Embraer ERJ-190 Series Installation guide

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 1
TRAINING MANUAL
Embraer ERJ-190 Series (GE CF34)
B1.1 and B2 (-sub) categories
AIRPLANE GENERAL
(ATA 05 –ATA12)
Level 1

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 2
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Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 3
TABLE OF CONTENTS
DOCUMENTATION .......................................................................................6
INTRODUCTION........................................................................................6
DOCUMENTATION ACCESS ....................................................................8
AMM PART I - SYSTEM DESCRIPTION SYSTEM (SDS)........................10
AMM PART II - MAINTENANCE PRACTICES AND PROCEDURES (MPP)
.................................................................................................................12
MAINTENANCE PRACTICES AND PROCEDURES (MPP).....................14
AIRCRAFT MAINTENANCE TASK ORIENTED SUPPORT SYSTEM
(AMTOSS)................................................................................................14
FUNCTION CODES.................................................................................14
AIRCRAFT MAINTENANCE MANUAL.....................................................16
FAULT ISOLATION MANUAL (FIM).........................................................18
RAMP MAINTENANCE MANUAL (RMM).................................................20
COMPONENT MAINTENANCE MANUAL (CMM)....................................20
WIRING MANUAL (WM)...........................................................................22
AIRCRAFT ILLUSTRATED PARTS CATALOGUE (AIPC) .......................24
STRUCTURAL REPAIR MANUAL PART 1 (SRM 1)................................26
STRUCTURAL REPAIR MANUAL PART 2 (SRM 2)................................28
OTHER DOCUMENTATION ....................................................................32
ATA 05 TIME LIMITS AND MAINTENANCE CHECKS................................52
INTRODUCTION......................................................................................52
SCHEDULED MAINTENANCE CHECKS.................................................52
UNSCHEDULED MAINTENANCE CHECKS............................................55
ATA 06 DIMENSIONS AND AREAS............................................................56
INTRODUCTION......................................................................................56
DESCRIPTION.........................................................................................58
ATA 07 AIRCRAFT JACKING......................................................................76
INTRODUCTION......................................................................................76
COMPLETE AIRCRAFT JACKING...........................................................78
BEFORE COMPLETE AIRCRAFT JACKING...........................................80
JACKING POINTS LOCATION.................................................................82
NOSE AND MAIN GEAR JACKING POINTS ...........................................84
ATA 08 LEVELING AND WEIGHING...........................................................86
INTRODUCTION......................................................................................86
WEIGHING THE AIRCRAFT....................................................................88
AIRCRAFT LEVELING.............................................................................90
ATA 09 TOWING AND TAXIING..................................................................92
INTRODUCTION......................................................................................92
TOWING WITH TOWBAR........................................................................94
TOWING OPERATION.............................................................................96
TOWBARLESS TOWING.........................................................................98
TAXIING REGULATIONS.......................................................................100
ATA 10 PARKING AND MOORING ...........................................................102
INTRODUCTION....................................................................................102
MINIMUM DISTANCES..........................................................................104
NORMAL AIRCRAFT PARKING.............................................................106
LONG TERM PARKING .........................................................................110
MOORING THE AIRCRAFT ...................................................................112
ATA 11 PLACARDS AND MARKINGS.......................................................114
INTRODUCTION....................................................................................114
ATA 12 SERVICING...................................................................................116
INTRODUCTION....................................................................................116
REPLENISHING.....................................................................................118
FUEL TANK SERVICING .......................................................................120
HYDRAULIC AND LANDING GEAR SYSTEM SERVICING...................122
ENGINE AND AUXILIARY POWER UNIT SERVICING..........................124
SERVICING WATER/WASTE.................................................................126
GASEOUS SERVICING .........................................................................128
SCHEDULED SERVICING.....................................................................130
UNSCHEDULED SERVICING................................................................132

