Apm-1346 08 December 2003 Revision 17 - 09 October 2015

EMBRAER S.A - P.O. BOX 8050 12227-901 SAO JOSE DOS CAMPOS - S.P. BRAZIL PHONE:++55123927-7517 FAX:++55123927-7546 http://www.embraer.com e-mail: [email protected] AIRPORT PLANNING MANUAL

In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose. 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 to the EAR and other laws regulations is strictly forbidden. The above restrictions may apply to data on all pages of this document.

APM-1346 08 DECEMBER 2003 REVISION 17 - 09 OCTOBER 2015

EMBRAER S.A. AV. BRIGADEIRO FARIA LIMA, 2.170 - CAIXA POSTAL 8050 - TELEFONE (55) 12 39277517 FAX (55) 12 39277546 - CEP 12.227-901 - SÃO JOSÉ DOS CAMPOS - SÃO PAULO - BRASIL e-mail: [email protected] - http://www.embraer.com

TO: HOLDERS OF PUBLICATION No. APM-1346 - ″AIRPORT PLANNING MANUAL″.

FRONT MATTER - REVISION No. 17 DATED OCTOBER 09/2015

Pages which have been added, revised, or deleted by the current revision are indicated by an asterisk, on the List of Effective Pages. This issue incorporates all preceding Temporary Revisions (if any). Modifications introduced by this revision are all editorial in nature, with no technical implications, they not being therefore highlighted and no substantiation source being presented herein.

Page1of2 HIGHLIGHTS Oct 09/15

AIRPORT PLANNING MANUAL

RECORD OF REVISIONS The user must update the Record of Revisions when a revision is put into the manual.

REV ISSUE DATE REV ISSUE DATE BY BY No. DATE INSERTED No. DATE INSERTED

RETAIN THIS RECORD IN THE FRONT OF MANUAL OR CHAPTER. ON RECEIPT OF REVISIONS, INSERT REVISED PAGES IN THE MANUAL, AND ENTER REVISION NUMBER, DATE INSERTED AND INITIALS. w-apm1346

AIRPORT PLANNING MANUAL

RECORD OF TEMPORARY REVISIONS

Temporary Page Issued Date By By Rev. No. Number Date Removed w-apm1346

AIRPORT PLANNING MANUAL

TEMPORARY REVISION STATUS REPORT

This list is intended to show the operator which temporary revisions are applicable to his fleet. The list consists of the temporary revision number, the related issue date, the incorporation date, and the affected subject.

S* INDICATES TR HAS BEEN SUPERSEDED BY THE TR REFERRED TO.

EFFECTIVITY: ALL TR STATUS REPORT Page 1 / 2

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AIRPORT PLANNING MANUAL

LIST OF SERVICE BULLETINS

This list is intended to let the operator know which Service Bulletins are incorporated to the APM.

The list consists of the Service Bulletin numbers and the respective revisions (if applicable), the affected section (s) (APM Section Number), information on whether the Service Bulletin affects the manual, the aircraft (Effectivity) affected by the Service Bulletins and the incorporation date.

A revision bar is placed on the left margin of the list whenever data are inserted or revised.

NOTE: The effectivity is indicated by means of two numerical groups separated by a dash. The first group presented in the effectivity column corresponds to the last digits of the lowest aircraft designation number to indicate the beginning of the effectivity, and the second group corresponds to the last digits of the highest aircraft designation number to indicate the end of the effectivity.

SERVICE BULLETIN APM SECTION INCORPORATION EFFECTIVITY NUMBER NUMBER DATE 170:00007-00029, SB 170-53-0080/00 02-1 Oct 07/2014 00045-00047

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Title Section 3 BLOCK PAGE REVISION3-1 ...... Jan 09/06 TRList 3-2 ...... Jan 09/06 1 ...... Oct 22/07 3-3 ...... Oct 31/12 2 Blank ...... Oct 22/07 3-4 ...... Oct 31/12 SBList 3-5 ...... Oct 31/12 * 1 (rev) ...... Oct 09/15 3-6 ...... Oct 31/12 2 Blank ...... Jan 09/06 3-7 ...... Oct 31/12 List of Effective Pages 3-8 ...... Oct 07/14 * 1 (rev) ...... Oct 09/15 3-9 ...... Oct 07/14 * 2 (rev) ...... Oct 09/15 3-10 ...... Oct 07/14 Table of Contents 3-11 ...... Oct 07/14 1 ...... Oct 31/12 3-12 ...... Oct 07/14 2 ...... Jan 09/06 3-13 ...... Oct 07/14 List of Tables 3-14 ...... Oct 07/14 1 ...... Dec 18/06 3-15 ...... Oct 07/14 2 Blank ...... Dec 08/03 3-16 ...... Oct 31/12 List of Figures 3-17 ...... Oct 31/12 1 ...... Oct 31/12 3-18 ...... Oct 31/12 2 ...... Oct 31/12 3-19 ...... Oct 31/12 3 ...... Oct 31/12 3-20 ...... Oct 31/12 4 Blank ...... Dec 08/03 Section 4 Section 1 4-1 ...... Oct 07/08 1-1 ...... Jan 09/06 4-2 ...... Oct 07/08 1-2 ...... Oct 06/11 4-3 ...... Oct 07/08 1-3 ...... Oct 06/11 4-4 ...... Jul 01/05 1-4 Blank ...... Dec 08/03 4-5 ...... Oct 07/08 Section 2 4-6 ...... Dec 08/03 2-1 ...... Oct 07/08 4-7 ...... Dec 08/03 2-2 ...... Oct 06/11 4-8 ...... Dec 08/03 2-3 ...... Oct 07/08 4-9 ...... Dec 08/03 2-4 ...... May 11/07 4-10 Blank ...... Dec 08/03 2-5 ...... Dec 08/03 Section 5 2-6 ...... Jan 09/06 5-1 ...... Dec 08/03 2-7 ...... Jan 09/06 5-2 ...... Dec 08/03 2-8 ...... Jan 09/06 5-3 ...... Dec 08/03 * 2-9 (rev) ...... Oct 09/15 5-4 ...... Dec 08/03 2-10 ...... Oct 07/08 5-5 ...... May 11/07 2-11 ...... Dec 18/04 5-6 ...... Dec 08/03 2-12 ...... Dec 18/04 5-7 ...... May 11/07 2-13 ...... Dec 18/04 5-8 ...... May 11/07 2-14 ...... Jun 29/06 5-9 ...... Oct 06/11 2-15 (del) ...... Dec 18/04 5-10 ...... Oct 06/11 2-16 (del) ...... Dec 18/04 5-11 ...... Oct 06/11 2-17 (del) ...... Dec 18/04 5-12 ...... Oct 06/11 2-18 (del) ...... Dec 18/04 5-13 ...... Oct 06/11 2-19 (del) ...... Dec 18/04 5-14 Blank ...... Oct 06/11 2-20 (del) ...... Dec 18/04 Section 6

Pages revised or added by the current revision are indicated by an asterisk (*). Pages deleted by the current revision are indicated by * (del). Pages deleted by the previous revision are indicated by (del).

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6-1 ...... Dec 08/03 9-6 ...... Dec 08/03 6-2 ...... Dec 08/03 6-3 ...... Dec 08/03 6-4 ...... Dec 08/03 6-5 ...... Dec 08/03 6-6 ...... Jan 09/06 6-7 ...... Jan 09/06 6-8 ...... Dec 18/06 6-9 ...... Jan 09/06 6-10 ...... Oct 07/10 6-11 ...... Oct 07/10 6-12 Blank ...... Oct 07/10 Section 7 7-1 ...... Dec 08/03 7-2 ...... Jul 01/05 7-3 ...... Jul 01/05 7-4 ...... Jul 01/05 7-5 ...... Dec 08/03 7-6 ...... Dec 08/03 7-7 ...... Jul 01/05 7-8 ...... Dec 08/03 7-9 ...... Dec 08/03 7-10 ...... Jul 01/05 7-11 ...... Dec 08/03 7-12 ...... Dec 08/03 7-13 ...... Jul 01/05 7-14 ...... Dec 08/03 7-15 ...... Dec 08/03 7-16 ...... Dec 08/03 7-17 ...... Dec 08/03 7-18 ...... Jul 01/05 7-19 ...... Dec 08/03 7-20 ...... Dec 08/03 7-21 ...... Oct 06/11 7-22 ...... Oct 06/11 7-23 ...... Oct 06/11 7-24 ...... Oct 06/11 7-25 ...... Oct 06/11 7-26 Blank ...... Oct 06/11 Section 8 8-1 ...... Dec 08/03 8-2 Blank ...... Dec 08/03 Section 9 9-1 ...... Dec 08/03 9-2 ...... Dec 08/03 9-3 ...... Dec 08/03 9-4 ...... Dec 08/03 9-5 ...... Dec 08/03

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TABLE OF CONTENTS

SECTION 1 - SCOPE

1. Scope ...... 1-1 1.1. Purpose ...... 1-1 1.2. Introduction ...... 1-1 1.3. Abbreviations ...... 1-2

SECTION 2 - AIRCRAFT DESCRIPTION

2. Aircraft Description ...... 2-1 2.1. Aircraft Characteristics ...... 2-1 2.2. General Aircraft Dimensions ...... 2-3 2.3. Ground Clearances ...... 2-5 2.4. Interior Arrangement ...... 2-8 2.5. Passenger Cabin Cross Section ...... 2-11 2.6. Lower Compartment Containers ...... 2-13 2.7. Door Clearances ...... 2-14

SECTION 3 - AIRCRAFT PERFORMANCE

3. Aircraft Performance ...... 3-1 3.1. General Information ...... 3-1 3.2. Payload X Range ...... 3-2 3.3. Takeoff Field Lengths ...... 3-7 3.4. Landing Field Lengths ...... 3-16

SECTION 4 - GROUND MANEUVERING

4. Ground Maneuvering ...... 4-1 4.1. General Information ...... 4-1 4.2. Turning Radii ...... 4-1 4.3. Minimum Turning Radii ...... 4-3 4.4. Visibility From Cockpit ...... 4-4 4.5. Runway and Taxiway Dimensions ...... 4-5 4.6. Runway Holding Bay ...... 4-9

SECTION5-TERMINAL SERVICING

5. Terminal Servicing ...... 5-1 5.1. Aircraft Servicing Arrangement ...... 5-2 5.2. Terminal Operations - Turnaround Station ...... 5-4 5.3. Terminal Operations - En Route Station ...... 5-6 5.4. Ground Servicing Connections ...... 5-7 5.5. Engine Starting Pneumatic Requirements ...... 5-9 5.6. Ground Pneumatic Power Requirements ...... 5-10 5.7. Preconditioned Airflow Requirements ...... 5-11 5.8. Ground Towing Requirements ...... 5-13

