Rev. 16 del SOPM-1755-001

In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose.

Copyright 2013 by Embraer S.A. All rights reserved.

EMBRAER 170/175/190/195

STANDARD OPERATING PROCEDURES MANUAL

EMBRAER S.A.

This manual is applicable to EMBRAER 170/175 and EMBRAER 190/195 airplanes equipped respectively with CF34-8E and CF34-10E series engines, operating under ANAC, FAA, EASA/JAA and TCCA certifications.

SOPM1755-001

DECEMBER 10, 2003 REVISION 16 JULY 02, 2013

STANDARD OPERATING

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HIGHLIGHTS OF CHANGE

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HIGHLIGHTS OF CHANGE The changes in this document are recognized by a vertical bar on the edge of the page matching with the changed lines. This bar will reflect the document revision number located at the bottom right of each page.

Here are presented the summary of these changes.

REVISION 16 JUL 02, 2013

Block Page Change Description

1-05 1 Editorial correction.


2-00 1 Added reference to the Engine Transfer Hose Start procedure.

2-13 4 Updated the DVDR Control Panel test procedure to include L3 DVDR model information.

2-17 4 Updated information regarding the step to check the reversionary panel.


2-35 1 Added the guidance to perform an in-flight assessment of the runway condition at destination.

2-63 2 to 6 Added a new procedure. Engine Transfer Hose Start.

2-65 2 Updated procedure. The step to disconnect ground cart was moved to the After Start checklist.

2-75 1, 2 Updated information regarding minimum fuel temperature.

3-00 3 to 7 Editorial correction and information update.

3-05-01 6 Added Maximum Performance Landing definition.

3-05-10 7

Updated information to clarify that placing the thrust lever to MAX the engine thrust will be set to GA-RSV If windshear happens during approach or TOx-RSV if it happens during takeoff.


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3-10 16, 18

Improved the Emergency Evacuation Procedure text regarding pilots announcement to the cabin crewmembers about the preferred airplane side for evacuation.

3-15-01 2 Added a NOTE with information about runway distance used during engine acceleration when a rolling takeoff is performed.

3-15-01 7 Editorial correction.

3-15-05 4

Updated procedure description to clarify that the TAKEOFF WITH TAILWIND ABOVE 10 KT technique is also applicable to EMBRAER 170/175 airplanes certified takeoff and landing operations with tailwind from 10 kt to 15 kt.

3-15-10 3 Added information that applicable local operations regulations regarding bank angle limit for OEI operations must be observed.

3-15-10 4 Added information that If TO RSV is not achieved PNF shall move thrust levers to MAX.

3-15-10 9

Updated the ENGINE __ FIRE callout to ENGINE __ FIRE/DAMAGE/SEPARATION on the ENGINE FIRE, SEVERE DAMAGE OR SEPARATION (ON TAKEOFF ABOVE V1) ACTIONS and CALLOUTS table.

3-15-10 9 Added information that If TO RSV is not achieved PNF shall move thrust levers to MAX.

3-20 2

Added a guidance to the climb technique to avoid TCAS resolution advisory during level offs when pilots are aware of traffic in close vicinity at the adjacent flight level.

3-25 8 Updated information about use of autothrottle during severe turbulence. 3-25 9 Editorial correction.

3-25 12 Updated the ENGINE __ FIRE/FAIL callout to ENGINE __ FIRE/DAMAGE/SEPARATION callout.

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3-25 21 to 26Included Controller to Pilot Data Link Communication System (CPDLC) information and actions and callouts tables.

3-25 27 Updated the Unreliable Airspeed procedure text to inform that in this scenario the FPA on PFD or FPV on HGS may also be unreliable.


3-25 28 Updated the PNF actions during a NOSE-UP recovery.

3-25 29 Updated the PNF actions during a NOSE-DOWN recovery. 3-25 34 Added Engine Vibration During Cruise information.

3-30 2

Added a guidance to the descent technique to avoid TCAS resolution advisory during level offs when pilots are aware of traffic in close vicinity at the adjacent flight level.

3-35-01 2 Included recommendations to avoid flap overspeed during approach. 3-35-01 3, 4 Updated the approach briefing recommendations.

3-35-01 7 Included guidance for nom precision approaches without FMS.

3-35-01 8 Included the information that VREF additives during normal operation have to be made only due to Wind correction.

3-35-01 8A Included information that with the airplane in the final configuration for landing, VAP and VREF can be lower than GD.

3-35-01 8A Included a NOTE to inform that any additive to the VREF shall be considered in the landing distance calculations.

3-35-05 2 Updated the deviation callout table.

3-35-10 3 Updated information about VPATH during VNAV APPROACH.

3-40 1, 2 Updated the stabilized approach criteria to clarify that VREF additives during normal operation have to be made only due to Wind correction.


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3-40 3 Added a note to clarify that Maximum Thrust Reverser has to be applied when operating in wet/slippery and contaminated runways.

3-40 4 Updated the BRAKES USAGE text.

3-40 5 Included MAXIMUM PERFORMANCE LANDING techniques.

3-40 6 Updated LANDING ON WET, SLIPPERY OR CONTAMINATED RUNWAYS techniques.

3-40 6A, 6B Updated OPERATIONAL FACTORS AFFECTING LANDING DISTANCE information.

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LIST OF EFFECTIVE PAGES

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ORIGINAL................ 0....................DEC 10, 2003 REVISION................ 1.................... FEB 20, 2004 REVISION................ 2....................MAY 31, 2004 REVISION................ 3....................DEC 23, 2004 REVISION................ 4....................AUG 07, 2006 REVISION................ 5....................MAY 29, 2007 REVISION................ 6..................... JUL 31, 2007 REVISION................ 7.................... JUN 30, 2008 REVISION................ 8....................NOV 20, 2008 REVISION................ 9....................AUG 03, 2009 REVISION................ 10..................DEC 18, 2009 REVISION................ 11..................APR 30, 2010 REVISION................ 12..................AUG 26, 2010 REVISION................ 13..................MAY 30, 2011 REVISION................ 14.................. SEP 19, 2011 REVISION................ 15................... JUL 16, 2012 REVISION................ 16................... JUL 02, 2013


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* Title ..............REVISION 16 0-LEP * 1 ...................REVISION 16 * 2 ...................REVISION 16 * 3 ...................REVISION 16 * 4 ...................REVISION 16 * 5 ...................REVISION 16 * 6 ...................REVISION 16 * 7 ...................REVISION 16 * 8 ...................REVISION 16 0-TOC 1 ...................REVISION 10 2 ...................REVISION 10 1-00 1 ...................REVISION 10 2 ...................REVISION 10 1-05 * 1 ...................REVISION 16 2 ...................REVISION 12 2-00 * 1 ...................REVISION 16 2 ...................REVISION 12 2-07 1 ...................REVISION 11 2 ...................REVISION 11 3 ...................REVISION 10 4 ...................REVISION 10 2-09 1 ...................REVISION 12 2 ...................REVISION 13 2-13 1 ...................REVISION 12 2 ...................REVISION 15