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 4
TABLE OF FIGURES
DOCUMENTATION.......................................................................................7
DOCUMENTATION ACCESS .......................................................................9
AMM PART I –SDS EXAMPLE ..................................................................11
AMM PART II –MPP EXAMPLE.................................................................13
AMTOSS CODES AND SUBDIVISION .......................................................15
AIRCRAFT MAINTENANCE MANUAL.......................................................17
FAULT ISOLATION MANUAL USED AWITH AIRCRAFT CMC (CENTRAL
MAINTENANCE COMPUTER)....................................................................19
RMM AND CMM..........................................................................................21
WIRING MANUAL AND SYSTEM SCHEMATIC MANUAL.........................23
AIRCRAFT ILLUSTRATED PARTS CATALOGUE (AIPC).........................25
SRM 1..........................................................................................................27
SRM 2, DAMAGE REPORT FORM EXAMPLE...........................................29
SRM 2 USAGE............................................................................................31
EXAMPLE OF ARM AND ITEM...................................................................33
EXAMPLE OF NDT MANUAL.....................................................................35
EMB 190 AND 195 ......................................................................................37
FUSELAGE AND AIR CONDITIONING PACKS .........................................39
COCKPIT AND CABIN SECTION...............................................................41
SEAT CAPACITY........................................................................................43
LANDING GEAR .........................................................................................45
TURNING RADIUS......................................................................................47
CF34-10E HIGH BYPASS TURBOFAN ENGINES......................................49
AIRCRAFT DATA........................................................................................51
CHAPTER 05...............................................................................................53
HORIZONTAL MEASUREMENTS ..............................................................57
AIRCRAFT MEASUREMENTS EMB 190....................................................59
AIRCRAFT MEASUREMENTS EMB 195....................................................61
AIRCRAFT DOORS.....................................................................................63
FUSELAGE STATIONS ..............................................................................65
WING STATIONS........................................................................................66
HORIZONTAL STABILIZER STATIONS.....................................................67
VERTICAL STABILIZER STATIONS ..........................................................68
POWERPLANT AND PYLON STATIONS...................................................69
MAJOR AIRCRAFT ZONES........................................................................71
SUB-ZONES................................................................................................73
ACCESS PANELS IDENTIFICATION .........................................................75
LANDING GEAR JACKING , JACKING POINTS........................................77
COMPLETE AIRCRAFT JACKING .............................................................79
CG POSITION..............................................................................................81
JACKING POINTS LOCATION ...................................................................83
MAIN AND NOSE GEAR JACKING POINTS..............................................85
WEIGHING PROCEDURES.........................................................................87
WEIGHING THE AIRCRAFT, WEIGHING KIT AND JACKS OR GROUND
SCALES ......................................................................................................89
AIRCRAFT LEVELING................................................................................91
CHAPTER 9 TOWING AND TAXIING .........................................................93
GROUND TOWING REQUIREMENTS (EXAMPLE)....................................95
BEFORE TOWING.......................................................................................97
TOWBARLESS USING GSE 200 OR GSE 422...........................................99
TAXI REGULATIONS................................................................................101
TYPES OF PARKING................................................................................103
MINIMUM DISTANCES .............................................................................105
NORMAL AIRCRAFT PARKING...............................................................107
NORMAL AICRAFT PARKING IN COLD WEATHER CONDITIONS........109
LONG TERM PARKING ............................................................................111
MOORING THE AIRCRAFT ......................................................................113
EXTERIOR SCREED –PRINTED MARKINGS .........................................115
CHAPTER 12.............................................................................................117
REPLENISHING ........................................................................................119
FUEL TANK SERVICING ..........................................................................121
HYDRAULIC AND LANDING GEAR SYSTEM SERVICING.....................123
ENGINE AND APU SERVICING................................................................125
WATER WASTE SERVICING....................................................................127
GASEOUS SERVICING.............................................................................129
SCHEDULED SERVICING ........................................................................131
UNSCHEDULED SERVICING ...................................................................133

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 5
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Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 6
DOCUMENTATION
INTRODUCTION
All maintenance checks, inspections, repairs, replacements and
troubleshooting must be performed in accordance with valid documentation.
The related documentation necessary to maintain the aircraft includes:

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 7
DOCUMENTATION

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 8
DOCUMENTATION ACCESS
Access to the available Aircraft Documentation is given in different ways.
Generally the data can be available in digital or hardcopy format.
Digital data can be available via CD/DVD, Server Access or through the
Internet.
Internet access is given via the FlyEmbraer Technical Publications tool
under: www.flyembraer.com
FlyEmbraer offers a user-friendly interface with easy navigation, a search
tool, filtering capabilities and features for downloading, updating and
distributing.

