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EMBRAER S.A.
12227-901 SAO JOSE DOS CAMPOS - S.P.
BRAZIL
PHONE: + 55 12 3927-7517
http://www.flyembraer.com
e-mail: [email protected]
AIRPORTPLANNING MANUAL
In connection with the use of this document, Embraer does not provide any express or implied warranties and expresslydisclaims any warranty of merchantability or fitness for a particular purpose.
This document contains trade secrets, confidential, proprietary information of Embraer and technical data subject to U.S.Export Administration Regulation ("EAR") and other countries export control laws and regulations. Diversion contrary tothe EAR and other laws and regulations is strictly forbidden. The above restrictions may apply to data on all pages of thisdocument.
APM - 582422 SEPTEMBER 2017
REVISION 15 - 27 SEPTEMBER 2019
Copyright © 2019 by Embraer S.A. All rights reserved.
TABLE OF CONTENTS
SUBJECTREVISIONSTATUS
REVISIONDATE
LIST OF EFFECTIVE AIRCRAFT R Sep 27/19
RECORD OF REVISIONS R Sep 27/19
HIGHLIGHTS R Sep 27/19
INTRODUCTION U Nov 09/18
SECTION 01 U Sep 22/17General Information
SECTION 02 U May 10/19Aircraft Description
SECTION 03 U Feb 08/19Aircraft Performance
SECTION 04 U Aug 09/19Ground Maneuvering
SECTION 05 U Nov 09/18Terminal Servicing
SECTION 06 U Nov 09/18Operation Conditions
SECTION 07 R Sep 27/19Pavement Data
SECTION 08 U Aug 10/18Possible EMBRAER 196 Derivative Aircraft
SECTION 09 U Nov 09/18Scaled Drawings
AIRPORTPLANNING MANUAL
Revision Status: U - Unchanged, R - Revised, N - New, D - Deleted
E-JETS E2 - APM 5824 TOC Page 1 of 1Rev 15 - Sep 27/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
LIST OF EFFECTIVE AIRCRAFT
The following list provides a cross-reference table of the aircraft to which the information contained in thismanual is applicable.
CommercialDesignation
CustomerAircraftNumber
ManufacturerSerial
Number
AircraftRegistration
Number
E190-E2 .......... EW 001 .......... 19020001 .......... TBDE190-E2 .......... EW 002 .......... 19020002 .......... TBDE190-E2 .......... EW 003 .......... 19020003 .......... TBDE190-E2 .......... EW 004 .......... 19020004 .......... TBDE195-E2 .......... EZ 001 .......... 19020005 .......... TBDE190-E2 .......... WI 001 .......... 19020009 .......... LN-WEAE190-E2 .......... WI 002 .......... 19020010 .......... LN-WEBE190-E2 .......... WI 003 .......... 19020011 .......... LN-WECE190-E2 .......... KZ 001 .......... 19020012 .......... P4-KHAE190-E2 .......... KZ 002 .......... 19020013 .......... P4-KHBE190-E2 .......... KZ 003 .......... 19020014 .......... P4-KHCE190-E2 .......... BH 001 .......... 19020015 .......... LN-WEXE190-E2 .......... BH 002 .......... 19020016 .......... TBDE190-E2 .......... KZ 004 .......... 19020017 .......... P4-KHDE195-E2 .......... ZL 001 .......... 19020018 .......... PR-PJNE190-E2 .......... KZ 005 .......... 19020019 .......... P4-KHEE195-E2 .......... ZL 002 .......... 19020020 .......... TBDE195-E2 .......... ZL 003 .......... 19020021 .......... TBDE190-E2 .......... HT 001 .......... 19020022 .......... HB-AZAE195-E2 .......... NT 001 .......... 19020023 .......... EC-NEZE195-E2 .......... NT 002 .......... 19020024 .......... TBDE195-E2 .......... ZL 004 .......... 19020025 .......... TBDE190-E2 .......... HT 002 .......... 19020026 .......... HB-AZBE195-E2 .......... NT 003 .......... 19020027 .......... TBDE195-E2 .......... ZL 005 .......... 19020028 .......... TBDE190-E2 .......... KI 001 .......... 19020029 .......... VH-IKJE190-E2 .......... HT 003 .......... 19020030 .......... HB-AZCE190-E2 .......... HT 004 .......... 19020031 .......... TBDE195-E2 .......... ZL 006 .......... 19020032 .......... TBDE195-E2 .......... ZL 007 .......... 19020033 .......... TBDE195-E2 .......... ZL 008 .......... 19020034 .......... TBDE195-E2 .......... ZL 009 .......... 19020035 .......... TBDE190-E2 .......... KI 002 .......... 19020036 .......... TBDE195-E2 .......... ZL 010 .......... 19020037 .......... TBDE190-E2 .......... HT 005 .......... 19020038 .......... TBDE195-E2 .......... PE 001 .......... 19020039 .......... TBDE195-E2 .......... ZL 011 .......... 19020040 .......... TBDE195-E2 .......... EZ 002 .......... 19020041 .......... PR-ZIQE195-E2 .......... ZL 012 .......... 19020042 .......... TBDE190-E2 .......... HT 006 .......... 19020043 .......... TBDE195-E2 .......... PE 002 .......... 19020045 .......... TBDE190-E2 .......... HT 007 .......... 19020046 .......... TBDE195-E2 .......... ZL 013 .......... 19020048 .......... TBDE195-E2 .......... ZL 014 .......... 19020049 .......... TBDE195-E2 .......... ZL 015 .......... 19020050 .......... TBD
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 LIST OF EFFECTIVE AIRCRAFT Page 1 of 2Rev 15 - Sep 27/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
CommercialDesignation
CustomerAircraftNumber
ManufacturerSerial
Number
AircraftRegistration
Number
E195-E2 .......... PE 003 .......... 19020051 .......... TBDE195-E2 .......... ZL 016 .......... 19020052 .......... TBDE195-E2 .......... ZL 017 .......... 19020053 .......... TBDE195-E2 .......... ZL 018 .......... 19020054 .......... TBDE195-E2 .......... ZL 019 .......... 19020055 .......... TBDE195-E2 .......... ZL 020 .......... 19020056 .......... TBDE195-E2 .......... ZL 021 .......... 19020057 .......... TBDE195-E2 .......... PE 004 .......... 19020058 .......... TBDE195-E2 .......... ZL 022 .......... 19020059 .......... TBDE195-E2 .......... ZL 023 .......... 19020060 .......... TBDE195-E2 .......... ZL 024 .......... 19020061 .......... TBDE195-E2 .......... ZL 025 .......... 19020062 .......... TBDE195-E2 .......... PE 005 .......... 19020064 .......... TBDE195-E2 .......... ZL 026 .......... 19020065 .......... TBDE190-E2 .......... HT 008 .......... 19020067 .......... TBDE190-E2 .......... HT 009 .......... 19020068 .......... TBDE195-E2 .......... ZL 027 .......... 19020069 .......... TBDE195-E2 .......... ZL 028 .......... 19020070 .......... TBDE190-E2 .......... XF 001 .......... 19020071 .......... TBDE195-E2 .......... ZL 029 .......... 19020072 .......... TBDE195-E2 .......... ZL 030 .......... 19020073 .......... TBDE195-E2 .......... ZL 031 .......... 19020075 .......... TBDE190-E2 .......... HT 010 .......... 19020078 .......... TBDE195-E2 .......... ZL 032 .......... 19020079 .......... TBDE195-E2 .......... ZL 033 .......... 19020080 .......... TBDE190-E2 .......... HT 011 .......... 19020082 .......... TBDE195-E2 .......... ZL 034 .......... 19020083 .......... TBDE195-E2 .......... ZL 035 .......... 19020084 .......... TBDE190-E2 .......... HT 012 .......... 19020087 .......... TBDE195-E2 .......... ZL 036 .......... 19020090 .......... TBDE195-E2 .......... ZL 037 .......... 19020094 .......... TBDE195-E2 .......... ZL 038 .......... 19020103 .......... TBDE195-E2 .......... ZL 039 .......... 19020104 .......... TBDE195-E2 .......... ZL 040 .......... 19020109 .......... TBDE195-E2 .......... ZL 041 .......... 19020111 .......... TBDE195-E2 .......... ZL 042 .......... 19020112 .......... TBDE195-E2 .......... ZL 043 .......... 19020114 .......... TBDE195-E2 .......... ZL 044 .......... 19020115 .......... TBDE195-E2 .......... ZL 103 .......... 19020117 .......... TBD
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 LIST OF EFFECTIVE AIRCRAFT Page 2 of 2Rev 15 - Sep 27/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
RECORD OF REVISIONS
This list is intended to show the Operator the cumulative issued revisions to his manual.The list consists of the revision number and the respective issuance date.
REV NO. ISSUE DATE
0 Sep 22/17
1 Oct 27/17
2 Nov 24/17
3 Dec 15/17
4 Jan 12/18
5 Feb 09/18
6 Mar 09/18
7 Apr 20/18
8 May 11/18
9 Jun 08/18
10 Aug 10/18
11 Nov 09/18
12 Feb 08/19
13 May 10/19
14 Aug 09/19
15 Sep 27/19
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 RECORD OF REVISIONS Page 1 of 1Rev 15 - Sep 27/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
HIGHLIGHTS
The table below lists the contents that have been technically revised in the current revision of this manual.Other revised contents, if any, that do not appear in the table below are considered editorially revised, theyhaving no technical implications.
SUBJECT DESCRIPTION
SECTION -07 Revised values for x and y of the table pavement evalua-tion
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 HIGHLIGHTS Page 1 of 1Rev 15 - Sep 27/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
INTRODUCTION
2. General
The APM has been prepared in accordance with NAS 3601.
It provides aircraft characteristics for general airport planning, airport operators, airlines, andengineering consultant organizations.
The APM is arranged as shown in the table below:
3. APM Arrangement
The APM is arranged as shown in the table below:
Table 1 - APM Arrangement
ARRANGEMENTS CONTENTS
Manual Front Matter
Title Page
Highlights
Record of Revision
List of Effective Aircraft
Table of Contents
Introduction
Section
General Information
Aircraft Description
Aircraft Performance
Ground Maneuvering
Terminal Servicing
Operating Conditions
Pavement Data
Possible Derivative Aircraft
Scaled Drawings
The front matter for the whole manual contains:
A. Title Page
Shows the manufacturer's masthead, identification of the manual, the initial issue date, andrevision number and date.
B. Highlights
It is a document that accompanies the manual revision and contains the detailed descriptionof the technical reasons that lead to the revision. It provides the operator with a clear view oftechnical issue of the revision.
C. Record of Revision
Lists the successive revision numbers, issue date, insertion date and incorporators initials,which must be kept current by the operator.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 INTRODUCTION Page 1 of 4Rev 11 - Nov 09/18
Copyright © by Embraer S.A. All rights reserved - See title page for details.
D. List of Effective Aircraft
It provides a cross-reference tabulation of commercial designation, customer aircraftnumber, manufacturing serial number and aircraft registration number.
E. Table of Contents
Lists front matter content with the latest issue dates and provides information to let thereader to quickly and accurately locate the material sought.
F. Introduction
This section present a description of the publication with:
1. General The general subsection describes the APM objectives and the directions for
Customers queries.
2. APM Arrangement This subsection present the APM arrangement as regard to its front matter and
sections contents. Queries concerning any printed material, including purchasing, copying, shipping
and handling, complaints, or compliments may be addressed to: Technical Publications Distribution: Embraer S.A. Attention of: Technical Publications Department CEP. 12.227-901- São José dos Campos - SP - Brazil Phone: (55 12) 3927-7517 http://www.embraer.com e-mail [email protected] For support regarding technical information contained in non-operational publication,
please contact: Routine Issues: Contact Embraer Customer Support Service AOG Issues: Contact Embraer AOG group directly
4. Revisions
Embraer may revise this manual periodically as required to update information or provide informationnot available at the time of printing. Revised data may result from Embraer approved aircraftmodifications and new available options. Changes to the text are indicated by a black bar in the pageleft-side margin, beside the revised, added, or deleted material. Relocated or rearranged text orillustrations will be indicated by a black bar beside the page number.
5. Acronyms and Abbreviations
The abbreviations shall be automatically generated by the editing system, and shall present all theacronyms and abbreviations, used throughout the manual sections.
6. Abbreviations
This list gives all the abbreviations, acronyms and measurement units used in this manual with theirdefinitions.
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E-JETS E2 - APM 5824 INTRODUCTION Page 2 of 4Rev 11 - Nov 09/18
Copyright © by Embraer S.A. All rights reserved - See title page for details.
Table 2 - List of Acronyms and Abbreviations used in the APM
ACRONYMS AND ABBREVIA-TIONS
DESCRIPTION
°C Degree Celsius
°F Degree Fahrenheit
ℓ Liter
ACN Aircraft Classification Number
AFM Airplane Flight Manual
AOM Airplane Operations Manual
APU Auxiliary Power Unit
AR As Required
BOW Basic Operation Weight
CBR California Bearing Rating
ECS Environmental Control System
FAA Federal Aviation Administration
FWD Forward
ICAO International Civil Aviation Organization
ISA International Standard Atmosphere
LCN Load Classification Number
LH Left-Hand
MLW Maximum Landing Weight
MOW Minimum Operating Weight
MRW Maximum Ramp Weight
MTBF Mean Time Between Failures
MTOW Maximum Takeoff Weight
MZFW Maximum Zero Fuel Weight
N Newton
RH Right-Hand
STD Standard
dBA A-Weighted Decibel
ft Foot
ft³ Cubic Foot
gal Gallon
in Inch
inHg Inch of Mercury
kPa Kilopascal
kg Kilogram
lb Pound
m Meter
m³ Cubic Meter
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 INTRODUCTION Page 3 of 4Rev 11 - Nov 09/18
Copyright © by Embraer S.A. All rights reserved - See title page for details.
(Continued)
Table 2 - List of Acronyms and Abbreviations used in the APM (Continued)
ACRONYMS AND ABBREVIA-TIONS
DESCRIPTION
min Minute
psi pound per square inch
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 INTRODUCTION Page 4 of 4Rev 11 - Nov 09/18
Copyright © by Embraer S.A. All rights reserved - See title page for details.
1. GENERAL INFORMATION
EFFECTIVITY: ALL
1.1. GENERAL
This document provides airplane characteristics for general airport planning. Since the operationalpractices vary among the airlines, specific data should be coordinated with the using airlines beforethe facility design is made.
The APM sections are presented as follows:
1.1.1. Section 1 - General Information
This section present general information applicable to all APM sections, and also scale aircraftdrawing and possible derivative aircraft required on NAS 3601.
1.1.2. Section 2 - Aircraft Description
This section present the aircraft characteristics, general aircraft dimensions, ground clearances,interior arrangements, passenger cabin cross section, lower compartment containers, doorclearances.
1.1.3. Section 3 - Aircraft Performance
This section present the general information, payload x range charts, takeoff field lengths andlanding field lengths.
1.1.4. Section 4 - Ground Maneuvering
This section present the general information, turning radii for various nose landing gear steeringangles, visibility from cockpit in static position, the minimum dimensions for runway and taxiwaywhere the aircraft can be operated and runway holding apron.
1.1.5. Section 5 - Terminal Servicing
This section present the terminal servicing information, the typical arrangements of equipment duringturnaround, the typical turnaround servicing time at an air terminal, the locations of ground servicingconnections in graphic and tabular forms, the typical sea level air pressure and flow requirements forstarting the engine, the air conditioning requirements and the ground towing requirements for varioustowing conditions.
1.1.6. Section 6 - Operation Conditions
This section provides the jet engine exhaust velocities and temperatures charts; the airport andcommunity noise levels and the hazard areas charts.
1.1.7. Section 7 - Pavement Data
This section provides the general information with a brief description of the pavement charts whichwill be helpful in their use for airport planning. Each aircraft configuration is depicted with a minimumrange of five loads imposed on the main landing gear to aid in the interpolation between the discretevalues shown. The tire pressure used for the aircraft charts will produce the recommended tiredeflection with the aircraft loaded to its maximum ramp weight and with center of gravity position.The tire pressure, where specifically designated in tables and on charts, are values obtained underloaded conditions as certificated for commercial use.
This section is presented as follows:
• The basic data on the landing gear footprint configuration, maximum design ramp loads, andtire sizes and pressures.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 01 Page 1 of 2Sep 22/17
Copyright © by Embraer S.A. All rights reserved - See title page for details.
• The maximum pavement loads for certain critical conditions at the tire-ground interfaces.
• A chart in order to determine the loads throughout the stability limits of the aircraft at rest onthe pavement.
Pavement requirements for commercial aircraft are customarily derived from the staticanalysis of loads imposed on the main landing gear struts.
These main landing gear loads are used to enter the pavement design charts which follow,interpolating load values where necessary.
• The flexible pavement curves prepared in accordance with the US Army Corps of EngineersDesign Method and the LCN Method.
• The rigid pavement design curves in accordance with the Portland Cement AssociationDesign Method and the LCN Method.
• The aircraft ACN values for flexible and rigid pavements.
1.1.8. Section 8 - Possible Embraer 190 E2 Derivative Aircraft
This sections provides information about derivative versions of the currently developed.
1.1.9. Section 9 - Scaled Drawings
This sections provides views to the following scales:
• English/American Customary Weights and Measures. 1 inch = 32 feet 1 inch = 50 feet 1 inch = 100 feet
• Metric. 1:500 1:1000
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 01 Page 2 of 2Sep 22/17
Copyright © by Embraer S.A. All rights reserved - See title page for details.
2. AIRCRAFT DESCRIPTION
EFFECTIVITY: ALL
2.1. AIRCRAFT CHARACTERISTICS
The aircraft is:
• Low winged;
• Conventional tail design;
• Two wing-mounted engines;
The PW1714G is the standard engine for the EMBRAER 175 E2.
The PW1919G is the standard engine for the EMBRAER 190 E2.
The PW1921G is the standard engine for the EMBRAER 195 E2.
The STD aircraft model has the following design weights:
2.1.1. Basic Characteristics
EFFECTIVITY: EMBRAER 190-E2 ACFT
• Maximum ramp weight of 56600 kg (124781 lb)
• Maximum take-off weight of 56400 kg (124340 lb)
• Maximum landing weight of 49050 kg (108136 lb)
• Basic Operational Weight 33000 kg (72752 lb)
• Maximum zero fuel weight of 46700 kg (102956 lb)
• Minimum operating weight of 32700 kg (72091 lb)
• Maximum usable fuel of 13500 kg (29762 lb)
2.1.2. Basic Characteristics
EFFECTIVITY: EMBRAER 195-E2 ACFT
• Maximum ramp weight of 61700 kg (136025 lb)
• Maximum take-off weight of 61500 kg (128419 lb)
• Maximum landing weight of 54000 kg (116734 lb)
• Basic Operational Weight 35750 kg ( 78815 lb)
• Maximum zero fuel weight of 51850 kg (111002 lb)
• Minimum operating weight of 34700 kg (76500 lb)
• Maximum usable fuel of 13690 kg (30181 lb)
2.1.3. Definitions
MRW
It is the maximum allowed aircraft weight for taxiing or maneuvering on the ground.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 1 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
MLW
It is the maximum allowed weight at which the aircraft may normally be landed.
MTOW
It is the maximum allowed total loaded aircraft weight at the start of the takeoff run.
BOW
It is the weight of the structure, powerplant, instruments, flight controls, hydraulic, electronic,electrical, air conditioning, oxygen, anti-icing and pressurization systems, interior furnishings,portable and emergency equipment and other items of equipment that are an integral part of theaircraft configuration. It also includes unusable fuel, total engine and APU oil, total hydraulic fluid,toilet fluid and water, potable water, crew and crew baggage, navigation kit (manuals, charts),catering (beverages and food) and removable service equipment for the galley.
MZFW
It is the maximum allowed weight without usable fuel in tanks.
MOW
This is the minimum aircraft authorized weight for flight as limited by aircraft strength andairworthiness requirements.
Maximum Payload
It is the difference between the MZFW and the BOW.
Maximum Seating Capacity
It is the maximum number of passengers specifically certified or anticipated for certification.
Maximum Cargo Volume
It is the maximum space available for cargo.
Usable Fuel
Fuel available for the aircraft propulsion.
Table 2.1 - Aircraft General CharacteristicsEffectivity: EMBRAER 190-E2 ACFT
DESIGN WEIGHTS [1]AIRCRAFT MODEL
STD
MRW 56600 kg (124781 lb)MTOW 56400 kg (124341 lb)MLW 49050 kg (108137 lb)
BOW [2] 33000 kg (72752 lb)MZFW 46700 kg (102956 lb)MOW 32700 kg (72091 lb)
Maximum Payload 13700 kg (30203 lb)[1] Applicable for standard models. For further information, refer to AFM and AOM.[2] Typical standard configuration (weights may vary according to optional equipment installed or interior layouts).
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E-JETS E2 - APM 5824 SECTION 02 Page 2 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
Table 2.1 - Aircraft General Characteristics (Continued)Effectivity: EMBRAER 190-E2 ACFT
DESIGN WEIGHTS [1]AIRCRAFT MODEL
STD
Maximum Seating Capacity 114 PassengersMaximum Cargo Volume [3] 22.63 m 3 (800 ft 3)
Maximum Usable Fuel [4] 13500 kg (29760 lb)16800 ℓ (4440 gal.)
[1] Applicable for standard models. For further information, refer to AFM and AOM.[3] Standard configuration (volume may vary according to optional equipment installed).[4] Based on 0.803 kg /ℓ (6.71 lb/gal) fuel density. Fuel density varies from 0.785 to 0.811 kg/ℓ (6.55 to 6.77 lb/gal) at 15 °C.
Table 2.2 - Aircraft General CharacteristicsEffectivity: EMBRAER 195-E2 ACFT
DESIGN WEIGHTS [1]AIRCRAFT MODEL
STD
MRW 61700 kg (136058 lb)MTOW 61500 kg (135584.6 lb)MLW 54000 kg (119049.6 lb)
BOW [2] 35750 kg (78715 lb)MZFW 51850 kg (114309 lb)MOW 34700 kg (76500 lb)
Maximum Payload 16100 kg (35494 lb)Maximum Seating Capacity 146 PassengersMaximum Cargo Volume [3] 29.97 m 3 1058 ft 3)
Maximum Usable Fuel [4] 13690 kg (30181 lb)17060 ℓ (4507 gal.)
[1] Applicable for standard models. For further information, refer to AFM and AOM.[2] Typical standard configuration (weights may vary according to optional equipment installed or interior layouts).[3] Standard configuration (volume may vary according to optional equipment installed).[4] Based on 0.803 kg /ℓ (6.71 lb/gal) fuel density. Fuel density varies from 0.785 to 0.811 kg/ℓ (6.55 to 6.77 lb/gal) at 15 °C.
2.2. GENERAL AIRCRAFT DIMENSIONS
2.2.1. External Dimensions
EFFECTIVITY: EMBRAER 190-E2 ACFT
• Span over Swept Back Wingtip - 33.72 m (110 ft 7.6 in)
• Height (maximum) - 10.95 m (35 ft 11.2 in)
• Overall length - 36.24 m (118 ft 11 in.)
2.2.2. External Dimensions
EFFECTIVITY: EMBRAER 195-E2 ACFT
• Span over Swept Back Wingtip - 35.12 m (115 ft 2.7 in)
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E-JETS E2 - APM 5824 SECTION 02 Page 3 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
• Height (maximum) - 10.78 m (35 ft 4.4 in)
• Overall length - 41.60 m (136 ft 5.76 in.)
2.2.3. Wing
• Reference area - 103 m 2 (1108.68 ft 2 )
• Reference aspect ratio - 9.4
2.2.4. Fuselage
EFFECTIVITY: EMBRAER 190-E2 ACFT
• Total length - 36.2 m (118 ft 2.7 in)
• Length of pressurized section - 29.1 m (95 ft 5.64 in)
2.2.5. Fuselage
EFFECTIVITY: EMBRAER 195-E2 ACFT
• Total length - 41.6 m (136 ft 5.76 in)
• Length of pressurized section - 34.3 m (112ft 6.36 in)
2.2.6. Horizontal Tail
• Span - 9.84 m (9 ft 10.1 in)
• Area - 23.25 m 2 (250.26ft 2 )
• Aspect ratio - 4.16
2.2.7. Vertical Tail
• Span - 5.27 m (9 ft 10.1 in)
• Area - 16.20 m 2 (174.38 ft 2 )
• Aspect ratio - 1.71
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E-JETS E2 - APM 5824 SECTION 02 Page 4 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTGeneral Aircraft Dimensions Figure 2.1
EM
170E
2A
PM
020001B
.ID
R
24.57 m(80 ft 7.3 in.)
10.72 m(35 ft 2.1 in.)
6.82 m(22 ft 4.5 in.)
4.55 m(14 ft 11.1 in.)
36.33 m(119 ft 2.3 in.)
12.77 m(41 ft 10.8 in.)
27.60 m(90 ft 6.6 in.)
27.60 m(90 ft 6.6 in.)
4.27 m(14 ft)
4.71 m(15 ft 5.4 in.)
20.10 m(65 ft 11.3 in.)
10.0 m(32 ft 3.4 in.)
6.73 m(22 ft 1.0 in.)
33.72 m(110 ft 7.6 in.)
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E-JETS E2 - APM 5824 SECTION 02 Page 5 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTGeneral Aircraft Dimensions Figure 2.2
EM
170E
2AP
M02
0014
C.ID
R
29.83 m(97 ft 10.44 in)6.82 m
(22 ft 4.5 in)
4.55 m(14 ft 11.1 in)
15.71 m(75 ft 6.48 in)
41.60 m(136 ft 5.76 in)
1
2
32.87 m(107 ft 10.08 in)
32.87 m(107 ft 10.08 in)
10.0 m(32 ft 3.4 in)
4.27 m(14 ft)
4.71 m(15 ft 5.4 in)
23.03 m(75 ft 6.72 in)
6.73 m(22 ft 1.0 in)
35.12 m(115 ft 2.7 in)
1 10.78 m (35 ft 4 in) MAXIMUM 54 ˚C (129.2 ˚F)
2 10.32 m (33 ft 10 in) MINIMUM -40 ˚C (-40 ˚F)
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTAircraft Ground Clearances Figure 2.3
EM
170E
2AP
M02
0002
B.ID
R
E K
MA
B
D
CJ L
N
FUSLG ANGLE (REF.)
H
F
G
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
Tabl
e 2.
3 - G
roun
d C
lear
ance
- S
TD A
ircra
ft M
odel
(@ -4
5 °C
)E
ffect
ivity
: EM
BR
AE
R 1
90-E
2 A
CF
T
WE
IGH
TC
G(%
MA
C)
FU
SA
NG
LE(D
EG
)(A
)
NO
SE
(B)
FO
R-
WA
RD
SE
RV
-IC
ED
OO
R(C
)
FO
R-
WA
RD
PA
S-
SE
N-
GE
RD
OO
R(D
)
FO
R-
WA
RD
CA
R-
GO
DO
OR
(E)
NA
-C
ELL
E(F
)
WIN
GT
IP (G)
OV
ER
WIN
GE
SC
AP
E(H
)
AF
TC
AR
-G
OD
OO
R(J
)
AF
TS
ER
V-
ICE
DO
OR
(K)
AF
TP
AS
-S
EN
-G
ER
DO
OR
(L)
VE
RT
I-C
AL
TA
IL(M
)
TA
ILS
KID
AN
GU
-LA
RC
LEA
RA
NC
E(D
EG
)(N
)
5660
0 kg
1247
84 lb
18-0
.73
2.26
m7
ft 5
in2.
77 m
9 ft
1 in
2.77
m9
ft 1
in
1.72
m5
ft 7.
7in
0.38
m1
ft 3
in
3.81
m12
ft 6
in
2.16
m7
ft 1
in
2.0
m6
ft 6.
7in
3.07
m10
ft 4
.7in
3.0
m9
ft 10
.1in
10.4
m34
ft 1
.5in
12.2
5660
0 kg
1247
84 lb
34-0
.54
2.30
m7
ft 6.
5in
2.80
m9
ft 2
in2.
80 m
9 ft
2 in
1.74
m5
ft 8.
5in
0.39
m1
ft 3.
3in
3.79
m12
ft 4
.8in
2.14
m7
ft 0.
25in
2.0
m6
ft 6.
7in
3.02
m9
ft 10
.9in
3.0
m9
ft 10
.1in
10.3
m33
ft 9
.5in
12.0
5640
0 kg
1243
43 lb
18-0
.73
2.26
m7
ft 5
in2.
77 m
9 ft
1 in
2.77
m9
ft 1
in
1.72
m5
ft 7.
7in
0.38
m1
ft 3
in
3.81
m12
ft 6
in
2.16
m7
ft 1
in
2.0
m6
ft 6.
7in
3.07
m10
ft 4
.7in
3.0
m9
ft 10
.1in
10.4
m34
ft 1
.5in
12.2
5640
0 kg
1243
43 lb
34-0
.54
2.30
m7
ft 6.
5in
2.80
m9
ft 2
in2.
80 m
9 ft
2 in
1.74
m5
ft 8.
5in
0.39
m1
ft 3.
3in
3.79
m12
ft 5
.2in
2.14
m7
ft 0.
25in
2.0
m6
ft 6.
7in
3.02
m9
ft 10
.9in
3.0
m9
ft 10
.1in
10.3
m33
ft 9
.5in
12.0
4905
0 kg
1081
39 lb
18-0
.82.
26 m
7 ft
5 in
2.78
m9
ft 1.
5in
2.78
m9
ft 1.
5in
1.73
m5
ft 8.
1in
0.40
m1
ft 3.
8in
3.85
m12
ft 7
.2in
2.18
m7
ft 1.
8 in
2.0
m6
ft 6.
7in
3.11
m10
ft 2
.4in
3.1
m10
ft 2
in
10.4
m34
ft 1
.5in
12.4
4905
0 kg
1081
39 lb
41-0
.49
2.34
m7
ft 8.
1in
2.83
m9
ft 3.
8in
2.84
m9
ft 3.
8in
1.77
m5
ft 9.
7in
0.42
m1
ft 4.
5in
3.80
m12
ft 5
.6in
2.16
m7
ft 1
in
2.0
m6
ft 6.
7in
3.03
m9
ft 11
.3in
3.0
m9
ft 10
.1in
10.3
m33
ft 9
.5in
12.0
4670
0 kg
1029
58 lb
18-0
.83
2.26
m7
ft 5
in
2.78
m9
ft 3.
4in
2.79
m9
ft 1.
8in
1.74
m5
ft 8.
5in
0.41
m1
ft 4.
1in
3.86
m12
ft 8
in
2.19
m7
ft 2.
2 in
2.0
m6
ft 6.
7in
3.12
m10
ft 2
.8in
3.1
m10
ft 2
in
10.5
m34
ft 5
.4in
12.4
4670
0 kg
1029
58 lb
41-0
.51
2.34
m7
ft 8.
1in
2.84
m9
ft 3.
8in
2.84
m9
ft 3.
8in
1.78
m5
ft 10
in
0.42
m1
ft 4.
5in
3.82
m12
ft 6
.4in
2.18
m7
ft 1.
8 in
2.0
m6
ft 6.
7in
3.05
m10
ft 2
.1in
3.0
m9
ft 10
.1in
10.3
m33
ft 9
.5in
12.1
3270
0 kg
7209
3 lb
22-0
.99
2.29
m7
ft 6.
2in
2.82
m9
ft 3.
4in
2.83
m9
ft 3.
4in
1.78
m5
ft 10
in
0.47
m1
ft 6.
5in
3.94
m12
ft11
.1 in
2.68
m8
ft 9.
5 in
2.20
m7
ft 2.
6in
3.22
m10
ft 6
.8in
3.2
m10
ft 6
in
10.6
m34
ft 9
.3in
12.9
3270
0 kg
7209
3 lb
32-0
.85
2.32
m7
ft 7.
3in
2.84
m9
ft 3
in
2.85
m9
ft 4.
2in
1.80
m5
ft 10
.8in
0.47
m1
ft 6.
5in
3.92
m12
ft10
.3 in
2.60
m8
ft 6.
3 in
2.10
m7
ft 10
.7in
3.19
m10
ft 5
.6in
3.2
m10
ft 6
in
10.5
m34
ft 5
.4in
12.7
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 8 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
Tabl
e 2.
4 - G
roun
d C
lear
ance
- S
TD A
ircra
ft M
odel
(@ +
20 °
C)
Effe
ctiv
ity: E
MB
RA
ER
190
-E2
AC
FT
WE
IGH
TC
G(%
MA
C)
FU
SA
NG
LE(D
EG
)(A
)
NO
SE
(B)
FO
R-
WA
RD
SE
RV
-IC
ED
OO
R(C
)
FO
R-
WA
RD
PA
S-
SE
N-
GE
RD
OO
R(D
)
FO
R-
WA
RD
CA
R-
GO
DO
OR
(E)
NA
-C
ELL
E(F
)
WIN
GT
IP (G)
OV
ER
WIN
GE
S-
CA
PE
(H)
AF
TC
AR
-G
OD
OO
R(J
)
AF
TS
ER
V-
ICE
DO
OR
(K)
AF
TP
AS
-S
EN
-G
ER
DO
OR
(L)
VE
RT
I-C
AL
TA
IL(M
)
TA
ILS
KID
AN
GU
-LA
RC
LEA
RA
NC
E(D
EG
)(N
)
5660
0 kg
1247
84 lb
18-0
.85
2.29
m7
ft 6.
2in
2.81
m9
ft 2.
6in
2.81
m9
ft 2.
6in
1.76
m5
ft 9.
3in
0.44
m1
ft 5.
3in
3.89
m12
ft 9
.1in
2.23
m7
ft 3.
8in
2.10
m6
ft 10
.7in
3.15
m10
ft 4
in
3.16
m10
ft 4
.4in
10.5
0 m
34 ft
5.4
in12
.6
5660
0 kg
1247
84 lb
34-0
.64
2.34
m7
ft 8.
1in
2.84
m9
ft 3
in
2.85
m9
ft 4.
2in
1.79
m5
ft 10
.5in
0.45
m1
ft 5.
7in
3.86
m12
ft 8
in
2.21
m7
ft 3
in
2.07
m6
ft 9.
5in
3.11
m10
ft 2
.4in
3.11
m10
ft 2
.4in
10.4
2 m
34 ft
2.2
in12
.3
5640
0 kg
1243
43 lb
18-0
.85
2.29
m7
ft 6.
2in
2.81
m9
ft 2.
6in
2.82
m9
ft 3
in
1.76
m5
ft 9.
3in
0.44
m1
ft 5.
3in
3.89
m12
ft 9
.1in
2.23
m7
ft 3.
8in
2.10
m6
ft 10
.7in
3.16
m10
ft 4
.4in
3.16
m10
ft 4
.4in
10.5
0 m
34 ft
5.4
in12
.6
5640
0 kg
1243
43 lb
34-0
.64
2.34
m7
ft 8.
1in
2.84
m9
ft 3
in
2.85
m9
ft 4.
2in
1.79
m5
ft 10
.5in
0.45
m1
ft 5.
7in
3.86
m12
ft 8
in
2.21
m7
ft 3
in
2.07
m6
ft 9.
5in
3.11
m10
ft 2
.4in
3.11
m10
ft 2
.4in
10.4
2 m
34 ft
2.2
in12
.3
4905
0 kg
1081
39 lb
18-1
.01
2.29
m7
ft 6.
2in
2.82
m9
ft 3.
4in
2.83
m9
ft 3.
4in
1.78
m5f
t 10
in
0.46
m1
ft 6.
1in
3.93
m12
ft10
.7 in
2.26
m7
ft 5
in
2.15
m7
ft 0.
65in
3.20
m10
ft 6
in
3.20
m10
ft 6
in
10.5
5 m
34 ft
7.4
in12
.8
4905
0 kg
1081
39 lb
41-0
.62
2.39
m7
ft 10
.1in
2.88
m9
ft 5.
4in
2.89
m9
ft 5.
8in
1.83
m6
ft 9.
7in
0.48
m1
ft 6.
9in
3.88
m12
ft 8
.7in
2.24
m7
ft 4.
2in
2.08
m6
ft 9.
9in
3.12
m10
ft 2
.8in
3.12
m10
ft 2
.8in
10.4
2 m
34 ft
2.2
in12
.4
4670
0 kg
1029
58 lb
18-0
.96
2.29
m7
ft 6.
2in
2.82
m9
ft 3.
4in
2.83
m9
ft 3.
4in
1.79
m5
ft 10
.5in
0.47
m1
ft 6.
5in
3.94
m12
ft 8
.7in
2.27
m7
ft 5.
4in
2.02
m6
ft 7.
5in
3.22
m10
ft 6
.8in
3.22
m10
ft 6
.8in
10.5
7 m
34 ft
8.1
in12
.8
4670
0 kg
1029
58 lb
41-0
.62.
39 m
7 ft
10.1
in
2.89
m9
ft 5.
8in
2.89
m9
ft 5.
8in
1.83
m6
ft 6
in
0.49
m1
ft 7.
3in
3.89
m12
ft11
.1 in
2.25
m7
ft 4.
6in
2.10
m6
ft 10
.7in
3.13
m10
ft 3
.2in
3.13
m10
ft 3
.2in
10.4
4 m
34 ft
3in
12.4
3270
0 kg
7209
3 lb
22-1
.16
2.32
m7
ft 7.
3in
2.86
m9
ft 4.
6in
2.87
m9
ft 5
in
1.84
m6
ft 0.
4in
0.54
m1
ft 9.
3in
4.04
m13
ft 3
.1in
2.36
m7
ft 8.
9in
2.27
m7
ft 5.
4in
3.34
m10
ft11
.5 in
3.34
m10
ft11
.5 in
10.7
2 m
35 ft
2in
13.3
3270
0 kg
7209
3 lb
32-0
.99
2.36
m7
ft 8.
9in
2.89
m9
ft 5.
8in
2.90
m9
ft 6.
2in
1.86
m6
ft 1.
2in
0.54
m1
ft 9.
3in
4.02
m13
ft 2
.3in
2.34
m7
ft 8.
1in
2.24
m7
ft 4.
2in
3.30
m10
ft 9
.9in
3.30
m10
ft 9
.9in
10.6
6 m
34 ft
11.7
in13
.1
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 9 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
Tabl
e 2.
5 - G
roun
d C
lear
ance
- S
TD A
ircra
ft M
odel
(@ +
54 °
C)
Effe
ctiv
ity: E
MB
RA
ER
190
-E2
AC
FT
WE
IGH
TC
G(%
MA
C)
FU
SA
NG
LE(D
EG
)(A
)
NO
SE
(B)
FO
R-
WA
RD
SE
RV
-IC
ED
OO
R(C
)
FO
R-
WA
RD
PA
S-
SE
N-
GE
RD
OO
R(D
)
FO
R-
WA
RD
CA
R-
GO
DO
OR
(E)
NA
-C
ELL
E(F
)
WIN
GT
IP (G)
OV
ER
WIN
GE
S-
CA
PE
(H)
AF
TC
AR
-G
OD
OO
R(J
)
AF
TS
ER
V-
ICE
DO
OR
(K)
AF
TP
AS
-S
EN
-G
ER
DO
OR
(L)
VE
RT
I-C
AL
TA
ILM
)
TA
ILS
KID
AN
GU
-LA
RC
LEA
RA
NC
E(D
EG
)(N
)
5660
0 kg
1247
84 lb
18-0
.91
2.31
m7
ft 6.
9in
2.83
m9
ft 3.
8in
2.84
m9
ft 3.
8in
1.79
m5
ft 10
.4in
0.47
m1
ft 6.
5in
3.93
m12
ft10
.7 in
2.27
m7
ft 5.
4in
2.15
m7
ft 0.
65in
3.21
m10
ft 6
.4in
3.21
m10
ft 6
.4in
10.5
6 m
34 ft
7.7
in12
.8
5660
0 kg
1247
84 lb
34-0
.72.
36 m
7 ft
8.9
in
2.87
m9
ft 5
in2.
87 m
9 ft
5 in
1.82
m5
ft 11
.6in
0.48
m1
ft 6.
9in
3.90
m12
ft 9
.5in
2.25
m7
ft 4.
6in
2.11
m6
ft 11
in
3.15
m10
ft 4
.0in
3.16
m10
ft 4
.4in
10.4
8 m
34 ft
4.6
in12
.5
5640
0 kg
1243
43 lb
18-0
.92
2.31
m7
ft 6.
9in
2.83
m9
ft 3.
8in
2.84
m9
ft 3.
8in
1.79
m5
ft 10
.4in
0.47
m1
ft 6.
5in
3.94
m12
ft 8
.7in
2.27
m7
ft 5.
4in
2.15
m7
ft 0.
65in
3.21
m10
ft 6
.4in
3.21
m10
ft 6
.4in
10.5
6 m
34 ft
7.7
in12
.8
5640
0 kg
1243
43 lb
34-0
.72.
36 m
7 ft
8.9
in
2.87
m9
ft 5
in2.
87 m
9 ft
5 in
1.82
m5
ft 11
.6in
0.48
m1
ft 6.
9in
3.90
m12
ft 9
.5in
2.25
m7
ft 4.
6in
2.11
m6
ft 11
in
3.16
m10
ft 4
.4in
3.16
m10
ft 4
.4in
10.4
8 m
34 ft
4.6
in12
.5
4905
0 kg
1081
39 lb
18-1
.01
2.31
m7
ft 6.
9in
2.84
m9
ft 3.
8in
2.85
m9
ft 4.
2in
1.81
m5
ft 11
.2in
0.50
m1
ft 7.
7in
3.97
m13
ft 3
in
2.30
m7
ft 6.
6in
2.20
m6
ft 2.
6in
3.25
m10
ft 8
.0in
3.26
m10
ft 8
.3in
10.6
2 m
34 ft
10
in13
.0
4905
0 kg
1081
39 lb
41-0
.62
2.41
m7
ft 10
.9in
2.91
m9
ft 7
in2.
92 m
9 ft
7 in
1.86
m6
ft 1.
2in
0.51
m1
ft 8.
1in
3.92
m12
ft10
.3 in
2.28
m7
ft 5.
7in
2.13
m6
ft 11
.8in
3.17
m10
ft 4
.8in
3.17
m10
ft 4
.8in
10.4
8 m
34 ft
4.6
in12
.5
4670
0 kg
1029
58 lb
18-1
.04
2.31
m7
ft 6.
9in
2.85
m9
ft 3.
8in
2.86
m9
ft 4.
6in
1.81
m5
ft 11
.2in
0.51
m1
ft 8.
1in
3.99
m13
ft10
.9 in
2.31
m7
ft 6.
9in
2.21
m7
ft 3
in
3.27
m10
ft 8
.7in
3.27
m10
ft 8
.7in
10.6
4 m
34 ft
11
in13
.1
4670
0 kg
1029
58 lb
41-0
.65
2.41
m7
ft 10
.9in
2.92
m9
ft 7
in2.
92 m
9 ft
7 in
1.86
m6
ft 1.
2in
0.52
m1
ft 8.
5in
3.94
m12
ft11
.1 in
2.29
m7
ft 6.
1in
2.14
m7
ft 0.
25in
3.18
m10
ft 5
.2in
3.18
m10
ft 5
.2in
10.5
0 m
34 ft
5.4
in12
.6
3270
0 kg
7209
3 lb
22-1
.25
2.34
m7
ft 8.
1in
2.89
m9
ft 7.
7in
2.90
m9
ft 7.
7in
1.87
m6
ft 1.
6in
0.58
m1
ft 10
.8in
4.10
m13
ft 5
.4in
2.40
m7
ft 10
.5in
2.33
m7
ft 7.
7in
3.40
m11
ft 1
.8in
3.40
m11
ft 1
.8in
10.8
0 m
35 ft
6in
13.6
3270
0 kg
7209
3 lb
32-1
.07
2.38
m7
ft 9.
7in
2.92
m9
ft 7
in
2.93
m9
ft 7.
3in
1.89
m6
ft 2.
4in
0.58
m1
ft 10
.8in
4.07
m13
ft 4
.2in
2.40
m7
ft 10
.5in
2.30
m7
ft 6.
6in
3.36
m11
ft 2
.8in
3.36
m11
ft 2
.8in
10.7
3 m
35 ft
2.4
in13
.4
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 10 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTAircraft Ground Clearances Figure 2.4
EM
170E
2AP
M02
0015
A.ID
R
F
G
N
M
LJHE
B
A
FUSELAGE ANGLE (REF.)
DK
C
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 11 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
Tabl
e 2.
6 - G
roun
d C
lear
ance
- S
TD A
ircra
ft M
odel
(@ -4
5 °C
)E
ffect
ivity
: EM
BR
AE
R 1
95-E
2 A
CF
T
WE
IGH
TC
G(%
MA
C)
FU
SA
NG
LE(D
EG
)(A
)
NO
SE
(B)
FO
R-
WA
RD
SE
RV
-IC
ED
OO
R(C
)
FO
R-
WA
RD
PA
S-
SE
N-
GE
RD
OO
R(D
)
FO
R-
WA
RD
CA
R-
GO
DO
OR
(E)
NA
-C
ELL
E(F
)
WIN
GT
IP (G)
OV
ER
WIN
GE
SC
AP
E(H
)
AF
TC
AR
-G
OD
OO
R(J
)
AF
TS
ER
V-
ICE
DO
OR
(K)
AF
TP
AS
-S
EN
-G
ER
DO
OR
(L)
VE
RT
I-C
AL
TA
IL(M
)
TA
ILS
KID
AN
GU
-LA
RC
LEA
RA
NC
E(D
EG
)(N
)
6010
0kg
1324
98 lb
13-0
.56
2.27
m7
ft 5.
4in
2.77
m9
ft 1
in2.
77 m
9 ft
1 in
1.71
m5
ft 7.
7in
0.37
m1
ft 3
in
3.90
m12
ft 9
.5in
2.15
m7
ft 1
in
2.0
m6
ft 6.
7in
3.05
m10
ft 0
.1in
3.0
m9
ft 10
.1in
10.4
m34
ft 1
.5in
10.5
6170
0 kg
1360
25 lb
34-0
.37
2.33
m7
ft 7.
7in
2.81
m9
ft 2.
6in
2.81
m9
ft 2.
6in
1.74
m5
ft 8.
5in
0.37
m1
ft 3.
3in
3.90
m12
ft 9
.5in
2.13
m7
ft 0.
25in
1.97
m6
ft 6.
7in
3.0
m9
ft 10
.1in
3.0
m9
ft 10
.1in
10.3
m33
ft 9
.5in
10.2
6150
0 kg
1355
84 lb
34-0
.37
2.33
m7
ft 7.
7in
2.81
m9
ft 2.
6in
2.81
m9
ft 2
in
1.74
m5
ft 8.
5in
0.37
m1
ft 3
in
3.90
m12
ft 9
.5in
2.13
m7
ft 1
in
1.97
m6
ft 6.
7in
3.0
m9
ft10
.08
in
3.0
m9
ft 10
.1in
10.3
m34
ft 1
.5in
10.2
5990
0 kg
1320
57 lb
13-0
.56
2.27
m7
ft 5.
4in
2.77
m9
ft 1
in2.
77 m
9 ft
1 in
1.71
m5
ft 7.
7in
0.37
m1
ft 3.
3in
3.90
m12
ft 9
.5in
2.15
m7
ft 0.
25in
2.0
m6
ft 6.
7in
3.05
m10
ft 0
.1in
3.0
m9
ft 10
.1in
10.4
m33
ft 9
.5in
10.5
5400
0 kg
1190
49 lb
13-0
.60
2.28
m7
ft 5.
8in
2.78
m9
ft 1.
5in
2.78
m9
ft 1.
5in
1.72
m5
ft 8.
1in
0.38
m1
ft 3.
8in
3.90
m12
ft 9
.5in
2.17
m7
ft 1.
8 in
2.0
m6
ft 6.
7in
3.08
m10
ft 1
.2in
3.1
m10
ft 2
in
10.4
m34
ft 1
.5in
10.6
5400
0 kg
1190
49 lb
40-0
.33
2.36
m7
ft 8.
9in
2.84
m9
ft 3.
8in
2.84
m9
ft 3.
8in
1.77
m5
ft 9.
7in
0.39
m1
ft 4.
5in
3.90
m12
ft 9
.5in
2.15
m7
ft 1
in
2.0
m6
ft 6.
7in
3.0
m9
ft 10
.1in
3.0
m9
ft 10
.1in
10.3
m33
ft 9
.5in
10.3
5185
0 kg
1140
39 lb
13-0
.62
2.28
m7
ft 5.
8in
2.78
m9
ft 1.
5in
2.79
m9
ft 1.
8in
1.73
m5
ft 8.
5in
0.39
m1
ft 4.
1in
3.90
m12
ft 9
.5in
2.18
m7
ft 2.
2 in
2.0
m6
ft 6.
7in
3.09
m10
ft 1
.7in
3.1
m10
ft 2
in
10.4
m34
ft 5
.4in
10.6
5185
0 kg
1140
39 lb
40-0
.35
2.36
m7
ft 8.
9in
2.84
m9
ft 3.
8in
2.84
m9
ft 3.
8in
1.78
m5
ft 10
in
0.39
m1
ft 4.
5in
3.90
m12
ft 9
.5in
2.16
m7
ft 1.
8 in
2.0
m6
ft 6.
7in
3.0
m9
ft 10
.1in
3.0
m9
ft 10
.1in
10.3
m33
ft 9
.5in
10.3
3470
0kg
7650
0 lb
18-0
.75
2.31
m7
ft 7
in2.
82 m
9 ft
3 in
2.83
m9
ft 3.
4in
1.77
m5
ft 10
in
0.45
m1
ft 6.
5in
4.0
m13
ft 1
.4in
2.26
m8
ft 9.
5 in
2.1
m7
ft 2.
6in
3.2
m10
ft 6
in
3.2
m10
ft 6
in
10.5
m34
ft 9
.3in
110
3470
0 kg
7650
0 lb
30-0
.62
2.35
m7
ft 8.
5in
2.85
m9
ft 4.
2in
2.85
m9
ft 4.
2in
1.80
m5
ft 10
.8in
0.46
m1
ft 6.
5in
4.0
m13
ft 1
.4in
2.25
m8
ft 6.
3 in
2.1
m7
ft 10
.7in
3.16
m10
ft 4
.4in
3.2
m10
ft 6
in
10.5
m34
ft 5
.4in
10.8
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 12 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
Tabl
e 2.
7 - G
roun
d C
lear
ance
- S
TD A
ircra
ft M
odel
(@ +
20 °
C)
Effe
ctiv
ity: E
MB
RA
ER
195
-E2
AC
FT
WE
IGH
TC
G(%
MA
C)
FU
SA
NG
LE(D
EG
)(A
)
NO
SE
(B)
FO
R-
WA
RD
SE
RV
-IC
ED
OO
R(C
)
FO
R-
WA
RD
PA
S-
SE
N-
GE
RD
OO
R(D
)
FO
R-
WA
RD
CA
R-
GO
DO
OR
(E)
NA
-C
ELL
E(F
)
WIN
GT
IP (G)
OV
ER
WIN
GE
S-
CA
PE
(H)
AF
TC
AR
-G
OD
OO
R(J
)
AF
TS
ER
V-
ICE
DO
OR
(K)
AF
TP
AS
-S
EN
-G
ER
DO
OR
(L)
VE
RT
I-C
AL
TA
IL(M
)
TA
ILS
KID
AN
GU
-LA
RC
LEA
RA
NC
E(D
EG
)(N
)
6010
0kg
1324
98 lb
13-0
.65
2.31
m7
ft 7
in
2.81
m9
ft 2.
6in
2.81
m9
ft 2.
6in
1.76
m5
ft 9.
3in
0.44
m1
ft 5.
3in
4.0m
12 ft
9.6
in
2.23
m7
ft 3.
8in
2.10
m6
ft 10
.7in
3.14
m10
ft 3
.6in
3.16
m10
ft 4
.4in
10.5
0 m
34 ft
5.4
in10
.7
6170
0 kg
1360
25 lb
34-0
.43
2.37
m7
ft 9.
4in
2.85
m9
ft 4.
2in
2.85
m9
ft 4.
2in
1.79
m5
ft 10
.5in
0.45
m1
ft 5.
7in
3.9
m12
ft 9
.6in
2.21
m7
ft 3
in
2.07
m6
ft 9.
5in
3.07
m10
ft 0
.8in
3.11
m10
ft 2
.4in
10.4
2 m
34 ft
2.2
in10
.5
6150
0 kg
1355
84 lb
34-0
.43
2.37
m7
ft 9.
4in
2.85
m9
ft 4.
2in
2.82
m9
ft 3
in
1.76
m5
ft 9.
3in
0.44
m1
ft 5.
3in
3.9
m12
ft 9
.6in
2.23
m7
ft 3.
8in
2.10
m6
ft 10
.7in
3.07
m10
ft 0
.8in
3.16
m10
ft 4
.4in
10.5
0 m
34 ft
5.4
in10
.5
5990
0 kg
1320
57 lb
13-0
.43
2.31
m7f
t 7 in
2.81
m9
ft 4.
2in
2.85
m9
ft 4.
2in
1.79
m5
ft 10
.5in
0.45
m1
ft 5.
7in
3.9
m12
ft 9
.6in
2.21
m7
ft 3
in
2.07
m6
ft 9.
5in
3.14
m10
ft 3
.6in
3.11
m10
ft 2
.4in
10.4
2 m
34 ft
2.2
in10
.8
5400
0 kg
1190
49 lb
13-0
.65
2.31
m7
ft 7
in
2.82
m9
ft 3.
4in
2.83
m9
ft 3.
4in
1.78
m5f
t 10
in
0.46
m1
ft 6.
1in
3.9
m12
ft 9
.6in
2.26
m7
ft 5
in
2.15
m7
ft 0.
65in
3.17
m10
ft 4
.8in
3.20
m10
ft 6
in
10.5
5 m
34 ft
7.4
in10
.9
5400
0 kg
1190
49 lb
40-0
.70
2.41
m7
ft 10
.9in
2.9
m9
ft 5.
8in
2.9
m9
ft 5.
8in
1.83
m6
ft 9.
7in
0.48
m1
ft 6.
9in
3.9
m12
ft 9
.6in
2.24
m7
ft 4.
2in
2.08
m6
ft 9.
9in
3.08
m10
ft 1
.2in
3.12
m10
ft 2
.8in
10.4
2 m
34 ft
2.2
in10
.5
5185
0 kg
1140
39 lb
13-0
.38
2.31
m7
ft 7
in
2.82
m9
ft 5.
8in
2.83
m9
ft 3.
4in
1.79
m5
ft 10
.5in
0.47
m1
ft 6.
5in
3.9
m12
ft 9
.6in
2.27
m7
ft 5.
4in
2.02
m6
ft 7.
5in
3.18
m10
ft 5
.2in
3.22
m10
ft 6
.8in
10.5
7 m
34 ft
8.1
in10
.9
5185
0 kg
1140
39 lb
40-0
.71
2.41
m7
ft 10
.9in
2.90
m9
ft 5.
8in
2.89
m9
ft 5.
8in
1.83
m6
ft 6
in
0.49
m1
ft 7.
3in
4.0
m12
ft 9
.6in
2.25
m7
ft 4.
6in
2.10
m6
ft 10
.7in
3.09
m10
ft 1
.7in
3.13
m10
ft 3
.2in
10.4
4 m
34 ft
3in
10.5
3470
0kg
7650
0 lb
18-0
.87
2.35
m7
ft 8.
5in
2.87
m9
ft 5
in2.
87 m
9 ft
5 in
1.84
m6
ft 0.
4in
0.54
m1
ft 9.
3in
4.0
m13
ft 5
.4in
2.36
m7
ft 8.
9in
2.27
m7
ft 5.
4in
3.30
m10
ft 1
0in
3.34
m10
ft11
.5 in
10.7
2 m
35 ft
2in
11.3
3470
0 kg
7650
0 lb
30-0
.71
2.39
m7
ft 10
.1in
2.90
m9
ft 6.
2in
2.90
m9
ft 6.
2in
1.86
m6
ft 1.
2in
0.54
m1
ft 9.
3in
4.0
m13
ft 5
.4in
2.34
m7
ft 8.
1in
2.24
m7
ft 4.
2in
3.26
m10
ft 8
.4in
3.30
m10
ft 9
.9in
10.6
6 m
34 ft
11.7
in11
.2
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 13 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
Tabl
e 2.
8 - G
roun
d C
lear
ance
- S
TD A
ircra
ft M
odel
(@ +
54 °
C)
Effe
ctiv
ity: E
MB
RA
ER
195
-E2
AC
FT
WE
IGH
TC
G(%
MA
C)
FU
SA
NG
LE(D
EG
)(A
)
NO
SE
(B)
FO
R-
WA
RD
SE
RV
-IC
ED
OO
R(C
)
FO
R-
WA
RD
PA
S-
SE
N-
GE
RD
OO
R(D
)
FO
R-
WA
RD
CA
R-
GO
DO
OR
(E)
NA
-C
ELL
E(F
)
WIN
GT
IP (G)
OV
ER
WIN
GE
S-
CA
PE
(H)
AF
TC
AR
-G
OD
OO
R(J
)
AF
TS
ER
V-
ICE
DO
OR
(K)
AF
TP
AS
-S
EN
-G
ER
DO
OR
(L)
VE
RT
I-C
AL
TA
ILM
)
TA
ILS
KID
AN
GU
-LA
RC
LEA
RA
NC
E(D
EG
)(N
)
6010
0kg
1324
98 lb
13-0
.70
2.33
m7
ft 7.
7in
2.84
m9
ft 3.
8in
2.84
m9
ft 3.
8in
1.79
m5
ft 10
.4in
0.47
m1
ft 6.
5in
4.0
m13
ft 5
.4in
2.27
m7
ft 5.
4in
2.15
m7
ft 0.
65in
3.18
m10
ft 5
.2in
3.21
m10
ft 6
.4in
10.5
6 m
34 ft
7.7
in10
.9
6170
0 kg
1360
25 lb
34-0
.47
2.39
m7
ft 10
.1in
2.88
m9
ft 5.
4in
2.87
m9
ft 5
in
1.82
m5
ft 11
.6in
0.48
m1
ft 6.
9in
4.0
m13
ft 5
.4in
2.25
m7
ft 4.
6in
2.11
m6
ft 11
in
3.12
m10
ft 2
.9in
3.16
m10
ft 4
.4in
10.4
8 m
34 ft
4.6
in10
.6
6150
0 kg
1355
84 lb
34-0
.47
2.39
m7
ft 10
.1in
2.88
m9
ft 5.
4in
2.84
m9
ft 3.
8in
1.79
m5
ft 10
.4in
0.47
m1
ft 6.
5in
4.0
m13
ft 5
.4in
2.27
m7
ft 5.
4in
2.15
m7
ft 0.
65in
3.12
m10
ft 2
.9in
3.21
m10
ft 6
.4in
10.5
6 m
34 ft
7.7
in10
.6
5990
0 kg
1320
57 lb
13-0
.70
2.33
m7
ft 7.
7in
2.84
m9
ft 3.
8in
2.87
m9
ft 5
in
1.82
m5
ft 11
.6in
0.48
m1
ft 6.
9in
4.0
m13
ft 5
.4in
2.25
m7
ft 4.
6in
2.11
m6
ft 11
in
3.19
m10
ft 5
.6in
3.16
m10
ft 4
.4in
10.4
8 m
34 ft
4.6
in10
.9
5400
0 kg
1190
49 lb
13-0
.75
2.33
m7
ft 7.
7in
2.84
m9
ft 3.
8in
2.85
m9
ft 4.
2in
1.81
m5
ft 11
.2in
0.50
m1
ft 7.
7in
4.0
m13
ft 5
.4in
2.30
m7
ft 6.
6in
2.20
m6
ft 2.
6in
3.22
m10
ft 6
.7in
3.26
m10
ft 8
.3in
10.6
2 m
34 ft
10
in11
.0
5400
0 kg
1190
49 lb
40-0
.42
2.44
m8
ft 1.
2in
2.92
m9
ft 7
in2.
92 m
9 ft
7 in
1.86
m6
ft 1.
2in
0.51
m1
ft 8.
1in
4.0
m13
ft 5
.4in
2.28
m7
ft 5.
7in
2.13
m6
ft 11
.8in
3.13
m10
ft 3
.2in
3.17
m10
ft 4
.8in
10.4
8 m
34 ft
4.6
in10
.7
5185
0 kg
1140
39 lb
13-0
.77
2.33
m7
ft 7.
7in
2.85
m9
ft 4.
2in
2.86
m9
ft 4.
6in
1.81
m5
ft 11
.2in
0.51
m1
ft 8.
1in
4.0
m13
ft 5
.4in
2.31
m7
ft 6.
9in
2.21
m7
ft 3
in
3.23
m10
ft 7
.2in
3.27
m10
ft 8
.7in
10.6
4 m
34 ft
11
in11
.1
5185
0 kg
1140
39 lb
40-0
.43
2.44
m8
ft 1.
2in
2.93
m9
ft 7.
3in
2.92
m9
ft 7
in
1.86
m6
ft 1.
2in
0.52
m1
ft 8.
5in
4.0
m13
ft 5
.4in
2.29
m7
ft 6.
1in
2.14
m7
ft 0.
25in
3.14
m10
ft 3
.6in
3.18
m10
ft 5
.2in
10.5
0 m
34 ft
5.4
in10
.7
3470
0kg
7650
0 lb
18-0
.93
2.37
m7
ft 9.
4in
2.90
m9
ft 6.
1in
2.90
m9
ft 7.
7in
1.87
m6
ft 1.
6in
0.58
m1
ft 10
.8in
4.1
m13
ft 5
.4in
2.40
m7
ft 10
.5in
2.33
m7
ft 7.
7in
3.36
m10
ft 0
.2in
3.40
m11
ft 1
.8in
10.8
0 m
35 ft
6in
11.5
3470
0 kg
7650
0 lb
30-0
.77
2.42
m7
ft 11
.3in
2.93
m9
ft 7.
3in
2.93
m9
ft 7.
3in
1.89
m6
ft 2.
4in
0.58
m1
ft 10
.8in
4.1
m13
ft 5
.4in
2.40
m7
ft 10
.5in
2.30
m7
ft 6.
6in
3.32
m10
ft10
.7 in
3.36
m11
ft 2
.8in
10.7
3 m
35 ft
2.4
in11
.4
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 14 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
2.3. INTERIOR ARRANGEMENTS
EFFECTIVITY: EMBRAER 190-E2 ACFT
The interior arrangement provides accommodation for two pilots, one observer, two flight attendants,104 passengers in 31 in pitch nominal configuration and 114 passengers in 29 in pitch maximumconfiguration. One additional flight attendant seat is available as optional.
2.3.1. Passenger Cabin
EFFECTIVITY: EMBRAER 190-E2 ACFT
The passenger cabin accommodates 104 passengers in 26 double seats on both sides, in 0.7874 m(31 in) pitch nominal configuration and 114 passengers in 28 double seats on LH and 29 doubleseats on RH, in 0.7366 m (29 in) pitch maximum configuration.
As optional, the passenger cabin is also provided with some double first-class seats on the RH sideand some single first-class seats on the LH side.
The main dimensions of passenger cabin are presented below:
• Height - 2.00 m (6 ft 7 in.)
• Width - 2.74 m (9 ft)
• Aisle wide - 0.49 m (1 ft 7 in.)
• Pitch - 0.79 m (31 in.) in pitch nominal configuration and 0.74 m (29 in.) in pitch maximumconfiguration.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 15 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTypical Interior Arrangements - 104 Pax Single Class at 0.7874 m (31 in) pitch nominal configuration Figure 2.5
0.74 m(2.43 ft)
1.83 m(6 ft)
3.38 m(11.1 ft)
1.79 m(5.88 ft)
EM
170E
2AP
M02
0003
C.ID
R
23 4
5
67
0.72 m(2.36 ft)
0.78 m(2.56 ft)
OVERHEAD BIN
UNDERSEAT VOLUME
CARGO COMPARTMENT 22.63 m³ (799.18 ft³)
0.06 m³ / pax (2.0 ft³ / pax)
0.04 m³ / pax (1.4 ft³ / pax)
CARGO/BAGGAGE VOLUME
1
8
42 3
8
8 - CARGO COMPARTMENT
1.77 m(5.81 ft)
6.36 m(20.87 ft)
1.09 m(3.58 ft)
1.18 m(3.88 ft)
22.55 m(74 ft)
1.18 m(3.88 ft)
7.89 m(25.88 ft)
1 - NO RECLINING SEAT AT THIS ROW
2 - GALLEY G1
3 - GALLEY G2/STOWAGE
4 - GALLEY G5
5 - AFT TOILET
6 - LH FWD STOWAGE
7 - FWD TOILET
99
9
9 - FLIGHT ATTENDANT SEAT
1.09 m(3.58 ft)
0.90 m(2 ft 11.4 in) 0.88 m
(2 ft 10.6 in)
0.78 m(2 ft 6.7 in)
4.88 m(16 ft)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 16 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTypical Interior Arrangements - 114 Pax Single Class at 0.7366 m (29 in) pitch maximum configuration Figure 2.6
0.65 m(2.13 ft)
0.99 m(3.25 ft)
0.62 m(2.03 ft)
EM
170E
2AP
M02
0004
C.ID
R
1
2
3
6
7
4
5
OVERHEAD BIN
UNDERSEAT VOLUME
CARGO COMPARTMENT 22.63 m³ (799.18 ft³)
0.06 m³ / pax (2.0 ft³ / pax)
0.04 m³ / pax (1.4 ft³ / pax)
CARGO/BAGGAGE VOLUME
8 - CARGO COMPARTMENT
0.99 m(3.25 ft)
8 8
42 3
1 - NO RECLINING SEAT AT THIS ROW
2 - GALLEY G1
3 - FWD PARTITION
4 - GALLEY G5
5 - AFT TOILET
6 - LH FWD STOWAGE
7 - FWD TOILET
0.74 m(2.43 ft)
1.83 m(6 ft)
3.38 m(11.1 ft)
1.79 m(5.88 ft)
1.77 m(5.81 ft)
6.36 m(20.87 ft)
1.18 m(3.88 ft)
22.55 m(74 ft)
4.88 m(16 ft)
1.18 m(3.88 ft)
7.89 m(25.88 ft)
9 - FLIGHT ATTENDANT SEAT
9
9
9
0.90 m(2 ft 11.4 in)
0.78 m(2 ft 6.7 in)0.88 m
(2 ft 10.6 in)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 17 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTypical Interior Arrangements - 96 Pax Dual Class at 0.9652/0.7874 m (38/31 in) pitch configuration Figure 2.7
1.64 m(5.38 ft)
0.97 m(3.18 ft)
0.96 m(3.15 ft)
0.79 m(2.59 ft)
1.17 m(3.84 ft)
0.96 m(3.15 ft)
EM
170E
2AP
M02
0005
C.ID
R
1
23
4
567
OVERHEAD BIN
UNDERSEAT VOLUME
CARGO COMPARTMENT 22.63 m³ (799.18 ft³)
0.06 m³ / pax (2.0 ft³ / pax)
0.04 m³ / pax (1.4 ft³ / pax)
CARGO/BAGGAGE VOLUME
8 - CARGO COMPARTMENT
8
4
8
2 3
1 - NO RECLINING SEAT AT THIS ROW
2 - GALLEY G1
3 - GALLEY G2
4 - GALLEY G5
5 - AFT TOILET
6 - FWD PARTITION
7 - FWD TOILET
9 - FLIGHT ATTENDANT SEAT
1.83 m(6 ft)
3.38 m(11.1 ft)
1.79 m(5.88 ft)
6.36 m(20.87 ft)
1.09 m(3.58 ft)
1.18 m(3.88 ft)
4.88 m(16 ft)
7.89 m(25.88 ft)
1.18 m(3.88 ft)
22.55 m(74 ft)
9 9
91.09 m(3.58 ft)
0.78 m(2 ft 6.7 in)0.88 m
(2 ft 10.6 in)0.90 m(2 ft 11.4 in)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 18 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
2.3.2. Cargo Compartments
EFFECTIVITY: EMBRAER 190-E2 ACFT
Two cargo compartments are available, located underfloor, one forward of the wing, and another aftof the wing.
The cargo compartments comply with the FAR-25/JAR-25/RBHA-25 “class C” compartmentclassification.
The table below contains the capacity for the cargo compartment:
Table 2.9 - Capacity for the Cargo CompartmentEffectivity: EMBRAER 190-E2 ACFT
CARGO COMPARTMENT LOADING VOLUME
FWD [1] 1850 kg (4078 lb) 12.41 m³ (438.26 ft³)Aft 1650 kg (3638 lb) 10.22 m³ (360.92 ft³)
Total 3500 kg (7716 lb) 22.63 m³ (799.18 ft³)[1] Standard configuration (loading and volume may vary according to optional equipment installed).
2.3.3. Cockpit
The cockpit is acoustically and thermally insulated for appearance and durability. It follows theworldwide trend of rounded edges, which avoids harm to the flight crew.
The cockpit is separated from the passenger cabin by a bulkhead with a lockable door. The cockpitdoor is provided with lockable means operable only from the cockpit side, spy hole and escapemechanism on the cockpit side.
2.4. INTERIOR ARRANGEMENTS
EFFECTIVITY: EMBRAER 195-E2 ACFT
The interior arrangement provides accommodation for two pilots, one observer, three flightattendants, 138 passengers in 29 in pitch nominal configuration and 146 passengers in 28 in pitchmaximum configuration. One additional flight attendant seat is available as optional.
2.4.1. Passenger Cabin
The passenger cabin accommodates 138 passengers in 35 double seats on the RH side and 34double seats on the LH side, in 0.7366 m (29 in) pitch nominal configuration and 146 passengers in36 double seats on LH and 37 double seats on RH, in 0.7112 m (28 in) pitch maximum configuration.
As optional, the passenger cabin is also provided with some double first-class seats on the RH sideand some single first-class seats on the LH side.
The main dimensions of passenger cabin are presented below:
• Height - 2.00 m (6 ft 7 in.)
• Width - 2.52 m (8 ft 3.24 in.)
• Aisle wide - 0.49 m (1 ft 7 in.)
• Pitch - 0.74 m (29 in.) in pitch nominal configuration and 0.71 m (28 in.) in pitch maximumconfiguration.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 19 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTypical Interior Arrangements - 132 Pax Single Class at 0.7874 m (31 in) pitch nominal configuration Figure 2.8
EM
170E
2AP
M02
0010
B.ID
R
1 - NO RECLINING SEAT AT THIS ROW
2 - GALLEY G1
3 - GALLEY G2
4 - FWD TOILET
5 - HARD PARTITION
6 - AFT TOILET
7 - GALLEY G5
1.01 m(39.7 in)
0.79 m(31 in)
1 1 1
23
45
6
7
10.3 m(33 ft 9.48 in)
9.23 m(30 ft 3.36 in)
0.99 m(39 in)
0.79 m(31 in)
0.88 m(2 ft 10.6 in)
0.78 m(2 ft 6.7 in)
0.90 m(2 ft 11.4 in)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 20 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTypical Interior Arrangements - 120 Pax Dual Class at 0.965/0.7874 m (38/31 in) pitch configuration Figure 2.9
1 - NO RECLINING SEAT AT THIS ROW
2 - GALLEY G1
3 - GALLEY G2
4 - FWD TOILET
5 - LH WINDSCREEN
6 - AFT TOILET
7 - GALLEY G5
1 1
2
3
4
5
6
7
9.23 m(30 ft 3.36 in)
10.3 m(33 ft 9.48 in)
1.27 m(50 in)
1.12 m(44 in)
1.01 m(39.7 in)
0.97 m(38 in)
0.79 m(31 in) 0.79 m
(31 in)
EM
170E
2A
PM
020011B
.ID
R
0.90 m(2 ft 11.4 in)
0.88 m(2 ft 10.6 in)
0.78 m(2 ft 6.7 in)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 21 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTypical Interior Arrangements - 138 Pax Single Class at 0.7366 m (29 in) pitch nominal configuration Figure 2.10
EM
170E
2AP
M02
0012
B.ID
R
1 - NO RECLINING SEAT AT THIS ROW
2 - GALLEY G1
3 - WINDSCREEN
4 - FWD TOILET
5 - LH STOWAGE
6 - AFT TOILET
7 - GALLEY G5
45
1
23
6
7
9.23 m(30 ft 3.36 in)
10.3 m(33 ft 9.48 in)
1.08 m(42.7 in)
1.12 m(44 in)
0.74 m(29 in)
0.74 m(29 in)
0.88 m(2 ft 10.6 in)
0.78 m(2 ft 6.7 in)
0.90 m(2 ft 11.4 in)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 22 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTypical Interior Arrangements - 146 Pax Single Class at 0.7112 m (28 in) pitch nominal configuration Figure 2.11
EM
170E
2AP
M02
0013
B.ID
R
1 - NO RECLINING SEAT AT THIS ROW
2 - GALLEY G1
3 - RH WINDSCREEN (HIGH DENSITY)
4 - FWD TOILET
5 - LH WINDSCREEN
6 - AFT TOILET
7 - GALLEY G5
1 1
2
3
45
8
6
7
8 - THIRD TOILET
9.23 m(30 ft 3.36 in)
10.3 m(33 ft 9.48 in)
0.58 m(22.8 in)
1.09 m(43 in)
1.01 m(39.7 in)
0.78 m(30.8 in)
0.71 m(28 in)
0.71 m(28 in)
0.88 m(2 ft 10.6 in)
0.78 m(2 ft 6.7 in)
0.90 m(2 ft 11.4 in)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 23 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
2.4.2. Cargo Compartments
EFFECTIVITY: EMBRAER 195-E2 ACFT
Two cargo compartments are available, located underfloor, one forward of the wing, and another aftof the wing.
The cargo compartments comply with the FAR-25/JAR-25/RBHA-25 “class C” compartmentclassification.
The table below contains the capacity for the cargo compartment:
Table 2.10 - Capacity for the Cargo CompartmentEffectivity: EMBRAER 195-E2 ACFT
CARGO COMPARTMENT LOADING VOLUME
FWD [1] 2375 kg (5235.9 lb) 15.01 m³ (530.1 ft³)Aft 2555 kg (5632.8 lb) 14.96 m³ (528.3 ft³)
Total 4930 kg (10868.8 lb) 29.97 m³ (1058.4 ft³)[1] Standard configuration (loading and volume may vary according to optional equipment installed).
2.4.3. Cockpit
The cockpit is acoustically and thermally insulated for appearance and durability. It follows theworldwide trend of rounded edges, which avoids harm to the flight crew.
The cockpit is separated from the passenger cabin by a bulkhead with a lockable door. The cockpitdoor is provided with lockable means operable only from the cockpit side, spy hole and escapemechanism on the cockpit side.
2.5. PASSENGER CABIN CROSS SECTION
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 24 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTEconomy Class Passenger Cabin Cross-Section Figure 2.12
2.50 m(8 ft 2.42 in)
0.95 m(3 ft 1.44 in)
3.35 m(10 ft 11.88 in)
2.0 m(6 ft 6.74 in)
1.41 m(4 ft 7.51 in)
0.496 m(1 ft 7.56 in)
0.56 m(1 ft 33.1 in)
0.05 m(1.96 in)
0.49 m(1 ft 7.32 in)
3.01 m(9 ft 10.5 in)
ROLL ON BAG SIZE0.56 x 0.35 x 0.25 m
(1 ft 10 in)
0.62 m(2 ft 0.40 in)
0.64 m(2 ft 1.19 in)
EM
170E
2AP
M02
0009
B.ID
R
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 25 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTEconomy Class Passenger Cabin Cross-Section Figure 2.13
EM
170E
2A
PM
020016A
.ID
R
2.52 m(8 ft 3.24 in)
0.95 m(3 ft 1.44 in)
3.35 m(10 ft 11.88 in)
2.0 m(6 ft 6.72 in)
1.42 m(4 ft 7.68 in)
0.47 m(1 ft 6.48 in)
0.56 m(1 ft 10.2 in)
0.50 m(1 ft 7.44 in)
3.01 m(9 ft 10.44 in)
ROLL ON BAG SIZE0.56 x 0.36 x 0.25 m
(1 ft 10.1 in) x (1 ft 2.16 in) x (9.84 in)
0.65 m(2 ft 1.44 in)
0.49 m(1 ft 7.32 in)
0.05 m(0.6 in)
0.6
3 m
(2 f
t 0
.6 in
)
0.55 m(1 ft 9.48 in)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 02 Page 26 of 26Rev 13 - May 10/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
3. AIRCRAFT PERFORMANCE
EFFECTIVITY: ALL
3.1. GENERAL INFORMATION
The performance of the aircraft and engine depends on the generation of forces by the interactionbetween the aircraft or engine and the air mass through which it flies. The atmosphere has apronounced effect on the temperature, pressure and density of the air.
The ICAO establishes standards to estimate and compare the aircraft and engine performance.Some ICAO standards are shown below:
1. Sea level standard day: Standard Temperature To = 15 °C (288.15 K) Standard Pressure Po = 101.3 kPa (29.92 inHg) Standard Density ρo = 0.002377 slug per cubic feet
2. ISA
Table 3.1 - ISA
ALTITUDE TEMPERATURE
m ft °C °F
0 0 15.0 59.0
305 1000 13.0 55.4
610 2000 11.0 51.9
915 3000 9.1 48.3
1220 4000 7.1 44.7
1524 5000 5.1 41.2
3049 10000 -4.8 23.3
4573 15000 -14.7 5.5
6098 20000 -24.6 -12.3
7622 25000 -34.5 -30.2
9146 30000 -44.4 -48.0
11003 36089 -56.5 -69.7
12195 40000 -56.5 -69.7
NOTE: The performance data shown in this section must not be used for operations.
NOTE: For further information about performance, refer to AOM and AFM.
Tire speed limits are not applicable to this specific aircraft.
This section provides the following information:
• The payload x range charts.
• The takeoff field length charts.
• The landing field length charts.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 1 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
NOTE: For other charts containing payload x ranges, takeoff field lengths and/or landing fieldlengths with conditions different from those presented in this section, contact Embraer to getthese charts.
3.2. PAYLOAD X RANGE
The Payload x Range charts are based on the following conditions:
• PW1919G and PW1922G engine models;
• Aircraft carrying passengers with 100 kg (220 lb) each;
• Flight level 350, that represents the cruising altitude equal to 10668 m (35000 ft);
• Atmosphere according to ISA or ISA + 10 °C conditions;
• MTOW.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 2 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTPayload x Range - ISA Conditions Figure 3.1
EM
170E
2AP
M03
0001
B.ID
R
PAYLOAD VS RANGEPW1919G, PW1922G ENGINES
FLIGHT LEVEL 370ISA
RESERVE: 100 nm ALTERNATE + 45 min FLIGHTMTOW = 56400 kg (124341 Ib)
3600016000
14000
12000
10000
8000
6000
4000
2000
00 500 1000 1500 2000 2500 3000 3500
RANGE - nm
04000
4000
8000
12000
16000
20000
24000
28000
32000
PA
YLO
AD
- k
g
PA
YLO
AD
- lb
LON
G R
AN
GE
0.78 MA
CH
MA
X C
RU
ISE
NOTES:
MAX TAKEOFF WEIGHT --------------------------- 56400 kg (124341 lb)
MAX ZERO FUEL WEIGHT------------------------ 46700 kg (102956 lb)
BASIC OPERATING WEIGHT--------------------- 33000 kg (72752 Ib)
MAX USABLE FUEL---------------------------------- 13500 kg (29760 lb)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 3 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTPayload x Range - ISA + 10 °C Conditions Figure 3.2
EM
170E
2A
PM
030002A
.ID
R
PAYLOAD VS RANGEPW1919G, PW1922G ENGINES
FLIGHT LEVEL 370ISA + 10 ˚C
RESERVE: 100 nm ALTERNATE + 45 min FLIGHTMTOW = 56400 kg (124341 Ib)
36000 16000
14000
12000
10000
8000
6000
4000
2000
00 500 1000 1500 2000 2500 3000 3500
04000
4000
8000
12000
16000
20000
24000
28000
32000
PA
YL
OA
D -
kg
PA
YL
OA
D -
lb
RANGE - nm
LO
NG
RA
NG
E
0.7
8 M
AC
H
MA
X C
RU
ISE
NOTES:
MAX TAKEOFF WEIGHT --------------------------- 56400 kg (124341 lb)
MAX ZERO FUEL WEIGHT------------------------ 46700 kg (102956 lb)
BASIC OPERATING WEIGHT--------------------- 33000 kg (72752 Ib)
MAX USABLE FUEL---------------------------------- 13500 kg (29760 lb)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 4 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTPayload x Range - ISA Conditions Figure 3.3
EM
170E
2AP
M03
0025
A.ID
R
PAYLOAD VS RANGEPW1921G, PW1923G, PW1923G-A ENGINES
FLIGHT LEVEL 370ISA
RESERVE: 100 nm ALTERNATE + 45 min FLIGHTMTOW = 61500 kg (135584 Ib)
16000
14000
12000
10000
8000
6000
4000
2000
0
PA
YLO
AD
- k
g
18000
0 500 1000 1500 2000
RANGE - nm
40002500 3000 3500
LRC
M0.78
MA
X C
RU
ISE
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 5 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTPayload x Range - ISA + 10 °C Conditions Figure 3.4
EM
170E
2A
PM
030026A
.ID
R
PAYLOAD VS RANGEPW1921G, PW1923G, PW1923G-A ENGINES
FLIGHT LEVEL 370ISA + 10 ˚C
RESERVE: 100 nm ALTERNATE + 45 min FLIGHTMTOW = 61500 kg (135584 Ib)
16000
14000
12000
10000
8000
6000
4000
2000
0
PA
YL
OA
D -
kg
18000
0 500 1000 1500 2000
RANGE - nm
40002500 3000 3500
LR
C
MA
X C
RU
ISE M0.7
8
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 6 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
3.3. TAKEOFF FIELD LENGTHS
The takeoff field lengths charts provide data about the maximum takeoff weights for compliance withthe operating regulations related to takeoff field lengths.
Data are presented according to the following associated conditions:
• PW1919G and PW1922G engine models;
• Takeoff Mode: 1;
• ATTCS MTBF positioning: ON and OFF;
• Flaps setting position: 1, 2 and 4;
• Pavement conditions: dry, hard paved and level runway surface with no obstacles;
• Zero wind and atmosphere according to ISA or ISA + 10 °C conditions;
• Pack OFF: No engine bleed extraction for air conditioning packs was considered in thetakeoff and landing charts.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 7 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTakeoff Field Lengths - ISA Conditions Figure 3.5
EM
170E
2AP
M03
0003
A.ID
R
TAKEOFF FIELD LENGTHPW1919G Engine @ T/O-1 MODE
ATTCS ON / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISANo Wind
WEIGHT (kg)
TA
KE
OF
F F
IELD
LE
NG
TH
(m
)
25000 30000 35000 40000 45000 50000 55000 60000 65000
4500
4000
3500
3000
2500
2000
1500
1000
500
1219(4000)
1829(6000)
3658(12000)
FLAP 4
FLAP 2
FLAP 1
1500
3000
4500
6000
7500
9000
10500
12000
13500
15000
TA
KE
OF
F F
IELD
LE
NG
TH
(ft)
60000 80000 100000 120000 140000
WEIGHT (lb)
4268(14000)
3048(10000)
2438(8000)
AIRPORT PRESSUREALTITUDE m (ft)
609(2000)
-570(-1870)
0
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 8 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTakeoff Field Lengths - ISA + 15 °C Conditions Figure 3.6
EM
170E
2A
PM
030004A
.ID
R
TA
KE
OF
F F
IEL
D L
EN
GT
H (
m)
4500
4000
3500
3000
2500
2000
1500
1000
500
25000 30000 35000 40000 45000 50000 55000 60000
WEIGHT (kg)
5000
5500
65000
FLAP 4
FLAP 2
FLAP 1
1500
3000
4500
6000
7500
9000
10500
12000
13500
15000
AIRPORT PRESSUREALTITUDE m (ft) 2438
(8000)
609(2000)
-570(-1870)
TA
KE
OF
F F
IEL
D L
EN
GT
H (
ft)
18000
16500
60000 80000 100000 120000 140000
WEIGHT (lb)
4268(14000) 3658
(12000)
3048(10000)
1829(6000)
1219(4000)
TAKEOFF FIELD LENGTHPW1919G Engine @ T/O-1 MODE
ATTCS ON / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISA + 15 ˚CNo Wind
0
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 9 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTakeoff Field Lengths - ISA + 20 °C Conditions Figure 3.7
EM
170E
2A
PM
030005A
.ID
R
1500
3000
4500
6000
7500
9000
10500
12000
13500
15000
TA
KE
OF
F F
IEL
D L
EN
GT
H (
ft)
60000 80000 100000 120000 140000
WEIGHT (lb)
WEIGHT (kg)
25000 30000 35000 40000 45000 50000 55000 60000 65000
4500
4000
3500
3000
2500
2000
1500
1000
500
FLAP 4
FLAP 2
FLAP 1
0
TA
KE
OF
F F
IEL
D L
EN
GT
H (
m)
AIRPORT PRESSUREALTITUDE m (ft)
4268(14000)
3658(12000)
1219(4000)
609(2000)
1829(6000)
3048(10000) 2438
(8000)
-570(-1870)
TAKEOFF FIELD LENGTHPW1919G Engine @ T/O-1 MODE
ATTCS ON / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISA + 20 ˚CNo Wind
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 10 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTakeoff Field Lengths - ISA Conditions Figure 3.8
EM
170E
2AP
M03
0006
A.ID
R
60000 80000 100000 120000 140000
WEIGHT (lb)
WEIGHT (kg)
TA
KE
OF
F F
IELD
LE
NG
TH
(m
)
25000 30000 35000 40000 45000 50000 55000 60000 65000
4500
4000
3500
3000
2500
2000
1500
1000
500
5000
1500
3000
4500
6000
7500
9000
10500
12000
13500
15000
TA
KE
OF
F F
IELD
LE
NG
TH
(ft)
17000
4268(14000) 3658
(12000)3048
(10000)
2438(8000)
1829(6000)
1219(4000)
609(2000)
-570(-1870)
AIRPORT PRESSUREALTITUDE m (ft)
0
FLAP 4
FLAP 2
FLAP 1
TAKEOFF FIELD LENGTHPW1922G Engine @ T/O-1 MODE
ATTCS OFF / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISANo Wind
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 11 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTakeoff Field Lengths - ISA + 15 °C Conditions Figure 3.9
EM
170E
2A
PM
030007A
.ID
R
4500
4000
3000
2500
2000
1500
1000
500
5000
3500
5500
WEIGHT (kg)
TA
KE
OF
F F
IEL
D L
EN
GT
H (
m)
25000 30000 35000 40000 45000 50000 55000 60000 65000
FLAP 1
FLAP 4
FLAP 2
0
1500
3000
4500
6000
7500
9000
10500
12000
13500
15000AIRPORT PRESSURE
ALTITUDE m (ft)
TA
KE
OF
F F
IEL
D L
EN
GT
H (
ft)
18000
16500
60000 80000 100000 120000 140000
WEIGHT (lb)
-570(-1870)
609(2000)
1219(4000)
1829(6000)
2438(8000)
3048(10000)
4268(14000)
3658(12000)
TAKEOFF FIELD LENGTHPW1922G Engine @ T/O-1 MODE
ATTCS OFF / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISA + 15 ˚CNo Wind
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 12 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTakeoff Field Lengths - ISA + 20 °C Conditions Figure 3.10
EM
170E
2A
PM
030008A
.ID
R
TA
KE
OF
F F
IEL
D L
EN
GT
H (
m)
1500
3000
4500
6000
7500
9000
10500
12000
13500
15000
TA
KE
OF
F F
IEL
D L
EN
GT
H (
ft)
18000
16500
60000 80000 100000 120000 140000
WEIGHT (lb)
4500
4000
3000
2500
2000
1500
1000
500
5000
3500
5500
25000 30000 35000 40000 45000 50000 55000 60000 65000
WEIGHT (kg)
FLAP 4
FLAP 2
FLAP 1
AIRPORT PRESSUREALTITUDE m (ft)
-570(-1870)
1219(4000)
2438(8000)
3048(10000)
3658(12000)
0
1829(6000)
4268(14000)
609(2000)
TAKEOFF FIELD LENGTHPW1922G Engine @ T/O-1 MODE
ATTCS OFF / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISA + 20 ˚CNo Wind
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 13 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTakeoff Field Lengths - ISA Conditions Figure 3.11
EM
170E
2AP
M03
0027
A.ID
R
500
1000
1500
2000
2500
3000
3500
4000
4500
5000
5500
6000
TA
KE
NO
FF
FIE
LD L
EN
GT
H (
m)
30000 35000 40000 45000 50000 55000 60000 65000
WEIGHT (kgf)
FLAP 4
FLAP 3
FLAP 2
FLAP 1
TAKEOFF FIELD LENGTHPW1921G ENGINE @ T/O-1 MODE
ATTCS ON / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISA 0No Wind
14000 ft
12000 ft
10000 ft
8000 ft
6000 ft
4000 ft
2000 ft
0 ft
-1870 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 14 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTakeoff Field Lengths - ISA + 15 °C Conditions Figure 3.12
EM
170E
2AP
M03
0028
A.ID
R
500
TA
KE
NO
FF
FIE
LD L
EN
GT
H (
m)
30000 35000 40000 45000 50000 55000 60000 65000
WEIGHT (kgf)
TAKEOFF FIELD LENGTHPW1921G ENGINE @ T/O-1 MODE
ATTCS ON / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISA 15No Wind
1000
1500
2000
2500
3000
3500
4000
4500
5000
5500
6000
6500
FLAP 4
FLAP 3
FLAP 2
FLAP 1
14000 ft
12000 ft
10000 ft
6000 ft
4000 ft
2000 ft
0 ft
8000 ft
-1870 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 15 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTakeoff Field Lengths - ISA Conditions Figure 3.13
EM
170E
2A
PM
030029A
.ID
R
TAKEOFF FIELD LENGTHPW1923G & PW1923GA ENGINES @ T/O-1 MODE
ATTCS ON / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISA 0NO WIND
500
1000
1500
2000
2500
3000
3500
4000
4500
5000
5500
6000
TA
KE
NO
FF
FIE
LD
LE
NG
TH
(m
)
30000 35000 40000 45000 50000 55000 60000 65000
WEIGHT (kgf)
12000 ft
10000 ft
8000 ft
6000 ft
4000 ft
0 ft
-1870 ft
2000 ft
FLAP 4
FLAP 3
FLAP 2
FLAP 1
14000 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 16 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTakeoff Field Lengths - ISA + 15 °C Conditions Figure 3.14
EM
170E
2AP
M03
0030
A.ID
R
500
TA
KE
NO
FF
FIE
LD L
EN
GT
H (
m)
30000 35000 40000 45000 50000 55000 60000 65000
WEIGHT (kgf)
TAKEOFF FIELD LENGTHPW1921G ENGINE @ T/O-1 MODE
ATTCS ON / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY
ISA 15No Wind
1000
1500
2000
2500
3000
3500
4000
4500
5000
5500
6000
6500
FLAP 4
FLAP 3
FLAP 2
FLAP 114000 ft
12000 ft
10000 ft
8000 ft
6000 ft
4000 ft
2000 ft
0 ft-1870 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 17 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
3.4. LANDING FIELDS LENGTHS
The landing field lengths charts provide data about the maximum landing weights for compliancewith the operating regulations related to landing field lengths.
Data is presented according to the following associated conditions:
• Landing gear: down;
• Flaps setting position: 5 or full;
• Pavement conditions: dry, hard paved and level runway surface with no obstacles;
• Zero wind and atmosphere according to ISA conditions;
• Pack OFF: No engine bleed extraction for air conditioning packs was considered in thetakeoff and landing charts.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 18 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap 5 - ISA Conditions Figure 3.15
LANDING FIELD LENGTHPW1919G ENGINE
DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP 5
ISA
1000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
0 ft
12000 ft
14000 ft
10000 ft
8000 ft
6000 ft
4000 ft
2000 ft
-1870 ft
28000 32000 36000 44000 48000 52000 56000 60000 6400040000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
WEIGHT - kg
4000
5000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
ft
6000
7000
8000
9000
10000
11000
12000
70000 80000 100000 110000 13000090000 120000 140000
AIRPORT PRESSUREALTITUDE m (ft)
WEIGHT - lb
3000
60000
EM
170E
2AP
M03
0009
A.ID
R
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 19 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap 5 - ISA + 15 °C Conditions Figure 3.16
EM
170E
2A
PM
030010A
.ID
R
28000 32000 36000 44000 48000 52000 56000 60000 6400040000
70000 80000 100000 110000 13000090000 120000 140000
1000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
4000
5000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
ft
6000
7000
8000
9000
10000
11000
12000
AIRPORT PRESSUREALTITUDE m (ft)
12000 ft
14000 ft
10000 ft
8000 ft
6000 ft
0 ft
2000 ft
4000 ft
-1870 ft
3000
60000
WEIGHT - lb
LANDING FIELD LENGTHPW1919G ENGINE
DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP 5
ISA + 15˚C
WEIGHT - kg
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 20 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap Full - ISA Conditions Figure 3.17
EM
170E
2AP
M03
0011
A.ID
R
28000 32000 36000 44000 48000 52000 56000 60000 6400040000
70000 80000 100000 110000 13000090000 120000 140000
1000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
4000
5000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
ft
6000
7000
8000
9000
10000
11000
12000
0 ft
2000 ft
4000 ft
6000 ft
8000 ft
10000 ft
12000 ft
14000 ft
-1870 ft
AIRPORT PRESSUREALTITUDE m (ft)
3000
60000
LANDING FIELD LENGTHPW1919G ENGINE
DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP FULL
ISA
WEIGHT - kg
WEIGHT - lb
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 21 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap Full - ISA + 15 °C Conditions Figure 3.18
EM
170E
2A
PM
030012A
.ID
R
28000 32000 36000 44000 48000 52000 56000 60000 6400040000
70000 80000 100000 110000 13000090000 120000 140000
1000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
4000
5000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
ft
6000
7000
8000
9000
10000
11000
12000
AIRPORT PRESSUREALTITUDE m (ft)
0 ft
2000 ft
4000 ft
6000 ft
8000 ft
10000 ft
12000 ft
14000 ft
-1870 ft
3000
60000
LANDING FIELD LENGTHPW1919G ENGINE
DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP FULLISA + 15˚C
WEIGHT - kg
WEIGHT - lb
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 22 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap 5 - ISA Conditions Figure 3.19
EM
170E
2AP
M03
0013
A.ID
R
28000 32000 36000 44000 48000 52000 56000 60000 6400040000
70000 80000 100000 110000 13000090000 120000 140000
1000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
4000
5000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
ft
6000
7000
8000
9000
10000
11000
12000
12000 ft
14000 ft
10000 ft
8000 ft
6000 ft
0 ft
2000 ft
4000 ft
-1870 ft
AIRPORT PRESSUREALTITUDE m (ft)
3000
60000
LANDING FIELD LENGTHPW1922G ENGINE
DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP 5
ISA
WEIGHT - kg
WEIGHT - lb
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 23 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap 5 - ISA + 15 °C Conditions Figure 3.20
EM
170E
2A
PM
030014A
.ID
R
28000 32000 36000 44000 48000 52000 56000 60000 6400040000
70000 80000 100000 110000 13000090000 120000 140000
1000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
4000
5000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
ft
6000
7000
8000
9000
10000
11000
12000
AIRPORT PRESSUREALTITUDE m (ft)
12000 ft
14000 ft
10000 ft
8000 ft
6000 ft
0 ft
2000 ft
4000 ft
-1870 ft
3000
60000
WEIGHT - lb
LANDING FIELD LENGTHPW1922G ENGINE
DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP 5
ISA + 15˚C
WEIGHT - kg
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 24 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap Full - ISA Conditions Figure 3.21
EM
170E
2AP
M03
0015
A.ID
R
28000 32000 36000 44000 48000 52000 56000 60000 6400040000
70000 80000 100000 110000 13000090000 120000 140000
1000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
4000
5000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
ft
6000
7000
8000
9000
10000
11000
12000
AIRPORT PRESSUREALTITUDE m (ft)
12000 ft
14000 ft
10000 ft
8000 ft
6000 ft
0 ft
2000 ft
4000 ft
-1870 ft
3000
60000
LANDING FIELD LENGTHPW1922G ENGINE
DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP FULL
ISA
WEIGHT - kg
WEIGHT - lb
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 25 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap Full - ISA + 15 °C Conditions Figure 3.22
28000 32000 36000 44000 48000 52000 56000 60000 6400040000
70000 80000 100000 110000 13000090000 120000 140000
1000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
4000
5000
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
ft
6000
7000
8000
9000
10000
11000
12000
12000 ft
14000 ft
10000 ft
8000 ft
6000 ft
0 ft
2000 ft
4000 ft
-1870 ft
AIRPORT PRESSUREALTITUDE m (ft)
3000
60000
EM
170E
2A
PM
030016A
.ID
R
LANDING FIELD LENGTHPW1922G ENGINE
DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP FULLISA + 15˚C
WEIGHT - kg
WEIGHT - lb
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 26 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Field Lengths - Flap 5 - ISA Conditions Figure 3.23
EM
170E
2AP
M03
0020
A.ID
R
LANDING FIELD LENGTHENGINE MODEL PW1921G
FLAP 5ISA 0
SURFACE TYPE NORMALRUNWAY CONDITION DRY
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
MAXIMUM LANDING WEIGHT - kg
32000 36000 40000 44000 48000 52000 56000 60000 640001000
1600
1200
1400
1800
2000
2200
2400
3000
2800
2600
Hp 4000 ft
Hp 2000 ft
Hp 0 ft
Hp -1870 ft
Hp 6000 ft
Hp 8000 ft
Hp 10000 ft
Hp 12000 ft
Hp 14000 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 27 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Field Lengths - Flap 5 - ISA + 15 °C Conditions Figure 3.24
EM
170E
2A
PM
030019A
.ID
R
LANDING FIELD LENGTHENGINE MODEL PW1921G
FLAP 5ISA + 15˚C
SURFACE TYPE NORMALRUNWAY CONDITION DRY
1000
1200
1400
1600
1800
2000
2200
2400
2600
2800
3000
MAXIMUM LANDING WEIGHT - kg
32000 36000 40000 44000 48000 52000 56000 6400060000
Hp 10000 ft
Hp 4000 ft
Hp 14000 ft
Hp 12000 ft
Hp 8000 ft
Hp 6000 ft
Hp 2000 ft
Hp 0 ft
Hp -1870 ft
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 28 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Field Lengths - Flap Full - ISA Conditions Figure 3.25
EM
170E
2AP
M03
0018
A.ID
R
1000
1200
1400
1600
1800
2000
2200
2400
2600
2800
3000
32000 36000 40000 44000 48000 52000 56000 6400060000
Hp -1870 ft
Hp 14000 ft
Hp 12000 ft
Hp 10000 ft
Hp 6000 ft
HP 8000 ft
Hp 4000 ft
Hp 2000 ft
Hp 0 ft
LANDING FIELD LENGTHENGINE MODEL PW1921G
FLAP FULLISA 0
SURFACE TYPE NORMALRUNWAY CONDITION DRY
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
MAXIMUM LANDING WEIGHT - kg
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 29 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Field Lengths - Flap Full - ISA + 15 °C Conditions Figure 3.26
EM
170E
2A
PM
030017A
.ID
R
LANDING FIELD LENGTHENGINE MODEL PW1921G
FLAP FULLISA + 15˚C
SURFACE TYPE NORMALRUNWAY CONDITION DRY
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E
- m
1000
1200
1400
1600
1800
2000
2200
2400
2600
2800
3000
MAXIMUM LANDING WEIGHT - kg
32000 36000 40000 44000 48000 52000 56000 6400060000
Hp 14000 ft
Hp 12000 ft
Hp 10000 ft
Hp 8000 ft
Hp 6000 ft
Hp 4000 ft
Hp 2000 ft
Hp -1870 ft
Hp 0 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 30 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Field Lengths - Flap 5 - ISA Conditions Figure 3.27
EM
170E
2AP
M03
0024
A.ID
R
32000 36000 40000 44000 48000 52000 56000 60000 640001000
1200
1400
1600
1800
2000
2200
2400
2600
2800
3000
MAXIMUM LANDING WEIGHT - kg
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
LANDING FIELD LENGTHENGINE MODEL PW1923G AND PW1923G-A
FLAP 5ISA 0
SURFACE TYPE NORMALRUNWAY CONDITION DRY
Hp 14000 ft
Hp 12000 ft
Hp 10000 ft
Hp 8000 ft
Hp 6000 ft
Hp 4000 ft
Hp 2000 ft
Hp 0 ft
Hp -1870 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 31 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Field Lengths - Flap 5 - ISA + 15 °C Conditions Figure 3.28
EM
170E
2A
PM
030023A
.ID
R
32000 36000 40000 44000 48000 52000 56000 60000 640001000
1200
1400
1600
1800
2000
2200
2400
2600
2800
3000
MAXIMUM LANDING WEIGHT - kg
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
LANDING FIELD LENGTHENGINE MODEL PW1923G AND PW1923G-A
FLAP 5ISA + 15˚C
SURFACE TYPE NORMALRUNWAY CONDITION DRY
Hp 14000 ft
Hp 12000 ft
Hp 10000 ft
Hp 8000 ft
Hp 6000 ft
Hp 4000 ft
Hp 2000 ft
Hp 0 ft
Hp -1870 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 32 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Field Lengths - Flap Full - ISA Conditions Figure 3.29
EM
170E
2AP
M03
0022
A.ID
R
32000 36000 40000 44000 48000 52000 56000 60000 640001000
1200
1400
1600
1800
2000
2200
2400
2600
2800
3000
MAXIMUM LANDING WEIGHT - kg
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
LANDING FIELD LENGTHENGINE MODEL PW1923G AND PW1923G-A
FLAP FULLISA 0
SURFACE TYPE NORMALRUNWAY CONDITION DRY
Hp 14000 ft
Hp 12000 ft
Hp 10000 ft
Hp 8000 ft
Hp 6000 ft
Hp 4000 ft
Hp 2000 ft
Hp 0 ft
Hp -1870 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 33 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Field Lengths - Flap Full - ISA + 15 °C Conditions Figure 3.30
EM
170E
2A
PM
030021A
.ID
R
32000 36000 40000 44000 48000 52000 56000 60000 640001000
1200
1400
1600
1800
2000
2200
2400
2600
2800
3000
MAXIMUM LANDING WEIGHT - kg
FA
CT
OR
ED
LA
ND
ING
DIS
TA
NC
E -
m
LANDING FIELD LENGTHENGINE MODEL PW1923G AND PW1923G-A
FLAP FULLISA + 15˚C
SURFACE TYPE NORMALRUNWAY CONDITION DRY
Hp 14000 ft
Hp 12000 ft
Hp 10000 ft
Hp 8000 ft
Hp 6000 ft
Hp 4000 ft
Hp 2000 ft
Hp 0 ft
Hp -1870 ft
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 03 Page 34 of 34Rev 12 - Feb 08/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
4. GROUND MANEUVERING
EFFECTIVITY: ALL
4.1. GENERAL INFORMATION
This section provides the aircraft turning capability and maneuvering characteristics. To facilitate thepresentation, the data was determined from theoretical limits imposed by the geometry of the aircraft.
As such, it reflects the turning capability of the aircraft in favorable operating circumstances. Thisdata should be used only as guideline for the method of determining such parameters and for themaneuvering characteristics of the aircraft.
In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted, to avoid excessive tire wear and reduce possible maintenance problems.
Variations from standard aircraft operating patterns may be necessary to satisfy physical constantswithin the maneuvering area, such as adverse grades, limited area, or high risk of jet blast damage.For these reasons, the ground maneuvering requirements should be coordinated with the usingairline prior to the layout planning.
This section is presented as follows:
• The turning radii for nose landing gear steering angles.
• The pilot's visibility from the cockpit and the limits of ambinocular vision through thewindows. Ambinocular vision is defined as the total field of vision seen by both eyes at thesame time.
• The performance of the aircraft on runway-to-taxiway, taxiway-to-taxiway and runwayholding bays dimensions.
4.2. TURNING RADII
This subsection presents the following information:
• The turning radii for various nose landing gear steering angles. The minimum turning radiusis determined considering that the maximum nose landing gear steering angle is 76 degreesleft and right.
• Data on the minimum width of the pavement for a 180° turn.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 1 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTTurning Radii - No Slip Angle Figure 4.1
EM
170E
2AP
M04
0001
B.ID
R
NOTE:DATA PRESENTED IS BASED ON THEORETICAL CALCULATIONS.ACTUAL OPERATING DATA MAY BE GREATER THAN SHOWN SINCETIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS.
35˚
40˚
45˚
50˚
55˚
60˚
65˚
70˚
76˚
25.30 m
23.20 m
21.60 m
20.42 m
19.53 m
18.53 m
18.33 m
17.94 m
17.61 m
76 ft 11 in
70 ft 87 in
67 ft
64 ft 08 in
61 ft 84 in
58 ft 86 in
57 ft 77 in
83 ft
60 ft 13 in
74 ft 21 in 22.26 m
19.24 m
16.80 m
14.74 m
13.00 m
11.40 m
9.98 m
8.67 m
7.20 m
73 ft 03 in
48 ft 36 in
42 ft 65 in
28 ft 44 in
23 ft 62 in
63 ft 12 in
55 ft 12 in
37 ft 74 in
32 ft 11 in
14.23 m
11.21 m
8.80 m
6.70 m
4.93 m
3.36 m
1.94 m
0.63 m
0.83 m
46 ft 70 in
22 ft
2 ft 07 in
36 ft 77 in
28 ft 87 in
16 ft 17 in11 ft 02 in
6 ft 36 in
35.47 m
32.49 m
30.07 m
28.05 m
26.30 m
24.76 m
23.38 m
22.10 m
20.68 m
106 ft 60 in
98 ft 65 in
92 ft 03 in
86 ft 30 in
81 ft 23 in
72 ft 50 in
67 ft 85 in
116 ft 37 in
76 ft 70 in
29.64 m
27.33 m
25.57 m
24.19 m
23.08 m
22.16 m
21.40 m
20.76 m
20.13 m
79 ft 36 in
83 ft 90 in
75 ft 72 in
72 ft 70 in
70 ft 21 in
97 ft 24 in
89 ft 66 in
68 ft 11 in
66 ft 04 in
STEERINGSTEEL
NOSE
R1
NOSE GEAR
R2
OUTBOARD GEAR
R3
INBOARD GEAR
R4 R5
RIGHT TAILTIP
R6
RIGHT WINGLET
22.62 m
20.22 m
18.42 m
17.03 m
15.94 m
15.10 m
14.44 m
13.94 m
13.52 m
66 ft 34 in
60 ft 43 in
55 ft 87 in
52 ft 30 in
49 ft 54 in
45 ft 73 in
44 ft 35 in
47 ft 37 in
2 ft 72 in
STEERING ANGLE
(RUNWAY MINIMUM WIDTH)
R1R3
R4
R4
R6
FRONT VIEWSCALE: 1:100
R2
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 2 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
4.3. MINIMUM TURNING RADII
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 3 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTMinimum Turning Radius Figure 4.2
EM
170E
2AP
M04
0002
B.ID
R
ACTUAL OPERATING DATA MAY BE GREATER THAN VALUES SHOWNSINCE TIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS.
NOTE:
76˚ 17.61 m 57 ft 77 in 44 ft 35 in 7.20 m 23 ft 62 in 0.83 m 2 ft 72 in 20.68 m 67 ft 85 in 20.13 m 66 ft 04 in
STEERINGSTEEL
NOSE
R1
NOSE GEAR
R2
OUTBOARD GEAR
R3
INBOARD GEAR
R4 R5
RIGHT TAILTIP
R6
RIGHT WINGLET
13.52 m
FRONT VIEWSCALE: 1:100
R1
R2
R3
R6
R4
(RUNWAY MINIMUM WIDTH)
R4
STEERING ANGLE
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 4 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTTurning Radii - No Slip Angle Figure 4.3
EM
170E
2AP
M04
0010
A.ID
RNOTE:DATA PRESENTED IS BASED ON THEORETICAL CALCULATIONS.ACTUAL OPERATING DATA MAY BE GREATER THAN SHOWN SINCETIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS.
35˚
40˚
45˚
50˚
55˚
60˚
65˚
70˚
76˚
30.62 m
27.91 m
25.91 m
24.40 m
23.26 m
22.39 m
21.71 m
21.21 m
20.78 m
91 ft 6.8 in
85 ft 0.1 in
80 ft 0.6 in
76 ft 3.7 in
73 ft 5.5 in
69 ft 7.0 in
68 ft 2.1 in
100 ft 5.5 in
71 ft 2.7 in
91 ft 10.0 in 26.63 m
22.89 m
19.85 m
17.30 m
15.10 m
13.15 m
11.39 m
9.76 m
7.95 m
87 ft 4.4 in
56 ft 9.1 in
49 ft 6.5 in
32 ft 0.3 in
26 ft 1.0 in
75 ft 1.2 in
65 ft 1.5 in
43 ft 1.7 in
37 ft 4.4 in
18.65 m
14.90 m
11.86 m
9.31 m
7.11 m
5.16 m
3.40 m
1.77 m
0.04 m
61 ft 2.3 in
30 ft 6.5 in
5 ft 9.7 in
48 ft 10.6 in
38 ft 10.9 in
23 ft 3.9 in16 ft 11.1 in
11 ft 1.9 in
40.48 m
36.76 m
33.74 m
31.22 m
29.05 m
27.13 m
25.39 m
23.80 m
22.02 m
120 ft 7.2 in
110 ft 8.3 in
102 ft 5.1 in
95 ft 3.7 in
89 ft 0.1 in
78 ft 1.0 in
72 ft 2.9 in
132 ft 9.7 in
83 ft 3.6 in
34.46 m
31.53 m
29.30 m
27.54 m
26.12 m
24.97 m
24.02 m
23.22 m
22.44 m
90 ft 4.3 in
96 ft 1.5 in
85 ft 8.3 in
81 ft 11.1 in
78 ft 9.7 in
113 ft 0.7 in
103 ft 5.3 in
76 ft 2.2 in
73 ft 7.5 in
STEERINGSTEEL
NOSE
R1
NOSE GEAR
R2
OUTBOARD GEAR
R3
INBOARD GEAR
R4 R5
RIGHT TAIL TIP
R6
RIGHT WINGLET
27.99 m
25.01 m
22.77 m
21.04 m
10.70 m
18.65 m
17.84 m
17.22 m
16.69 m
82 ft 0.6 in
74 ft 8.5 in
69 ft 0.3 in
35 ft 1.3 in
61 ft 2.3 in
56 ft 6.0 in
54 ft 9.1 in
58 ft 6.4 in
0 ft 1.6 in
R3
R6
R5
R4
R2
R1
STEERING ANGLE
(RUNWAY MINIMUM WIDTH)
FRONT VIEWSCALE: 1:110
54.62 m
38.34 m
34.80 m
31.80 m
29.22 m
26.98 m
24.63 m
125 ft 9.4 in
139 ft 9.6 in
114 ft 2.1 in
104 ft 4.0 in
95 ft 10.4 in
179 ft 2.4 in
88 ft 6.2 in
80 ft 9.7 in
RUNWAY WIDTH
47.90 m
42.61 m
157 ft 1.8 in
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 5 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTMinimum Turning Radius Figure 4.4
EM
170E
2AP
M04
0011
A.ID
R
R3
R6
R5
R4
R2
R1
FRONT VIEWSCALE: 1:110
76˚ 20.78 m 68 ft 2.1 in 7.95 m 26 ft 1.0 in 0.04 m 22.02 m 72 ft 2.9 in 22.44 m 73 ft 7.5 in
STEERINGSTEEL
NOSE
R1
NOSE GEAR
R2
OUTBOARD GEAR
R3
INBOARD GEAR
R4 R5
RIGHT TAIL TIP
R6
RIGHT WINGLET
16.69 m 54 ft 9.1 in 0 ft 1.6 in 24.63 m 80 ft 9.7 in
RUNWAY WIDTH
(RUNWAY MINIMUM WIDTH)
STEERING ANGLE
ACTUAL OPERATING DATA MAY BE GREATER THAN VALUES SHOWNSINCE TIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS.
NOTE:
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 6 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
4.4. VISIBILITY FROM COCKPIT
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 7 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLVisibility from Cockpit in Static Position Figure 4.5
EM
170E
2A
PM
040003B
.ID
R
REF. GROUND (BOW)
PILOT'S EYE POSITIONMAXIMUM AFT VISIONWITH HEAD ROTATEDABOUT SPINAL COLUMN
VISUAL ANGLE IN PLANEPERPENDICULAR TO LONGITUDINALAXIS THROUGH PILOT'S EYE POSITION
120˚
24.6˚
0.53 m(1 ft 9 in.)
0.53 m(1 ft 9 in.)
15.1˚
0.75 m(2 ft 6 in.)
15.52 m(50 ft 11 in.)
23.8˚3.91 m(12 ft 10 in.)
2.84 m(9 ft 3.8 in.)
PILOT'S EYE POSITION
PILOT'S EYE POSITION
VISUAL ANGLE IN PLANEPARALLEL TO LONGITUDINALAXIS THROUGH PILOT'S EYEPOSITION
25.8˚
L FUS HORC
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 8 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
4.5. RUNWAY AND TAXIWAY DIMENSIONS
To determine the minimum dimensions for runway and taxiway where the aircraft can be operated,the reference code of the aircraft must be determined.
The reference code of a specific aircraft is obtained in accordance with the Aerodrome Design andOperations - Volume 1, by the ICAO.
The code is composed of two elements which are related to the aircraft performance characteristicsand dimensions:
• Element 1 is a number based on the aircraft reference field length;
• Element 2 is a letter based on the aircraft wingspan and outer main landing gear wheel span.
The table below shows the reference codes:
Table 4.1 - Reference Codes
CODE ELEMENT 1 CODE ELEMENT 2
CODENUM-BER
AIRCRAFT REFERENCEFIELD LENGTH
CODELETTER
WING SPANOUTER MAIN LAND-ING GEAR WHEEL
SPAN
1less than 800 m
(2624 ft 8 in)A
Up to 15 m(49 ft 3 in)
Up to 4.5 m(14 ft 9 in)
2800 m (2624 ft 8 in) up to
1200 m (3937 ft)B
15 m (49 ft 3 in) to24 m (78 ft 9 in)
4.5 m (14 ft 9 in) to6 m (19 ft 8 in)
31200 m (3937 ft) up to1800 m (5905 ft 6 in)
C24 m (78 ft 9 in) to36 m (118 ft 1 in)
6 m (19 ft 8 in) to9 m (29 ft 6 in)
41800 m
(5905 ft 6 in) and overD
36 m (118 ft 1 in) to52 m (170 ft 7 in)
9 m (29 ft 6 in) to14 m (45 ft 11 in)
5 _ E52 m (170 ft 7 in) to
65 m (213 ft 3 in)9 m (29 ft 6 in) to14 m (45 ft 11 in)
In accordance with the table, the reference code for the EMBRAER 190-300 and 190-400 models is3C.
With the reference code, it is possible to obtain the limits of the runway and taxiway where theaircraft can be operated. For reference code 3C the limits are:
• The width of a runway should not be less than 30 m (98 ft 5 in);
• The width of a taxiway should not be less than 15 m (49 ft 2 in);
• The design of the curve in a taxiway should be such that, when the cockpit is on the taxiwaycenterline marking, the clearance distance between the outer main landing gear wheels ofthe aircraft and the edge of the taxiway should not be less than 3 m (9 ft 10 in);
• The clearance between a parked aircraft and one moving along the taxiway in a holding bayshould not be less than 15 m (49 ft 2 in).
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 9 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLMore than 90° Turn - Runway to Taxiway Figure 4.6
EM
170E
2AP
M04
0004
A.ID
R
COORDINATE WITH AIRLINE OPERATORFOR THE SPECIFIC PLANNED OPERATINGPROCEDURE.
45˚
100 ft RADIUS(30 m)
NOTE:
PATH OF MAIN LANDINGGEAR TIRE EDGE
NOSE LANDING GEAR STEERING ANGLE ISAPPROXIMATELY 15.
15 m(49 ft 2 in.)
45 m(147 ft 7.6 in.)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 10 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALL90° Turn - Runway to Taxiway Figure 4.7
EM
170E
2AP
M04
0005
A.ID
R
COORDINATE WITH AIRLINE OPERATORFOR THE SPECIFIC PLANNED OPERATINGPROCEDURE.
100 ft RADIUS(30 m)
100 ft RADIUS(147 ft 7.6 in.)
NOTE:
PATH OF MAIN LANDINGGEAR TIRE EDGE.
NOSE LANDING GEAR STEERING ANGLE ISAPPROXIMATELY 30.
15 m(49 ft 2 in.)
90˚
45 m(147 ft 7.6 in.)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 11 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALL90° Turn - Taxiway to Taxiway Figure 4.8
EM
170E
2A
PM
040006A
.ID
R
COORDINATE WITH AIRLINE OPERATORFOR THE SPECIFIC PLANNED OPERATINGPROCEDURE.
NOTE:
NOSE LANDING GEAR STEERING ANGLE ISAPPROXIMATELY 28.
15 m(49 ft 2 in.)
15 m(49 ft 2 in.)
100 ft RADIUS(30 m)
90˚
PATH OF MAIN LANDINGGEAR TIRE EDGE.
3 m(9 ft 10 in.)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 12 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
4.6. RUNWAY HOLDING APRON
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 13 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLRunway Holding Bay Figure 4.9
EM
170E
2AP
M04
0007
A.ID
R
75 m(246 ft)
PATH OF MAIN LANDINGGEAR TIRE EDGE.
MINIMUMCLEARENCES
15 m(49 ft 2 in.)
3 m(9 ft 10 in.)
3 m(9 ft 10 in.)
15 m(49 ft 2 in.)
RUNWAY
TAXIWAY
45 m(147 ft 7.6 in.)PATH OF MAIN LANDING
GEAR TIRE EDGE.
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 04 Page 14 of 14Rev 14 - Aug 09/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
5. TERMINAL SERVICING
EFFECTIVITY: ALL
5.1. GENERAL INFORMATION
During turnaround at the air terminal, certain services must be performed on the aircraft, usuallywithin a given time to meet flight schedules. This section shows service vehicle arrangements,schedules, locations of servicing points, and typical servicing requirements. The data presentedherein reflects ideal conditions for a single aircraft. Servicing requirements may vary according to theaircraft condition and airline operational (servicing) procedures.
This section provides the following information:
• The typical arrangements of equipment during turnaround;
• The typical turnaround servicing time at an air terminal;
• The locations of ground servicing connections in graphic and tabular forms;
• The typical sea level air pressure and flow requirements for starting the engine;
• The air conditioning requirements;
• The ground towing requirements for various towing conditions. Towbar pull and total tractionwheel load may be determined by considering aircraft weight, pavement slope, coefficient offriction, and engine idle thrust.
5.2. AIRCRAFT SERVICING ARRANGEMENT
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 05 Page 1 of 20Rev 11 - Nov 09/18
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLAircraft Servicing Arrangement With Passenger Stairs Figure 5.1
EM
170E
2A
PM
050001A
.ID
R
5 - GALLEY SERVICE ADJUSTABLE RAMP
RAMP (REF)SERVICING ARRANGEMENT
2 - PASSENGER STAIR3 - BAGGAGE LOADER4 - BAGGAGE CARGO5 - GALLEY SERVICE ADJUSTABLE RAMP6 - FUEL SERVICE7 - POTABLE WATER
8 - LAVATORY SERVICE9 - CLEANING SERVICE
10 - GPU (GROUND POWER UNIT)
FOR SAFE OPERATION, KEEP A MINUMUM DISTANCE OF 0.80 m (2.62 ft)
LE
NG
HT
- (
FT
)
LE
NG
HT
- (
M)
LENGHT - (FT)
LENGHT - (M)
10
5 5
7
9
2 2
4
6
4
83
3
0 30 60 90 120 150
120
90
60
30
0 00
10 15 20 25 30 35 40 45 505
10
20
15
25
30
40
35
5
1.82 m(5.97 ft)
1
1
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLAircraft Servicing Arrangement With Passenger Bridge (Galley Service Adjustable Ramp) Figure 5.2
EM
170E
2A
PM
050002A
.ID
R
5 - GALLEY SERVICE ADJUSTABLE RAMP
RAMP (REF)
LE
NG
HT
- (
FT
)
LE
NG
HT
- (
M)
LENGHT - (FT)
LENGHT - (M)
10
5 5
7
9
12
4
6
4
83
3
0 30 60 90 120 150
120
90
60
30
0 00
10 15 20 25 30 35 40 45 505
10
20
15
25
30
40
35
5
SERVICING ARRANGEMENT
2 - PASSENGER STAIR3 - BAGGAGE LOADER4 - BAGGAGE CARGO5 - GALLEY SERVICE ADJUSTABLE RAMP6 - FUEL SERVICE7 - POTABLE WATER
8 - LAVATORY SERVICE9 - CLEANING SERVICE
10 - GPU (GROUND POWER UNIT)
1 - PASSENGER BRIDGE
FOR SAFE OPERATION, KEEP A MINUMUM DISTANCE OF 0.80 m (2.62 ft)1
1
1.82 m(5.97 ft)
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLAircraft Servicing Arrangement With Passenger Bridge (Galley Service Adjustable Left Ramp) Figure 5.3
EM
170E
2A
PM
050010A
.ID
R
LE
NG
HT
- (
FT
)
LE
NG
HT
- (
M)
LENGHT - (FT)
LENGHT - (M)
10
11 11
7
9
12
4
6
4
83
3
0 30 60 90 120 150
120
90
60
30
0 00
10 15 20 25 30 35 40 45 505
10
20
15
25
30
40
35
5
SERVICING ARRANGEMENT
2 - PASSENGER STAIR3 - BAGGAGE LOADER4 - BAGGAGE CARGO6 - FUEL SERVICE7 - POTABLE WATER
8 - LAVATORY SERVICE9 - CLEANING SERVICE
10 - GPU (GROUND POWER UNIT)
1 - PASSENGER BRIDGE
11 - GALLEY SERVICE ADJUSTABLE LEFT RAMP11 - GALLEY SERVICE LEFT RAMP
RAMP (REF)
1
1.82 m(5.97 ft)
FOR SAFE OPERATION, KEEP A MINUMUM DISTANCE OF 0.80 m (2.62 ft)1
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLAircraft Servicing Arrangement With Passenger Bridge (Galley Service Adjustable Right Ramp) Figure 5.4
EM
170E
2A
PM
050011A
.ID
R
LE
NG
HT
- (
FT
)
LE
NG
HT
- (
M)
LENGHT - (FT)
LENGHT - (M)
10
1212
7
9
12
4
6
4
83
3
0 30 60 90 120 150
120
90
60
30
0 00
10 15 20 25 30 35 40 45 505
10
20
15
25
30
40
35
5
1.82 m(5.97 ft)
FOR SAFE OPERATION, KEEP A MINUMUM DISTANCE OF 0.80 m (2.62 ft)1
1
SERVICING ARRANGEMENT
2 - PASSENGER STAIR3 - BAGGAGE LOADER4 - BAGGAGE CARGO
1 - PASSENGER BRIDGE
6 - FUEL SERVICE7 - POTABLE WATER
8 - LAVATORY SERVICE9 - CLEANING SERVICE
10 - GPU (GROUND POWER UNIT)12 - GALLEY SERVICE ADJUSTABLE RIGHT RAMP 12 - GALLEY SERVICE
RIGHT RAMP
RAMP (REF)
AIRPORTPLANNING MANUAL
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
5.3. TERMINAL OPERATIONS - TURNAROUND STATION
This section presents the typical turnaround servicing time at an air terminal. The chart gives typicalschedules for performing servicing on the aircraft within a given time.
The time of each service in the chart was calculated taking the following into consideration:
• Load factor - 100%;
• Passenger deplane - 24 pax/min;
• Passenger enplane - 16 pax/min;
• Baggages checked per passenger - 1,2;
• Refuel (fuel quantity) - 80%;
• Flow - 290 gpm;
• Potable water - 70% to be refilled (56 ℓ);
• Galley service FWD and aft sequence - in parallel;
• Toilet type - vacuum;
• Baggages unloading/loading FWD/aft sequence - in parallel;
• Only FWD passenger door to be used to deplane and enplane passengers.
Servicing times can be rearranged to suit availability of personnel, aircraft configuration, and degreeof servicing required.
The data illustrates the general scope and tasks involving airport terminal operations. Airline-specificpractices and operating experience will result in different sequences and intervals.
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EFFECTIVITY: EMBRAER 190-E2 ACFTAir Terminal Operation - Turnaround Station Figure 5.5
EM
170E
2AP
M05
0003
A.ID
R
min.
5
OPERATIONS
ELAPSED TIME(MINUTES)
FWD BAGGAGE/CARGO LOAD
AIRCRAFTSERVICING
FUEL SERVICE
POTABLE WATER SERVICE
TOILET SERVICE
1 3 7 9 11 13 17 19
GALLEY SERVICING-AFT
AFT BAGGAGE/CARGO LOAD
PAXSERVICES
1,0
GALLEY SERVICING-FWD
PASSENGERS DEPLANE 4.1
AIRPLANE INTERIOR SERVICES
PASSENGERS ENPLANE
6.1
6.1
BRIDGE / STAIRS REMOVAL 1,0
2,0PUSH BACK / ENGINES START
2 4 8 10 126 141516 18 20
FWD BAGGAGE / CARGO UNLOAD
REAR BAGGAGE / CARGO UNLOAD
TIME BETWEEN UNLOADING / LOADINGBAGGAGE& CARGO
5,0
3,0
11.7
5.8
7.1
0,5
3.5
4.3
7,0
7,0
BRIDGE / STAIRS POSITIONING
NOTE:THIS DATA ILUSTRATES THE GENERAL SCOPE AND TASKS INVOLVINGAIRPORT TERMINAL OPERATIONS.AIRLINE PARTICULAR PRACTICES AND OPERATING EXPERIENCE WILLRESULT IN DIFFERENT SEQUENCES AND INTERVALS.
LEGEND:
TRUCK POSITIONING/REMOVAL/SETTINGS
AIRPORTPLANNING MANUAL
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTAir Terminal Operation - Turnaround Station Figure 5.6
EM
170E
2A
PM
050012A
.ID
R
min.
5
OPERATIONS
ELAPSED TIME(MINUTES)
FWD BAGGAGE / CARGO LOAD
AIRCRAFTSERVICING
FUEL SERVICE
POTABLE WATER SERVICE
TOILET SERVICE
1 3 7 9 11 13 17 19
GALLEY SERVICING-AFT
AFT BAGGAGE / CARGO LOAD
PAXSERVICES
1.0
GALLEY SERVICING-FWD
PASSENGERS DEPLANE 5.6
AIRPLANE INTERIOR SERVICES
PASSENGERS ENPLANE
6.1
7.5
BRIDGE / STAIRS REMOVAL 1.0
2.0PUSH BACK / ENGINES START
2 4 8 10 126 141516 18 20
FWD BAGGAGE / CARGO UNLOAD
REAR BAGGAGE / CARGO UNLOAD
TIME BETWEEN UNLOADING / LOADINGBAGGAGE& CARGO
5.0
3.0
11.7
8.0
8.5
0.5
5.0
5.2
7.0
7.0
BRIDGE / STAIRS POSITIONING
NOTE:THIS DATA ILLUSTRATES THE GENERAL SCOPE AND TASKS INVOLVING
AIRPORT TERMINAL OPERATIONS.
AIRLINE PARTICULAR PRACTICES AND OPERATING EXPERIENCE WILL
RESULT IN DIFFERENT SEQUENCES AND INTERVALS.
LEGEND:
TRUCK POSITIONING / REMOVAL / SETTINGS
AIRPORTPLANNING MANUAL
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5.4. TERMINAL OPERATIONS - EN ROUTE STATION
Not Applicable
5.5. GROUND SERVICING CONNECTIONS
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTGround Servicing Connections Figure 5.7
EM
170E
2AP
M05
0004
C.ID
R
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
FWD RAMP HEADSET
REAR RAMP HEADSET
STEERING DISCONNECT SWITCH
EXTERNAL POWER SUPPLY 115 VAC
EXTERNAL POWER SUPPLY 28 VDC
ENGINE AIR STARTING
AIR CONDITIONING LOW PRESSURE
WASTE SERVICING PANEL
POTABLE WATER SERVICING PANEL
OXYGEN REFILL / REPLACE BOTTLE
PRESSURE REFUELING / DEFUELING
RIGHT GRAVITY FUEL PORT
LEFT GRAVITY FUEL PORT
GROUNDING POINT (RIGHT MLG)
LEFT FUEL DRAIN VALVE
RIGHT FUEL DRAIN VALVE
HYDRAULIC SYS 1 SERVICING PANEL
HYDRAULIC SYS 2 SERVICING PANEL
HYDRAULIC SYS 3 SERVICING PANEL
RIGHT MLG WHEEL JACKING POINT
LEFT MLG WHEEL JACKING POINT
NLG WHEEL JACKING POINT
ITEM DESCRIPTION
1944
3092
830
1935
3065
1370
1373
2660
2680
2411
3250
3460
3460
1976
1825
1825
1816
1816
3614
522
522
280
HEIGHT ABOVE GROUND (mm)
THE GROUND CLEARANCES IN THE TABLE REFER TO THE AIRCRAFT WITH THE MINIMUMOPERATING WEIGHT (MOW), CGF, 20 ˚C.
NOTE:
13
2117 09 05 02
15
06010304
2210
0716
11
12
20
1418 1908
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EFFECTIVITY: EMBRAER 195-E2 ACFTGround Servicing Connections Figure 5.8
EM
170E
2A
PM
050016A
.ID
R
2210 07
06010304
16
15
13
21
20
14
11
12
18
17
08 19
0209 05
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
19
20
21
22
FWD RAMP HEADSET
REAR RAMP HEADSET
STEERING DISCONNECT SWITCH
EXTERNAL POWER SUPPLY 115 VAC
EXTERNAL POWER SUPPLY 28 VDC
ENGINE AIR STARTING
AIR CONDITIONING LOW PRESSURE
WASTE SERVICING PANEL
POTABLE WATER SERVICING PANEL
OXYGEN REFILL / REPLACE BOTTLE
PRESSURE REFUELING / DEFUELING
RIGHT GRAVITY FUEL PORT
LEFT GRAVITY FUEL PORT
GROUNDING POINT (RIGHT MLG)
LEFT FUEL DRAIN VALVE
RIGHT FUEL DRAIN VALVE
HYDRAULIC SYS 1 SERVICING PANEL-197DL
HYDRAULIC SYS 2 SERVICING PANEL-198DR
HYDRAULIC SYS 3 SERVICING PANEL-314BR
RIGHT MLG WHEEL JACKING POINT
LEFT MLG WHEEL JACKING POINT
NLG WHEEL JACKING POINT
ITEM DESCRIPTION
1944
3161
944
1935
3142
1201
1433
2644
2455
2376
3240
3499
3499
2007
1862
1862
1847
2416
1817
522
522
280
HEIGHT ABOVE GROUND (mm)
HYDRAULIC SYS 3 SERVICING PANEL-314AR
18HYDRAULIC SYS 2 SERVICING PANEL-198FR
HYDRAULIC SYS 1 SERVICING PANEL-197FL
2392
3177
3935
THE GROUND CLEARANCES IN THE TABLE REFER TO THE AIRCRAFT WITH THE MINIMUMOPERATING WEIGHT (MOW), CGF, 20 ˚C.
NOTE:
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5.6. ENGINE STARTING PNEUMATIC REQUIREMENTS
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLEngine Starting Pneumatic Requirements Figure 5.9
Altitude(ft)
AmbientTemp (˚F)
MinimumPressure (psia)
MinimumTemp (˚F)
MinimumFlow (lb/min)
15,000 59 24.4 446 46.115,000 5 25.3 392 49.015,000 -40 32.9 352 66.613,000 71 26.7 458 49.613,000 12 27.2 399 52.213,000 -40 36.0 352 71.39000 86 28.9 474 53.49000 23 30.0 409 57.39000 -40 37.7 350 74.5SL 120 40.7 505 73.7SL 59 43.7 443 82.0SL -40 48.0 349 95.1
TABLE 1 - PNEUMATIC ENGINE START REQUIREMENTS
EM
170E
2AP
M05
0006
A.ID
R
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5.7. GROUND PNEUMATIC POWER REQUIREMENTS
AIRPORTPLANNING MANUAL
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLGround Pneumatic Power Requirements Figure 5.10
EM
170E
2A
PM
050014A
.ID
R
-50
-40
-30
-20
-10
0
CA
BIN
TE
MP
ER
AT
UR
E (
˚C)
CA
BIN
TE
MP
ER
AT
UR
E (
˚F)
TIME TO HEAT CABIN - min
10
20
30
HEATING
Initial cabin temp: -38˚C (-36.4˚F)Outside air temp: -45˚C (-49˚F)Relative Humidity: 16%No crew or passengersNo other heat load
Bleed air from APU:90.7 kg/min. (200 lbm/min)417 kPa (60.5 psia)2 operating packs (ECS)
-58
-40
-22
-4
14
32
50
68
86
0 5 10 15 20 25 30
20
25
30
35
40
45
0 10 20 30 40 50 60 70
COOLING
Initial cabin temp: 43.6˚C (110.48˚F)Outside air temp: 32˚C (89.6˚F)Relative Humidity: 36%No crew or passengersNo other heat load
Bleed air from APU:48 kg/min (106 lbm/min)393 kPa (57 psia)2 operating packs (ECS)
TIME TO COOL CABIN - min
CA
BIN
TE
MP
ER
AT
UR
E (
˚C)
68
77
86
95
104
113
CA
BIN
TE
MP
ER
AT
UR
E (
˚F)
AIRPORTPLANNING MANUAL
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
5.8. PRECONDITIONED AIRFLOW REQUIREMENTS
This subsection presents the following information:
• The air conditioning requirements for heating and cooling using ground conditioned air. Thecurves show airflow requirements to heat or cool the aircraft within a given time at ambientconditions.
• The air conditioning requirements for heating and cooling to keep a constant cabin airtemperature using low-pressure conditioned air. This conditioned air is supplied through aground connection air directly to the passenger cabin, bypassing the aircraft's airconditioning cooling packs.
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLPreconditioned Airflow Requirements Figure 5.11
EM
170E
2AP
M05
0015
A.ID
R
PRESSURE AT GROUND CONNECTION 6.2 kPa (25 IN H2O)
PRESSURE AT GROUND CONNECTION 5.0 kPa (20 IN H2O)
PRESSURE AT GROUND CONNECTION 3.0 kPa (12 IN H2O)
PRESSURE AT GROUND CONNECTION 2.5 kPa (10 IN H2O)
PRESSURE AT GROUND CONNECTION 1.25 kPa (5 IN H2O)
PRESSURE AT GROUND CONNECTION 0.25 kPa (1 IN H2O)
1
2
3
[lb/min] [kg/min]
0
10
20
30
40
50
55
65
5
15
60
35
45
0
11
22
44
66
88
110
121
143
33
132
99
2555
77
-5 0 5 10 15 20 25 30 35 40 45 50 55 [˚C]60 65 70 75
23 32 41 50 59 68 77 86 95 104 113 122 131 140 149 158 167 [˚F]
4
5
6
AIR SUPPLY TEMPERATURE
CASE 1 - CABIN AT 24˚C (75.2˚F), 124 OCCUPANTS, BRIGHT DAY (SOLAR IRRADIATION), 39˚C (102.2˚F) DAY.
CASE 2 - CABIN AT 27˚C (80.6˚F), 124 OCCUPANTS, BRIGHT DAY (SOLAR IRRADIATION), 39˚C (102.2˚F) DAY.
CASE 3 - CABIN AT 24˚C (75.2˚F), 4 CREW MEMBERS, BRIGHT DAY (SOLAR IRRADIATION), 39˚C (102.2˚F) DAY.
CASE 4 - CABIN AT 24˚C (75.2˚F), NO CABIN OCCUPANTS, FOUR CREW MEMBERS ONLY, OVERCAST DAY (NO SOLAR IRRADIATION), -40˚C (-40˚F) DAY.
CASE 5 - CABIN AT 24˚C (75.2˚F), NO CABIN OCCUPANTS, FOUR CREW MEMBERS ONLY, OVERCAST DAY (NO SOLAR IRRADIATION), -29˚C (-20.2˚F) DAY.