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SECTION 6 - OPERATING CONDITIONS

6. Operating Conditions ...... 6-1 6.1. Engine Exhaust Velocities and Temperatures ...... 6-2 6.2. Airport and Community Noise ...... 6-8 6.3. Hazard Areas ...... 6-9

SECTION 7 - PAVEMENT DATA

7. Pavement Data ...... 7-1 7.1. General Information ...... 7-1 7.2. Footprint ...... 7-2 7.3. Maximum Pavement Loads ...... 7-3 7.4. Landing Gear Loading on Pavement ...... 7-4 7.5. Flexible Pavement Requirements, U.S. Corps of Engineers Design Method ...... 7-5 7.6. Flexible Pavement Requirements, LCN Method ...... 7-8 7.7. Rigid Pavement Requirements, Portland Cement Association Design Method ...... 7-11 7.8. Rigid Pavement Requirements, LCN Method ...... 7-14 7.9. ACN - PCN System - Flexible and Rigid Pavements ...... 7-19

SECTION 8 - POSSIBLE EMBRAER 170 DERIVATIVE AIRCRAFT

8. Possible EMBRAER 170 Derivative Aircraft ...... 8-1 8.1. Not Applicable ...... 8-1

SECTION 9 - SCALED DRAWINGS

9. Scaled Drawings ...... 9-1 9.1. General ...... 9-1

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LIST OF TABLES

TABLE TITLE SECTION PAGE

1.1 APM Arrangement ...... 01 1

2.1 Aircraft General Characteristics ...... 02 2

2.2 Aircraft General Characteristics ...... 02 2

2.3 Ground Clearance - STD Aircraft Model ...... 02 6

2.4 Ground Clearance - LR, SU or SE Aircraft Models ...... 02 7

2.5 Capacity of the Cargo Compartment ...... 02 10

3.1 ISA ...... 03 1

4.1 Reference Codes...... 04 5

7.1 Pavement Evaluation...... 07 19

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LIST OF FIGURES

FIGURE TITLE SHEET SECTION PAGE

2.1 General Aircraft Dimensions ...... 02 4

2.2 Ground Clearances ...... 02 5

2.3 Typical Interior Arrangements ...... 02 9

2.4 Economy Class Passenger Cabin Cross-Section...... 02 11

2.5 First Class Passenger Cabin Cross-Section...... 02 12

2.6 Door Dimensions...... 02 14

3.1 Payload x Range - ISA Conditions ...... 03 3

3.2 Payload x Range - ISA + 10 °C Conditions ...... 03 4

3.3 Payload x Range - ISA Conditions ...... 03 5

3.4 Payload x Range - ISA + 10 °C Conditions ...... 03 6

3.5 Takeoff Field Lengths - ISA Conditions ...... 03 8

3.6 Takeoff Field Lengths - ISA + 15 °C Conditions...... 03 9

3.7 Takeoff Field Lengths - ISA Conditions ...... 03 10

3.8 Takeoff Field Lengths - ISA + 15 °C Conditions...... 03 11

3.9 Takeoff Field Lengths - ISA Conditions ...... 03 12

3.10 Takeoff Field Lengths - ISA + 15 °C Conditions...... 03 13

3.11 Takeoff Field Lengths - ISA Conditions ...... 03 14

3.12 Takeoff Field Lengths - ISA + 15 °C Conditions...... 03 15

3.13 Landing Field Lengths - Flaps 5 ...... 03 17

3.14 Landing Field Lengths - Flaps Full ...... 03 18

3.15 Landing Field Lengths - Flaps 5 ...... 03 19

3.16 Landing Field Lengths - Flaps Full ...... 03 20

4.1 Turning Radii - No Slip Angle ...... 04 2

4.2 Minimum Turning Radius ...... 04 3

4.3 Visibility from Cockpit in Static Position...... 04 4

4.4 More than 90° Turn - Runway to Taxiway ...... 04 6

4.5 90° Turn - Runway to Taxiway...... 04 7

4.6 90° Turn - Taxiway to Taxiway ...... 04 8

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FIGURE TITLE SHEET SECTION PAGE

4.7 Runway Holding Bay...... 04 9

5.1 Aircraft Servicing Arrangement With Passenger Stairs ...... 05 2

5.2 Aircraft Servicing Arrangement With Passenger Bridge...... 05 3

5.3 Air Terminal Operation - Turnaround Station ...... 05 5

5.4 Ground Servicing Connections ...... 05 7

5.5 Ground Servicing Connections ...... 05 8

5.6 Engine Starting Pneumatic Requirements...... 05 9

5.7 Ground Pneumatic Power Requirements ...... 05 10

5.8 Preconditioned Airflow Requirements ...... 05 12

5.9 Ground Towing Requirements...... 05 13

6.1 Jet Wake Velocity Profile - Takeoff Power ...... 06 2

6.2 Jet Wake Temperature Profile - Takeoff Power ...... 06 3

6.3 Jet Wake Velocity Profile - Ground Idle...... 06 4

6.4 Jet Wake Temperature Profile - Ground Idle ...... 06 5

6.5 Jet Wake Velocity Profile - Breakaway Power...... 06 6

6.6 Jet Wake Temperature Profile - Breakaway Power...... 06 7

6.7 Hazard Areas - Takeoff Power ...... 06 9

6.8 Hazard Areas - Ground Idle...... 06 10

6.9 Hazard Areas - Breakaway Power...... 06 11

7.1 Footprint ...... 07 2

7.2 Maximum Pavement Loads...... 07 3

7.3 Landing Gear Loading on Pavement...... 07 4

7.4 Flexible Pavement Requirements - US Army Corps of En- gineers Design Method ...... 07 6

7.5 Flexible Pavement Requirements - US Army Corps of En- gineers Design Method ...... 07 7

7.6 Flexible Pavement Requirements - LCN Method ...... 07 9

7.7 Flexible Pavement Requirements - LCN Method ...... 07 10

7.8 Rigid Pavement Requirements - Portland Cement Associa- tion Design Method ...... 07 12

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FIGURE TITLE SHEET SECTION PAGE

7.9 Rigid Pavement Requirements - Portland Cement Associa- tion Design Method ...... 07 13

7.10 Radius of Relative Stiffness ...... 07 15

7.11 Radius of Relative Stiffness (other values)...... 07 16

7.12 Rigid Pavement Requirements - LCN Method ...... 07 17

7.13 Rigid Pavement Requirements - LCN Method ...... 07 18

7.14 ACN For Flexible Pavement ...... 07 20

7.15 ACN For Flexible Pavement ...... 07 21

7.16 ACN For Flexible Pavement ...... 07 22

7.17 ACN For Rigid Pavement...... 07 23

7.18 ACN For Rigid Pavement...... 07 24

7.19 ACN For Rigid Pavement...... 07 25

9.1 Scale: 1 Inch Equals 32 Feet...... 09 2

9.2 Scale: 1 Inch Equals 50 Feet...... 09 3

9.3 Scale: 1 Inch Equals 100 Feet...... 09 4

9.4 Scale: 1 to 500...... 09 5

9.5 Scale: 1 to 1000...... 09 6

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AIRPORT PLANNING MANUAL

1. SCOPE

1.1. PURPOSE

This document provides airplane characteristics for general airport planning. Since the operational practices vary among the airlines, specific data should be coordinated with the using airlines before the facility design is made. EMBRAER should be contacted for any additional information required.

1.2. INTRODUCTION

The APM has been prepared in accordance with NAS 3601. It provides aircraft characteristics for general airport planning, airport operators, airlines, and engineer- ing consultant organizations. The APM is arranged as shown in the table below:

Table 1.1 - APM Arrangement ARRANGEMENTS CONTENTS Title Page Costumer Comment Form Highlights Record of Revision Sheet Temporary Revision Sheet Manual Front Matter List of Service Bulletins List of Effective Pages Table of Contents List of Tables List of Figures Scope Aircraft Description Aircraft Performance Ground Maneuvering Section Terminal Servicing Operating Conditions Pavement Data Possible Derivative Aircraft Scaled Drawings

The front matter for the whole manual contains: • Title Page: Shows the manufacturer’s masthead, identification of the manual, the initial issue date, and revision number and date. • Highlights: Advises the operator on the revised pages. • Record of Revisions Sheet: Lists the successive revision numbers, issue date, insertion date and incorporators initials, which must be kept current by the operator.

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• List of Service Bulletins: Lists the Service Bulletins, including all issued revisions, which affect the manual as well as the affected section(s) (APM Section Number), the aircraft affected by the Service Bulletin, and the date of incorporation of the SB in the manual. • Temporary Revision Sheet: Lists the temporary revision numbers, page number, issue date, person responsible for the insertion and insertion date. • List of Effective Pages: Lists all sections and their list of effective pages with the latest issue dates. • 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 P.O. BOX 8050 CEP. 12.227-901- São José dos Campos - SP - Brazil Phone: (55 12) 3927-7517 FAX: (55 12) 3927-7546 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 • For Digital Technical Publications support: [email protected]

1.2.1. Revisions

Embraer may revise this manual periodically as required to update information or provide information not available at the time of printing. Revised data may result from Embraer approved aircraft modifications and new available options. Changes to the text are indicated by a black bar in the page left-side margin, beside the revised, added, or deleted material. Relocated or rearranged text or illustrations will be indicated by a black bar beside the page number.

1.3. ABBREVIATIONS

This list gives all the abbreviations, acronyms and measurement units used in this manual with their definitions.

Table 1.2 - List of Acronyms and Abbreviations used in the APM ACRONYMS AND ABBREVIATIONS DESCRIPTION °C Degree Celsius °F Degree Fahrenheit Liter ACN Aircraft Classification Number AFM Airplane Flight Manual AOM Airplane Operations Manual

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Table 1.2 - List of Acronyms and Abbreviations used in the APM

ACRONYMS AND ABBREVIATIONS DESCRIPTION APM Airport Planning Manual APU Auxiliary Power Unit ATTCS Automatic Takeoff-Thrust Control-System BOW Basic Operating Weight CBR California Bearing Ratio ECS Environmental Control System FAA Federal Aviation Administration FAR Federal Aviation Regulations FWD Forward GEAE General Electric Aircraft Engines ICAO International Civil Aviation Organization ISA International Standard Atmosphere JAR Joint Aviation Requirements LCN Load Classification Number LH Left-Hand LR Long Range MLW Maximum Landing Weight MRW Maximum Ramp Weight MTOW Maximum Takeoff Weight MZFW Maximum Zero Fuel Weight N Newton RBHA Requisitos Brasileiros de Homologação Aeronáutica RH Right-Hand STD Standard dBA A-Weighted Decibel ft Foot ft2 Square Foot ft3 Cubic Foot gal. Gallon in Inch in2 Square Inch inHg Inch of Mercury kPa Kilopascal kg Kilogram lb Pound lb/in3 Pound per Cubic Inch lbf Pound Force m Meter m2 Square Meter m3 Cubic Meter min Minute psi Pounds per Square Inch

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AIRPORT PLANNING MANUAL

2. AIRCRAFT DESCRIPTION

2.1. AIRCRAFT CHARACTERISTICS

The aircraft is: • Predominantly metallic; • Low winged; • Conventional tailed; • Monoplane; • Retractable tricycle-type with twin-wheeled landing-gear.

