PLANNING MANUAL 22 SEPTEMBER 2017 AIRPORT APM - 5824

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


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


E-JETS E2 - APM 5824 LIST OF EFFECTIVE AIRCRAFT Page 1 of 2Rev 15 - Sep 27/19


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


E-JETS E2 - APM 5824 LIST OF EFFECTIVE AIRCRAFT Page 2 of 2Rev 15 - Sep 27/19


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


E-JETS E2 - APM 5824 RECORD OF REVISIONS Page 1 of 1Rev 15 - Sep 27/19


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


E-JETS E2 - APM 5824 HIGHLIGHTS Page 1 of 1Rev 15 - Sep 27/19


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.


E-JETS E2 - APM 5824 INTRODUCTION Page 1 of 4Rev 11 - Nov 09/18


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.




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




(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




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.


E-JETS E2 - APM 5824 SECTION 01 Page 1 of 2Sep 22/17


• 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


E-JETS E2 - APM 5824 SECTION 01 Page 2 of 2Sep 22/17


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 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


• 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.


E-JETS E2 - APM 5824 SECTION 02 Page 1 of 26Rev 13 - May 10/19


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).




Table 2.1 - Aircraft General Characteristics (Continued)Effectivity: EMBRAER 190-E2 ACFT


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


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


• 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


• Span over Swept Back Wingtip - 35.12 m (115 ft 2.7 in)




• 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


• 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


• 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




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.)




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)




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

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3.81

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m6

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3.07

m10

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10.4

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5660

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1.74

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m9

ft 10

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3.0

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10.3

m33

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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

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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

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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

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.7in

3.19

m10

ft 5

.6in

3.2

m10

ft 6

in

10.5

m34

ft 5

.4in

12.7




Tabl

e 2.

4 - G

roun

d C

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- S

TD A

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ft M

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C)

Effe

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FT

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TC

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MA

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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

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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

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1in

3.93

m12

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2.26

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in

2.15

m7

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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

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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




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

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MA

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5660

0 kg

1247

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18-0

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2.31

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9in

2.83

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ft 3.

8in

2.84

m9

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8in

1.79

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0.47

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3.93

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ft10

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2.27

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ft 5.

4in

2.15

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ft 0.

65in

3.21

m10

ft 6

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3.21

m10

ft 6

.4in

10.5

6 m

34 ft

7.7

in12

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5660

0 kg

1247

84 lb

34-0

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36 m

7 ft

8.9

in

2.87

m9

ft 5

in2.

87 m

9 ft

5 in

1.82

m5

ft 11

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0.48

m1

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9in

3.90

m12

ft 9

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2.25

m7

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6in

2.11

m6

ft 11

in

3.15

m10

ft 4

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3.16

m10

ft 4

.4in

10.4

8 m

34 ft

4.6

in12

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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

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2.27

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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

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5640

0 kg

1243

43 lb

34-0

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36 m

7 ft

8.9

in

2.87

m9

ft 5

in2.

87 m

9 ft

5 in

1.82

m5

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0.48

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9in

3.90

m12

ft 9

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2.25

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2.11

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in

3.16

m10

ft 4

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3.16

m10

ft 4

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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

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3.25

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3.26

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10.6

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34 ft

10

in13

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4905

0 kg

1081

39 lb

41-0

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2.41

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2.91

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92 m

9 ft

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1.86

m6

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0.51

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3.92

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2.28

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3.17

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3.17

m10

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10.4

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34 ft

4.6

in12

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4670

0 kg

1029

58 lb

18-1

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2.31

m7

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9in

2.85

m9

ft 3.

8in

2.86

m9

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6in

1.81

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0.51

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3.99

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2.31

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34 ft

11

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4670

0 kg

1029

58 lb

41-0

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2.92

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92 m

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0.52

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3.94

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2.29

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2.14

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3.18

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3.18

m10

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10.5

0 m

34 ft

5.4

in12

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3270

0 kg

7209

3 lb

22-1

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2.34

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2.89

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1.87

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0.58

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4.10

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2.40

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2.33

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7in

3.40

m11

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3.40

m11

ft 1

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10.8

0 m

35 ft

6in

13.6

3270

0 kg

7209

3 lb

32-1

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2.38

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2.92

m9

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2.93

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1.89

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0.58

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4.07

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2.40

m7

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2.30

m7

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3.36

m11

ft 2

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3.36

m11

ft 2

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10.7

3 m

35 ft

2.4

in13

.4




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




Tabl

e 2.

