne

• In air, Everything regardless of ice detection.  
• On ground, WING and STAB are inhibited if wheel speed < 25 kts

• Pack valve closes
• Associated recirc fan is deactivated

• Cabin/Cockpit Smoke or Fumes
• Hot soaked aircraft

• Individual gasper outlets
• O2 bottle compartment
• Relay box
• Rear electronics compartment