There are two high bypass ratio turbofan GEAE CF34–8E with 63.2 kN (14200 lbf) maximum takeoff thrust (sea level, static and ISA + 15 °C) installed under the wings. The aircraft has two versions, with different ranges as a function of the difference between the MTOWs: • The STD aircraft model - MTOW 35990 kg (79344 lb) • The LR, SU or SE aircraft models - MTOW 37200 kg (82012 lb)

2.1.1. Definitions

MRW

It is the maximum allowed aircraft weight for taxiing or maneuvering on the ground.

MLW

It is the maximum allowed weight with which the aircraft can 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 emer- gency equipment and other items of equipment that are an integral part of the aircraft 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 the tanks.

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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 Characteristics EFFECTIVITY: ON ACFT 170:00001-00006 00030-00044 00048-00058 00060-00065 OR PRE-MOD SB 170-53-0080 AIRCRAFT MODELS DESIGN WEIGHTS[1] STD LR, SU or SE MRW 36150 kg (79697 lb) 37360 kg (82365 lb) MTOW 35990 kg (79344 lb) 37200 kg (82012 lb) MLW 32800 kg (72311 lb) BOW [2] 20700 kg (45636 lb) MZFW 29600 kg (65257 lb) Maximum Payload [2] 9100 kg (20062 lb) MOW - Minimum Operating Weight 21800 kg (48060 lb) 70 passengers (SE) Maximum Seating Capacity 78 passengers 76 passengers (SU) 78 passengers (LR) Maximum Cargo Volume [3] 14.39 m3 (508.18 ft3) Usable 9428 kg (20785 lb) Fuel [4] 11625 (3071 gal.)

1. Applicable for standard models. For further information, refer to AFM and AOM. 2. 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. Adopted fuel density of 0.811 kg/ (6.77 lb/gal.).

Table 2.2 - Aircraft General Characteristics EFFECTIVITY: ON ACFT 170:00059-00059 00066-99999 OR POST-MOD SB 170-53-0080 AIRCRAFT MODELS DESIGN WEIGHTS[1] STD LR, SU or SE MRW 36150 kg (79697 lb) 37360 kg (82365 lb) MTOW 35990 kg (79344 lb) 37200 kg (82012 lb)

1. Applicable for standard models. For further information, refer to AFM and AOM.

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Table 2.2 - Aircraft General Characteristics (Continued) EFFECTIVITY: ON ACFT 170:00059-00059 00066-99999

AIRCRAFT MODELS DESIGN WEIGHTS[1] STD LR, SU or SE MLW [2] 32800 kg (72311 lb) BOW [3] 20700 kg (45636 lb) MZFW 30140 kg (66447 lb) Maximum 9640 kg (21252 lb) Payload [3] MOW - Minimum Operating Weight 21800 kg (48060 lb) 70 passengers (SE) Maximum Seating Capacity 78 passengers 76 passengers (SU) 78 passengers (LR) Maximum Cargo Volume [4] 14.39 m3 (508.18 ft3) Usable 9428 kg (20785 lb) Fuel [5] 11625 (3071 gal.)

1. Applicable for standard models. For further information, refer to AFM and AOM. 2. For aircraft POST-MOD. S.B. 170-00-0003, consider MLW = 33300 kg (73414 lb). 3. Standard configuration (weights may vary according to optional equipment installed or interior layouts). 4. Standard configuration (volume may vary according to optional equipment installed). 5. Adopted fuel density of 0.811 kg/ (6.77 lb/gal.).

2.2. GENERAL AIRCRAFT DIMENSIONS

2.2.1. External Dimensions • Span over winglets - 26.00 m (85 ft 4 in.) • Height (maximum) - 9.85 m (32 ft 3 in.) • Overall length - 29.90 m (98 ft 1 in.)

2.2.2. Wing • Reference area - 72.72 m2 (783 ft2) • Reference aspect ratio - 8.6

2.2.3. Fuselage • Total Length - 29.90 m (98 ft 1 in.) • Length of pressurized section - 22.74 m (74 ft 7 in.)

2.2.4. Horizontal Tail • Span - 10.00 m (32 ft 9 in) • Area - 23.25 m2 (250 ft2 37 in2)

2.2.5. Vertical Tail • Reference area - 16.20 m2 (174 ft2 55 in2)

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18.23 m (59 ft 9.7 in.)

6.82 m (22 ft 4.5 in.) 9.85 m (32 ft 3 in.)

4.13 m 10.60 m (13 ft 6 in.) (34 ft 9 in.) 29.90 m (98 ft 1 in.)

21.26 m (69 ft 9 in.) 4.27 m (14 ft )

10.00 m (32 ft 9 in.)

4.71 m (15 ft 5.4 in.) 21.26 m (69 ft 9 in.)

16.62 m (54 ft 6 in.)

5.20 m (17 ft) 26.00 m (85 ft 4 in.) EM170APM020003C.DGN

General Aircraft Dimensions Figure 2.1

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2.3. GROUND CLEARANCES

A FUSLG ANGLE L (REF.)

M B

J K E H C D

F EM170APM020005.DGN

Ground Clearances Figure 2.2 Section 2 EFFECTIVITY: ALL Page 2-5 Dec 08/03 b-apm1346 FETVT:ALL EFFECTIVITY: Table 2.3 - Ground Clearance - STD Aircraft Model FOR- TAIL SKID FOR- FOR- FUS WARD AFT AFT SER- AFT PAS- VERTI- ANGULAR CG WARD WARD NACELLE WINGLET WEIGHT ANGLE NOSE (B) PASSEN- CARGO VICE SENGER CAL TAIL CLEAR- (%MAC) SERVICE CARGO (F) (G) (DEG) (A) GER DOOR (H) DOOR (J) DOOR (K) (L) ANCE DOOR (C) DOOR (E) DOOR (D) (DEG) (M) 36150 kg 2.13 m 2.54 m 2.54 m 1.47 m 0.48 m 4.50 m 1.48 m 2.45 m 2.45 m 9.65 m 10 0.3 12.6 79697 lb 7ft 8ft4in. 8ft4in. 4ft10in. 1ft6in. 14 ft 9 in. 4ft10in. 8ft 8ft 31 ft 8 in. 36150 kg 2.20 m 2.58 m 2.58 m 1.49 m 0.49 m 4.47 m 1.45 m 2.41 m 2.41 m 9.57 m 27 0.6 12.3 79697 lb 7ft2in. 8ft5in. 8ft5in. 4ft11in. 1ft7in. 14 ft 8 in. 4ft9in. 7ft10in. 7ft10in. 31 ft 5 in. 35990 kg 2.13 m 2.54 m 2.54 m 1.47 m 0.48 m 4.50 m 1.48 m 2.45 m 2.45 m 9.65 m 9.8 0.3 12.7 79344 lb 7ft 8ft4in. 8ft4in. 4ft10in. 1ft6in. 14 ft 9 in. 4ft10in. 8ft 8ft 31 ft 8 in. 35990 kg 2.20 m 2.58 m 2.58 m 1.49 m 0.49 m 4.47 m 1.45 m 2.41 m 2.41 m 9.57 m 27 0.6 12.3 79344 lb 7ft2in. 8ft5in. 8ft5in. 4ft11in. 1ft7in. 14 ft 8 in. 4ft9in. 7ft10in. 7ft10in. 31 ft 5 in. 32800 kg 2.13 m 2.55 m 2.54 m 1.48 m 0.49 m 4.53 m 1.50 m 2.48 m 2.48 m 9.69 m 7 0.2 12.8 72311 lb 7ft 8ft4in. 8ft4in. 4ft11in. 1ft7in. 14 ft 10 in. 4ft11in. 8ft2in. 8ft2in. 31 ft 9 in. 32800 kg 2.20 m 2.59 m 2.59 m 1.50 m 0.50 m 4.49 m 1.47 m 2.43 m 2.43 m 9.60 m 27 0.6 12.4 72311 lb 7ft2in. 8ft6in. 8ft6in. 4ft11in. 1ft6in. 14 ft 9 in. 4ft10in. 8ft 8ft 31 ft 6 in. 9.72 m 29600 kg 2.13 m 2.55 m 2.55 m 1.49 m 0.51 m 4.55 m 1.52 m 2.50 m 2.50 m 7 0.2 31 ft 10 12.9 65257 lb 7ft 8ft4in. 8ft4in. 4ft11in. 1ft8in. 14 ft 11 in. 4ft11in. 8ft2in. 8ft2in. in.

29600 kg 2.21 m 2.60 m 2.60 m 1.52 m 0.52 m 4.51 m 1.49 m 2.45 m 2.45 m 9.62 m MANUAL PLANNING AIRPORT 27 0.5 12.5 65257 lb 7ft3in. 8ft6in. 8ft6in. 4ft11in. 1ft8in. 14 ft 9 in. 4ft10in. 8ft1in. 8ft1in. 31 ft 7 in. 21800 kg 2.15 m 2.58 m 2.58 m 1.52 m 0.56 m 4.62 m 1.60 m 2.59 m 2.59 m 9.83 m 70 13.4 48061 lb 7ft1in. 8ft6in. 8ft6in. 4ft11in. 1ft10in. 15 ft 2 in. 5ft3in. 8ft6in. 8ft6in. 32 ft 3 in. 9.71 m 21800 kg 2.24 m 2.64 m 2.63 m 1.56 m 0.57 m 4.58 m 1.55 m 2.52 m 2.52 m 27 0.4 31 ft 10 12.9 48061 lb 7ft5in. 8ft8in. 8ft7in. 5ft1in. 1ft10in. 15 ft 5ft1in. 8ft3in. 8ft3in. in. eto 2 Section a 09/06 Jan ae2-6 Page

