-
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
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HIGHLIGHTS OF CHANGE
0-HOC REVISION 16 Page 1
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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 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.
2-17 7 Editorial correction.
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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Block Page Change Description
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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Block Page Change Description
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 27 Editorial correction.
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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Block Page Change Description
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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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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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
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1-05 * 1 ...................REVISION 16 2
...................REVISION 12 2-00 * 1 ...................REVISION
16 2 ...................REVISION 12 2-07 1
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2-09 1 ...................REVISION 12 2 ...................REVISION
13 2-13 1 ...................REVISION 12 2
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3................... REVISION 15 * 4................... REVISION
16 5................... REVISION 15 6................... REVISION
15 2-15 1................... REVISION 14 2...................
REVISION 14 3................... REVISION 15 4...................
REVISION 15 5................... REVISION 15 6...................
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REVISION 14 9................... REVISION 14 10.................
REVISION 15 11................. REVISION 15 12.................
REVISION 15 2-17 1................... REVISION 10
2................... REVISION 10 3................... REVISION 12 *
4................... REVISION 16 5................... REVISION 13
6................... REVISION 12 * 7................... REVISION 16
8................... REVISION 12 9................... REVISION 15
10................. REVISION 15 11................. REVISION 11
12................. REVISION 15 13................. REVISION 15
14................. REVISION 15 2-25 1................... REVISION
13 2................... REVISION 10 2-29 1...................
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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
2................... REVISION 10 2-60 1...................
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16 * 5................... REVISION 16 * 6...................
REVISION 16 2-65 1................... REVISION 15 *
2................... REVISION 16 2-67 1................... REVISION
14 2................... REVISION 12 2-70 1...................
REVISION 14 2................... REVISION 12 2-73
1................... REVISION 12 2................... REVISION 12
2-75 * 1................... REVISION 16 * 2...................
REVISION 16 3................... REVISION 12 4...................
REVISION 12 5................... REVISION 12 6...................
REVISION 12 7................... REVISION 12 8...................
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13 2 ...................REVISION 12 2-83 1
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3-00 1 ...................REVISION 10 2 ...................REVISION
10 * 3 ...................REVISION 16 * 4
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6 ...................REVISION 16 * 7 ...................REVISION 16
8 ...................REVISION 10 3-05-01 1
...................REVISION 15 2 ...................REVISION 11 3
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3-05-05 1 ...................REVISION 10 2
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5................... REVISION 11 6................... REVISION
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10 3-05-10 1................... REVISION 10 2...................
REVISION 10 3................... REVISION 10 4...................
REVISION 10 5................... REVISION 10 6...................
REVISION 15 * 7................... REVISION 16 8...................
REVISION 10 9................... REVISION 10 10.................
REVISION 10 11................. REVISION 14 12.................
REVISION 10 13................. REVISION 10 14.................
REVISION 13 15................. REVISION 10 16.................
REVISION 10 3-10 1................... REVISION 12
2................... REVISION 15 3................... REVISION 13
4................... REVISION 11 5................... REVISION 13
6................... REVISION 15 7................... REVISION 15
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5................... REVISION 12 6................... REVISION 11 *
7................... REVISION 16 8................... REVISION 10
3-15-05 1................... REVISION 14 2...................
REVISION 14 2A ................ REVISION 13 2B ................
REVISION 13 3................... REVISION 10 * 4...................
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REVISION 15 3-15-10 1................... REVISION 10
2................... REVISION 11 * 3................... REVISION 16
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6................... REVISION 11
7................... REVISION 13 8................... REVISION
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15 11................. REVISION 15 12................. REVISION 15
3-20 1................... REVISION 13 * 2...................
REVISION 16 3................... REVISION 10 4...................
REVISION 15 5................... REVISION 11 6...................
REVISION 10 3-25 1................... REVISION 10
2................... REVISION 10 3................... REVISION 10
4................... REVISION 10 5................... REVISION 10
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10................. REVISION 15 11................. REVISION 15 *
12................. REVISION 16 12A .............. REVISION 15 12B
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16................. REVISION 10 17................. REVISION 14
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20................. REVISION 15 * 21................. REVISION 16 *
22................. REVISION 16 * 23................. REVISION
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3 ...................REVISION 16 * 4 ...................REVISION 16
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16 3-35-01 1 ...................REVISION 11 * 2
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4 ...................REVISION 16 * 5 ...................REVISION 16
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16................. REVISION 16 * 17................. REVISION 16 *
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REVISION 16 * 2................... REVISION 16 *
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16 * 6C ................ REVISION 16 * 6D ................ REVISION
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20................. REVISION 11 21................. REVISION 11
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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 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
-
STANDARD OPERATING
PROCEDURES
NORMAL PROCEDURES
2-07 REVISION 10 Page 3 S
OPM
-17
55
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
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-07 Page 4 REVISION 10 SO
PM-17
55
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
-
STANDARD OPERATING
PROCEDURES
NORMAL PROCEDURES
2-09 REVISION 12 Page 1
SO
PM
-175
5
INTERNAL SAFETY INSPECTION
The Internal Safety Inspection procedures must be performed
before the Power Up on a particular airplane.
CHALLENGE ACTION PERFORMED BY
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
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-09 Page 2 REVISION 13
SO
PM
-175
5
CHALLENGE ACTION PERFORMED BY
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
2-13 REVISION 12 Page 1
SO
PM
-175
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.
CHALLENGE ACTION PERFORMED BY
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.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-13 Page 2 REVISION 15
SO
PM
-175
5
CHALLENGE ACTION PERFORMED BY
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
2-13 REVISION 15 Page 3
SO
PM
-175
5
CHALLENGE ACTION PERFORMED BY
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.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-13 Page 4 REVISION 16
SO
PM
-175
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
2-13 REVISION 15 Page 5
SO
PM
-175
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.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-13 Page 6 REVISION 15
SO
PM
-175
5
INTENTIONALLY BLANK
-
STANDARD OPERATING
PROCEDURES
NORMAL PROCEDURES
2-15 REVISION 14 Page 1
SO
PM
-175
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:
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-15 Page 2 REVISION 14
SO
PM
-175
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
2-15 REVISION 15 Page 3
SO
PM
-175
5 c0
1
RAT Safety Lock
Pin.............................................. REMOVED
FWD Service Door
................................................. CHECK
If not in use, visibly secured.
Oxygen Discharge Indicator.................................
GREEN DISC
FWD Cargo
Door.................................................... CHECK
If not in use, visibly secured.
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
Clean and undamaged.
Right Ram Air Inlet
................................................ NO OBSTRUCTION
No obstruction or damage.
Air Inlets and
Outlets............................................. NO
OBSTRUCTION
No obstruction or damage.
Collector Tank Water Drain Valve Door............... SECURED
If not in use, visibly secured.
Wing Tank Water Drain Valve...............................
CONDITION AND NO LEAKS
Applicable only to E170/175 airplanes.
Clean and undamaged.
(Continued)
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-15 Page 4 REVISION 15
SO
PM
-175
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
2-15 REVISION 15 Page 5
SO
PM
-175
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
Clean and undamaged.
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)
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-15 Page 6 REVISION 15
SO
PM
-175
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
If not in use, visibly secured.
Drain
Mast...............................................................CONDITION
No obstruction or damage.
AFT Cargo Door
.....................................................CHECK
If not in use, visibly secured.
AFT Service
Door...................................................CHECK
If not in use, visibly secured.
Lower AFT Antennas/AFT Drain Mast .................CONDITION
Undamaged.
Battery Air Outlet
...................................................NO
OBSTRUCTION
No obstruction or damage.
(Continued)
-
STANDARD OPERATING
PROCEDURES
NORMAL PROCEDURES
2-15 REVISION 15 Page 7
SO
PM
-175
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
If not in use, visibly secured.
Overboard
Vent...................................................... NO
OBSTRUCTION
No obstruction or damage.
Pressurization Static Port.....................................
NO OBSTRUCTION
No obstruction or damage.
Potable Water Service Panel ................................
SECURED
If not in use, visibly secured.
AFT PAX Door
........................................................ CHECK
If not in use, visibly secured.
Lower AFT Antennas.............................................
CONDITION
Undamaged.
(Continued)
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-15 Page 8 REVISION 14
SO
PM
-175
5 c0
1
Access Doors and Panels
.....................................SECURED
If not in use, visibly 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
2-15 REVISION 14 Page 9
SO
PM
-175
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)
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-15 Page 10 REVISION 15
SO
PM
-175
5 c0
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
Clean and undamaged.
Left Ram Air Inlet
...................................................NO
OBSTRUCTION
No obstruction or damage.
(Continued)
-
STANDARD OPERATING
PROCEDURES
NORMAL PROCEDURES
2-15 REVISION 15 Page 11
SO
PM
-175
5 c0
1
Air Inlets and
Outlets............................................. NO
OBSTRUCTION
Wing Tank Water Drain Valve...............................
CONDITION AND NO LEAKS
Applicable only to E170/175 airplanes.
Clean and undamaged.
Collector Tank Water Drain Valve Door............... SECURED
If not in use, visibly secured.
Air Conditioning Connection Access Door......... CHECK
No obstruction or damage.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-15 Page 12 REVISION 15
SO
PM
-175
5c01
INTENTIONALLY BLANK
-
STANDARD OPERATING
PROCEDURES
NORMAL PROCEDURES
2-17 REVISION 10 Page 1
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
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NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-17 Page 2 REVISION 10
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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
2-17 REVISION 12 Page 3
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CHALLENGE ACTION / RESPONSE PERFORMED BY
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.
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NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-17 Page 4 REVISION 16
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CHALLENGE ACTION / RESPONSE PERFORMED BY
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
2-17 REVISION 13 Page 5
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CHALLENGE ACTION / RESPONSE PERFORMED BY
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.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-17 Page 6 REVISION 12
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CHALLENGE ACTION / RESPONSE PERFORMED BY
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
2-17 REVISION 16 Page 7
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CHALLENGE ACTION / RESPONSE PERFORMED BY
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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NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-17 Page 8 REVISION 12
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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-------------------------
CHALLENGE ACTION / RESPONSE PERFORMED BY
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
2-17 REVISION 15 Page 9
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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
CHALLENGE ACTION / RESPONSE PERFORMED BY
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.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-17 Page 10 REVISION 15
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CHALLENGE ACTION / RESPONSE PERFORMED BY
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
PROCEDURES
NORMAL PROCEDURES
2-17 REVISION 11 Page 11
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CHALLENGE ACTION / RESPONSE PERFORMED BY
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.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-17 Page 12 REVISION 15
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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
PROCEDURES
NORMAL PROCEDURES
2-17 REVISION 15 Page 13
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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.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-17 Page 14 REVISION 15
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INTENTIONALLY BLANK
-
STANDARD OPERATING
PROCEDURES
NORMAL PROCEDURES
2-25 REVISION 13 Page 1
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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.
-
NORMAL PROCEDURES STANDARD OPERATING
PROCEDURES
2-25 Page 2 REVISION 10
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CHALLENGE ACTION / RESPONSE PERFORMED BY
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
PROCEDURES
NORMAL PROCEDURES
2-29 REVISION 12 Page 1
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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................