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2 ................... REVISION 10 2-31 1................... REVISION 15 2................... REVISION 10 2-33 1................... REVISION 12 2................... REVISION 10 2-34 1................... REVISION 10 2................... REVISION 10 2-35 * 1................... REVISION 16 * 2................... REVISION 16 2-37 1................... REVISION 10 2................... REVISION 10 2-41 1................... REVISION 12 2................... REVISION 10 2-42 1................... REVISION 12 2................... REVISION 10 2-45 1................... REVISION 10 2................... REVISION 10 2-49 1................... REVISION 14 2................... REVISION 10 2-53 1................... REVISION 10

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TABLE OF CONTENTS

1 - INTRODUCTION

2 - NORMAL PROCEDURES

3 - PROCEDURES AND TECHNIQUES

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SECTION 1

INTRODUCTION TABLE OF CONTENTS

Block Page Introduction ........................................................................ 1-05.......... 01

Procedural Deviation and Its Relation to Safety........... 1-05.......... 02 Airplane Sophistication and Checklists ........................ 1-05.......... 02

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INTRODUCTION The SOP provides information and guidance for the efficient operation of the E-Jets. This manual is not a replacement of any of the operational manuals required by applicable regulations such as the Airplane Flight Manual or the Company Operations Manual. This SOP is optimized for passenger-carrying operation in a commercial airline environment and the philosophy behind this manual is based on reducing crew workload while maintaining the highest possible level of safety. Standard operating procedures are a set of procedures that serve to provide common ground for all crewmembers, usually unfamiliar with each other's experience and technical capabilities. In a well-standardized operation, another qualified pilot could replace an active cockpit crewmember during the flight, and the operation would continue safely and smoothly. The Normal Procedures section presents the AFM/AOM Normal Procedures. The intention is to eliminate any doubts regarding Flight Standards that may occur during the operation of the airplane. The Procedures and Techniques section brings operational practices and flight profiles to a standard cockpit concept throughout flight phases. It has directives related to how the operation should be conducted. Topics like Crew Coordination, Captain authority and Areas of responsibility are included. It also contains guidelines to be observed should a specific situation arise regardless of when and where it occurs during the flight. Topics such as handling of the autopilot and task sharing when hand-flying the airplane are covered in those sections. Information regarding Low Visibility standardizes the procedures under this scenario emphasizing the crew coordination and presents the configurations approved to perform the operation with low visibility divided in flight phases. Emergency/Abnormal Procedures are also presented according to its flight phase in the Procedures and Techniques section. It is presented some AFM/AOM Emergency/Abnormal Procedures in a detailed manner. The intention is to guide the crew on how to perform the required tasks to correct a situation or condition. Only the QRH procedures requiring high level of crew coordination are presented.

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PROCEDURAL DEVIATION AND ITS RELATION TO SAFETY

The highest percentage of problems that generate crew-caused accidents and incidents manifest themselves in the form of procedural deviation. If the flight goes well, these deviations are not perceived and in most cases are left unresolved but they become apparent following an incident or an accident.

AIRPLANE SOPHISTICATION AND CHECKLISTS

The degree of technological sophistication in the design of this family of airplanes directly affects the checklist. On older airplanes, the flight crew must manually select and monitor most items. In more advanced airplanes the same items are accomplished by automatic systems that relieve the flight crew of these tasks. Checklists for these airplanes tend to be shorter and simpler but require a more careful task analysis with improved monitoring skills.

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SECTION 2

NORMAL PROCEDURES

TABLE OF CONTENTS

Block Page

Normal Checklist................................................................ 2-07.......... 01

Internal Safety Inspection .................................................. 2-09.......... 01

Power Up ........................................................................... 2-13.......... 01

External Inspection ............................................................ 2-15.......... 01

Before Start........................................................................ 2-17.......... 01

Engine Start ....................................................................... 2-17.......... 12

After Start........................................................................... 2-25.......... 01

Before Takeoff ................................................................... 2-29.......... 01

Takeoff ...............................................................................2-31.......... 01

After Takeoff ...................................................................... 2-33.......... 01

Climb..................................................................................2-34.......... 01

Descent..............................................................................2-35.......... 01

Approach ...........................................................................2-37.......... 01

Before Landing .................................................................. 2-41.......... 01

Go Around ......................................................................... 2-42.......... 01

After Landing ..................................................................... 2-45.......... 01

Shutdown...........................................................................2-49.......... 01

Leaving the Airplane.......................................................... 2-53.......... 01

ECS OFF Takeoff .............................................................. 2-60.......... 01

Engine Crossbleed Start....................................................2-63.......... 01

Engine Transfer Hose Start ............................................... 2-63.......... 02

Engine Ground Pneumatic Start........................................ 2-65.......... 01

Engine Battery Start........................................................... 2-67.......... 01

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Block Page

Single Engine Taxi .............................................................2-70 ..........01

Hot Weather .......................................................................2-73 ..........01

Ice Conditions, Cold Weather and Cold Soak ...................2-75 ..........01

Lightning Strike ..................................................................2-77 ..........01

Turbulent Air Penetration ...................................................2-80 ..........01

Windshear ..........................................................................2-83 ..........01

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NORMAL PROCEDURES

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NORMAL CHECKLIST INTERNAL SAFETY INSPECTION

CHALLENGE ACTION PERFORMED BY

Maintenance Status...........CKD .........................LSP/RSP Cockpit Emer Equip...........CKD ................................ RSP ELECTRIC Panel...............SET ................................. RSP FUEL Panel .......................CKD ................................ RSP Windshield Wiper...............OFF................................. RSP HYDRAULIC Panel............CKD ................................ RSP AIR COND/PNEU Panel....CKD ................................ RSP PAX OXY Panel.................CKD ................................ RSP ELT ....................................ARM ................................ RSP Landing Gear Lever...........DOWN............................. RSP START/STOP Selectors ....STOP .............................. RSP Speed Brake Lever............CLOSED ......................... RSP RAT Manual Deploy ..........STOWED ........................ RSP SLAT/FLAP Lever..............VERIFY POS .................. RSP Circuit Breakers .................CKD ................................ RSP


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POWER UP CHALLENGE ACTION PERFORMED BY

CAUTION: ENSURE THE AIRPLANE IS NOT MOVED BEFORE THE IESS IS INITIALIZED.

Battery 1 ............................ON................................... RSP Battery 2 ............................AUTO .............................. RSP CAUTION: VERIFY THAT ONLY DISPLAYS 2 AND 3

ARE AVAILABLE. IF MORE THAN DISPLAYS 2 AND 3 ARE AVAILABLE, THE AIRPLANE MUST NOT BE DISPATCHED.