w-apm1346 w-apm1346

FETVT:ALL EFFECTIVITY: Table 2.4 - Ground Clearance - LR, SU or SE Aircraft Models TAIL SKID FOR- FOR- FOR- ANGU- FUS WARD AFT AFT SER- AFT PAS- VERTI- CG WARD WARD NACELLE WINGLET LAR WEIGHT ANGLE NOSE (B) PASSEN- CARGO VICE SENGER CAL TAIL (%MAC) SERVICE CARGO (F) (G) CLEAR- (DEG) (A) GER DOOR (H) DOOR (J) DOOR (K) (L) DOOR (C) DOOR (E) ANCE DOOR (D) (DEG) (M) 37360 kg 2.14 m 2.54 m 2.54 m 1.47 m 0.48 m 4.49 m 1.47 m 2.44 m 2.44 m 9.63 m 11.8 0.4 12.6 82365 lb 7ft 8ft4in 8ft4in 4ft10in 1ft6in 14 ft 10 in 4ft10in 8ft 8ft 31 ft 7 in 37360 kg 2.19 m 2.58 m 2.57 m 1.49 m 0.48 m 4.47 m 1.44 m 2.40 m 2.40 m 9.56 m 27 0.6 12.3 82362 lb 7ft2in. 8ft5in. 8ft5in. 4ft11in. 1ft6in. 14 ft 8 in. 4ft9in. 7ft10in. 7ft10in. 31 ft 4 in. 37200 kg 2.14 m 2.54 m 2.54 m 1.47 m 0.48 m 4.49 m 1.47 m 2.44 m 2.44 m 9.64 m 11.8 0.4 12.6 82011 lb 7ft 8ft4in. 8ft4in. 4ft10in. 1ft6in. 14 ft 10 in. 4ft10in. 8ft 8ft 31 ft 8 in. 37200 kg 2.19 m 2.58 m 2.57 m 1.49 m 0.48 m 4.47 m 1.44 m 2.40 m 2.40 m 9.56 m 27 0.6 12.3 82011 lb 7ft2in. 8ft5in. 8ft5in. 4ft11in. 1ft6in. 14 ft 8 in. 4ft9in. 7ft10in. 7ft10in. 31 ft 4 in. 32800 kg 2.13 m 2.55 m 2.54 m 1.48 m 0.49 m 4.53 m 1.50 m 2.48 m 2.48 m 9.69 m 7 0.2 12.8 72311 lb 7ft 8ft4in. 8ft4in. 4ft11in. 1ft7in. 14 ft 10 in. 4ft11in. 8ft2in. 8ft2in. 31 ft 9 in. 32800 kg 2.20 m 2.59 m 2.59 m 1.50 m 0.50 m 4.49 m 1.47 m 2.43 m 2.43 m 9.60 m 27 0.6 12.4 72311 lb 7ft2in. 8ft6in. 8ft6in. 4ft11in. 1ft6in. 14 ft 9 in. 4ft10in. 8ft 8ft 31 ft 6 in. 29600 kg 2.13 m 2.55 m 2.55 m 1.49 m 0.51 m 4.55 m 1.52 m 2.50 m 2.50 m 9.72 m 7 0.2 12.9 65257 lb 7ft 8ft4in. 8ft4in. 4ft11in. 1ft8in. 14 ft 11 in. 4ft11in. 8ft2in. 8ft2in. 31 ft 10 in.

29600 kg 2.21 m 2.60 m 2.60 m 1.52 m 0.52 m 4.51 m 1.49 m 2.45 m 2.45 m 9.62 m MANUAL PLANNING AIRPORT 27 0.5 12.5 65257 lb 7ft3in. 8ft6in. 8ft6in. 4ft11in. 1ft8in. 14 ft 9 in. 4ft10in. 8ft1in. 8ft1in. 31 ft 7 in. 21800 kg 2.15 m 2.58 m 2.58 m 1.52 m 0.56 m 4.62 m 1.60 m 2.59 m 2.59 m 9.83 m 70 13.4 48061 lb 7ft1in. 8ft6in. 8ft6in. 4ft11in. 1ft10in. 15 ft 2 in. 5ft3in. 8ft6in. 8ft6in. 32 ft 3 in. 21800 kg 2.24 m 2.64 m 2.63 m 1.56 m 0.57 m 4.58 m 1.55 m 2.52 m 2.52 m 9.71 m 27 0.4 12.9 48061 lb 7ft5in. 8ft8in. 8ft7in. 5ft1in. 1ft10in. 15 ft 5ft1in. 8ft3in. 8ft3in. 31 ft 10 in. eto 2 Section a 09/06 Jan ae2-7 Page AIRPORT PLANNING MANUAL

2.4. INTERIOR ARRANGEMENT

The interior arrangement provides accommodation for two pilots, one observer, two flight attendants, and 70 passengers in 32 in pitch standard configuration. One additional flight attendant seat is available as an option.

2.4.1. Passenger Cabin

The passenger cabin accommodates 70 passengers in 17 double seats on the LH side, and 18 double seats on the RH side. As an option, the passenger cabin can be provided with double first-class seats on the RH side and single first-class seats on the LH side. The main dimensions of the passenger cabin are presented below: • Height - 2.00 m (6 ft 7 in.) • Width - 2.74 m (9 ft) • Aisle width - 0.49 m (1 ft 7 in.) • Pitch - 0.82 m (32 in.)

Section 2 EFFECTIVITY: ALL Page 2-8 Jan 09/06 w-apm1346 AIRPORT PLANNING MANUAL

4 9 5 3

0.90 m 0.88 m 0.78 m (2 ft 11.4 in.) (2 ft 10.6 in.) (2 ft 6.7 in.) 8 8 1.82 m 2.41 m 1.31 m 1.85 m (5 ft 11.7 in) (7 ft 11.4 in.) (4 ft 3.6 in.) (6 ft 07 in.) 5.41 m 4.30 m (17 ft 9 in.) (14 ft 1.3 in.) 19.44 m (63 ft 9 in.)

3 410 5

0.81 m 1 7 61211 (2 ft 8 in.)

1 − FLIGHT ATTENDANT SEAT 7 − AFT LAVATORY 2 − WARDROBE 8 − CARGO COMPARTMENT

3 − FWD RH G1 GALLEY 9 − OVERHEAD BIN 4 − FWD RH G2 GALLEY 10 − PASSENGER SEAT 5 − AFT RH GALLEY 11 − AIRSTAIR STOWAGE

6 − FWD LAVATORY

CARGO/BAGGAGE VOLUME

3 3 CARGO COMPARTMENT 14.39 m (508.18 ft )

3 3 OVERHEAD BIN 0.06 m / pax (2.0 ft / pax)

3 3 UNDERSEAT VOLUME 0.04 m / pax (1.4 ft / pax) EM170APM020004D.DGN

Typical Interior Arrangements Figure 2.3

Section 2 EFFECTIVITY: ALL Page 2-9 Oct 09/15 w-apm1346 AIRPORT PLANNING MANUAL

2.4.2. Cargo Compartments

Two cargo compartments located underfloor are available, one forward of the wing, and the other aft of the wing. The cargo compartments comply with the FAR-25/JAR-25/RBHA-25 “class C” compartment classification. The table below contains the capacity of the cargo compartment:

Table 2.5 - Capacity of the Cargo Compartment CARGO COMPARTMENT LOADING VOLUME FWD [1] 1370 kg (3020 lb) 8.59 m3 (303.35 ft3) AFT 1030 kg (2270 lb) 5.80 m3 (204.83 ft3) Total 2400 kg (5290 lb) 14.39 m3 (508.18 ft3)

1. Standard configuration (loading and volume may vary according to optional equipment installed).

The cargo compartments are provided with the following features: • Optional vertical nets; • Door net at each cargo door.

2.4.3. Cockpit

The cockpit is acoustically and thermally insulated for appearance and durability. It follows the worldwide trend of rounded edges to avoid harm to the flight crew. The cockpit is separated from the passenger cabin by a bulkhead provided with a lockable door. The cockpit door has a locking system, which can only be opened from the cockpit side, a peep hole and an escape mechanism on the cockpit side.

Section 2 EFFECTIVITY: ALL Page 2-10 Oct 07/08 w-apm1346 AIRPORT PLANNING MANUAL

2.5. PASSENGER CABIN CROSS SECTION

0.78 m (2 ft 7 in.)

0.46 m 0.05 m (1 ft 6 in.) (2.0 in.) 2.00 m (6 ft 7 in.)

1.44 m (4 ft 9 in.)

3.35 m (11 ft 0 in.) 0.49 m

(1 ft 7 in.)

1.66 m 0.45 m (5 ft 5 in.) (1 ft 6 in.) 0.94 m 2.72 m (3 ft 1 in.) (8 ft 11 in.)

0.75 m (2 ft 5 in.)

2.74 m (9 ft) 3.01 m (9 ft 11 in.) EM170APM020001A.DGN

Economy Class Passenger Cabin Cross-Section Figure 2.4

Section 2 EFFECTIVITY: ALL Page 2-11 Dec 18/04 w-apm1346 AIRPORT PLANNING MANUAL

0.86 m (3 ft)

2.00 m (6 ft 7 in.) 0.6 m 0.69 m (1 ft 10 in.) (2 ft 3 in.) 0.20 m 0.51 m 0.07 m 1.44 m (8 in.) (1 ft 8 in.) (3 in.) (4 ft 9 in.) 1.1 m (3 ft 8 in.) 3.35 m (11 ft 0 in.) 0.61 m (2 ft)

1.66 m 0.45 m (5 ft 5 in.) (1 ft 6 in.) 0.94 m 2.72 m (3 ft 1 in.) (8 ft 11 in.)

0.75 m (2 ft 5 in.)

2.74 m (9 ft) 3.01 m (9 ft 11 in.) EM170APM020002A.DGN

First Class Passenger Cabin Cross-Section Figure 2.5

Section 2 EFFECTIVITY: ALL Page 2-12 Dec 18/04 w-apm1346 AIRPORT PLANNING MANUAL

2.6. LOWER COMPARTMENT CONTAINERS

Not applicable

Section 2 EFFECTIVITY: ALL Page 2-13 Dec 18/04 w-apm1346 AIRPORT PLANNING MANUAL

2.7. DOOR CLEARANCES

1.71 m (5 ft 7.3 in.) 1.82 m (5 ft 11.6 in.) 1.36 m 1.37 m (4 ft 5.5 in.) (4 ft 5.9 in.)

SEE FIGURE 2.2 FOR HEIGHT ABOVE 0.87 m 0.78 m GROUND 0.90 m (2 ft 10 in.) (2 ft 6.7 in.) (2 ft 11.4 in.)

1.10 m 0.99 m (3 ft 7.3 in.) (3 ft 3 in.) 0.61 m 0.63 m (2 ft 0 in.) (2 ft 0.8 in.)

0.75 m 0.63 m (2 ft 6.7 in.) (2 ft 0.8 in.)