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9 ft

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1.71

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3.05

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ft 10

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10.4

m34

ft 1

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10.5

6170

0 kg

1360

25 lb

34-0

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2.33

m7

ft 7.

7in

2.81

m9

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6in

2.81

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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




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

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ED

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)

FO

R-

WA

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S-

SE

N-

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RD

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FO

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(E)

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WIN

GT

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WIN

GE

S-

CA

PE

(H)

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TC

AR

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R(J

)

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TS

ER

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AS

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EN

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(L)

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TA

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)

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




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

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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-

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DO

OR

(K)

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EN

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(L)

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RT

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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




2.3. INTERIOR ARRANGEMENTS


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


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.




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)




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


0.06 m³ / pax (2.0 ft³ / pax)

0.04 m³ / pax (1.4 ft³ / pax)



0.99 m(3.25 ft)

8 8

42 3


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

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)




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


0.06 m³ / pax (2.0 ft³ / pax)

0.04 m³ / pax (1.4 ft³ / pax)



8

4

8

2 3


2 - GALLEY G1

3 - GALLEY G2

4 - GALLEY G5

5 - AFT TOILET

6 - FWD PARTITION

7 - FWD TOILET


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)




2.3.2. Cargo Compartments


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


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.





EM

170E

2AP

M02

0010

B.ID

R


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)




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


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)





EM

170E

2AP

M02

0012

B.ID

R


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)





EM

170E

2AP

M02

0013

B.ID

R


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)




2.4.2. Cargo Compartments


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




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




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)




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.


E-JETS E2 - APM 5824 SECTION 03 Page 1 of 34Rev 12 - Feb 08/19


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.




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)




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


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)




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


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




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


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




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.




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




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)



ISA + 15 ˚CNo Wind

0





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)


4268(14000)

3658(12000)

1219(4000)

609(2000)

1829(6000)

3048(10000) 2438

(8000)

-570(-1870)



ISA + 20 ˚CNo Wind





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)


0

FLAP 4

FLAP 2

FLAP 1


ATTCS OFF / ECS OFFDRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY

ISANo Wind





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)



ISA + 15 ˚CNo Wind





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


-570(-1870)

1219(4000)

2438(8000)

3048(10000)

3658(12000)

0

1829(6000)

4268(14000)

609(2000)



ISA + 20 ˚CNo Wind





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


ISA 0No Wind

14000 ft

12000 ft

10000 ft

8000 ft

6000 ft

4000 ft

2000 ft

0 ft

-1870 ft





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)



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





EM

170E

2A

PM

030029A

.ID

R

TAKEOFF FIELD LENGTHPW1923G & PW1923GA ENGINES @ T/O-1 MODE


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





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)



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




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.




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

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EM

170E

2AP

M03

0009

A.ID

R




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

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0 ft

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-1870 ft

3000

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WEIGHT - lb



ISA + 15˚C

WEIGHT - kg




EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap Full - ISA Conditions Figure 3.17

EM

170E

2AP

M03

0011

A.ID

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-1870 ft


3000

60000


DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP FULL

ISA

WEIGHT - kg

WEIGHT - lb




EFFECTIVITY: EMBRAER 190-E2 ACFTLanding Field Lengths - Flap Full - ISA + 15 °C Conditions Figure 3.18

EM

170E

2A

PM

030012A

.ID

R

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DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP FULLISA + 15˚C

WEIGHT - kg

WEIGHT - lb





EM

170E

2AP

M03

0013

A.ID

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ISA

WEIGHT - kg

WEIGHT - lb





EM

170E

2A

PM

030014A

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ISA + 15˚C

WEIGHT - kg





EM

170E

2AP

M03

0015

A.ID

R

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DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP FULL