Battery voltage...................CKD................................. RSP GPU Button (if applicable) .PUSHED IN..................... RSP Fire Ext panel.....................CKD................................. RSP APU....................................AS RQRD........................ RSP NAV light ............................ON................................... RSP HYDRAULIC panel ............AS RQRD........................ RSP Electronic CBs ...................CKD..................................LSP Electronic Checklist (if applicable) ................CKD................................. RSP DVDR panel .......................CKD................................. RSP Cockpit reinforced door

panel (if applicable) ......CKD................................. RSP Photoluminescent Strips ....CKD................................. RSP

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BEFORE START CHALLENGE RESPONSE ANSWERED BY

Pax signs panel .................SET ..................................LSP PRESSURIZATION Panel.SET ..................................LSP Oxygen masks...................CKD .........................LSP/RSP Flight instruments ..............X-CKD..............................LSP Thrust levers...................... IDLE .................................LSP ------------------------------------------------------------------------------------------------

Fuel QTY ...........................CKD .........................LSP/RSP MCDU................................SET ..................................LSP TRIM Panel........................___ SET/ZERO/ZERO.....LSP Doors & windows...............CLSD .......................LSP/RSP Red beacon .......................ON....................................LSP Emergency/Parking brake .AS RQRD.........................LSP

AFTER START CHALLENGE RESPONSE ANSWERED BY

Ground equipment.............REMOVED.......................LSP SLAT/FLAP........................___ SET ...........................LSP Flight controls ....................CKD .................................LSP

BEFORE TAKEOFF CHALLENGE RESPONSE ANSWERED BY

Brakes temp ......................CKD ............................... ..LSP EICAS................................CKD ............................... ..LSP Transponder ......................TA/RA ..............................LSP Takeoff configuration .........CKD ............................... ..LSP

AFTER TAKEOFF CHALLENGE RESPONSE ANSWERED BY

Landing gear......................UP ....................................PNF SLAT/FLAP........................0 .......................................PNF


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APPROACH CHALLENGE RESPONSE ANSWERED BY

Pax signs panel .................SET ................................. PNF Altimeters...........................SET/X-CKD ................PF/PNF

BEFORE LANDING CHALLENGE RESPONSE ANSWERED BY

Landing gear......................DOWN .......................PF/PNF SLAT/FLAP........................___ SET .....................PF/PNF

SHUTDOWN CHALLENGE RESPONSE ANSWERED BY

Emergency/Parking brake .SET .................................LSP START/STOP selectors.....STOP ...............................LSP Hyd pump 3A .....................OFF ..................................LSP

LEAVING THE AIRPLANE CHALLENGE RESPONSE ANSWERED BY

Pax signs panel .................OFF ..................................LSP GPU/APU...........................OFF ..................................LSP Batteries 1 and 2................OFF ..................................LSP

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INTERNAL SAFETY INSPECTION

The Internal Safety Inspection procedures must be performed before the Power Up on a particular airplane.


Maintenance Status..................................... CHECK .....LSP&RSP

Cockpit Emergency Equipment ................. CHECK ...............RSP

Check for the availability, status and proper location of the following equipment:

Protective Breathing Equipment (PBE). Fire Extinguishers. Crash Axe. Life Vests. Escape Ropes. Flashlights.

ELECTRIC Panel ................................................SET ...............RSP

IDG 1 Selector .................................................... AUTO IDG 2 Selector .................................................... AUTO AC BUS TIES Selector....................................... AUTO GPU Button ........................................................ PUSHED OUT APU GEN Button................................................ PUSHED IN TRU 1 ................................................................. AUTO TRU ESS............................................................ AUTO TRU 2 ................................................................. AUTO DC BUS TIES..................................................... AUTO Battery 1 Selector............................................... OFF Battery 2 Selector............................................... OFF


PROCEDURES


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PM

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5


FUEL Panel ...................................................CHECK .............. RSP

Verify all fuel pump knobs in AUTO position and XFEED in the desired position.

WINDSHIELD WIPER Selectors ....................... OFF .............. RSP

HYDRAULIC Panel .......................................CHECK .............. RSP

SYS 1 ENG PUMP SHUTOFF Button................ PUSHED OUT PTU Selector ...................................................... AUTO SYS 2 ENG PUMP SHUTOFF Button................ PUSHED OUT SYS 1 and 2 ELEC PUMP Selectors.................. AUTO SYS 3 ELEC PUMP A ........................................ OFF SYS 3 ELEC PUMP B ........................................ AUTO

AIR COND/PNEUMATIC Panel ....................CHECK .............. RSP

Verify all buttons pushed in.

PASSENGER OXYGEN Panel .................... CHECK .............. RSP

Verify Masks Deploy Selector Knob in AUTO.

ELT .................................................................... ARM .............. RSP

Landing Gear Lever ...................................... DOWN .............. RSP

START/STOP Selectors..................................STOP .............. RSP

Speed Brake Lever ....................................CLOSED .............. RSP

RAT Manual Deploy ..................................STOWED .............. RSP

SLAT/FLAP Lever...................... VERIFY POSITION .............. RSP

Verify and make sure that the actual SLAT/FLAP lever position agrees with the surface position.

Circuit Breakers ...........................................CHECK .............. RSP

Verify both sidewall panels to ensure agreement with maintenance status.

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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5

POWER UP

The POWER UP procedures and checklist must be performed every crews first flight of the day on a particular airplane or when a power down was required.

If receiving the airplane already powered up, verify compliance with all items and perform FIRE EXTINGUISH panel, Electronic CBs and DVDR CONTROL panel.

CAUTION: ENSURE THE AIRPLANE IS NOT MOVED BEFORE THE IESS IS INITIALIZED.


Battery 1 .............................................................. ON ...............RSP

Battery 2 ..........................................................AUTO ...............RSP

CAUTION: VERIFY THAT ONLY DISPLAYS 2 AND 3 ARE AVAILABLE. IF MORE THAN DISPLAYS 2 AND 3 ARE AVAILABLE, THE AIRPLANE MUST NOT BE DISPATCHED.

Batteries Voltage ......................................... CHECK ...............RSP

Verify batteries voltage at or above 22 V (ANAC/TCCA certification) or 22.5 V (FAA/EASA certification).

If batteries voltage is between 21 V and 22 V (ANAC/TCCA certification) or 21 V and 22.5 V (FAA/EASA certification), recharge the batteries prior to takeoff, through any AC source (including engines during taxi) for:

30 minutes if batteries temperature is at or above 0oC or; 35 minutes if batteries temperature is at or above -5oC and

below 0oC or; 40 minutes if batteries temperature is at or above -10oC and

below -5oC or; 50 minutes if batteries temperature is below -10oC;

If batteries voltage is below 21 V, report to maintenance.

NOTE: Minimize the time the airplane is left with batteries as the unique power source, to avoid discharging.


PROCEDURES


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5


EICAS Messages....................CHECK DISPLAYED .............. RSP

GPU Button (if applicable) ...................PUSHED IN .............. RSP

Verify AVAIL light illuminated before pushing in. When GPU is not available, or is not necessary, maintain GPU Button pushed out.

NOTE: - The Electrical PBIT is automatically performed after the airplane is powered by any AC source and takes about 3 minutes to complete. The Electrical PBIT will be interrupted if any electric hydraulic pump is running, the FLIGHT CONTROLS MODE Panel switches are cycled or if AC power is interrupted while the test is running.

- A FLT CTRL TEST IN PROG Status message is displayed to inform the pilot that the Electrical PBIT is in progress.