NOTE: FOR DIMENSIONS OF ALL DOORS, CONSIDER THAT AIRCRAFT IS IN OPERATION, THAT IS, EQUIPPED WITH DOOR LININGS AND DOOR SURROUNDS. EM170APM020008C.DGN

Door Dimensions Figure 2.6 Section 2 EFFECTIVITY: ALL Page 2-14 Jun 29/06 w-apm1346 AIRPORT PLANNING MANUAL

3. AIRCRAFT PERFORMANCE

3.1. GENERAL INFORMATION

The performance of the aircraft and engine depends on the generation of forces by the interaction between the aircraft or engine, and the air mass through which it flies. The atmosphere has a pronounced effect on the temperature, pressure and density of the air. The ICAO establishes standard basics for estimating and comparing aircraft and engine performance. Some ICAO standard basics 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 mft°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

NOTE: For other charts containing payload x ranges, takeoff field lengths and/or landing field lengths with conditions different from those presented in this section, Embraer should be contacted so that these charts can be obtained.

Section 3 EFFECTIVITY: ALL Page 3-1 Jan 09/06 w-apm1346 AIRPORT PLANNING MANUAL

3.2. PAYLOAD X RANGE

The payload x range charts are based on the following conditions; • CF34 - 8E5 and CF34 - 8E5A1 engine models; • Aircraft carrying passengers at 100 kg (220 lb) each one; • Flight level 350, that represents the cruising altitude equal to 10668 m (35000 ft); • Atmosphere according to ISA or ISA + 10 °C conditions; • MTOW.

Section 3 EFFECTIVITY: ALL Page 3-2 Jan 09/06 w-apm1346 AIRPORT PLANNING MANUAL

PAYLOAD VS RANGE CF34 − 8E5A1 & − 8E5 ENGINES FLIGHT LEVEL 350 ISA RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 35990 kg (79344 lb)

22000 10000

21000

20000 9000

19000

18000 8000 17000

16000 7000 70 PAX @ 100 kg 15000

14000 6000 13000

12000

11000 5000 PAYLOAD − kg

PAYLOAD − lb 10000 0.78 MACH 9000 4000

8000

7000 LONG RANGE 3000 6000

5000 2000 4000 MAX CRUISE 3000 1000 2000

1000

0 0 0 500 1000 1500 2000 2500 3000 RANGE − nm NOTES: MAX TAKEOFF WEIGHT 35990 kg (79344 lb) MAX ZERO FUEL WEIGHT 30140 kg (66447 lb) BASIC OPERATING WEIGHT 20736 kg (45715 lb)

MAX USABLE FUEL 9428 Kg (20785 lb) EM170APM030003D.DGN

Payload x Range - ISA Conditions Figure 3.1

Section 3 EFFECTIVITY: EMBRAER 170 STD ACFT MODEL Page 3-3 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

PAYLOAD VS RANGE CF34 − 8E5A1 & − 8E5 ENGINES FLIGHT LEVEL 350 ISA + 10°C RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 35990 kg (79344 lb)

22000 10000

21000

20000 9000

19000

18000 8000 17000

16000 7000 70 PAX @ 100 kg 15000

14000 6000 13000

12000

11000 5000 PAYLOAD − lb PAYLOAD − kg 10000

9000 4000 0.78 MACH

8000

7000 3000 6000 LONG RANGE 5000 2000 4000

3000 MAX CRUISE

2000 1000

1000

0 0 0 500 1000 1500 2000 2500 3000 RANGE − nm NOTES: MAX TAKEOFF WEIGHT 35990 kg (79344 lb) MAX ZERO FUEL WEIGHT 30140 kg (66447 lb) BASIC OPERATING WEIGHT 20736 kg (45715 lb)

MAX USABLE FUEL 9428 Kg (20785 lb) EM170APM030004D.DGN

Payload x Range - ISA + 10 °C Conditions Figure 3.2

Section 3 EFFECTIVITY: EMBRAER 170 STD ACFT MODEL Page 3-4 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

PAYLOAD VS RANGE CF34 − 8E5A1 & − 8E5 ENGINES FLIGHT LEVEL 350 ISA RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 37200 kg (82012 lb)

22000 10000

21000

20000 9000

19000

18000 8000 17000

16000 7000 70 PAX @ 100 kg 15000

14000 6000 13000

12000

11000 5000 PAYLOAD − lb 10000 PAYLOAD − kg

9000 4000

8000 0.78 MACH

7000 3000 LONG RANGE 6000 MAX CRUISE 5000 2000 4000

3000 1000 2000

1000

0 0 0 500 1000 1500 2000 2500 3000 RANGE − nm NOTES: MAX TAKEOFF WEIGHT 37200 kg (82012 lb) MAX ZERO FUEL WEIGHT 30140 kg (66447 lb) BASIC OPERATING WEIGHT 20736 kg (45715 lb)

MAX USABLE FUEL 9428 Kg (20785 lb) EM170APM030002D.DGN

Payload x Range - ISA Conditions Figure 3.3

Section 3 EFFECTIVITY: EMBRAER 170 LR ACFT MODEL Page 3-5 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

PAYLOAD VS RANGE CF34 − 8E5A1 & − 8E5 ENGINES FLIGHT LEVEL 350 ISA + 10°C RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 37200 kg (82012 lb)

22000 10000

21000

20000 9000

19000

18000 8000 17000

16000 7000 70 PAX @ 100 kg 15000

14000 6000 13000

12000

11000 5000 PAYLOAD − kg PAYLOAD − lb 10000

9000 4000

8000

7000 0.78 MACH 3000 6000

5000 2000 4000 LONG RANGE

3000

1000 2000 MAX CRUISE 1000

0 0 0 500 1000 1500 2000 2500 3000 RANGE − nm NOTES: MAX TAKEOFF WEIGHT 37200 kg (82012 lb) MAX ZERO FUEL WEIGHT 30140 kg (66447 lb) BASIC OPERATING WEIGHT 20736 kg (45715 lb)

MAX USABLE FUEL 9428 Kg (20785 lb) EM170APM030001C.DGN

Payload x Range - ISA + 10 °C Conditions Figure 3.4

Section 3 EFFECTIVITY: EMBRAER 170 LR ACFT MODEL Page 3-6 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

3.3. TAKEOFF FIELD LENGTHS

The takeoff performance is based on the requirements of JAR 25, Change 14, plus amendment 25/96/1. The takeoff field length charts provide data about the maximum takeoff weights, for compliance with the operating regulations relating to takeoff field lengths. Data are presented according to the following associated conditions: • CF34 - 8E5 and CF34 - 8E5A1 engine models; • Takeoff Mode: 1; • ATTCS 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 + 15 °C conditions; • Pack OFF: No engine bleed extraction for air conditioning packs was considered in the takeoff and landing charts.

Section 3 EFFECTIVITY: ALL Page 3-7 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

TAKEOFF FIELD LENGTH CF 34−8E5 ENGINE@T/O−1 MODE ATTCS: ON / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA 4000 AIRPORT PRESSURE ALTITUDE m (ft) 14000 3800

3600

3400 12000

3200 2438 (8000) 3048 3000 (10000) 10000 1829 2800 FLAP 1 (6000) 1219 (4000)

2600

8000 2400 609 FLAP 2 (2000) 2200

6000 2000 FIELD LENGTH − ft FIELD LENGTH − m SEA LEVEL 1800

−570 5000 1600 FLAP 4 (−1870)

1400

1200 4000

1000

800 3000 600

400 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 WEIGHT − kg 45000 49000 53000 57000 61000 65000 69000 73000 77000 81000 85000 WEIGHT − lb EM170APM030009H.DGN

Takeoff Field Lengths - ISA Conditions Figure 3.5

Section 3 EFFECTIVITY: ALL Page 3-8 Oct 07/14 w-apm1346 AIRPORT PLANNING MANUAL

TAKEOFF FIELD LENGTH CF 34−8E5 ENGINE@T/O−1 MODE ATTCS: ON / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA+15°C

4000 13000 AIRPORT PRESSURE ALTITUDE m (ft) 3800

12000 3600

3400 11000 1829 (6000) 3200 3048 2438 (10000) (8000) 10000 3000 1219 FLAP 1 (4000) 2800 9000

2600 609 (2000) 8000 2400 FLAP 2

2200 7000

2000 FIELD LENGTH − ft FIELD LENGTH − m SEA LEVEL 6000 1800 FLAP 4 −570 (−1870) 1600 5000

1400

4000 1200

1000 3000 800

2000 600

400 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 WEIGHT − kg 45000 49000 53000 57000 61000 65000 69000 73000 77000 8100085000 89000 93000

WEIGHT − lb EM170APM030013I.DGN

Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.6

Section 3 EFFECTIVITY: ALL Page 3-9 Oct 07/14 w-apm1346 AIRPORT PLANNING MANUAL

TAKEOFF FIELD LENGTH CF 34−8E5 ENGINE@T/O−1 MODE ATTCS: OFF / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA 4000 13000 AIRPORT PRESSURE ALTITUDE m (ft) 3800

12000 3600

3400 11000

3200

10000 3000 1219 1829 (4000) 3048 2438 (6000) 2800 (10000) (8000) 9000

2600 FLAP 1 609 (2000) 8000 2400

SEA LEVEL 2200 7000 FLAP 2 −570 2000 (−1870) FIELD LENGTH − ft FIELD LENGTH − m

6000 1800

1600 5000 FLAP 4 1400

4000 1200

1000 3000 800

2000 600

400 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 WEIGHT − kg 45000 49000 53000 57000 61000 65000 69000 73000 77000 8100085000 89000 93000

WEIGHT − lb EM170APM030094B.DGN

Takeoff Field Lengths - ISA Conditions Figure 3.7

Section 3 EFFECTIVITY: ALL Page 3-10 Oct 07/14 w-apm1346 AIRPORT PLANNING MANUAL

TAKEOFF FIELD LENGTH CF 34−8E5 ENGINE@T/O−1 MODE ATTCS: OFF / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA+15°C

4000 13000 AIRPORT PRESSURE ALTITUDE m (ft) 3800

12000 3600

3400 11000

3200

10000 3000 3048 2438 (10000) (8000) 609 (2000)

2800 9000 FLAP 1 1829 1219 2600 (6000) (4000) SEA LEVEL 8000 2400 FLAP 2 2200 −570 7000 (−1870)

2000 FIELD LENGTH − ft FIELD LENGTH − m

6000 1800

1600 FLAP 4 5000

1400

4000 1200

1000 3000 800

2000 600

400 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 WEIGHT − kg 45000 49000 53000 57000 61000 65000 69000 73000 77000 8100085000 89000 93000

WEIGHT − lb EM170APM030095B.DGN

Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.8

Section 3 EFFECTIVITY: ALL Page 3-11 Oct 07/14 w-apm1346 AIRPORT PLANNING MANUAL

TAKEOFF FIELD LENGTH CF 34−8E5A1 ENGINE@T/O−1 MODE ATTCS: ON / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA

4000 13000 AIRPORT PRESSURE ALTITUDE m (ft) 3800

12000 3600

3400 11000

3200 2438 10000 3048 (8000) 3000 (10000)