CASE 6 - CABIN AT 24˚C (75.2˚F), NO CABIN OCCUPANTS, FOUR CREW MEMBERS ONLY, OVERCAST DAY (NO SOLAR IRRADIATION), -18˚C (-0.4˚F) DAY.STATIC PRESSURE AT GROUND CONNECTION - 0.25 kPa (1 IN H2O)
STATIC PRESSURE AT GROUND CONNECTION - 1.25 kPa (5 IN H2O)
STATIC PRESSURE AT GROUND CONNECTION - 2.5 kPa (10 IN H2O)
STATIC PRESSURE AT GROUND CONNECTION - 3.0 kPa (12 IN H2O)
STATIC PRESSURE AT GROUND CONNECTION - 5.0 kPa (20 IN H2O)
STATIC PRESSURE AT GROUND CONNECTION - 6.2 kPa (25 IN H2O)
LEGEND:
PRE-CONDITIONED AIRFLOW REQUIREMENTS
TO
TA
L A
IRF
LOW
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5.9. GROUND TOWING REQUIREMENTS
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTGround Towing Requirements Figure 5.12
EM
170E
2A
PM
050009A
.ID
R
GR
OU
ND
TO
WIN
G R
EQ
UIR
EM
EN
TS
NO
TE
S:
- S
TR
AIG
HT
-LIN
E T
OW
- U
NU
SU
AL B
RE
AK
AW
AY
C
ON
DIT
ION
S N
OT
SH
OW
N-
CO
EF
FIC
IEN
TS
OF
F
RIC
TIO
N (
)
AR
E E
ST
IMA
TE
D F
OR
R
UB
BE
R-T
IRE
D T
OW
V
EH
ICLE
S6
00
0(1
32
27
)
50
00
(11
02
3)
0
10
00
(22
04
)
20
00
(44
09
)
30
00
(66
13
)
40
00
(88
18
)
70
00
(15
43
2)
80
00
(17
63
6)
90
00
(19
84
1)
TOWBAR PULL - Kg (lb)
TO
TA
L T
RA
CT
ION
WH
EE
L -
kg
(lb
)(D
RA
WB
AR
PU
LL
)
20
00
(44
09
)4
00
0(8
81
8)
80
00
(17
63
6)
60
00
(13
22
7)
10
00
0(2
20
46
)1
20
00
(26
45
5)
12
PE
RC
EN
T S
LO
PE
(%
)
0%
1%
2%
3%
4%
5%
6%
7%
NU
MB
ER
OF
EN
GIN
ES
BA
CK
ING
AG
AIN
ST
ID
LE
TH
RU
ST
0
AIR
CR
AFT M
ASS - k
g (lb
)
Friction C
oeff =
0.0
5F
riction C
oeff =
0.0
5Ic
e =
0.0
5
Frict
ion C
oeff =
0.2
0
Hard
Snow
=
0.2
0
Sno
w C
hain
s =
0.45
Frictio
n Coe
ff = 0
.57
Wet
Con
cret
e =
0.57
Wet A
sphalt
=0.7
5
Dry Concre
te o
r Asp
ahlt =
0.80
48
00
0 (
10
58
21
)
58
00
0 (
12
78
68
)
56
00
0 (
12
34
58
)
54
00
0 (
11
90
49
)
52
00
0 (
11
46
40
)
50
00
0 (
11
02
31
)
32
00
0 (
70
54
7)
34
00
0 (
74
95
7)
46
00
0 (
10
14
12
)
44
00
0 (
97
00
3)
42
00
0 (
92
59
4)
40
00
0 (
88
18
4)
36
00
0 (
79
36
6)
38
00
0 (
83
77
5)
AIRPORTPLANNING MANUAL
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTGround Towing Requirements Figure 5.13
EM
170E
2A
PM
050017A
.ID
R
60
00
(13
22
7)
50
00
(11
02
3)
0
10
00
(22
04
)
20
00
(44
09
)
30
00
(66
13
)
40
00
(88
18
)
70
00
(15
43
2)
80
00
(17
63
6)
90
00
(19
84
1)
TOWBAR PULL - Kg (lb)
TO
TA
L T
RA
CT
ION
WH
EE
L -
kg
(lb
)(D
RA
WB
AR
PU
LL
)
20
00
(44
09
)4
00
0(8
81
8)
80
00
(17
63
6)
60
00
(13
22
7)
10
00
0(2
20
46
)1
20
00
(26
45
5)
12
PE
RC
EN
T S
LO
PE
(%
)
0%
1%
2%
3%
4%
5%
6%
7%
NU
MB
ER
OF
EN
GIN
ES
BA
CK
ING
AG
AIN
ST
ID
LE
TH
RU
ST
0
GR
OU
ND
TO
WIN
G R
EQ
UIR
EM
EN
TS
Frict
ion C
oeff =
0.2
0
Friction C
oeff =
0.0
5
Frictio
n Coe
ff = 0
.57
Friction C
oeff =
0.0
5
45
00
0 (
99
20
7)
43000 (
94798)
41
00
0 (
90
38
9)
37000 (
81570)
47
00
0 (
10
36
17
)
49
00
0 (
10
80
26
)
51000 (
112435)
63
00
0 (
13
88
91
)
61
00
0 (
13
44
81
)
59
00
0 (
13
00
72
)
57000 (
125663)
55000 (
121254)
53
00
0 (
11
68
44
)
35000 (
77161)
33
00
0 (
72
75
2)
39000 (
85980)
AIR
CR
AFT M
ASS - k
g (lb
)
NO
TE
S:
- S
TR
AIG
HT
-LIN
E T
OW
- U
NU
SU
AL B
RE
AK
AW
AY
C
ON
DIT
ION
S N
OT
SH
OW
N-
CO
EF
FIC
IEN
TS
OF
F
RIC
TIO
N (
)
AR
E E
ST
IMA
TE
D F
OR
R
UB
BE
R-T
IRE
D T
OW
V
EH
ICLE
S
Wet A
sphalt
=0.7
5
Wet
Con
cret
e =
0.57
Sno
w C
hain
s =
0.45
Hard
Snow
=
0.2
0
Ice =
0.0
5
Dry Concre
te o
r Asp
ahlt =
0.80
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 05 Page 20 of 20Rev 11 - Nov 09/18
Copyright © by Embraer S.A. All rights reserved - See title page for details.
6. OPERATION CONDITIONS
EFFECTIVITY: ALL
6.1. OPERATING CONDITIONS
This section provides the following information:
• The jet engine exhaust velocities;
• The airport and community noise levels;
• The hazard areas.
6.2. ENGINE EXHAUST VELOCITIES
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 06 Page 1 of 4Rev 11 - Nov 09/18
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLJet Wake Velocity Profile - Ground Idle and Maximum Takeoff Power Figure 6.1
EM
170E
2AP
M06
0008
A.ID
R
0
FEET(Meters)
10(3)
20(6)
30(9)
40(12)
50(15)
60(18)
10(3)
20(6)
30(9)
40(12)
50(15)
60(18)
MAXIMUM TAKE OFF THRUST0 FEET
477 MPH(33 FEET / 10 m)
409 MPH(51 FEET / 16 m)
341 MPH(63 FEET / 19 m)
273 MPH(78 FEET / 24 m)
204 MPH(98 FEET / 30 m)
137 MPH(138 FEET / 42 m)68 MPH(248 FEET / 76 m)34 MPH(475 FEET / 145 m)
GROUND IDLE THRUST
0 FEET
68 MPH(68 FEET / 21 m)
34 MPH(124 FEET / 38 m)
20 MPH(199 FEET / 61 m)
CONVERSION FACTOR:1 MPH = 1.6 Km/Hr
NOTE:
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
6.3. AIRPORT AND COMMUNITY NOISE
Aircraft noise is a major concern for the airport and community planner. The airport is a basicelement in the community's transportation system and, thus, is vital to its growth. However, theairport must also be a good neighbor, and this is only possible with proper planning. Since aircraftnoise extends beyond the boundaries of the airport, it is vital to consider the noise impact on thesurrounding communities.
Many means have been devised to provide the planner with a tool to estimate the impact of airportoperations. Too often they oversimplify noise to the point where the results become erroneous.Noise is not a simple matter; therefore, there are no simple answers.
The cumulative noise contour is an effective tool. However, care must be taken to ensure that thecontours, used correctly, estimate the noise resulting from aircraft operations conducted at anairport.
The size and shape of the single-event contours, which are inputs into the cumulative noisecontours, are dependent upon numerous factors. They include operational factors (aircraft weight,engine power setting, airport altitude), atmospheric conditions (wind, temperature, relative humidity,surface condition), and terrain.
6.3.1. External Certification Noise Levels
The aircraft complies with the following noise certification requirements:
• ANAC RBAC 36 Amendment 28 corresponding to 14 CFR Part 36, incorporatingAmendments 36-1 throughout 36-28
• 14 CFR Part 36, Amendment 36-1 to 36-29
• ICAO Annex 16, Volume 1, Chapter 4, Amendment 11-B
6.3.2. Ramp Noise Levels
The aircraft APUoperation complies with the noise limits as defined in ICAO Annex 16, Vol. 1,Chapter 9, Attachment C, sixth edition, effective 17th November 2011.
With the normal operation of APU, environmental control system (ECS), equipment cooling fans andventilation fans, in any combination, corresponding to outside air temperatures up to 25 °C and withmeasurement positions as defined in ICAO Annex 16, Vol. 1, Chapter 9, Attachment C, sixth edition,effective 17th November 2011:
• The A-weighted sound levels at the FWD passenger and FWD service doors must not bemore than 75 dBA.
• The A-weighted sound levels at the fuel servicing point, GPU connection point and rearpassenger door must not be more than 80 dBA.
• The A-weighted sound levels at the FWD and rear cargo doors, lavatory servicing point andrear service door must not be more than 85 dBA.
• The A-weighted sound levels on a rectangular perimeter 20 meter from the aircraftcenterline, nose and tail must not be more than 80 dBA.
6.4. HAZARD AREAS
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLHazard Areas - Ground Idle and Takeoff Power Figure 6.2
EM
170E
2A
PM
060007A
.ID
R
30˚
0
FEET(Meters)
GROUND IDLE HAZARD AREA
TAKE OFF POWER HAZARD AREA
20 FT6.10 m9 FT
2.74 m3.3 FT1.00 m
6 FT1.83 m
10(3)
20(6)
30(9)
40(12)
50(15)
60(18)
10(3)
20(6)
30(9)
40(12)
50(15)
60(18)
30˚
INTAKE SUCTION DANGER AREA1
ENTRY CORRIDOR 2
EXHAUST DANGER AREA (AFT EXHAUST NOZZLE)199 FEET (61 m) - GROUND IDLE (20 kt HEADWIND)475 FEET (145 m) - TAKE OFF POWER (20 kt HEADWIND)
3
1
33
2 2
1
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7. PAVEMENT DATA
EFFECTIVITY: ALL
7.1. GENERAL INFORMATION
Pavement is defined as a structure which has one or more layers of processed materials.
The primary function of a pavement is to distribute concentrated loads to prevent the supportingcapacity of the subgrade soil from being exceeded. The subgrade soil is defined as the material onwhich the pavement rests, whether it is an embankment or excavation.
Several methods to the airport pavements design, with considerable differences in their approach,have been developed.
The design methods are derived from observation of pavements in service or experimentalpavements. Thus, the reliability of any method is proportional to the amount of experimentalverification behind the method, and all methods require a considerable amount of common senseand judgment on the part of the engineer who applies them.
A brief description of the following pavement charts will be helpful for their use for airport planning.Each aircraft configuration is depicted with a minimum range of five loads on the main landing gearto help in the interpolation between the discrete values shown. The tire pressure used for the aircraftcharts will produce the recommended tire deflection with the aircraft loaded to its maximum rampweight and with the center of gravity position. The tire pressure, where specifically designated intables and on charts, are values obtained under loaded conditions as certificated for commercial use.
This section provides the information that follows:
• The basic data on the landing gear footprint configuration, maximum design ramp loads, andtire sizes and pressures.
• The maximum pavement loads for certain critical conditions at the tire-ground interfaces.
• A chart to determine the loads throughout the stability limits of the aircraft at rest on thepavement. Pavement requirements for commercial aircraft are generally determined from thestatic analysis of loads on the main landing gear struts. These main landing gear loads areused in the pavement design charts that follow, interpolating load values where necessary.
• The flexible pavement curves prepared in accordance with the US Army Corps of EngineersDesign Method and LCN Method.
• The rigid pavement design curves in accordance with the Portland Cement AssociationDesign Method and LCN Method.
• The aircraft AR values for flexible and rigid pavements.
7.2. FOOTPRINT
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTFootprint Figure 7.1
EM
170E
2AP
M07
0001
B.ID
R
MAXIMUM RAMP WEIGHT
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
12.61 m
(ERJ 190-300)
0.42 m
AIRCRAFT MODEL
56600 kg (124781 lb)
H27X8.5R12 16PR
1.007 - 1.055 kPa (146 - 153 psi)
H42X16.0R20 24PR
1.082 - 1.131 kPa (157 - 164 psi)
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
(41 ft 4 in.)(1 ft 4 in.)
0.87 m(2 ft 9 in.)
6.73 m(22 ft 1 in.)
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EFFECTIVITY: EMBRAER 195-E2 ACFTFootprint Figure 7.2
0.41 m(1 ft 4.2 in)
MAXIMUM RAMP WEIGHT
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
15.7 m(51 ft 6.1 in)
AIRCRAFT MODEL (E195-E2)
61715 kg (136058 lb)
H27X8.5R12 16PR
965.3 - 1.013 kPa (140 - 147 psi)
H42X16.0R20 24PR
1.172 - 1.227 kPa (170 - 178 psi)
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
0.87 m(2 ft 9 in)
6.73 m(22 ft 1 in)
EM
170E
2A
PM
070018A
.ID
R
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7.3. MAXIMUM PAVEMENT LOADS
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTMaximum Pavement Loads Figure 7.3
EM
170E
2AP
M07
0002
A.ID
R56601 kg(124784 lb)
7636 kg(16835 lb)
11469 kg(25285 lb)
26244 kg(57859 lb)
8136 kg(17937 lb)
20995 kg(46286 lb)
MAXIMUMRAMP
WEIGHT STATIC AT MOSTFOWARD C.G.
STEADYBRAKING WITH
DECELERATION OF 3,0 m/sec
STATIC ATMOST AFT C.G.
STEADYBRAKING WITH
DECELERATION OF 3,0 m/sec
INSTANTANEOUSBRAKING
(FRICTION COEF. OF 0.8)
VNLG V (PER STRUT)MLG
2 2
H (PER STRUT)
V = MAIN LANDING GEAR MAXIMUM VERTICAL GROUND LOAD AT MOST AFT C.G. MLG
V = NOSE LANDING GEAR MAXIMUM VERTICAL GROUND LOAD AT MOST FORWARD C.G.NLG
H = MAIN GEAR MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING
NOTES: ALL LOADS CALCULATED USING AIRCRAFT MAXIMUM RAMP WEIGHT
LEGEND:
INSTANTANEOUS BRAKING: H = 0.79*V
STEADY BRAKING: H = 0.30*V MLG
NOTES:
MLG
V MLG
V NLG
H
X
Z
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EFFECTIVITY: EMBRAER 195-E2 ACFTMaximum Pavement Loads Figure 7.4
EM
170E
2AP
M07
0025
A.ID
R60100 kg(132498 lb)
7273 kg(16034 lb)
10599 kg(23367 lb)
26921 kg(59352 lb)
8346 kg(18400 lb)
21537 kg(47481 lb)
MAXIMUMRAMP
WEIGHT STATIC AT MOSTFOWARD C.G.
STEADYBRAKING WITH
DECELERATION OF 3,0 m/sec
STATIC ATMOST AFT C.G.
STEADYBRAKING WITH
DECELERATION OF 3,0 m/sec
INSTANTANEOUSBRAKING
(FRICTION COEF. OF 0.8)
VNLG V (PER STRUT)MLG
2 2
H (PER STRUT)
V = MAIN LANDING GEAR MAXIMUM VERTICAL GROUND LOAD AT MOST AFT C.G. MLG
V = NOSE LANDING GEAR MAXIMUM VERTICAL GROUND LOAD AT MOST FORWARD C.G.NLG
H = MAIN GEAR MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING
NOTES: ALL LOADS CALCULATED USING AIRCRAFT MAXIMUM RAMP WEIGHT
LEGEND:
INSTANTANEOUS BRAKING: H = 0.80*V
STEADY BRAKING: H = 0.31*V MLG
NOTES:
MLG
61700 kg(136025 lb)
5430 kg(11971 lb)
8817 kg(19438 lb)
29185 kg(64342 lb)
9047 kg(19945 lb)
23348 kg(51473 lb)
V MLG
H
Z
X
V NLG
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
7.4. LANDING GEAR LOADING ON PAVEMENT
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Gear Loading on Pavement Figure 7.5
EM
170E
2A
PM
070003A
.ID
R
55000
50000
45000
40000
35000
30000
25000
2000085 87 89 91 93 95
PERCENT OF WEIGHT ON MAIN LANDING GEARS (%)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
S (
kgf)
18.0% 41.0%
(%MAC)
32700
33250
37201
40301
42000
46701
49051
52000
56601
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
kg)
50000
60000
70000
80000
90000
100000
110000
120000
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
S (
lb)
50000
60000
70000
80000
90000
100000
110000
120000
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
lb)
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E-JETS E2 - APM 5824 SECTION 07 Page 8 of 28Rev 15 - Sep 27/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTLanding Gear Loading on Pavement Figure 7.6
EM
170E
2AP
M07
0026
A.ID
R
13.0% 40.0%
25000
30000
35000
40000
45000
50000
55000
60000
65000
61700
60000
58000
56000
54000
52000
50000
48000
46000
44000
42000
40000
38000
3600034700
86 88 90 92 94 96
PERCENT OF WEIGHT ON MAIN LANDING GEARS (%)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
S (
kgf)
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
kg)
60000
70000
80000
90000
100000
110000
120000
130000
140000
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
S (
lb)
60000
70000
80000
90000
100000
110000
120000
130000
140000
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
lb)
[%MAC]
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7.5. FLEXIBLE PAVEMENT REQUIREMENTS, US CORPS OF ENGINEERS DESIGN METHOD
The flexible pavement curves that are based on procedures set forth in Instruction Report No.S-77-1, “Procedures for Development of CBR Design Curves”, dated June 1977, and as modifiedaccording to the methods described in FAA Advisory Circular 150/5320-6D, “Airport PavementDesign and Evaluation”, dated July 7, 1995. Instruction Report No. S-77-1 were prepared by the USArmy Corps of Engineers Waterways Experiment Station, Soils and Pavements Laboratory,Vicksburg, Mississippi. The line showing 10,000 coverages is used to calculate AR.
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EFFECTIVITY: EMBRAER 190-E2 ACFTFlexible Pavement Requirements - US Army Corps of Engineers Design Method Figure 7.7
EM
170E
2A
PM
070004A
.ID
R
NOTES: TIRE SIZE: H42x16R20/24TIRE PRESSURE: 10.76 kgf/cm² (153 psi)
SUBGRADE STRENGHT - CBR
10
FLEXIBLE PAVEMENT THICKNESS (IN)
3 4 5 6 7 8 9 20 30
FLEXIBLE PAVEMENT THICKNESS (CM)
108 9 20 30 40 50 7060
12478056600
12434156400
49050
32700
108137
72091
WEIGHT ON MAIN
LANDING GEAR
(kg) (lb)
ANNUAL
DEPARTURES
1200
3200
6000
15000
25000
10000 COVERAGES(USED FOR ACNCALCULATIONS)
103 4 5 6 7 8 9 20 30
FLEXIBLE PAVEMENT THICKNESS (IN)
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EFFECTIVITY: EMBRAER 195-E2 ACFTFlexible Pavement Requirements - US Army Corps of Engineers Design Method Figure 7.8
EM
170E
2A
PM
070021A
.ID
R
10
FLEXIBLE PAVEMENT THICKNESS (IN)
3 4 5 6 7 8 9 20 30
FLEXIBLE PAVEMENT THICKNESS (CM)
108 9 20 30 40 50 7060
13602561700
13249760100
54000
34700
119049
76500
WEIGHT ON MAIN
LANDING GEAR
(kg) (lb)
ANNUAL
DEPARTURES
1200
3200
6000
15000
25000
10000 COVERAGES(USED FOR ACNCALCULATIONS)
103 4 5 6 7 8 9 20 30
NOTES: TIRE SIZE: H42x16R20/24TIRE PRESSURE: 11.95 kgf/cm² (170 psi)(UNLOADED)
SUBGRADE STRENGHT - CBR
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E-JETS E2 - APM 5824 SECTION 07 Page 12 of 28Rev 15 - Sep 27/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
7.6. FLEXIBLE PAVEMENT REQUIREMENTS, LCN METHOD
The LCN Method curves for flexible pavements. They have been built using procedures and curvesin the ICAO Aerodrome Design Manual, Part 3 - Pavements, Document 9157-AN/901, 1983. Thesame chart includes the data of equivalent single-wheel load versus pavement thickness.
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 190-E2 ACFTFlexible Pavement Requirements - LCN Method Figure 7.9
32700 (72091)
EM
170E
2AP
M07
0005
A.ID
R
NOTES: TIRE SIZE: H42x16R20/24TIRE PRESSURE: 10.76 kgf/cm² (153 psi)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
- (
lb)
1001010000
100000
7
50000
20
WEIGHT ON MAINLANDING GEAR
kg (lb)
LCN - LOAD CLASSIFICATION NUMBER
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
- (
lb)
1001010000
100000
50000
FLEXIBLE PAVEMENT THICKNESS - (cm)
FLEXIBLE PAVEMENT THICKNESS - (in.)
53 2010 30
NOTE: EQUIVALENT SINGLE WHEEL LOADSARE DERIVED BY METHODS SHOWNIN ICAO AERODROME MANUAL.PART 2, PAR. 4.1.3
56400 (124341)49050 (108137)
56600 (124782)
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTFlexible Pavement Requirements - LCN Method Figure 7.10
EM
170E
2AP
M07
0022
A.ID
R
80000700006000050000
40000
30000
20000
1000025 50 75
3 6 9 15 21 30 60 90 120
80000700006000050000
40000
30000
20000
10000
WEIGHT ON MAINLANDING GEAR
kg (lb)
LCN - LOAD CLASSIFICATION NUMBER
EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL.PART 2, PAR. 4.1.3
NOTE:
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
- (
lb)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
- (
kg)
NOTES: TIRE SIZE: H42x16R20/24TIRE PRESSURE: 11.95 kgf/cm² (170 psi)(UNLOADED)
FLEXIBLE PAVEMENT THICKNESS - (cm)
FLEXIBLE PAVEMENT THICKNESS - (in.)
2 126 244 9 35 45
34700 (76500)
54000 (119049)
61700 (136025)60100 (132497)
61500 (135584)
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7.7. RIGID PAVEMENT REQUIREMENTS, PORTLAND CEMENT ASSOCIATION DESIGN METHOD
This method has a chart that has been prepared with the use of the Westergaard Equation in generalaccordance with the procedures outlined in the 1955 edition of “Design of Concrete AirportPavement” published by the Portland Cement Association, 33 W. Grand Ave., Chicago 10, Illinois,but modified to the new format described in the 1968 Portland Cement Association publication,“Computer Program for Concrete Airport Pavement Design” by Robert G. Packard. The followingprocedure is used to develop rigid pavement design curves such as that shown in the chart:
• Once the scale for the pavement thickness to the left and the scale for allowable workingstress to the right have been established, an arbitrary load line is drawn representing themain landing gear maximum weight to be shown.
• All values of the subgrade modulus (k-values) are then plotted.