- If the displays 2 and/or 4 are configured as PFD, set the respective reversionary panel selector knob to MFD then to AUTO. After 8 seconds, the affected display configuration will return to MFD.

FIRE EXTINGUISHER Panel (Overhead)....CHECK .............. RSP

Verify there are no fire protection fail messages displayed on the EICAS after Power Up.

Press and hold the TEST button and observe the following EICAS messages, lights and warnings:

Aural warning. Fire handles illuminated. CARGO SMOKE FWD/AFT buttons illuminated. APU button illuminated. Upper half of the APU Emergency Stop Button

illuminated. WARNING lights flashing. CARGO FWD (AFT) SMOKE EICAS message. APU FIRE EICAS message. ENG 1 (2) FIRE EICAS message. FIRE warning annunciation displayed inside ITT

indicators.

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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5


APU CONTROL Panel......................AS REQUIRED ...............RSP

Verify EMER STOP Button is pushed out and not illuminated.

NOTE: If AC source is lost due to unintentional GPU or APU generator disconnection, power down the airplane and perform the power up procedure.

Navigation Light ................................................. ON ...............RSP

HYDRAULIC Panel...........................AS REQUIRED ...............RSP

Only after the electrical PBIT is completed and if the FLT CTRL BIT EXPIRED EICAS message is displayed, perform the hydraulic panel checks.

Do not move any flight control surface. SYS 1 and 2 ELEC Pumps ON. SYS 3 ELEC PUMP A ON. Wait 1 minute. At this point the

FLT CTRL BIT EXPIRED EICAS message should extinguish. SYS 1 and 2 ELEC Pumps AUTO. SYS 3 ELEC PUMP A OFF.

NOTE: - The FLT CTRL TEST IN PROGRESS Status message is displayed while hydraulic PBIT is in progress.

- If the FLT CTRL BIT EXPIRED EICAS message is still displayed, power down the airplane and perform the power up procedure.

Electronic CBs ............................................. CHECK ............... LSP

Select CB OUT/LOCK page on MCDU and check the CBs status to ensure agreement with maintenance status.

If the NEW TRIP prompt is displayed on the MCDU press it to check the electronic CBs status.

Electronic Checklist (if applicable)............ CHECK ...............RSP

Verify that this ECL database corresponds to the paper QRH revision present in the cockpit.


PROCEDURES


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PM

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5

DVDR CONTROL Panel ...............................CHECK .............. RSP

Honeywell or L3 DVDR: Press and hold TEST Button for three seconds and verify no fail messages displayed on EICAS.

Universal DVDR: Press and hold TEST button for two seconds.

Verify no fail messages displayed on EICAS and observe the following test result:

The FDR 1 and CVR 1 PASS/FAIL lights flash during

ten seconds. After ten seconds the FDR 1 and CVR 1 PASS/FAIL lights illuminate steady in green, indicating the completion of a successful test.

After the DVDR 1 test finishes, the DVDR 2 test will automatically start. Verify the following test result:

The FDR 2 and CVR 2 PASS/FAIL lights flash during ten seconds. After ten seconds the FDR 2 and CVR 2 PASS/FAIL lights illuminate steady in green, indicating the completion of a successful test.

If a failure is found, the corresponding FDR/CVR fail light indicator will illuminate steady in amber.

Electronic Flight Bag (if applicable).................. ON ...LSP & RSP

Cockpit Reinforced Door Panel (if applicable) ......................CHECK .............. RSP

Close the cockpit door; Press and hold the TEST button; Check DING-DONG alarm and UNLOCKED indication ON; Push in the LOCK button and check the electromechanical

latch normal operation; Press the EMERG ENTRY button on the door control panel in

the passenger cabin. Check the UNLOCKED indication flashing and check normal operation of the DING-DONG alarm sequence according to the system logic (refer to AOM 14-01-22 and 14-01-60);

Push out the LOCK button.

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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PM

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5

Photoluminescent Strips ............................ CHECK ...............RSP Check in the AOM section 3-05 how much time of ceiling and entrance lighting exposure in bright or daylight would be necessary to charge the photoluminescent strips.


PROCEDURES


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PM

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5

INTENTIONALLY BLANK

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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PM

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5c01

EXTERNAL INSPECTION The External Inspection procedures are usually performed by the RSP prior to each flight. While conducting the external inspection, pilots must be aware of moving vehicles around the airplane and surroundings. In case of suspicious object is identified, inform immediately the security staff.

Prior to starting the external inspection: CHALLENGE ACTION

External Lights .......................................................AS REQUIRED If the external lights check was not performed by the maintenance, turn the external lights ON and check them. Turn the lights OFF immediately after check.

Emergency/Parking Brake ....................................ON Check if there is sufficient hydraulic pressure to activate the Emergency/Parking Brake to check the Brake Wear Indicators.

Recommended walk-around sequence:


PROCEDURES


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5 c0

1

1. LEFT FWD FUSELAGE

FWD Passenger Door ............................................CHECK

External Power Receptacle ...................................SECURED

Left Smart Probes/TAT Sensor/Ice Detector .......CHECK Verify condition with no obstructions, covers or damage.

2. NOSE SECTION

Windshield Wipers .................................................CHECK

Radome ...................................................................CONDITION AND LATCHED

Forward Avionics Compartment...........................SECURED

If not in use, visibly secured.

Lower FWD Antenna ..............................................CONDITION Undamaged.

3. NOSE LANDING GEAR

Wheels and Tires....................................................CONDITION

Up Lock Hook .........................................................UNLOCKED

Strut/Wheel Well/Doors .........................................CONDITION AND NO LEAKS

Ground Locking Pin ...............................................REMOVED

Landing and Taxi Lights........................................CONDITION

Clean and undamaged.

4. RIGHT FWD FUSELAGE

Right Smart Probes/TAT Sensor/Ice Detector.....CHECK

Verify condition with no obstructions, covers or damage.

(Continued)

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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PM

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5 c0

1

RAT Safety Lock Pin.............................................. REMOVED

FWD Service Door ................................................. CHECK


Oxygen Discharge Indicator................................. GREEN DISC

FWD Cargo Door.................................................... CHECK


5. LOWER CENTER FUSELAGE

Lower FWD Antennas/Fwd Drain Mast................ CONDITION

Undamaged.

Lower Red Beacon Light ...................................... CONDITION

Clean and undamaged

6. RIGHT CENTER WING

Wing Inspection Landing and Taxi Lights .......... CONDITION


Right Ram Air Inlet ................................................ NO OBSTRUCTION

No obstruction or damage.

Air Inlets and Outlets............................................. NO OBSTRUCTION


Collector Tank Water Drain Valve Door............... SECURED


Wing Tank Water Drain Valve............................... CONDITION AND NO LEAKS

Applicable only to E170/175 airplanes.


(Continued)


PROCEDURES


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PM

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5 c0

1

Magnetic Level Indicators .....................................PUSHED IN AND NO LEAKS

E170/175: Verify RH1 Magnetic Level Indicator.

E190/195: Verify RH1 and RH2 Magnetic Level Indicators.