2800 1829 9000 (6000) FLAP 1 1219 (4000) 2600

8000 2400 609 FLAP 2 (2000) 2200 7000

2000 FIELD LENGTH − ft FIELD LENGTH − m SEA LEVEL 6000 1800

1600 5000 −570 (−1870) 1400 FLAP 4

4000 1200

1000 3000 800

2000 600

400 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 WEIGHT − kg 45000 49000 53000 57000 61000 65000 69000 73000 77000 8100085000 89000 93000

WEIGHT − lb EM170APM030005I.DGN

Takeoff Field Lengths - ISA Conditions Figure 3.9

Section 3 EFFECTIVITY: ALL Page 3-12 Oct 07/14 w-apm1346 AIRPORT PLANNING MANUAL

TAKEOFF FIELD LENGTH CF 34−8E5A1 ENGINE@T/O−1 MODE ATTCS: ON / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA+15°C

4000 13000 AIRPORT PRESSURE ALTITUDE m (ft) 3800

12000 3600

3400 11000 1829 3200 3048 2438 (6000) (10000) (8000) 10000 3000

FLAP 1 1219 2800 (4000) 9000

2600

609 8000 2400 (2000) FLAP 2 2200 7000

2000 FIELD LENGTH − ft FIELD LENGTH − m SEA LEVEL 6000 1800

−570 1600 (−1870) 5000 FLAP 4

1400

4000 1200

1000 3000 800

2000 600

400 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 WEIGHT − kg 45000 49000 53000 57000 61000 65000 69000 73000 77000 8100085000 89000 93000

WEIGHT − lb EM170APM030006I.DGN

Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.10

Section 3 EFFECTIVITY: ALL Page 3-13 Oct 07/14 w-apm1346 AIRPORT PLANNING MANUAL

TAKEOFF FIELD LENGTH CF 34−8E5A1 ENGINE@T/O−1 MODE ATTCS: OFF / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA 4000 13000 AIRPORT PRESSURE ALTITUDE m (ft) 3800

12000 3600

3400 11000

3200

10000 3000 1219 (4000) 1829 3048 (6000) 2800 9000 (10000)

2600 FLAP 1 2438 (8000)

8000 609 2400 (2000)

2200 SEA LEVEL 7000 FLAP 2 2000 −570 FIELD LENGTH − ft FIELD LENGTH − m (−1870)

6000 1800

1600 5000

1400 FLAP 4

4000 1200

1000 3000 800

2000 600

400 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 WEIGHT − kg 45000 49000 53000 57000 61000 65000 69000 73000 77000 8100085000 89000 93000

WEIGHT − lb EM170APM030096B.DGN

Takeoff Field Lengths - ISA Conditions Figure 3.11

Section 3 EFFECTIVITY: ALL Page 3-14 Oct 07/14 w-apm1346 AIRPORT PLANNING MANUAL

TAKEOFF FIELD LENGTH CF 34−8E5A1 ENGINE@T/O−1 MODE ATTCS: OFF / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA+15°C

4000 13000 AIRPORT PRESSURE ALTITUDE m (ft) 3800

12000 3600

3400 11000

3200 1219 1829 (4000) 10000 (6000) 3000 3048 (10000)

2800 9000 2438 FLAP 1 (8000) 609 2600 (2000)

8000 2400

SEA LEVEL 2200 7000 FLAP 2 −570 2000 (−1870) FIELD LENGTH − ft FIELD LENGTH − m

6000 1800

1600 5000

1400 FLAP 4

4000 1200

1000 3000 800

2000 600

400 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 WEIGHT − kg 45000 49000 53000 57000 61000 65000 69000 73000 77000 8100085000 89000 93000

WEIGHT − lb EM170APM030097B.DGN

Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.12

Section 3 EFFECTIVITY: ALL Page 3-15 Oct 07/14 w-apm1346 AIRPORT PLANNING MANUAL

3.4. LANDING FIELD LENGTHS

The landing field length charts provide data about the maximum landing weights, for compliance with the operating regulations relating to landing field lengths. Data are presented according to the following associated conditions: • Landing gear: down; • Flaps setting position: 5 and 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 the takeoff and landing charts; • For EASA Certification, Landing Field Lengths are factored as per EU OPS 1.515 (a) (1) - Landing; • For FAA Certification, Landing Field Lengths are factored as per FAR Part 121, Paragraph 121.195 (b) - Airplanes.

Section 3 EFFECTIVITY: ALL Page 3-16 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

LANDING FIELD LENGTH FLAP 5 DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY

1900

6000

10000

9000

1700 8000 5500 7000

6000

AIRPORT PRESSURE 5000 ALTITUDE m (ft) 5000 4000 1500 3000

2000

1000

4500 SEA LEVEL −1000

−1870 1300 FAR LANDING RUNWAY LENGTH − m FAR LANDING RUNWAY LENGTH − ft 4000

1100 3500 34000 kg (74957 lb) 3000 900 15000 20000 25000 30000 35000 40000 WEIGHT − kg

35000 40000 45000 50000 55000 60000 65000 70000 75000 80000 85000

WEIGHT − lb EM170APM030014H.DGN

Landing Field Lengths - Flaps 5 Figure 3.13

Section 3 EFFECTIVITY: FAA-CERTIFIED ACFT Page 3-17 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

LANDING FIELD LENGTH FLAPS FULL DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY

5500

1600 10000 AIRPORT PRESSURE ALTITUDE m (ft) 9000 5000 8000

7000

6000

1400 5000

4500 4000

3000

2000

1000

SEA LEVEL

−1000 4000 −1870 1200 FAR LANDING RUNWAY LENGTH − m FAR LANDING RUNWAY LENGTH − ft

3500

1000

3000 34000 kg (74957 lb)

800 15000 20000 25000 30000 35000 40000 WEIGHT − kg

35000 40000 45000 50000 55000 60000 65000 70000 75000 80000 85000

WEIGHT − lb EM170APM030015G.DGN

Landing Field Lengths - Flaps Full Figure 3.14

Section 3 EFFECTIVITY: FAA-CERTIFIED ACFT Page 3-18 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

LANDING FIELD LENGTH FLAP 5 DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY

5500 1900

AIRPORT PRESSURE ALTITUDE m (ft)

10000 5000 1700 9000

8000

7000

6000

4500 1500 5000

4000

3000

2000

1000

SEA LEVEL 4000 1300 −1000 −1870 FAR LANDING RUNWAY LENGTH − ft FAR LANDING RUNWAY LENGTH − m

3500 1100 34000 kg (74957 lb)

3000 900 15000 20000 25000 30000 35000 40000 WEIGHT − kg

3500040000 45000 5000055000 60000 6500070000 75000

WEIGHT − lb EM170APM030028D.DGN

Landing Field Lengths - Flaps 5 Figure 3.15

Section 3 EFFECTIVITY: EASA-CERTIFIED ACFT Page 3-19 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

LANDING FIELD LENGTH FLAPS FULL DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY

5500

1600 10000

AIRPORT PRESSURE 9000 ALTITUDE m (ft) 5000 8000

7000

6000

5000 1400 4000 4500 3000

2000

1000

SEA LEVEL

−1000 −1870 4000 1200 FAR LANDING RUNWAY LENGTH − ft 3500 FAR LANDING RUNWAY LENGTH − m

1000

3000 34000 kg (74957 lb)

800 15000 20000 25000 30000 35000 40000 WEIGHT − kg

3500040000 45000 5000055000 60000 6500070000 75000 80000 85000 WEIGHT − lb EM170APM030029D.DGN

Landing Field Lengths - Flaps Full Figure 3.16

Section 3 EFFECTIVITY: EASA-CERTIFIED ACFT Page 3-20 Oct 31/12 w-apm1346 AIRPORT PLANNING MANUAL

4. GROUND MANEUVERING

4.1. GENERAL INFORMATION

This section provides the aircraft turning capability and maneuvering characteristics. To facilitate the presentation, the data have been determined from theoretical limits imposed by the geometry of the aircraft. As such, they reflect the turning capability of the aircraft in favorable operating circumstances. These data should be used only as a guideline for the method of determining such parameters and for the maneuvering characteristics of the aircraft. In the ground operating mode, varying airline practices may demand that more conservative turning procedures be adopted, to avoid excessive tire wear and reduce possible maintenance problems. Variations from standard aircraft operating patterns may be necessary to satisfy physical constraints within 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 airline before the layout is planned. 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 the windows. Ambinocular vision is defined as the total field of vision seen by both eyes at the same time. • The performance of the aircraft on runway-to-taxiway, taxiway-to-taxiway and runway holding bay dimensions.

4.2. TURNING RADII

This subsection presents the following information: • The turning radii for various nose landing gear steering angles. The minimum turning radius is determined, considering the maximum nose landing gear steering angle as 76 degrees left and right. • Data on the minimum width of the pavement for a 180° turn.

Section 4 EFFECTIVITY: ALL Page 4-1 Oct 07/08 w-apm1346 AIRPORT PLANNING MANUAL

R5 R6

76° 70° 65° R4 60° 55° R1 50° 45° 40° R 5.28 m 35° (17 ft 4 in.)

R 10.97 m (35 ft 11 in.)

NOTE: DATA PRESENTED IS BASED ON THEORETICAL CALCULATIONS. ACTUAL OPERATING DATA MAY BE GREATER THAN SHOWN SINCE TIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS.

NOSE LANDING NOSE OUTBOARD GEAR INBOARD GEAR RIGHT WINGLET RIGHT TAILTIP STEERING GEAR STEEL R1 R2 R3 R4 R5 R6 35° 21.19 m 69 ft 6 in. 18.76 m 61 ft 6 in. 18.31 m 60 ft 1 in. 12.06 m 39 ft 7 in. 28.45 m 93 ft 5 in. 24.91 m 81 ft 9 in.

40° 19.47 m 63 ft 10 in. 16.78 m 55 ft 0 in. 15.80 m 51 ft 10 in. 9.55 m 31 ft 4 in. 25.98 m 85 ft 3 in. 22.92 m 75 ft 2 in.

45° 18.21 m 59 ft 9 in. 15.28 m 50 ft 2 in. 13.76 m 45 ft 2 in. 7.51 m 24 ft 8 in. 23.96 m 78 ft 7 in. 21.38 m 70 ft 2 in.

50° 17.26 m 56 ft 8 in. 14.14 m 46 ft 5 in. 12.05 m 39 ft 6 in. 5.80 m 19 ft 0 in. 22.28 m 73 ft 1 in. 20.17 m 66 ft 2 in.

55° 16.55 m 54 ft 3 in. 13.25 m 43 ft 6 in. 10.57 m 34 ft 8 in. 4.32 m 14 ft 2 in. 20.83 m 68 ft 4 in. 19.18 m 62 ft 11 in.

60° 16.00 m 52 ft 6 in. 12.55 m 41 ft 2 in. 9.26 m 30 ft 5 in. 3.02 m 9 ft 11 in. 19.54 m 64 ft 1 in. 18.35 m 60 ft 3 in.

65° 15.58 m 51 ft 2 in. 12.01 m 39 ft 5 in. 8.08 m 26 ft 6 in. 1.84 m 6 ft 0 in. 18.39 m 60 ft 4 in. 17.66 m 57 ft 11 in.

70° 15.28 m 50 ft 1 in. 11.60 m 38 ft 1 in. 6.99 m 22 ft 11 in. 0.75 m 2 ft 5 in.17.33 m 56 ft 10 in. 17.07 m 56 ft 0 in.

76° 15.02 m 49 ft 3 in. 11.25 m 36 ft 11 in. 5.80 m 19 ft 0 in. 0.445 m 1 ft 5.5 in. 16.17 m 53 ft 1 in. 16.48 m 54 ft 1 in. EM170APM040007C.DGN

Turning Radii - No Slip Angle Figure 4.1

Section 4 EFFECTIVITY: ALL Page 4-2 Oct 07/08 w-apm1346 AIRPORT PLANNING MANUAL

4.3. MINIMUM TURNING RADII

R5 R6

76°

R1 R 10.97 m (35 ft 12 in.) 1

R2 17.05 m R 5.28 m (55 ft 11 in.) (17 ft 4 in.) (RUNWAY MINIMUM WIDTH)

NOTE: ACTUAL OPERATING DATA MAY BE GREATER THAN VALUES SHOWN SINCE TIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS.

NOSE LANDING NOSE OUTBOARD GEAR RIGHT WINGLET RIGHT TAILTIP STEERING GEAR ANGLE R1 R2 R3 R5 R6 76° 15.02 m 49 ft 3 in. 11.25 m 36 ft 11 in. 5.80 m 19 ft 0 in. 16.17 m 53 ft 1 in. 16.48 m 54 ft 1 in.

1 THEORETICAL CENTER OF TURN FOR MINIMUN RADIUS. SHOWS CONTINUOUS TURNING WITH ENGINE THRUST AS REQUIRED.

NO DIFFERENTIAL BRAKING. EM170APM040001A.DGN

Minimum Turning Radius Figure 4.2 Section 4 EFFECTIVITY: ALL Page 4-3 Oct 07/08 w-apm1346 AIRPORT PLANNING MANUAL

4.4. VISIBILITY FROM COCKPIT

VISUAL ANGLE IN PLANE PARALLEL TO LONGITUDINAL AXIS THROUGH PILOT’S EYE POSITION PILOT’S EYE POSITION 27.8° 3.91 m (12 ft 10 in.) 15°

CL FUS HOR

0.75 m (2 ft 6 in.)

REF. GROUND (BOW)

2.92 m (9 ft 7 in.) 14.58 m (47 ft 10 in.)

MAXIMUM AFT VISION PILOT’S EYE POSITION WITH HEAD ROTATED ABOUT SPINAL COLUMN

0.53 m (1 ft 9 in.) 120.6°

0.53 m (1 ft 9 in.) PILOT’S EYE POSITION VISUAL ANGLE IN PLANE PERPENDICULAR TO LONGITUDINAL AXIS THROUGH PILOT’S EYE POSITION

27.5°

28.1° EM170APM040006C.DGN

Visibility from Cockpit in Static Position Figure 4.3 Section 4 EFFECTIVITY: ALL Page 4-4 Jul 01/05 w-apm1346 AIRPORT PLANNING MANUAL

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 and Operations - Volume 1, by the ICAO. The code is composed of two elements which are related to the aircraft performance characteristics and 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 CODE AIRCRAFT REFERENCE CODE OUTER MAIN LANDING WING SPAN NUMBER FIELD LENGTH LETTER GEAR WHEEL SPAN Less than 800 m Up to 15 m Up to 4.5 m 1 A (2624 ft 8 in) (49 ft 3 in) (14 ft 9 in) 800 m (2624 ft 8 in) up to 15 m (49 ft 3 in) to 4.5 m (14 ft 9 in) to 2 B 1200 m (3937 ft) 24 m (78 ft 9 in) 6 m (19 ft 8 in) 1200 m (3937 ft) up to 24 m (78 ft 9 in) to 6 m (19 ft 8 in) to 3 C 1800 m (5905 ft 6 in) 36m(118ft1in) 9 m (29 ft 6 in) 1800 m 36m(118ft1in)to 9 m (29 ft 6 in) to 4 D (5905 ft 6 in) and over 52 m (170 ft 7 in) 14 m (45 ft 11 in) 52 m (170 ft 7 in) to 9 m (29 ft 6 in) to __ __ E 65 m (213 ft 3 in) 14 m (45 ft 11 in)

In accordance with the table, the reference code for the EMBRAER 170STD and 170LR is 3C.

NOTE: • Classification considering CF34-8E5A1 engines. • This classification may change depending on aircraft engine model and takeoff weight.

With the reference code it is possible to obtain the limits of the runway and taxiway where the aircraft 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 remains over the taxiway center line marking, the clearance distance between the outer main landing gear wheels of the aircraft and the edge of the taxiway should not be less than3m(9ft10in). • The clearance between a parked aircraft and one moving along the taxiway in a holding bay should not be less than 15 m (49 ft 3 in).

Section 4 EFFECTIVITY: ALL Page 4-5 Oct 07/08 w-apm1346 FETVT:ALL EFFECTIVITY: (98 ft5in.) 30 m 45° oeta 0 un-Rna oTaxiway to Runway - Turn 90° than More GEAR TIREEDGE PATH OFMAINLANDING iue4.4 Figure LNIGMANUAL PLANNING AIRPORT 100 ftRadius (30 m) PROCEDURE. FOR THESPECIFICPLANNEDOPERATING COORDINATE WITHAIRLINEOPERATOR NOTE: APPROXIMATELY 15. NOSE LANDINGGEARSTEERINGANGLEIS (49 ft2in.) 15 m e 08/03 Dec eto 4 Section ae4-6 Page

EM170APM040002.DGN

b-apm1346 b-apm1346 FETVT:ALL EFFECTIVITY: (98 ft5in.) 30 m 90° 0 un-Rna oTaxiway to Runway - Turn 90° iue4.5 Figure LNIGMANUAL PLANNING AIRPORT 100 ftRadius 100 ftRadius (30 m) (30 m) PROCEDURE. FOR THESPECIFICPLANNEDOPERATING COORDINATE WITHAIRLINEOPERATOR APPROXIMATELY 30. NOSE LANDINGGEARSTEERINGANGLEIS NOTE: GEAR TIREEDGE. PATH OFMAINLANDING (49 ft2in.) e 08/03 Dec eto 4 Section 15 m ae4-7 Page

EM170APM040003.DGN FETVT:ALL EFFECTIVITY: (49 ft2in.) 15 m 90° 0 un-Txwyt Taxiway to Taxiway - Turn 90° (9 ft10in.) iue4.6 Figure 3 m 100 ftRadius (30 m) LNIGMANUAL PLANNING AIRPORT GEAR TIREEDGE. PATH OFMAINLANDING NOTE: PROCEDURE. FOR THESPECIFICPLANNEDOPERATING COORDINATE WITHAIRLINEOPERATOR APPROXIMATELY 28. NOSE LANDINGGEARSTEERINGANGLEIS (49 ft2in.) 15 m e 08/03 Dec eto 4 Section ae4-8 Page

EM170APM040004.DGN

b-apm1346 AIRPORT PLANNING MANUAL

4.6. RUNWAY HOLDING BAY

RUNWAY 30 m (98 ft 5 in.)

MINIMUM CLEARENCES 15 m 75 m (49 ft 2 in.) (246 ft)

3 m (9 ft 10 in.)

PATH OF MAIN LANDING GEAR TIRE EDGE.

TAXIWAY 15 m (49 ft 2 in.)

PATH OF MAIN LANDING GEAR TIRE EDGE. EM170APM040005.DGN

Runway Holding Bay Figure 4.7 Section 4 EFFECTIVITY: ALL Page 4-9 / 10 Dec 08/03 b-apm1346

AIRPORT PLANNING MANUAL

5. TERMINAL SERVICING

During turnaround at the air terminal, certain services must be performed on the aircraft, usually within a given time to meet flight schedules. This section shows service vehicle arrangements, schedules, locations of servicing points, and typical servicing requirements. The data presented herein reflect ideal conditions for a single aircraft. Servicing requirements may vary according to the aircraft condition and airline operational (servicing) procedures. This section provides the following information: • The typical arrangements of equipment during turnaround; • The typical turnaround servicing time at an air terminal; • The locations of ground servicing connections in graphic and tabular forms; • The typical sea level air pressure and flow requirements for starting the engine; • The air conditioning requirements; • The ground towing requirements for various towing conditions. Towbar pull and total traction wheel load may be determined by considering aircraft weight, pavement slope, coefficient of friction, and engine idle thrust.

Section 5 EFFECTIVITY: ALL Page 5-1 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

5.1. AIRCRAFT SERVICING ARRANGEMENT

35 110 4 6 4

100 30

8 90 3 3 25 80 5 5

70 20

60 LENGTH − m LENGTH − ft 50 15

10 30 11

20 2 2 5

10 7 9 10 0 0 0510 15 20 25 30 35 40 LENGTH − m

01020 30 40 50 60 70 80 90 100 110 120 130 LENGTH − ft

SERVICING ARRANGEMENT

02 − PASSENGER STAIRS 03 − CARGO LOADER 04 − BAGGAGE / CARGO TROLLEY AND TUG 05 − GALLEY SERVICE VEHICLE 06 − FUEL SERVICE 07 − POTABLE WATER 08 − LAVATORY SERVICE VEHICLE 09 − AIR CONDITIONING UNIT 10 − PNEUMATIC STARTER 11 − GROUND POWER UNIT EM170APM050001.DGN

Aircraft Servicing Arrangement With Passenger Stairs Figure 5.1 Section 5 EFFECTIVITY: ALL Page 5-2 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

35 6 110 4 4

100 30

8 90 3 3 25 80 5 5

70 20

60 LENGTH − ft LENGTH − m 50 15

40 1

10 30

20 5

10 9 7 10 0 0 051015 20 25 30 35 40 LENGTH − m

01020 30 40 50 60 70 80 90 100 110 120 130 LENGTH − ft

SERVICING ARRANGEMENT

01 − PASSENGER BRIDGE 03 − CARGO LOADER 04 − BAGGAGE / CARGO TROLLEY AND TUG 05 − GALLEY SERVICE VEHICLE 06 − FUEL SERVICE 07 − POTABLE WATER 08 − LAVATORY SERVICE VEHICLE 09 − AIR CONDITIONING UNIT 10 − PNEUMATIC STARTER EM170APM050002.DGN

Aircraft Servicing Arrangement With Passenger Bridge Figure 5.2

Section 5 EFFECTIVITY: ALL Page 5-3 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

5.2. TERMINAL OPERATIONS - TURNAROUND STATION

This section presents the typical turnaround servicing time at an air terminal. The chart gives typical schedules for servicing 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 ); • 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 could be rearranged to suit availability of personnel, aircraft configuration, and degree of servicing required. The data illustrates the general scope and tasks involving airport terminal operations. Airline particular practices and operating experience will result in different sequences and intervals.