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 9
DOCUMENTATION ACCESS

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 10
AMM PART I - SYSTEM DESCRIPTION SYSTEM (SDS)
Purpose:
Detailed description and explanation of the location, configuration,
function, operation and control of the complete system (chapter), and
its subsystems.
Enable the operator / mechanic / trainee to understand the three
levels of overall construction, operation and function to the extent
necessary to perform adequate maintenance and fault isolation of the
system.
Available links: FIM, AIPC, ITEM, MPP, SM, SSM, WM.
Arrangement:

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 11
AMM PART I –SDS EXAMPLE

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 12
AMM PART II - MAINTENANCE PRACTICES AND PROCEDURES (MPP)
Purpose:
Contains all necessary maintenance practice and procedure data to
enable the mechanic to maintain the aircraft properly, at the level of
line, hangar / service centre maintenance actions, or line ramp level.
Available links:
WM, AIPC, CMM, SWPM, CPM, FIM, MPP, SDS, SM, SRM, SSM, ITEM.
Arrangement:

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 13
AMM PART II –MPP EXAMPLE

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 14
MAINTENANCE PRACTICES AND PROCEDURES (MPP)
The AMM provides sufficient information to enable a mechanic to service
troubleshoot, test, adjust and repair systems and to remove and install any
component on the line or in the hangar. This AMM is written in accordance
with the ATA 100 Revision 28 recommendations. Revision
28 has, among other things, these two recommendations
Simplified English
Prepared for AMTOSS (Aircraft Maintenance Task Oriented Support
System)
AIRCRAFT MAINTENANCE TASK ORIENTED SUPPORT SYSTEM
(AMTOSS)
AMTOSS eases maintenance procedures by giving the specific procedure
(task) and the primary steps of procedures (sub tasks) a different number
identification code.
The identification code numbers have a minimum of five elements and a
maximum of seven. The elements are:
An extension to the three ATA 100 Chapter, section and subject
numbering.
After the first three elements a function code will follow. This code
identifies the type of work that has to be done.
The fifth element shows the task or sub task identification number.
This number is applicable to the task/sub task only and is counting the
sequence of the task or sub task. Numbers 801 thru 999 are for tasks
and 001 thru 800 for sub tasks.
The sixth element identifies the differences in configuration and the
related procedures and techniques.
Tasks/sub tasks that are special to the operator, or which are written
by sub contractors are identified in the seventh element.
FUNCTION CODES
The function codes used in AMTOSS are from 000 thru 900. Each code
represents the following function:
000 Removal
100 Cleaning
200 Inspection/Check
300 Repair
400 Installation
500 Material Handling
600 Servicing, preserving, lubrication
700 Testing
800 Miscellaneous,e.g.rigging, fault isolation
900 Change - Removal and installation
Each of the codes represents the task. The codes are subdivided to identify
the tasks or sub tasks following. The page below shows the application of the
function codes 400.
Further information is found in the AMM Introduction section.

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 15
AMTOSS CODES AND SUBDIVISION

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 16
AIRCRAFT MAINTENANCE MANUAL
Division of Subject Matter:
The first section of the AMM is the “Introduction”.
This section provides an introduction to the manual and instructions how to
use the manual correctly. It is strongly recommended to read this section of
the manual.
The introduction section also includes a list of the chapters that are included
in the manual.
Each chapter has the following items filed at the front:
Effectivity Code Cross Reference List
Highlights page(s) for each revision
List of Effective Pages
List of Effective Temporary Revisions
Service Bulletins
Table of Content
Effectivity:
Effectivity Codes are used in the AMM to allow many operators with different
configuration aircraft to correctly apply the manual to their aircraft. The
effectivity is shown in the lower left hand corner of each page in the AMM.
The following are the effectivities used:
MASTER
ALL OPERATORS
An operators prefix e.g. “LX” (Swiss)
An “E” Code (E + a number, e.g. E26-018)
If a chapter has one or more pages with an E code, there will be a green
“Effectivity code cross reference list” in the beginning of the chapter. This list
identifies the aircraft serial numbers that are affected by the E-code.
An Effectivity box may have more information, e.g. “Collins”, to point out an
item that differs in configuration.
MASTER:
Always means a “master” manual. It is possible for an operator to have a
master manual.
ALL:
“All” is always shown together with an operator prefix or “ALL OPERATORS”
in the box. Example:
EFFECTIVITY: ALL LX
In this case, it means that the page applies to all LX aircraft. EFFECTIVITY:
ALL OPERATORS
This page applies to all aircraft. E Codes:
The E code is shown together with MASTER or an operator prefix. Example:
EFFECTIVITY: E26-018 MASTER
If a chapter has one or more pages with an E code, there will be a green
“Effectivity code cross reference list” in the beginning of the chapter. This list
identifies the aircraft serial numbers that are affected by the E code.