• Additional load lines for the incremental values of weight on the main landing gear are thenestablished on the basis of the curve for k=300, already established.
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EFFECTIVITY: EMBRAER 190-E2 ACFTRigid Pavement Requirements - Portland Cement Association Design Method Figure 7.11
EM
170E
2A
PM
070006A
.ID
R
PA
VE
ME
NT
TH
ICK
NE
SS
(cm
)
PA
VE
ME
NT
TH
ICK
NE
SS
(in
.)
0
5
10
15
20
25
30
35
40
45
50
55
60
2
4
6
8
10
12
14
16
18
20
22
24
0
MAXIMUM POSSIBLE MAIN-GEARLOAD AT MAXIMUM DESIGN RAMPWEIGHT AND AFT C.G.
THE VALUES OBTAINED BY USING THEMAXIMUM LOAD REFERENCE LINE ANDANY VALUE OF "K" ARE EXACT. FORLOADS LESS THAN MAXIMUM, THE CURVESARE EXACT FOR K=300 BUT DEVIATESLIGHTLY FOR OTHER VALUES OF "K".
NOTE:
NOTES: TIRE SIZE: H42x16R20/24TIRE PRESSURE: 10.76 kgf/cm² (153 psi) (UNLOADED)
4010 20 300
k=550 lb/in
k=150 lb/in
k=300 lb/in
k=75 lb/in
56400 (124341)
49050 (108137)
56600 (124782)
32700 (72091)
WEIGHT ON MAIN LANDING GEAR - kg (lb
)
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 07 Page 17 of 28Rev 15 - Sep 27/19
Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: EMBRAER 195-E2 ACFTRigid Pavement Requirements - Portland Cement Association Design Method Figure 7.12
EM
170E
2A
PM
070024A
.ID
R
0
10
20
30
40
50
60
70
80
90
100
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40 42 44
34700 (76500)
61700 (136025)
60100 (132497)
54000 (119049)
MAXIMUM POSSIBLE MAIN-GEARLOAD AT MAXIMUM DESIGN RAMPWEIGHT AND AFT C.G.
k = 550 lb/ink = 300 lb/in
k = 150 lb/in
k = 75 lb/in
WEIGHT ON MAIN LANDING GEAR - kg (lb)
PA
VE
ME
NT
TH
ICK
NE
SS
(cm
)
0
4
8
12
16
20
24
28
32
36
40
PA
VE
ME
NT
TH
ICK
NE
SS
(in
)
10
20
30
40
50
60
70
80
90
100
0
AL
LO
WA
BL
E W
OR
KIN
G S
TR
ES
S (
kg
f/cm
)
2
AL
LO
WA
BL
E W
OR
KIN
G S
TR
ES
S (
psi)
150
285
427
569
710
850
995
1135
1280
1422
THE VALUES OBTAINED BY USING THEMAXIMUM LOAD REFERENCE LINE ANDANY VALUE OF "K" ARE EXACT. FORLOADS LESS THAN MAXIMUM, THE CURVESARE EXACT FOR K=300 BUT DEVIATESLIGHTLY FOR OTHER VALUES OF "K".
NOTE:
TIRE SIZE: H42x16R20/24NOTES:TIRE PRESSURE: 11.95 kgf/cm² (170 psi) (UNLOADED)
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7.8. RIGID PAVEMENT REQUIREMENTS, LCN METHOD
This LCN Method presents curves for rigid pavements. They have been built using procedures andcurves in ICAO Aerodrome Design Manual, Part 3 - Pavements, Document 9157-AN/901, 1983. Thesame chart includes the data of equivalent single-wheel load versus radius of relative stiffness.
To determine the aircraft weight that can be accommodated on a particular rigid airport pavement,both the LCN of the pavement and the radius of relative stiffness must be known.
The radius of relative stiffness values is obtained from a table. This table presents the radius ofrelative stiffness values that are based on Young's modulus (E) of 4,000,000 psi and Poisson's ratio(μ) of 0.15.
For convenience in finding this radius based on other values of E and μ, the curves are included. Forexample, to find an RRS value based on an E of 3,000,000 psi, the “E” factor of 0.931 is multipliedby the RRS value found in figure 7.6.3. The effect of the variations of μ on the RRS value is treatedin a similar manner.
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLRadius of Relative Stiffness Figure 7.13
EM
170E
2AP
M07
0007
A.ID
R
RADIUS OF RELATIVE STIFFNESS ( ) VALUES IN INCHES
=4 Ed =24.16522
4 dk
33
6
3
12( 1- )k
WHERE: E = YOUNG'S MODULUS = 4 x 10 psi k = SUBGRADE MODULUS, lb/in.
d = RIGID-PAVEMENT THICKNESS. in. = POISSON'S RATIO = 0.15
d(in) k=75 k=100 k=150 k=200 k=250 k=300 k=350 k=400 k=500 k=550
6.06.57.0
7.58.08.5
9.09.510.0
10.511.011.5
12.012.513.0
13.514.014.5
15.015.516.0
16.517.017.5
18.018.519.0
19.520.020.5
21.021.522.0
22.523.023.5
24.024.525.0
31.4833.4335.34
37.2239.0640.88
42.6744.4346.18
47.9049.6051.28
52.9454.5956.22
57.8359.4361.02
62.5964.1565.69
67.2368.7570.26
71.7673.2574.73
76.2077.6679.11
80.5581.9983.41
84.8386.2487.64
89.0490.4391.81
29.3031.1132.89
34.6336.3538.04
39.7141.3542.97
44.5746.1647.72
49.2750.8052.32
53.8255.3156.78
58.2559.7061.13
62.5663.9865.38
66.7868.1769.54
70.9172.2773.62
74.9676.3077.63
78.9580.2681.56
82.8684.1585.44
26.4728.1129.72
31.2932.8534.37
35.8837.3638.83
40.2841.7143.12
44.5245.9047.27
48.6349.9851.31
52.6353.9455.24
56.5357.8159.08
60.3461.6062.84
64.0865.3066.52
67.7468.9470.14
71.3472.5273.70
74.8776.0477.20
24.6326.1627.65
29.1230.5731.99
33.3934.7736.14
37.4838.8140.13
41.4342.7243.99
45.2646.5147.75
48.9850.2051.41
52.6153.8054.98
56.1557.3258.48
59.6360.7761.91
63.0464.1665.28
66.3867.4968.59
69.6870.7671.84
23.3024.7426.15
27.5428.9130.25
31.5832.8934.17
35.4536.7137.95
39.1840.4041.61
42.8043.9845.16
46.3247.4748.62
49.7550.8852.00
53.1154.2155.31
56.3957.4758.55
59.6260.6861.73
62.7863.8364.86
65.9066.9267.95 64.92
63.9462.96
61.9760.9859.99
58.9857.9756.96
55.9454.9153.88
52.8451.8050.74
49.6848.6147.54
46.4545.3644.26
43.1542.0240.89
39.7538.6037.44
36.2635.0733.87
32.6531.4230.17
28.9127.6226.32
24.9923.6422.26 21.42
22.7424.04
25.3226.5827.81
29.0330.2331.42
32.5933.7534.89
36.0237.1438.25
39.3540.4441.51
42.5843.6444.70
45.7446.7747.80
48.8249.8450.84
51.8452.8453.83
54.8155.7856.75
57.7258.6859.63
60.5861.5262.46
20.7222.0023.25
24.4925.7026.90 25.44
24.3123.16
21.9920.8019.59 19.13
20.3121.47
22.61
28.0829.2430.39
31.5232.6433.74
34.8435.9236.99
38.0639.1140.15
41.1942.2143.23
44.2445.2446.23
47.2248.2049.17
50.1451.1052.06
53.0153.9554.89
55.8256.7557.67
58.5959.5060.41
23.7424.84
25.9327.0028.06
29.1130.1431.16
32.1733.1734.16
35.1436.1237.08
38.0338.9839.92
40.8541.7842.70
43.6144.5145.41
46.3047.1948.07
48.9549.8250.69
51.5552.4153.26
54.1154.9555.7957.14
56.2855.41
54.5453.6752.79
51.9151.0250.13
49.2348.3347.42
46.5145.5944.66
43.7242.7841.84
40.8839.9238.95
37.9736.9935.99
34.9933.9732.95
31.9130.8729.81
28.7427.6526.55
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Copyright © by Embraer S.A. All rights reserved - See title page for details.
EFFECTIVITY: ALLRadius of Relative Stiffness (other values) Figure 7.14
EM
170E
2A
PM
070008A
.ID
R
0 1 2 3 4 5
0 0.05 0.10 0.15 0.20 0.25
0
0.995
1.000
1.005
1.010
1.015
0
1.10
1.05
1.00
0.95
0.90
0.85
0.80
E FACTOR
FACTOR
6E, YOUNG'S MODULUS (10 ,PSI)
, POISSON'S RATIO
EFFECT OF E ON -VALUES
EFFECT OF ON -VALUES
NOTE:BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE -VALUES.
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EFFECTIVITY: EMBRAER 190-E2 ACFTRigid Pavement Requirements - LCN Method Figure 7.15
56400 (124341)49050 (108137)
100000
1000010 1000100 10 100
10000
100000
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
- (
kg)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
- (
lb)
LCN - LOAD CLASSIFICATION NUMBER
RADIUS OF RELATIVE STIFFNESS - (cm)
RADIUS OF RELATIVE STIFFNESS - (in.)
4 40040
32700 (72091)
56600 (124782)
WEIGHT ON MAINLANDING GEAR
kg (lb)
NOTE: EQUIVALENT SINGLE WHEEL LOADSARE DERIVED BY METHODS SHOWNIN ICAO AERODROME MANUAL.PART 2, PAR. 4.1.3
NOTES: TIRE SIZE: H42x16R20/24TIRE PRESSURE: 10.76 kgf/cm² (153 psi)
EM
170E
2AP
M07
0009
A.ID
R
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EFFECTIVITY: EMBRAER 195-E2 ACFTRigid Pavement Requirements - LCN Method Figure 7.16
EM
170E
2AP
M07
0023
A.ID
R
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
- (
lb)
10000
20000
30000
40000
50000
60000
30 60 90 120 150 210180 60 804020
20000
30000
40000
50000
60000
10000
LCN - LOAD CLASSIFICATION NUMBERRADIUS OF RELATIVE STIFFNESS - (cm)
34700 (76500)
54000 (119049)
61700 (136025)
60100 (132497)
RADIUS OF RELATIVE STIFFNESS - (in)
12 35.4 82.7
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
- (
kg)
TIRE SIZE: H42x16R20/24NOTES:TIRE PRESSURE: 11.95 kgf/cm² (170 psi) (UNLOADED)
NOTE: EQUIVALENT SINGLE WHEEL LOADSARE DERIVED BY METHODS SHOWNIN ICAO AERODROME MANUAL.PART 2, PAR. 4.1.3
WEIGHT ON MAINLANDING GEAR
kg (lb)
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7.9. ACN - PCN SYSTEM - FLEXIBLE AND RIGID PAVEMENTS
The ACN/PCN system as referenced in Amendment 35 to ICAO Annex 14, “Aerodromes”, provides astandardized international aircraft/pavement rating system.
The PCN is an index rating of the mass which an evaluation shows the pavement can withstandwhen applied by a standard single wheel. The ACN is established for the particular pavement typeand subgrade category of the rated pavement as well as for the particular aircraft mass andcharacteristics.
An aircraft must have an ACN equal to or less than the PCN to operate without restriction on thepavement.
The method of pavement evaluation is left to the airport with the results of their evaluation presentedas follows:
Table 7.1 - Pavement Evaluation
PAVEMENTTYPE
SUBGRADE CATEGORY TIRE PRESSURE CATEGORY METHOD
R – Rigid A – High W – No Limit T – Technical
F – Flexible B – Medium X – to 1.75 Mpa (254 psi) U – Using aircraft
C – Low Y – to 1.25 Mpa (181 psi)
D – Ultra Low Z – to 0.5 Mpa (73 psi)
Report example: PCN 80/R/B/X/T, where:
80 = PCN
R = Pavement Type: Rigid
B = Subgrade Category: Medium
X = Tire Pressure Category: Medium (limited to 1.5 Mpa)
T = Evaluation Method: Technical
The flexible pavements have four subgrade categories:
A. High Strength - Pavement Data 15.
B. Medium Strength - Pavement Data 10.
C. Low Strength - Pavement Data 6.
D. Ultra Low Strength - Pavement Data 3.
The rigid pavements have four subgrade categories:
A. High Strength - Subgrade k = 150 MN/m³ (550 lb/ft³).
B. Medium Strength - k = 80 MN/m³ (300 lb/ft³).
C. Low Strength - k = 40 MN/m³ (150 lb/ft³).
D. Ultra Low Strength - k = 20 MN/m³ (75 lb/ft³).
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EFFECTIVITY: EMBRAER 190-E2 ACFTACN For Flexible Pavement Figure 7.17
EM
170E
2A
PM
070010A
.ID
R
30000
5,0
10,0
15,0
20,0
25,0
30,0
35,0
40,0
35000 40000 45000 50000 55000 60000
AIR
CR
AF
T C
LA
SS
IFIC
AT
ION
NU
MB
ER
-AC
N
FLEXIBLE PAVEMENT SUBGRADE
AIRCRAFT GROSS WEIGHT-lb
AIRCRAFT GROSS WEIGHT-kg
72000 80000 88000 96000 104000 112000 120000 128000
2NOTES:
TIRE PRESSURE: 10.62 kgf/cm (151psi) (UNLOADED)
TIRE SIZE: H42 x 16 - 20 24 PR
56600
124782
SUBGRADE STRENGTH ULTRA LOW - CBR=3%LOW - CBR=6%MEDIUM-CBR=10%HIGH-CBR=15%
MA
XIM
UM
RA
MP
WE
IGH
T
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EFFECTIVITY: EMBRAER 195-E2 ACFTACN For Flexible Pavement Figure 7.18
EM
170E
2AP
M07
0019
A.ID
R
AIRCRAFT GROSS WEIGHT (kg)
10,0
15,0
20,0
25,0
30,0
35,0
40,0
45,0
30000 35000 40000 45000 50000 55000 60000 65000
AIR
CR
AF
T C
LAS
SIF
ICA
TIO
N N
UM
BE
R-A
CN
FLEXIBLE PAVEMENT SUBGRADE
NOTES:TIRE PRESSURE: 11.95 kgf/cm² (170psi) (UNLOADED)TIRE SIZE: H42 x 16.0R 20
MA
XIM
UM
RA
MP
WE
IGH
T
AIRCRAFT GROSS WEIGHT-lb
72000 80000 88000 96000 104000 112000 120000 128000 136000
MEDIUM-CBR=10%LOW-CBR=6%ULTRA LOW-CBR=3%
SUBGRADE STRENGTH
HIGH-CBR=15%
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EFFECTIVITY: EMBRAER 190-E2 ACFTACN For Rigid Pavement Figure 7.19
EM
170E
2AP
M07
0011
A.ID
R
300005,0
10,0
15,0
20,0
25,0
30,0
35,0
40,0
35000 40000 45000 50000 55000 60000
2NOTES:
RIGID PAVEMENT SUBGRADE
TIRE SIZE: H42 x 16 - 20 24 PRTIRE PRESSURE: 10.62 kgf/cm (151psi) (UNLOADED)
AIRCRAFT GROSS WEIGHT-kg
AIRCRAFT GROSS WEIGHT-lb
72000 80000 88000 96000 104000 112000 120000 128000
AIR
CR
AF
T C
LAS
SIF
ICA
TIO
N N
UM
BE
R-A
CN
56600
124782
MA
XIM
UM
RA
MP
WE
IGH
T
SUBGRADE STRENGTH ULTRA LOW - K=20 MN/m³ (75 lb/in³)LOW - K=40 MN/m³ (150 lb/in³)MEDIUM- K=80 MN/m³ (300 lb/in³)HIGH- K=150 MN/m³ (550 lb/in³)
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EFFECTIVITY: EMBRAER 195-E2 ACFTACN For Rigid Pavement Figure 7.20
10,030000
15,0
20,0
25,0
30,0
35,0
40,0
45,0
35000 40000 45000 50000 55000 60000 65000
AIRCRAFT GROSS WEIGHT (kg)
EM
170E
2AP
M07
0020
A.ID
R
RIGID PAVEMENT SUBGRADE
NOTES:TIRE PRESSURE: 11.95 kgf/cm² (170psi) (UNLOADED)TIRE SIZE: H42 x 16.0R 20
AIR
CR
AF
T C
LAS
SIF
ICA
TIO
N N
UM
BE
R-A
CN
MA
XIM
UM
RA
MP
WE
IGH
T
AIRCRAFT GROSS WEIGHT-lb
72000 80000 88000 96000 104000 112000 120000 128000 136000
MEDIUM K=80 MN/m³ (300 lb/in³)LOW K=40 MN/m³ (150 lb/in³)ULTRA LOW K=20 MN/m³ (75 lb/in³)
HIGH K=150 MN/m³ (550 lb/in³)
SUBGRADE STRENGTH
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8. POSSIBLE EMBRAER 196 DERIVATIVE AIRCRAFT
EFFECTIVITY: EMBRAER 175-E2, 190-E2 AND 195-E2 SERIES ACFT
8.1. NOT APPLICABLE
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9. SCALED DRAWINGS
EFFECTIVITY: ALL
9.1. GENERAL
This section provides plan views to the following scales:
• English/American Customary Weights and Measures:
1 in = 32 ft
1 in = 50 ft
1 in = 100 ft
• Metric
1:500
1:1000
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EFFECTIVITY: EMBRAER 190-E2 ACFTScale: 1 Inch Equals 32 Feet Figure 9.1
EM
170E
2A
PM
090001A
.ID
R
1 8
2
3
4
5
6
7
9
10
11
12
13
EXTERNAL POWER SUPPLY 115 VAC
EXTERNAL POWER SUPPLY 28 VDC
HIGH PRESSURE AIR GROUND SUPPLY
WASTE SERVICING PANEL
POTABLE WATER SERVICING PANEL
OXYGEN REFILL / REPLACE BOTTLE
GROUNDING POINT (RIGHT MLG)
PRESSURE REFUELING / DEFUELING
CARGO DOOR
MAIN LANDING GEAR
NOSE LANDING GEAR
PASSENGER DOOR
14 SERVICE DOOR
LOW PRESSURE AIR GROUND SUPPLY
0
0 16 32 48 64
5 10 15 20 25 m
80 ft
1
3 4
8
13
12
14
10
7
91111
10
6
14
5
13
2
WING SPAN:33.72 m
(110 ft 7.6 in.)
DESCRIPTIONITEM DESCRIPTIONITEM
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EFFECTIVITY: EMBRAER 190-E2 ACFTScale: 1 Inch Equals 50 Feet Figure 9.2
0 5 10 15 20 25 m
0 16 32 48 64 80 ft
EM
170E
2A
PM
090002A
.ID
R
1 8
2
3
4
5
6
7
9
10
11
12
13
EXTERNAL POWER SUPPLY 115 VAC
EXTERNAL POWER SUPPLY 28 VDC
HIGH PRESSURE AIR GROUND SUPPLY
WASTE SERVICING PANEL
POTABLE WATER SERVICING PANEL
OXYGEN REFILL / REPLACE BOTTLE
GROUNDING POINT (RIGHT MLG)
PRESSURE REFUELING / DEFUELING
CARGO DOOR
MAIN LANDING GEAR
NOSE LANDING GEAR
PASSENGER DOOR
14 SERVICE DOOR
LOW PRESSURE AIR GROUND SUPPLY
WING SPAN:33.72 m
(110 ft 7.6 in.)
1
3
4
8
13
12
14
10
7
91111
106
14
5
13
2
DESCRIPTIONITEM DESCRIPTIONITEM
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EFFECTIVITY: EMBRAER 190-E2 ACFTScale: 1 Inch Equals 100 Feet Figure 9.3
0 5 10 15 20 25 m
0 16 32 48 64 80 ft
WING SPAN:33.72 m
(110 ft 7.6 in.)
EM
170E
2A
PM
090003A
.ID
R
1 8
2
3
4
5
6
7
9
10
11
12
13
EXTERNAL POWER SUPPLY 115 VAC
EXTERNAL POWER SUPPLY 28 VDC
HIGH PRESSURE AIR GROUND SUPPLY
WASTE SERVICING PANEL
POTABLE WATER SERVICING PANEL
OXYGEN REFILL / REPLACE BOTTLE
GROUNDING POINT (RIGHT MLG)
PRESSURE REFUELING / DEFUELING
CARGO DOOR
MAIN LANDING GEAR
NOSE LANDING GEAR
PASSENGER DOOR
14 SERVICE DOOR
LOW PRESSURE AIR GROUND SUPPLY
1
34
8
13
12
14
107
9111110
6
145
13
2
DESCRIPTIONITEM DESCRIPTIONITEM
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EFFECTIVITY: EMBRAER 190-E2 ACFTScale: 1 to 500 Figure 9.4
EM
170E
2A
PM
090004A
.ID
R
1 8
2
3
4
5
6
7
9
10
11
12
13
EXTERNAL POWER SUPPLY 115 VAC
EXTERNAL POWER SUPPLY 28 VDC
HIGH PRESSURE AIR GROUND SUPPLY
WASTE SERVICING PANEL
POTABLE WATER SERVICING PANEL
OXYGEN REFILL / REPLACE BOTTLE
GROUNDING POINT (RIGHT MLG)
PRESSURE REFUELING / DEFUELING
CARGO DOOR
MAIN LANDING GEAR
NOSE LANDING GEAR
PASSENGER DOOR
14 SERVICE DOOR
LOW PRESSURE AIR GROUND SUPPLY
WING SPAN:33.72 m
(110 ft 7.6 in.)
0 5 10 15 20 25 m
160 32 6448 80 ft
14
10
7
911
5
1
3 4
8
13
12
11
10
6
1413
2
DESCRIPTIONITEM DESCRIPTIONITEM
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EFFECTIVITY: EMBRAER 190-E2 ACFTScale: 1 to 1000 Figure 9.5
EM
170E
2A
PM
090005A
.ID
R
ITEM DESCRIPTION
1
ITEM DESCRIPTION
8
2
3
4
5
6
7
9
10
11
12
13
EXTERNAL POWER SUPPLY 115 VAC
EXTERNAL POWER SUPPLY 28 VDC
HIGH PRESSURE AIR GROUND SUPPLY
WASTE SERVICING PANEL
POTABLE WATER SERVICING PANEL
OXYGEN REFILL / REPLACE BOTTLE
GROUNDING POINT (RIGHT MLG)
PRESSURE REFUELING / DEFUELING
CARGO DOOR
MAIN LANDING GEAR
NOSE LANDING GEAR
PASSENGER DOOR
14 SERVICE DOOR
LOW PRESSURE AIR GROUND SUPPLY
0 5 10 15 20
160 32 6448 80 ft
WING SPAN:33.72 m
(110 ft 7.6 in.)
1
34
8
13
12
14
107
911 11
106
145
13
2
25 m
AIRPORTPLANNING MANUAL
E-JETS E2 - APM 5824 SECTION 09 Page 6 of 11Rev 11 - Nov 09/18
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