Pylon .......................................................................CONDITION

7. ENGINE 2 LH SIDE

Engine Inlet.............................................................CONDITION

Check for FOs and leaks inside air inlet. Ensure that there is no damage to the T12 Sensor and that the FADEC Cooling Inlet is clear

Fan Blades..............................................................CHECK

Check for damaged Fan Blades and ensure Fan is free to rotate.

Check for damages on spinner.

LH Nacelle Strake...................................................CONDITION

Anti-ice Pressure Relief Door ...............................CLOSED AND LATCHED

LH Fan Cowl Doors................................................CONDITION AND LATCHED

LH Thrust Reverser................................................CONDITION AND LATCHED

Core Pressure Relief Door ....................................CLOSED

Turbine Exhaust.....................................................CLEAR AND NO LEAKS

After engine shutdown the scavenge system is no longer effective. A small amount of oil may leak through the aft sump drain and pool in the engine chevron nozzle.

E170/175: If the puddle size exceeds 4 in (102 mm), maintenance should be contacted.

E190/195: If the puddle size exceeds 9 in x 6 in (229 mm x 152 mm), maintenance should be contacted. For airplanes equipped with Improved Acoustic Chevron Nozzle (IACN) the puddle should not exceed 7.5 in x 4.5 in (190 mm x 114 mm). (Continued)

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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5 c0

1

8. ENGINE 2 RH SIDE

Core Pressure Relief Door.................................... CLOSED

RH Thrust Reverser ............................................... CONDITION AND LATCHED

RH Fan Cowl Doors ............................................... CONDITION AND LATCHED

FADEC Cooling Vent ............................................. CLEAR

RH Nacelle Strake.................................................. CONDITION

Oil Fill Access Door............................................... CLOSED

9. RIGHT WING LEADING EDGE

Wing Leading Edges ............................................. CONDITION

Refueling Compartment Door .............................. SECURED

Magnetic Level Indicators..................................... PUSHED IN AND NO LEAKS

E170/175: Verify RH2 and RH3 Magnetic Level Indicators.

E190/195: Verify RH3 Magnetic Level Indicator.

Access Doors and Panels..................................... SECURED

Pressure Relief Valve ............................................ CHECK

Wing Vents ............................................................. NO OBSTRUCTION

Navigation and Strobe Lights............................... CONDITION


10. RIGHT WING TRAILING EDGE

Static Dischargers ................................................. NUMBER AND CONDITION

Verify 3 Static Discharges on the aileron and 6 on the winglet. Refer to the CDL for dispatch with missing items.

(Continued)


PROCEDURES


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5 c0

1

Flight Control Surfaces and Fairings...................CONDITION

Surfaces clear and unobstructed.

11. RIGHT LANDING GEAR

Right Main Gear .....................................................CHECK

Wheels and Tires ...................................................CONDITION

Up Lock Hook.........................................................UNLOCKED

Strut/Wheel Wells...................................................CONDITION AND NO LEAKS

Ground Locking Pin...............................................REMOVED

Brakes Wear Indicators .........................................CHECK

12. RIGHT AFT FUSELAGE

Access Doors and Panels .....................................SECURED


Drain Mast...............................................................CONDITION


AFT Cargo Door .....................................................CHECK


AFT Service Door...................................................CHECK


Lower AFT Antennas/AFT Drain Mast .................CONDITION

Undamaged.

Battery Air Outlet ...................................................NO OBSTRUCTION


(Continued)

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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5 c0

1

13. TAIL SECTION

Flight Control Surfaces......................................... CONDITION

Surfaces Clear and Unobstructed.

Empennages Leading Edges................................ CONDITION

Static Dischargers ................................................. NUMBER AND CONDITION

E170/175: Verify 4 Static Dischargers on the rudder, 4 on each elevator and 1 on vertical stabilizer.

E190/195: Verify 4 Static Dischargers on the rudder, 3 on each elevator, 3 on each horizontal stabilizer and 1 on vertical stabilizer.

Refer to the CDL for dispatch with missing items.

APU ......................................................................... CONDITION

14. LEFT AFT FUSELAGE

APU External Power Receptacle .......................... CHECK


Overboard Vent...................................................... NO OBSTRUCTION


Pressurization Static Port..................................... NO OBSTRUCTION


Potable Water Service Panel ................................ SECURED


AFT PAX Door ........................................................ CHECK


Lower AFT Antennas............................................. CONDITION

Undamaged.

(Continued)


PROCEDURES


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5 c0

1

Access Doors and Panels .....................................SECURED


15. LEFT LANDING GEAR

Left Main Gear ........................................................CHECK

Wheels and Tires ...................................................CONDITION

Up Lock Hook.........................................................UNLOCKED

Strut/Wheel Wells...................................................CONDITION AND NO LEAKS

Ground Locking Pin...............................................REMOVED

Brakes Wear Indicators .........................................CHECK

16. LEFT WING TRAILING EDGE

Flight Control Surfaces and Fairings...................CONDITION

Surfaces clear and unobstructed.

Static Dischargers .................................................NUMBER AND CONDITION

Verify 3 static dischargers on the aileron and 6 static dischargers on the winglet. Refer to the CDL for dispatch with missing items.

Navigation, Strobe Lights and Upper red Beacon Lights..........................CONDITION Clean and undamaged.

Upper Antennas .....................................................CONDITION

Undamaged.

17. LEFT WING LEADING EDGE

Wing Leading Edges..............................................CONDITION

(Continued)

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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5 c0

1

Wing Vents ............................................................. NO OBSTRUCTION

Pressure Relief Valve ............................................ CHECK

Access Doors and Panels..................................... SECURED

Wing Leading Edges ............................................. CONDITION

Magnetic Level Indicator....................................... PUSHED IN AND NO LEAKS

E170/175: Verify LH3 and LH2 Magnetic Level Indicators.

E190/195: Verify LH3 Magnetic Level Indicator.

18. ENGINE 1 LH SIDE

Engine Inlet ............................................................ CONDITION

Check for FOs and leaks inside air inlet. Ensure that there is no damage to the T12 Sensor and that the FADEC Cooling Inlet is clear

Fan Blades.............................................................. CHECK

Check for damaged Fan Blades and ensure Fan is free to rotate.

Check for damages on spinner.

LH Nacelle Strake .................................................. CONDITION

Anti-ice Pressure Relief Door............................... CLOSED AND LATCHED

LH Fan Cowl Doors................................................ CONDITION AND LATCHED

LH Thrust Reverser ............................................... CONDITION AND LATCHED

Core Pressure Relief Door.................................... CLOSED

Turbine Exhaust..................................................... CLEAR/NO LEAKS

(Continued)


PROCEDURES


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1

After engine shutdown the scavenge system is no longer effective. A small amount of oil may leak through the aft sump drain and pool in the engine chevron nozzle.

E170/175: If the puddle size exceeds 4 in (102 mm), maintenance should be contacted.