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 17
AIRCRAFT MAINTENANCE MANUAL

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 18
FAULT ISOLATION MANUAL (FIM)
Purpose:
Provides summarized information and procedures to isolate and
repair faults of the aircraft, in order to avoid or reduce dispatch delays
and improve the dispatch reliability. It will at all times give sensible
and practical fault diagnosis to the users of this publication.
The Fault Reporting Section of the FIM provides means to effectively
report failures of the aircraft to the maintenance crew using the
appropriate fault codes and nomenclature. By doing this,
communication time and errors are reduced and fault reporting and
fault history consistency and accuracy are increased.
The procedures in this FIM were not prepared to cover intermittent
faults. However, if you have an intermittent fault, you should search
on the FIM a troubleshooting procedure that corresponds to this
intermittent fault and try to troubleshoot it, but only if your airline’s
policies for intermittent faults allow you to do so. If you do not solve
the fault, please contact EMBRAER Technical Support Department.
Available links: AMM, WM, AIPC.
The Fault Isolation Manual covers these faults:
CAS Messages
These are the messages displayed on the CAS message window of the
EICAS display. CAS messages are displayed on the cockpit displays to tell
the flight crew of any problem with the aircraft or any other conditions of the
aircraft. Each CAS message has a unique 8-digit fault code. The category
and color of the message are defined according to its criticality:
Warning (Red)
Caution (Amber)
Advisory (Cyan)
Status (White)
Observed Faults
Observed faults are problems that may be sensed by the flight crew or by the
ground crew and are not annunciated by the CAS. Each observed fault has
an unique 8-digit fault code.
Cabin Faults
Cabin faults are the problems or malfunctions which can occur with the
systems and equipment in the passenger cabin area. Each cabin fault has an
unique 8-digit fault code.
Maintenance Messages
Maintenance messages are those stored in the Central Maintenance
Computer (CMC), that help to find the cause of a CAS message or any other
fault. Each maintenance message has an unique 11-digit fault code.
The CMC receives fault reports from several aircraft systems. It processes
the data received and shows the applicable maintenance message on the
CMC screen on the MFD 2 or on the screen of a PC connected to the Local
Area Network (LAN). Maintenance messages can be CAS-correlated or
uncorrelated. When a CAS message is shown to the flight crew and there are
correlated maintenance messages, the CMC will show the CAS and the
correlated maintenance message(s).
The purpose of maintenance messages is to give information that help the
troubleshooting routine and are not necessarily related to the need of an
immediate maintenance action.

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 19
FAULT ISOLATION MANUAL USED AWITH AIRCRAFT CMC (CENTRAL MAINTENANCE COMPUTER)

Embraer ERJ-190 Series (GE CF34) ATA 05 –ATA12
B1.1. and B2 AIRPLANE GENERAL
ISSUE 1, 24 Sep 2014 FOR TRAINING PURPOSES ONLY Page: 20
RAMP MAINTENANCE MANUAL (RMM)
Purpose:
Provides information which can improve the ground handling and
avoid delays when difficulties are encountered for the dispatchability,
at ramp level.
Arrangement:
COMPONENT MAINTENANCE MANUAL (CMM)
Purpose :
Provides information and procedures applicable to a workshop
environment for the return of a component to a serviceable condition.
Arrangement: