19
ENGINE START ENGINE START SEQUENCE LSP RSP “STARTING ENGINE 1 (2) Turn the START/STOP selector to START and back to RUN Start Clock Check N2 rising Check N2 rising Monitor IGN A (B) at 7% N2, fuel flow at 20% N2 Start Clock only if fuel flow is initiated with no ITT indication Make sure that N2 and N1 accelerate normally and that positive oil pressure is indicated Verify the annunciation IGN A (B) goes out at approximately 50% N2 Stop clock at 50% N2 (Starter limitation) Verify that the engine stabilizes at idle and call out: “NORMAL START”

SOPs all E190

Embed Size (px)

DESCRIPTION

SOP E195

Citation preview

Page 1: SOPs all E190

ENGINE START

ENGINE START SEQUENCE

LSP RSP

“STARTING ENGINE 1 (2)

Turn the START/STOP selector to START and back to RUN

Start Clock

Check N2 rising Check N2 rising

Monitor IGN A (B) at 7% N2, fuel flow at 20% N2

Start Clock only if fuel flow is initiated with no ITT indication

Make sure that N2 and N1 accelerate normally and that

positive oil pressure is indicated

Verify the annunciation IGN A (B) goes out at approximately

50% N2

Stop clock at 50% N2 (Starter limitation)

Verify that the engine stabilizes at idle and call out:

“NORMAL START”

Page 2: SOPs all E190

AFTER START

After Engine Start is completed and

Airplane is Stopped

LSP RSP

“SET FLAPS___,FLIGHTS CONTROL CHECK”

Selects Flaps position and verify EICAS indication

“FLAPS____SET”

Presses the STEERING DISENGAGE SWITCH

Checks the flight controls before taxi

ELEVATOR, AILERON and RUDDER (full deflection)

Check flight control free travel on the MFD synoptic page

Perform the rudder check following the LSP movement

Selects Map on MFD and presses the Steering Handle

“APU OFF (if its use is not required), AFTER START

CHECKLIST”

Confirms power transfer through Electrical Synoptic page (or 30

seconds after N2 stabilizes) and turn off the APU

Reads the list and calls:“AFTER START CHECKLIST

COMPLETED”

Page 3: SOPs all E190

ENGINE FIRE ON GROUND

With the airplane static, taxing in, taxi out or after a RTO

LSP RSP

The pilot first noticing the malfunction identifies and announces it

“ENGINE 1 (2) FIRE”

“MEMORY ITEMS”

Disengage AT

Reduce thrust levers to idle

With the airplane static or when the

airplane has stopped

Sets Parking Brake ON

Sets affected engine START/STOP selector to STOP

Pulls the associated engine Fire Extinguisher Handle

Alerts cabin crew: (PA)

“ATTENTION CREW, WAIT FOR INSTRUCTIONS”

“ENGINE 1 (2) FIRE CHECKLIST” Accomplish checklist

Page 4: SOPs all E190

EMERGENCY EVACUATION

When airplane has stopped

LSP RSP

“EMERGENCY EVACUATION”

“MEMORY ITEMS”

Sets Parking Brake ON Set Flap Lever to 5

Sets Thrust Levers to IDLE

Sets both START/STOP selectors to STOP

Pulls and rotates (1L/2R) both engine Fire

Extinguisher HandlesAlerts Cabin Crew (PA):

“ATTENTION CREW, WAIT FOR INSTRUCTIONS”

Presses APU Emergency Stop Button

Set Fasten Belts OFFPresses APU Fire

Extinguisher Button

Presses the DUMP Button

Alerts Cabin Crew (PA):“ATTENTION CREW,

EMERGENCY EVACUATION”Notifies ATC

“EMERGENCY EVACUATION CHECKLIST”

Selects Batteries OFF

Accomplishes Checklist

“EMERGENCY EVACUATION CHECKLIST

COMPLETED”

Page 5: SOPs all E190

TAKE OFF

Airplane on the runway

PF PM

Advance thrust levers to 40% N1

Make sure the AT has advanced the thrust levers to TOGA detent

before 60 kt

“CHECK THRUST”Verifies that the N1 reached is the target N1 and the ATTCS

is as desired“THRUST CHECKED”

Airplane accelerates past 80 KIAS

“EIGHTY KNOTS”

“CHECKED"

Airplane passes V1 and VR

“V1”“ROTATE”

Positive Rate of Climb

“POSITIVE RATE”

“GEAR UP”

Select Gear lever Up

At 400 ft AGL

“SELECT HEADING (NAV)(if was no selected on ground)

Selects or verifies Lateral Mode

Acceleration Altitude

“CLIMB SEQUENCE”

Selects VNAV and FMS Speeds

Retracts flaps on schedule

“FLAPS ZERO”

After Flaps Retraction

“AFTER TAKE OFF CHECK LIST”

“AFTER TAKE OFF CHECK LIST COMPLETED”

Transition Altitude“TRANSITION ALTITUDE”

Pushes the BARO SET (STD) Pushes the BARO SET (STD)

Upon passing 10000 ft AFE

“TEN THOUSAND”

“TEN THOUSAND CHECKED” External lights off, except NAV, STROBE y BEACON

FSTN BELTS OFF at Captain discretion

Page 6: SOPs all E190

REJECTED TAKE OFF

If decision was REJECTED

LSP RSP

The pilot first noticing the malfunction identifies and announces it

“REJECT"

Reduce thrust levers to idle, disconnect AT and apply reverse

as required Monitor airplane

deceleration

Apply or verify maximum braking Verifies the reverse status

Use reverse as necessary Cancels any aural warnings

Smoothly return thrust levers to idle

Calls out:“SIXTY KNOTS”

Advice ATC

When airplane has stopped

Set parking brake ON

Alert Cabin Crew (PA):“ATTENTION CREW, WAIT FOR

INSTRUCTIONS”Request appropriate checklist if

applicablePerform appropriate

checklist

If emergency evacuation is

requiredComply with Emergency Evacuation Procedures

Page 7: SOPs all E190

ENGINE FAILURE AT OR ABOVE V1

Before VR

PF PM

(pilot first noticing the engine failure)“ENGINE___FAILURE”

Controls airplane using ruder Cancels aural warnings

“CHECK THRUST” Verifies maximum thrust on operating engine

“THRUST CHECKED”(if TO x-RSV is not achieved PM shall move thrust levers to MAX)

At VR“ROTATE”

Rotate to appropriate pitch

After lift-off

“POSITIVE RATE”

“GEAR UP”

Select gear lever UP

Climbs at V2 to V2 + 10 Monitors speed and attitude

Controls the airplane using rudder and yaw trim in the amount

necessary to keep the aileron control in neutral position to avoid

roll spoilers to be deployed

400 AGL“SELECT HEADING, BANK”

Selects HDG and BANK

At Acceleration Altitude

"SELECT FLCH”

Selects FLCH (verifies or set VFS)

“ENGAGE AUTOPILOT”

Engages AP

At flaps retraction speed: “FLAPS___”

Retracts flaps on schedule, then calls:

“FLAPS ZERO”

Reaching VFS:“CONTINUOUS”

Sets or verifies thrust rate to continuous

ENGINE FAILURE AT OR ABOVE V1

Page 8: SOPs all E190

Climbing to Safe Altitude

Climbs at VFS to a safe altitude defined on the take off briefing or

as assigned by ATCAdvise ATC

“(APPLICABLE ABNORMAL) CHECKLIST, I HAVE ATC” Monitor thrust, altitude and speed

Reading and performing the Engine Failure

Checklist

“THURST LEVER 1(2) IDLE”

“THRUST LEVER 1(2) IDLE CONFIRM?”

“CONFIRMED"

Reduces affected engine Thrust Lever to idle.“1(2) IDLE”

“START/STOP 1(2) STOP CONFIRM?”

“CONFIRM”

Selects the START/STOP Selector to STOP

Completes the Engine Failure Checklist

“(APPLICABLE ABNORMAL) CHECKLIST COMPLETED”

When Engine Failure

Checklist is completed

“AFTER TAKE OFF CHECKLIST”

Accomplish the procedures and checklist.

“AFTER TAKE OFF CHECKLIST COMPLETED”

ENGINE FAILURE AT OR ABOVE V1ENGINE FAILURE AT OR ABOVE V1

Page 9: SOPs all E190

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION (ON TAKEOFF ABOVE V1)

Before VR

PF PM

“ENGINE 1(2) FIRE/DAMAGE/SEPARATION”(pilot first noticing the engine failure)

Controls airplane using rudder Cancels aural warnings

“CHECK THRUST”

Verifies maximum thrust on operating engine

“THURST CHECKED”(if TOx RSV is not achieved

PM shall move thrust levers to MAX)

At VR“ROTATE"

Rotate to appropriate pitch

After lift-off

“POSITIVE RATE”

“GEAR UP” Selects Gear Up

Climbs at V2 to V2+10 Monitors speed and attitude

Controls the airplane using rudder and yaw trim to keep the aileron control in neutral position to avoid roll spoilers

to be deployed

At 400 ft AGL “SELECT HEADING, BANK” Selects HDG and BANK

At Acceleration Altitude

"SELECT FLCH” Selects FLCH.(verifies or set VFS)

“ENGAGE AUTOPILOT” Engages AP

At flap retraction speed:“FLAPS____”

Retracts flaps on schedule,“FLAPS ZERO”

Reaching VFS:“CONTINUOUS”

Sets or verifies thrust rate to continuous

“MEMORY ITEMS”

Climbing to Safe AltitudeClimbs at VFS to a safe

altitude defined bon the take off briefing or assigned by ATC

Advise ATCMonitor thrust, attitude and

speed

Performing Engine Fire,

Severe Damage or Separation MEMORY Items

Disengages the AUTOTHROTTLE

“THRUST LEVER 1(2) IDLE CONFIRM?” “CONFIRMED"

“1(2) IDLE”

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION (ON TAKEOFF ABOVE V1)

Page 10: SOPs all E190

“START/STOP 1(2) STOP CONFIRM?”

“CONFIRMED"

Selects the affected engine Start/Stop selector to STOP

“FIRE HANDLE 1(2) PULL CONFIRM?”

"CONFIRMED"

Pulls the affected engine Fire Extinguisher Handle

"ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECKLIST, I HAVE ATC”

Reads the Checklist

"ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECKLIST COMPLETED”

When Engine Fire Severe Damage or Separation Checklist completed

“AFTER TAKE OFF CHECKLIST”

“AFTER TAKE OFF CHECKLIST COMPLETED”

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION (ON TAKEOFF ABOVE V1)

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION (ON TAKEOFF ABOVE V1)

Page 11: SOPs all E190

ENGINE FAILURE/FIRE,SEVERE DAMAGE OR SEPARATION (IN FLIGHT)

PF PM

Failure indication “ENGINE 1(2) FAIL/FIRE/DAMAGE/SEPARATION”(Pilot first noticing the engine problem)

Preparation for descent

Disengages Autothrottle

Sets operative engine Thrust Lever to TO/GA position

“CONTINUOUS" Sets or verifies thrust rate to continuous

Sets Altitude capability (OEI) on altitude selector and Driftdown speed (Green Dot indicates

Driftdown speed)

Informs ATC: report emergency type and intentions

Fasten belts to ON

Press FLCH

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION (IN FLIGHT)

Performing Engine Fire, Severe Damage or

Separation MEMORY Items

“MEMORY ITEMS”

Disengages AUTOTHROTTLE

“THRUST LEVER 1(2) IDLE CONFIRM?” “CONFIRMED"

Reduces affected engine thrust lever to idle

“START/STOP 1(2) STOP CONFIRM?”

“CONFIRMED"

Selects the affected engine Start/Sop selector to STOP

“FIRE HANDLE 1(2) PULL CONFIRM?

“CONFIRMED"

Pulls the affected engine Fire Extinguisher Handle

Performing Engine Fire, Severe Damage or

Separation checklist reading

"ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECKLIST, I HAVE ATC”

Takes ATC communicationsReads the checklist

“ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECKLIST COMPLETED”

Page 12: SOPs all E190

ENGINE FAILURE (IN FLIGHT)

Reading and performing the Engine Failure checklist reading

PF PM

“ENGINE FAILURE CHECKLIST, I HAVE ATC”

Reads the checklist aloud:“THRUST LEVER 1(2) IDLE”

“THRUST LEVER 1(2) IDLE CONFIRM?”

“CONFIRMED"

Reduces affected engine Thrust Lever to idle

“START/STOP 1(2) STOP CONFIRM?”

“CONFIRMED"

Selects the Start/Stop selector to STOP

Complete the Engine Failure Checklist

“ENGINE FAILURE CHECKLIST COMPLETED”

ENGINE FAILURE/FIRE,SEVERE DAMAGE OR SEPARATION (IN FLIGHT)

PF PM

Failure indication “ENGINE 1(2) FAIL/FIRE/DAMAGE/SEPARATION”(Pilot first noticing the engine problem)

Preparation for descent

Disengages Autothrottle

Sets operative engine Thrust Lever to TO/GA position

“CONTINUOUS" Sets or verifies thrust rate to continuous

Sets Altitude capability (OEI) on altitude selector and Driftdown speed (Green Dot indicates

Driftdown speed)

Informs ATC: report emergency type and intentions

Fasten belts to ON

Press FLCH

Page 13: SOPs all E190

EMERGENCY DESCENT/RAPID DEPRESSURIZATION

In flight

PF PM

“EMERGENCY DESCENT”

Don crew oxygen masks and check communications

“MEMORY ITEMS”

Alerts cabin crew (PA):“ATTENTION CREW,

EMERGENCY DESCENT”Selects seat belts ON

Selects no smoking ON

Selects altitude (MEA or 10000 ft whichever is higher)

Selects squawk 7700

If VNAV is engaged presses VNAV button on the GP

Monitors cabin altitude

Selects FLCH

Verifies thrust levers IDLE Advises ATC:“(CALL SIGN) EMERGENCY

DESCENTSets speed brake lever to FULL Checks flight instruments and

engine parametersSelects Speed Selector Knob to

MANUAL and target speed to maximum appropriate

Monitor descent path and speed

Select MFD TERRAIN and monitor terrain clearance

After all memory items complete, call for the

appropriate QRH procedureAccomplish checklist

2000 ft to MEA or 10000 ft

“TWO THOUSAND TO LEVEL OFF”

1000 ft to MEA or 1000 ft

“ONE THOUSAND TO LEVEL OFF”

Retract speed brakes

At Safe Altitude

Inform cabin crew:“ATTENTION CREW WE HAVE REACHED SAFE ALTITUDE”

Page 14: SOPs all E190

PRECISION APPROACHPF PM

Before starting the approach “APPROACH CHECKLIST”

Perform the checklist“APPROACH CHECKLIST

COMPLETED”

When cleared for the approach

Presses the APP button on guidance panel

Checks proper annunciation on FMA

First positive inward motion of localizer “LOCALIZER ALIVE”

Glide slope alive “GLIDE SLOPE ALIVE”

On final inbound before FAF (2NM) or one dot to

intercept the glide“LANDING GEAR DOWN,

FLAPS 3”Selects Landing Gear down

and Flaps 3

At Glide Slope “SET GO AROUND HEADING AND ALTITUDE”

“HEADING____ AND ____SET”

Final approach fix inbound or outer marker

“FLAPS____, BEFORE LANDING CHECKLIST”

Selects landing flaps and performs before landing

checklist“BEFORE LANDING

CHECKLIST COMPLETED”

1000 ft RA“ONE THOUSAND”

“CHECKED" Call any deviation below 1000 ft

500 ft RA

“FIVE HUNDRED”

“CHECKED"Start to follow thrust lever

movement or manually control

80 ft to minimums EGPWS callout

“APPROACHING MINIMUMS”

Verifies EGPWS callout

Start looking for visual cues

If visual is established“VISUAL"

“LANDING"

If no visual is established

“MINIMUMS"“GO AROUND”

Page 15: SOPs all E190

NON PRECISION APPROACHPF PM

Before starting the Approach “APPROACH CHECKLIST”

Performs the checklist“APPROACH CHECKLIST

COMPLETED”

For VGP(on the heading to

intercept final approach course)

Presses the APP button on guidance panel

Checks proper annunciation on FMA

First positive inward motion of radial (Final

approach course)“CDI ALIVE”

On final inbound before FAF (2 NM) or one dot to intercept

the glide (VGP)

“LANDING GEAR DOWN, FLAPS 3”

Selects landing gear down and flaps 3

At FAF

“FINAL APPROACH FIX”Start timer (if applicable)

“SET MINIMUMS” (for FPA or V/S)

“GO AROUND” (for VGP)When not using VGP, reaching MDA with ALT mode engaged,

set the Go Around Altitude

Sets minimums (or Go Around altitude for VGP)

Verifies altimeters, instruments and no flags

“FLAPS___, BEFORE LANDING CHECKLIST”

Selects landing flaps and perform the checklist“BEFORE LANDING

CHECKLIST COMPLETED”

1000 ft RA“ONE THOUSAND”

“CHECKED" Call any deviation below 1000 ft RA

500 FT RA

“FIVE HUNDRED”

"CHECKED"Start to follow thrust lever

movement or manually control

Page 16: SOPs all E190

At 80 ft minimuns, EGPWS callout:“APPROACHING

MINIMUS

Verifies EGPWS callout

Starts looking for visual cues.

If visual reference is established

“VISUAL""LANDING"

If no visual reference is established

“MINIMUMS"“GO AROUND”

Page 17: SOPs all E190

NORMAL GO AROUND

Go Around

PF PM

“GO AROUND”Press either TOGA buttons Verify GA annunciations

Verify or move thrust levers to TO/GA detent Verify engine at GA thrust

With the airspeed greater than VREF:”FLAPS___” Selects GA flaps

Verifies rotation or rotates towards GA initial pitch

attitude (8º)

Positive rate of climb

“POSITIVE RATE”“GEAR UP” Selects Gear Up

Selects VFSAsvises ATC

400 ft AGL

“SELECTS FMS (when FMS is not the navigation source) AND HEADING

(NAV)

Selects appropriate navigation primary source

Selects Lateral Mode

Acceleration Altitude

“CLIMB SEQUENCE” Selects VNAV and FMS speeds

Executes published missed approach or proceed as

instructed by ATCRetracts Flaps on schedule

At flap zero calls:“FLAPS ZERO”

Monitor missed approach procedure

Page 18: SOPs all E190

ONE ENGINE INOPERATIVE GO AROUND

Go around becomes necessary

PF PM

“GO AROUND”

Press either TO/GA buttons Verify GA annuncates

Verify or move thrust levers to the TO/GA detent

Verify engine thrust at GA RSV

“FLAPS___” Selects GA Flaps

Verify or rotate towards GA pitch attitude

Positive rate of climb

“POSITIVE RATE”

“GEAR UP” Selects GEAR UP

Climbs at VAC Selects VFS on the Speed Selector Knob

Controls the airplane using rudder and yaw trim (avoid roll

spoilers to be deployed) Advice ATC

400 ft AGL “SELECT HEADING, BANK” Selects HDG and BANK

Acceleration Altitude

“SELECT FLCH” Selects FLCH

At flaps retraction speeds:“FLAPS____”

Retracts flaps and calls:“FLAPS ZERO”

Reaching VFS:“CONTINUOUS”

Sets or verifies thrust rate to continuous

Climbing to Safe Altitude

Climbs at VFS to a safe altitude or as assigned by ATC Advises ATC

Monitor thrust, altitude, speed and missed

approach procedures

Page 19: SOPs all E190

REJECTED LANDING

Go Around

PF PM

“GO AROUND”

Press either TOGA buttons Verify GA annunciations

Verify or move thrust levers to TO/GA detent

Verify engine at Go Around thrust

With the airspeed greater than VREF:

“FLAPS___”Selects GA Flaps

Verifies rotation or rotates towards GA pitch attitude

Positive Rate of Climb

“POSITIVE RATE”

“GEAR UP” Selects Gear Up

Selects VFS

Advises ATC

400 ft AGL“SELECT HEADING (NAV)” Selects appropriate

navigation primary source

Selects Lateral Mode

Acceleration Altitude

“CLIMB SEQUENCE”

Executes published missed approach or proceed as

instructed by ATCSelects FLCH

Selects VFS

Retract Flaps on schedule

At Flaps zero call:“FLAPS ZERO”

Monitor missed approach procedures