E190/195: If the puddle size exceeds 9 in x 6 in (229 mm x 152 mm), maintenance should be contacted. For airplanes equipped with Improved Acoustic Chevron Nozzle (IACN) the puddle should not exceed 7.5 in x 4.5 in (190 mm x 114 mm).

19. ENGINE 1 RH SIDE

Core Pressure Relief Door ....................................CLOSED

RH Thrust Reverser ...............................................CONDITION AND LATCHED

RH Fan Cowl Doors ...............................................CONDITION AND LATCHED

FADEC Cooling Vent .............................................CLEAR

RH Nacelle Strake ..................................................CONDITION

Oil Fill Access Door ...............................................CLOSED

20. LEFT CENTER WING

Magnetic Level Indicators .....................................PUSHED IN AND NO LEAKS

E170/175: Verify LH1 Magnetic Level Indicator.

E190/195: Verify LH2 and LH1 Magnetic Level Indicators.

Landing, Taxi and Wing Inspection Lights..........CONDITION


Left Ram Air Inlet ...................................................NO OBSTRUCTION


(Continued)

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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5 c0

1

Air Inlets and Outlets............................................. NO OBSTRUCTION

Wing Tank Water Drain Valve............................... CONDITION AND NO LEAKS

Applicable only to E170/175 airplanes.


Collector Tank Water Drain Valve Door............... SECURED


Air Conditioning Connection Access Door......... CHECK



PROCEDURES


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5c01

INTENTIONALLY BLANK

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


SOPM

-17

55c0

1

BEFORE START CHALLENGE ACTION / RESPONSE PERFORMED BY

Airplane Manuals & Documents.......... ON BOARD ...............RSP Check all the required documents including:

Technical log. AOM. QRH. If applicable, verify if the ECL database version is

compatible with the paper QRH revision. Airworthiness certificate. Weight and balance. Radio station certificate. Nav kit.

Jump Seat Oxy Mask, Regulators and Audio Panel ..................................... CHECK ...............RSP

The RSP must verify the observers masks. Carry out the test as follows:

Set the regulator control knob to 100%. Press and hold the TEST/RESET Button. Verify a short illumination or blink of the flow indicator. Verify audible oxygen flow in the headset or

loudspeakers. Once the mask fully pressurizes the indicator must go

out, showing that the system is leak free. Release the TEST/RESET Button.

ELECTRIC Panel ................................................SET ...............RSP IDG 1 Selector .................................................... AUTO IDG 2 Selector .................................................... AUTO AC BUS TIES Selector ....................................... AUTO GPU Button ........................................................ AS REQUIRED APU GEN Button ................................................ PUSHED IN TRU 1 ................................................................. AUTO TRU ESS ............................................................ AUTO TRU 2 ................................................................. AUTO DC BUS TIES ..................................................... AUTO Battery 1 Selector ............................................... ON Battery 2 Selector ............................................... AUTO


PROCEDURES


SOPM

-17

55 c0

1

CHALLENGE ACTION / RESPONSE PERFORMED BY

COCKPIT LIGHTS Panel ................. AS REQUIRED .............. RSP Adjust MAIN PNL, OVHD PNL and PEDESTAL lights. Push ANNUCIATORS TEST button and verify all associated

lights. Set DOME light as required.

Engine 1 Fire Handle ................................STOWED .............. RSP

FUEL Panel .........................................................SET .............. RSP FUEL XFEED selector as required. DC PUMP selector AUTO. AC PUMP 1 and AC PUMP 2 selectors AUTO.

For ETOPS operation perform the Ejector Fuel Pump Check Valve according to the AOM SUPPLEMENTARY PROCEDURES ETOPS. PASSENGER SIGNS Panel ...............................SET .............. RSP (Answered by LSP)

Emergency lights selector knob ON and verify EMERG LT ON and EMERG LT NOT ARMED appear on the EICAS.

Emergency lights selector knob ARMED. STERILE light as required. Turn NO SMKG ON (NO ELEC DEVICES in some

configurations). Turn FSTN BELTS ON after finishing refueling the airplane.

FIRE EXTINGUISHER Panel ........................CHECK .............. RSP CARGO SMOKE FWD/AFT Buttons PUSHED OUT and no

lights. APU fire extinguishing Button PUSHED OUT and no lights.

APU CONTROL Panel ..................... AS REQUIRED .............. RSP Emergency stop button pushed out and not illuminated.

EXTERNAL LIGHTS Panel.............. AS REQUIRED .............. RSP

Engine 2 Fire Handle ................................STOWED .............. RSP

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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1


HYDRAULIC Panel...............................CHECK/SET ...............RSP

Verify ENG PUMP SHUTOFF 1 and 2 Buttons with no lights and guarded.

Verify PTU Selector to AUTO. Verify the HYDRAULIC SYS 1 and SYS 2 ELEC PUMPs to

AUTO. Verify the HYDRAULIC SYS 3 ELEC PUMP A to OFF. Verify the HYDRAULIC SYS 3 ELEC PUMP B to AUTO.

PRESSURIZATION Panel ..................................SET ...............RSP (Answered by LSP)

CABIN ALT Selector knob STOP. MODE Selector knob AUTO. DUMP Button, no lights and guarded. LFE Selector knob STOP.

WINDSHIELD HEATING button ........... PUSHED IN ...............RSP

ICE PROTECTION Panel ...................................SET ...............RSP

WINDSHIELD, ENGINE 1 and ENGINE 2 Button PUSHED IN;

Mode Selector Knob AUTO; WING Button PUSHED IN; TEST Selector knob OFF.

AIR COND/PNEUMATIC Panel..........................SET ...............RSP

COCKPIT and PAX CABIN temperature control as required. RECIRC, PACK 1, PACK 2, XBLEED, BLEED 1,

APU BLEED and BLEED 2 buttons pushed in.


PROCEDURES


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1


PASSENGER OXYGEN Panel ...........................SET .............. RSP

Mask Deploy selector knob AUTO. MASK DEPLOYED indicator no light.

HGS Combiner (If Applicable) ..........................SET ...LSP & RSP The LSP (and the RSP dual installation) must move the combiner to the operating position detent, remove the cover, verify that the ALIGN HUD message is not displayed and adjust the brightness.

Oxygen Masks & Regulators ........... CHECK/100% ...LSP & RSP (Answered by LSP/RSP)

Check masks for supply of oxygen and for microphone functionality.

The MFD STATUS page must be checked and the available oxygen supply and pressure must be adequate for use.

Carry out the test as follows: Set the regulator control knob to 100%. Press and hold the TEST/RESET Button. Verify a short illumination or blink of the flow indicator. Verify audible oxygen flow in the headset or

loudspeakers. Once the mask fully pressurizes the indicator must go

out, showing that the system is leak free. Release the TEST/RESET Button.

Glareshield Lights Control Panel .. AS REQUIRED ...LSP & RSP

DISPLAY CONTROLLER Panel.........................SET ...LSP & RSP

Set BARO SET knob to actual pressure. Push HSI button for Full Compass, ARC or MAP. Select the FMS as the primary NAV source (if raw data

information is intended, use preview mode or Bearing pointers).