ISA

WEIGHT - kg

WEIGHT - lb





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EM

170E

2A

PM

030016A

.ID

R


DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAYFLAP FULLISA + 15˚C

WEIGHT - kg

WEIGHT - lb





EM

170E

2AP

M03

0020

A.ID

R

LANDING FIELD LENGTHENGINE MODEL PW1921G

FLAP 5ISA 0

SURFACE TYPE NORMALRUNWAY CONDITION DRY

FA

CT

OR

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LA

ND

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DIS

TA

NC

E -

m

MAXIMUM LANDING WEIGHT - kg

32000 36000 40000 44000 48000 52000 56000 60000 640001000

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Hp 10000 ft

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Hp 14000 ft





EM

170E

2A

PM

030019A

.ID

R


FLAP 5ISA + 15˚C


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32000 36000 40000 44000 48000 52000 56000 6400060000

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FA

CT

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EM

170E

2AP

M03

0018

A.ID

R

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HP 8000 ft

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Hp 0 ft


FLAP FULLISA 0


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EM

170E

2A

PM

030017A

.ID

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FLAP FULLISA + 15˚C


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E

- m

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Hp 0 ft





EM

170E

2AP

M03

0024

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LANDING FIELD LENGTHENGINE MODEL PW1923G AND PW1923G-A

FLAP 5ISA 0


Hp 14000 ft

Hp 12000 ft

Hp 10000 ft

Hp 8000 ft

Hp 6000 ft

Hp 4000 ft

Hp 2000 ft

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Hp -1870 ft





EM

170E

2A

PM

030023A

.ID

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Hp 6000 ft

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EM

170E

2AP

M03

0022

A.ID

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Hp -1870 ft





EM

170E

2A

PM

030021A

.ID

R

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FLAP FULLISA + 15˚C


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




4. GROUND MANEUVERING

EFFECTIVITY: ALL


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.


E-JETS E2 - APM 5824 SECTION 04 Page 1 of 14Rev 14 - Aug 09/19


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




4.3. MINIMUM TURNING RADII




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


R1

R2

R3

R6

R4


R4

STEERING ANGLE




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



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




EFFECTIVITY: EMBRAER 195-E2 ACFTMinimum Turning Radius Figure 4.4

EM

170E

2AP

M04

0011

A.ID

R

R3

R6

R5

R4

R2

R1


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


STEERING ANGLE

ACTUAL OPERATING DATA MAY BE GREATER THAN VALUES SHOWNSINCE TIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS.

NOTE:




4.4. VISIBILITY FROM COCKPIT




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




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).




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.)




EFFECTIVITY: ALL90° Turn - Runway to Taxiway Figure 4.7

EM

170E

2AP

M04

0005

A.ID

R


100 ft RADIUS(30 m)

100 ft RADIUS(147 ft 7.6 in.)

NOTE:

PATH OF MAIN LANDINGGEAR TIRE EDGE.


15 m(49 ft 2 in.)

90˚

45 m(147 ft 7.6 in.)




EFFECTIVITY: ALL90° Turn - Taxiway to Taxiway Figure 4.8

EM

170E

2A

PM

040006A

.ID

R


NOTE:


15 m(49 ft 2 in.)

15 m(49 ft 2 in.)

100 ft RADIUS(30 m)

90˚


3 m(9 ft 10 in.)




4.6. RUNWAY HOLDING APRON




EFFECTIVITY: ALLRunway Holding Bay Figure 4.9

EM

170E

2AP

M04

0007

A.ID

R

75 m(246 ft)


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.




5. TERMINAL SERVICING

EFFECTIVITY: ALL


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.


• 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


E-JETS E2 - APM 5824 SECTION 05 Page 1 of 20Rev 11 - Nov 09/18


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




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



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)




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


2 - PASSENGER STAIR3 - BAGGAGE LOADER4 - BAGGAGE CARGO6 - FUEL SERVICE7 - POTABLE WATER




11 - GALLEY SERVICE ADJUSTABLE LEFT RAMP11 - GALLEY SERVICE LEFT RAMP

RAMP (REF)

1

1.82 m(5.97 ft)





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)


1


2 - PASSENGER STAIR3 - BAGGAGE LOADER4 - BAGGAGE CARGO


6 - FUEL SERVICE7 - POTABLE WATER


10 - GPU (GROUND POWER UNIT)12 - GALLEY SERVICE ADJUSTABLE RIGHT RAMP 12 - GALLEY SERVICE

RIGHT RAMP

RAMP (REF)




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.




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




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




5.4. TERMINAL OPERATIONS - EN ROUTE STATION

Not Applicable

5.5. GROUND SERVICING CONNECTIONS




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



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




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



ENGINE AIR STARTING

AIR CONDITIONING LOW PRESSURE





RIGHT GRAVITY FUEL PORT

LEFT GRAVITY FUEL PORT


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:




5.6. ENGINE STARTING PNEUMATIC REQUIREMENTS




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




5.7. GROUND PNEUMATIC POWER REQUIREMENTS




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)




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.




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)






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)





LEGEND:

PRE-CONDITIONED AIRFLOW REQUIREMENTS

TO

TA

L A

IRF

LOW




5.9. GROUND TOWING REQUIREMENTS




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)




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




6. OPERATION CONDITIONS

EFFECTIVITY: ALL

6.1. OPERATING CONDITIONS


• The jet engine exhaust velocities;

• The airport and community noise levels;

• The hazard areas.

6.2. ENGINE EXHAUST VELOCITIES




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:




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




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




7. PAVEMENT DATA

EFFECTIVITY: ALL


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


E-JETS E2 - APM 5824 SECTION 07 Page 1 of 28Rev 15 - Sep 27/19


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.)




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




7.3. MAXIMUM PAVEMENT LOADS




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


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




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


STATIC ATMOST AFT C.G.

STEADYBRAKING WITH


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




7.4. LANDING GEAR LOADING ON PAVEMENT




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)




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]




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.




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





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


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




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.




EFFECTIVITY: EMBRAER 190-E2 ACFTFlexible Pavement Requirements - LCN Method Figure 7.9

32700 (72091)

EM

170E

2AP

M07

0005

A.ID

R


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)




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


kg (lb)


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)




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.




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

)




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)




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.




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




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.




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)


RADIUS OF RELATIVE STIFFNESS - (cm)

RADIUS OF RELATIVE STIFFNESS - (in.)

4 40040

32700 (72091)

56600 (124782)


kg (lb)



EM

170E

2AP

M07

0009

A.ID

R




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)



kg (lb)




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).




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




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


72000 80000 88000 96000 104000 112000 120000 128000 136000

MEDIUM-CBR=10%LOW-CBR=6%ULTRA LOW-CBR=3%

SUBGRADE STRENGTH

HIGH-CBR=15%




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


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)




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


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




8. POSSIBLE EMBRAER 196 DERIVATIVE AIRCRAFT

EFFECTIVITY: EMBRAER 175-E2, 190-E2 AND 195-E2 SERIES ACFT

8.1. NOT APPLICABLE




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




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



HIGH PRESSURE AIR GROUND SUPPLY






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





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









CARGO DOOR

MAIN LANDING GEAR

NOSE LANDING GEAR

PASSENGER DOOR

14 SERVICE DOOR


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






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









CARGO DOOR

MAIN LANDING GEAR

NOSE LANDING GEAR

PASSENGER DOOR

14 SERVICE DOOR


1

34

8

13

12

14

107

9111110

6

145

13

2





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









CARGO DOOR

MAIN LANDING GEAR

NOSE LANDING GEAR

PASSENGER DOOR

14 SERVICE DOOR


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





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









CARGO DOOR

MAIN LANDING GEAR

NOSE LANDING GEAR

PASSENGER DOOR

14 SERVICE DOOR


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




PLANNING MANUAL 22 SEPTEMBER 2017 AIRPORT APM - 5824

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