For HGS LVTO operations, set V/L. BRG circle () to OFF, VOR1, ADF1 or FMS1 as required. BRG diamond () to OFF, VOR2, ADF2 or FMS2 as

required. REVERSIONARY PANEL...................................SET ...LSP & RSP

Displays selector knob in AUTO. Sensors selectors (ADS/IRS) normal configuration.

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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1


Flight Instruments ..................................SET/XCKD ...LSP & RSP (Answered by LSP)

Verify: Airspeed tapes not showing speed. Set altimeter setting and cross check it with the field

elevation. EADIs leveled and flag-free. Initial assigned altitude on the ALT SEL. Altitude tape indications cross-check. Both VSIs showing zero. EHSIs with the courses selected according to the

intended departure procedure and NAV source selected. For LVTO using the HGS set the CDI to the runway

course. EHSIs and magnetic compass flag free and showing the

same magnetic heading. Heading bug set according to the proposed departure

procedure. Check IESS and adjust the altimeter setting. Weather set on PFD and/or MFDs MAP page as required. It is recommended that PNF sets the Terrain on MFD up

to MSA. Set the MFDs MAP page menu as required. TCAS should be always displayed on both MFDs.

STATUS Page............................................... CHECK ...LSP & RSP

Verify on the status page ENG OIL LEVEL and BRAKES EMER ACCU pressure. LSP should select FLIGHT CONTROL synoptic page. RSP should remain on STATUS synoptic page.

AUTOBRAKE (If Applicable)............................ RTO ............... LSP

GND PROX TERR INHIB Button ................. CHECK ............... LSP

Verify button pushed out and no striped white bar illuminated.

EICAS............................................................CHECK ............... LSP

Check EICAS messages to ensure agreement with airplane status.


PROCEDURES


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Clock ...................................................................SET .............. RSP

Select GPS on the GPS/INT/SET Selector. If the clock displays dashes (-- -- --), adjust the clock INT position.

GND PROX G/S INHIB Button .....................CHECK .............. RSP

Verify no striped white bar illuminated.

LG WRN INHIB Button.................................CHECK .............. RSP

Verify no striped white bar illuminated.

FLIGHT CONTROLS MODE Panel ..............CHECK ...............LSP

Verify ELEVATORS, RUDDER and SPOILER Buttons guarded and no striped white bar illuminated.

SHAKER 1 and 2 CUTOUT Buttons............CHECK ...............LSP

Verify the SHAKER 1 CUTOUT and SHAKER 2 CUTOUT buttons pushed out and no striped white bars illuminated.

IGNITION Selector Knobs ............................. AUTO ...............LSP

EICAS FULL..................................................CHECK ...............LSP

Verify the EICAS Full button in the desired position.

Speed Brake Lever ....................................CLOSED ...............LSP

Thrust Levers ................................................... IDLE ...............LSP (Answered by LSP)

GND PROX FLAP OVRD..............................CHECK .............. RSP

Verify button pushed out, guarded and no striped white bar illuminated.

AUDIO CONTROL Panel................. AS REQUIRED ...LSP & RSP

Select the microphone and audio reception buttons as required and adjust the volume levels. To avoid background noise do not set the SPKR volume higher than 55.

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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5 c0

1


TRIM Panel ................................................... CHECK ...LSP & RSP

Verify that ROLL, YAW and PITCH (Captain, First Officer and Backup) trims are operating properly both ways and check that Position Indication on EICAS changes accordingly. Verify systems 3 second protection working properly. Adjust YAW and ROLL trims to the neutral position and PITCH trim to the green band.

NOTE: The PITCH TRIM Backup Switch may be checked once a day only, by flight crew or maintenance personnel, at the operators discretion.

Pre-Mod. LOAD 21.2

NOTE: The SPOILER FAULT EICAS message may be displayed during the ROLL trim check and removed when all hydraulic systems are pressurized.

Flight Control DISCONNECT Handles ....... CHECK ...............RSP

Alternate Gear Extension Compartment........................ CHECK ...............RSP

Verify the alternate gear extension lever is fully down and the electrical override switch is in the NORMAL position.

MCDU..................................................................SET ...LSP & RSP (Answered by LSP)

On PROGRESS page, activate the FMS AUTOTUNE by deleting the NAV1 frequency for FMS1 and NAV2 frequency for FMS2 displayed on LSK 5L and 5R, respectively. In case of FMS AUTOTUNE OFF takeoff is selected in order to hard-tune a specific VOR, return to FMS AUTOTUNE ON as soon as the VOR frequency is no longer necessary.

Select NAV IDENT page and check its contents; Select POSITION INIT page and load the present position; It is recommended that PF sets the route in the FMS

according to the flight plan and both pilots check course, distance, time, altitude on each waypoint and LFE in the EICAS according to the destination landing field elevation;


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It is recommended that PF sets on PERF INIT page 1/1 the CLIMB, CRUISE, DESCENT and DEP/APPROACH speed schedule, select page 2/3 and check/set its contents, on page 3/3 set all fields with the available data;

If applicable select MENU HGS page and set the COMBINER MODE;

If applicable (ETOPS configuration), select ETOPS or non ETOPS flight on MENU MISC MENU OPR CONFIG Page;

If applicable (AUTOLAND configuration), select enable or disable on MENU MISC MENU OPR CONFIG Page.

Pre-Mod. LOAD 21.2

Select FLIGHT SUMMARY page and reset fuel used. --------------------------SHORTLY BEFORE STARTUP-------------------------


FUEL QTY .....................................................CHECK ...LSP & RSP (Answered by LSP & RSP)

MCDU ..................................................................SET ...LSP & RSP (Answered by LSP)

Insert the intended SID or the departing runway on the FMS and both pilots must check the accuracy of the procedure retrieved by FMS database. Select LNAV if intended to takeoff with lateral mode armed on ground.

For HGS operation if the previous action is not possible select MENU HGS page and check the Runway Length and Elevation.

Set the Performance initialization data on PERF INIT page. If it is already available enter the zero fuel weight and press CONFIRM INIT prompt on page 3/3. If performance is confirmed and taking off with vertical mode armed on ground is desired, select VNAV.

Select T/O DATASET MENU page on the MCDU and set the data below: Thrust rate mode (TO-1, TO-2 or TO-3). TO TEMP (__C). ATTCS ON or OFF. REF ECS (ON or OFF). REF A/I (OFF, ENG or ALL). FLEX T/O (ON or OFF).

STANDARD OPERATING

PROCEDURES

NORMAL PROCEDURES


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5c01

R1

13O 212O

14O FS

4O

1OO

EM17

0AO

M98

0001

.DG

N

FLEX TEMP (__C). Press ENTER Prompt to confirm the settings.

Select TAKEOFF page and set all data in accordance with the runway analysis and airplane configuration for takeoff.

At pilots discretion, select the LANDING page on the MCDU and set the landing speeds for the takeoff weight in case of immediate return is necessary.

Select RADIO page 1/2 and insert assigned transponder code and for LVTO using HGS set the ILS frequency for the departing runway on both NAV windows.

VSPEED READOUTS AND BUGS Four speeds are displayed prior to takeoff:

V1 .................1 ................... MAGENTA VR.................R .................. CYAN V2 .................2 ................... WHITE VFS...............FS ............... GREEN


SPEED Selector Knob.......................................SET ............... LSP

At pilots discretion set the SPEED Selector knob to FMS or MANUAL.

IF FMS, set the departure speed on the DEP/APP speeds page on the FMS. If MANUAL, set the speed VFS on the speed window. In case of Noise Abatement procedure set V2+10.

TOGA Button.................................................PRESS ............... LSP

Verify if the pitch cross bar on PFD agrees with the pitch indicated on PERF INIT page on MCDU.


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TRIM Panel............................... __SET/ZERO/ZERO .............. RSP (Answered by LSP)

Set the PITCH trim according to load sheet and verify YAW and ROLL trims to the neutral position.

Doors and Windows ..................................CLOSED ...LSP & RSP (Answered by LSP/RSP)

Both pilots must verify that their respective cockpit window is closed and the RSP should select MFD status page to check all airplane doors closed indications. It is recommended to assure that escape slides are armed. Check the cockpit door securely closed.

Takeoff Briefing..................................COMPLETED ...LSP & RSP

The takeoff briefing should be performed by the PF and the left seat pilot must state the Reject Takeoff procedures.

The briefing should describe the departure procedures, taxi out routes, power reductions, weather, terrain/MSA, noise abatement procedures, low visibility procedures, inoperative airplane components, runway in use/condition, return alternate airports, NOTAMs and any required operational procedures that differ from the normal procedures. It is recommended to perform the takeoff briefing before engine start.

Red beacon.......................................................... ON .............. RSP (Answered by LSP)

Electric Hydraulic Pump 3A............................... ON .............. RSP

Ground Equipment ......................... AS REQUIRED ...............LSP

If performing a push back assure that the ground equipment not used for this procedure is removed.

STANDARD OPERATING

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Emergency/Parking Brake..............AS REQUIRED ............... LSP (Answered by LSP)

Verify if the Emergency/Parking brake is set in accordance with the engine start procedures.

Steering Disengage Switch .........................PRESS .............. LSP

Verify the STEER OFF message displayed on the EICAS.


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ENGINE START

ENGINE START PROCEDURE CHALLENGE ACTION

Associated START/STOP Selector............................ START, then RUN

Hold the START/STOP Selector at START position for at least 2 seconds.

NOTE: During ground starts only, the transition of the cockpit START/STOP switch from STOP to START must be less than 30 seconds or the FADEC will prevent an engine start until the switch is cycled through STOP.

Engine Parameters ..................................................... MONITOR

Repeat the sequence for the other engine.

ABNORMAL ENGINE START INDICATIONS

Although FADEC provides automatic over-temperature protection and will automatically abort the start in the event of a hot start, hot restart or hung start, the engine start must be manually aborted when:

No positive oil pressure indication within 10 seconds after N2 speed starts to increase.

During engine start with tailwind, if a positive increase of N1 is not indicated before starter cutout (50% N2). In this case the airplane should be repositioned prior to engine start to minimize tailwind effects.

For E170/175, no ITT indication within 30 seconds after fuel is applied.

For E190/195, no ITT indication within 1 minute after fuel is applied (15 seconds after fuel is re-applied).

ITT exceeds start limit (815C - Hot Start for E170/175 and 740C Hot Start for E190/195).

If oil pressure stabilizes below the engine limits. N1 and/or N2 failing to accelerate to stable idle speed (Hung

Start). An intermittent electrical pneumatic or starter malfunction

occurs before the starter disengagement.

STANDARD OPERATING

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NOTE: In case an automatic abort occurs or engine start is manually aborted due to abnormal engine indications, its cause must be investigated and corrected before further attempts to start the engines.


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INTENTIONALLY BLANK

STANDARD OPERATING

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NORMAL PROCEDURES


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AFTER START CHALLENGE ACTION / RESPONSE PERFORMED BY

Ground Equipment .................................REMOVED ............... LSP (Answered by LSP)

Captain must be sure that the emergency/parking brake is set, nose gear/RAT pins and ground equipment have been removed.

N1 Target ......................................................CHECK ...............RSP

The N1 target indication on the EICAS must be equivalent to the N1 target indication available via performance calculation. The difference between N1 given by FADEC (indicated on EICAS) and the computed value is zero or this difference is positive and lower than or equal to 0.5%.

Transponder.....................................AS REQUIRED ...............RSP

RSP selects the transponder to TA/RA or in accordance with local requirements.

SLAT/FLAP.....................................................SET__ ...............RSP (Answered by LSP)

Adjust SLAT/FLAP to a setting consistent with the intended takeoff configuration and performance. If the SLAT/FLAP lever setting is different from the input made on TAKEOFF page 2/3 of the FMS the aural message NO TAKEOFF FLAP will sound during the takeoff configuration check.

APU ...................................................AS REQUIRED ...............RSP

Set the APU ON or OFF according to the electrical and pressurization systems or for ETOPS operation. The APU usage shall be defined for a specific operation in order to minimize the overall costs. APU shutting down can only be performed after confirmation of the power transfer through the Electrical Synoptic page or wait 30 seconds after %N2 stabilizes.


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Flight Controls .............................................CHECK ...... LSP/RSP (Answered by LSP)

The LSP should press the STEERING DISENGAGE SWITCH, check the control column and rudder pedals. The RSP should follow the LSP during rudder check. Flight controls should be checked for freedom of movement in a smooth and continuous manner. A full green box indication on the synoptic page is not a requirement for a successful check.

LSP selects MFD Flight Control synoptic; Elevator - full up, neutral, full down and neutral; Aileron - full left, neutral, full right and neutral; Rudder - full left, neutral, full right and neutral; The LSP should press the steering handle to engage the

STEERING and select MAP on the MFD prior to start the taxi.

NOTE: A FLT CTRL TEST IN PROG status message is displayed to inform the pilot that the Hydraulic P-BIT is in progress. The Hydraulic P-BIT starts when all the three hydraulic systems are pressurized and takes about one minute to complete. Performing the flight controls check while the Hydraulic P-BIT is running may interrupt the P-BIT.

STANDARD OPERATING

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NORMAL PROCEDURES


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BEFORE TAKEOFF The Before Takeoff Procedures and checklist must be performed when cleared to line up on the runway. Use all available information such as heading and FMS course indication (PFD), lateral profile (MFD) and departure runway (MCDU) to ensure the airplane is at the assigned runway for takeoff.

CHALLENGE ACTION/RESPONSE PERFORMED BY

Cabin Crew.................................................. ADVISE ...............RSP

After receiving Cabin OK from the Purser, RSP notifies via PA the cabin crew: Cabin Crew prepare for take-off.

Taxi Lights..........................................................OFF ...............RSP

RSP turns off the taxi lights. Taxi (side) may be used to assist takeoff from takeoff to 10000 ft AFE at pilots discretion.

Landing Lights................

Rev. 16 del SOPM-1755-001

Documents

Transcript of Rev. 16 del SOPM-1755-001