Section 5 EFFECTIVITY: ALL Page 5-4 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

ELAPSED TIME 1 243 5 6 7 810129 11 13 14 15 16 17 1819 20 (MINUTES)

OPERATIONS min.

BRIDGE/STAIRS POSITIONING 1,0

PASSENGERS DEPLANE 2.9

GALLEY SERVICING−FWD 6,0

PAX GALLEY SERVICING−AFT 6,0 SERVICES AIRPLANE INTERIOR SERVICES 4,4

PASSENGERS ENPLANE 4,4

BRIDGE / STAIRS REMOVAL 1,0

PUSH BACK / ENGINES START 2,0

FWD BAGGAGE / CARGO UNLOAD 3,4

REAR BAGGAGE / CARGO UNLOAD 2,2

BAGGAGE TIME BETWEEN UNLOADING / LOADING 0,5 & CARGO FWD BAGGAGE/CARGO LOAD 5,5

AFT BAGGAGE/CARGO LOAD 3,7

FUEL SERVICE 8,5

AIRCRAFT POTABLE WATER SERVICE 3,0 SERVICING TOILET SERVICE 5,0

LEGEND:

TRUCK POSITIONING/REMOVAL/SETTINGS

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. EM170APM050003B.DGN

Air Terminal Operation - Turnaround Station Figure 5.3

Section 5 EFFECTIVITY: ALL Page 5-5 May 11/07 w-apm1346 AIRPORT PLANNING MANUAL

5.3. TERMINAL OPERATIONS - EN ROUTE STATION

Not Applicable

Section 5 EFFECTIVITY: ALL Page 5-6 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

5.4. GROUND SERVICING CONNECTIONS

4 1 2 5

8 9 12

6 7 3

10 11 14 13 15

16 17 18

19 20 21 22

HEIGHT COORD. X COORD. Y COORD. Z ABOVE ITEM DESCRIPTION (mm) (mm) (mm) GROUND (mm) 1 PRESSURE REFUELING PANEL 13491.27 5702.96 −623.30 2469.26 2 GRAVITY REFUELING PORT (RH) 14789.49 7413.99 −243.75 2848.49 3 GRAVITY REFUELING PORT (LH) 14789.49 −7413.99 −243.75 2848.49 4 EXTERNAL POWER SUPPLY 115 VAC 4146.90 −810.70 −1339.53 1755.33 5 FORWARD RAMP HEADSET 4164.44 −936.13 −1262.71 1832.15 6 STEERING SWITCH DISENGAGE 4136.97 −951.46 −1279.29 1815.58 7 WHEEL JACK POINT − NLG 4121.90 0.00 −2877.81 217.06 8 AIR COND. GROUND CONNECTION 10487.32 80.00 −1979.71 1113.60 9 ENGINE AIR STARTING (LOW PRESSURE UNIT) 10778.80 4.28 −2010.20 1083.03 10 GROUNDING POINT (ELECTRICAL) 14592.10 2560.25 −1343.60 1748.70 11 WHEEL JACK POINT− MLG (RH) 14476.67 2600.00 −2679.11 413.20 12 WHEEL JACK POINT− MLG (LH) 14476.67 −2600.00 −2679.11 413.20 13 HYD. SYS # 1 SERVICE PANEL 16560.17 −808.01 −1602.04 1489.76 14 HYD. SYS # 2 SERVICE PANEL 16560.17 808.01 −1602.04 1489.76 15 WATER SERVICING PANEL 21524.83 −329.37 −1178.74 1911.84 16 EXTERNAL POWER SUPPLY 28 VDC 24084.65 −471.73 −605.30 2484.65 17 AFT RAMP HEADSET 24225.26 −449.47 −585.54 2504.39 18 OXYGEN SERVICING PANEL / BOTTLE 6562.14 1159.87 −961.05 2133.22 19 FUEL TANK DRAIN VALVE (RH) 13352.80 398.47 −1413.71 1678.89 20 FUEL TANK DRAIN VALVE (LH) 13352.80 −398.47 −1413.71 1678.89 21 WASTE SERVICING PANEL 22447.01 349.20 −991.80 2098.55 22 HYD. SYS # 3 SERVICE PANEL 24061.86 519.15 −590.09 2499.87 NOTE: THE GROUND CLEARANCES IN THE TABLE REFER TO THE AIRCRAFT WITH THE MINIMUM

OPERATING WEIGHT (MOW) = 21800 kg (CG FWD 7.0% CMA) EM170APM050005D.DGN

Ground Servicing Connections Figure 5.4 Section 5 EFFECTIVITY: ALL Page 5-7 May 11/07 w-apm1346 AIRPORT PLANNING MANUAL

4 1 2 5

8 9 12

6 7 3

10 11 14 13 15

16 17 18

19 20 21 22

HEIGHT COORD. X COORD. Y COORD. Z ABOVE ITEM DESCRIPTION (mm) (mm) (mm) GROUND (mm) 1 PRESSURE REFUELING PANEL 13491.27 5702.96 −623.30 2461.54 2 GRAVITY REFUELING PORT (RH) 14789.49 7413.99 −243.75 2830.76 3 GRAVITY REFUELING PORT (LH) 14789.49 −7413.99 −243.75 2830.76 4 EXTERNAL POWER SUPPLY 115 VAC 4146.90 −810.70 −1339.53 1819.58 5 FORWARD RAMP HEADSET 4164.44 −936.13 −1262.71 1896.25 6 STEERING SWITCH DISENGAGE 4136.97 −951.46 −1279.29 1879.90 7 WHEEL JACK POINT − NLG 4112.770.00 −2942.27 217.16 8 AIR COND. GROUND CONNECTION 10487.32 80.00 −1979.71 1129.04 9 ENGINE AIR STARTING (LOW PRESSURE UNIT) 10778.80 4.28 −2010.20 1096.23 10 GROUNDING POINT (ELECTRICAL) 14592.10 2560.25−1343.60 1732.52 11 WHEEL JACK POINT− MLG (RH) 14475.492600.00 −2662.17 414.90 12 WHEEL JACK POINT− MLG (LH) 14475.49−2600.00 −2662.17 414.90 13 HYD. SYS # 1 SERVICE PANEL 16560.17 −808.01 −1602.04 1458.44 14 HYD. SYS # 2 SERVICE PANEL 16560.17 808.01 −1602.04 1458.44 15 WATER SERVICING PANEL 21524.83 −329.37 −1178.74 1842.28 16 EXTERNAL POWER SUPPLY 28 VDC 24084.65 −471.73 −605.30 2395.36 17 AFT RAMP HEADSET 24225.26 −449.47 −585.54 2414.01 18 OXYGEN SERVICING PANEL / BOTTLE 6562.14 1159.87 −961.05 2178.86 19 FUEL TANK DRAIN VALVE (RH) 13352.80 398.47 −1413.71 1672.25 20 FUEL TANK DRAIN VALVE (LH) 13352.80 −398.47 −1413.71 1672.25 21 WASTE SERVICING PANEL 22447.01 349.20 −991.80 2021.88 22 HYD. SYS # 3 SERVICE PANEL 24061.86 519.15 −590.09 2410.75 NOTE: THE GROUND CLEARANCES IN THE TABLE REFER TO THE AIRCRAFT WITH THE MINIMUM

OPERATING WEIGHT (MOW) = 21800 kg (CG REAR 27.0% CMA) EM170APM050006A.DGN

Ground Servicing Connections Figure 5.5

Section 5 EFFECTIVITY: ALL Page 5-8 May 11/07 w-apm1346 AIRPORT PLANNING MANUAL

5.5. ENGINE STARTING PNEUMATIC REQUIREMENTS

TABLE 1 − PNEUMATIC ENGINE START REQUIREMENTS

Altitude Ambient Minimum Minimum Minimum ft Temp °F Pressure psia Temp °F Flow lb/min SL −40 48.0 349 95.1 SL 59 43.7 443 82.0 SL 120 40.7 505 73.7 9000 −40 37.7 350 74.5 9000 23 30.0 409 57.3 9000 86 28.9 474 53.4 13,000 −40 36.0 352 71.3 13,000 12 27.2 399 52.2 13,000 71 26.7 458 49.6 15,000 −40 32.9 352 66.6 15,000 5 25.3 392 49.0 15,000 59 24.4 446 46.1 EM170APM050030A.DGN

Engine Starting Pneumatic Requirements Figure 5.6 Section 5 EFFECTIVITY: ALL Page 5-9 Oct 06/11 w-apm1346 AIRPORT PLANNING MANUAL

5.6. GROUND PNEUMATIC POWER REQUIREMENTS

80 25

20 70

15 60

10 50 HEATING

Initial cabin temp: −32°C (−25°F) 5 40 Outside air temp: −40°C (−40°F) Relative Humidity: 0% 0 30 No crew or passengers No other heat load −5 20 Bleed air from APU: −10 87 kg/min. (192.0 lb/min.) 10 452 kPa (65.5 psia) −15 2 operating packs (ECS)

0 CABIN TEMPERATURE (°F) CABIN TEMPERATURE (°C) −20 −10 −25 −20 −30 0 5 10 15 20 25 30 TIME TO HEAT CABIN − min.

120

45 110 COOLING 40 Initial cabin temp: 47°C (116°F) 100 Outside air temp: 40°C (104°F) Relative Humidity: 40% 35 No crew or passengers No other heat load 90 Bleed air from APU: 30 56 kg/min. (122.9 lb/min.) 413 kPa (59.9 psia) 80 2 operating packs (ECS) 25 CABIN TEMPERATURE (°F) CABIN TEMPERATURE (°C)

70 20

60 0 5 10 15 20 25 30 TIME TO COOL CABIN − min. EM170APM050007B.DGN

Ground Pneumatic Power Requirements Figure 5.7 Section 5 EFFECTIVITY: ALL Page 5-10 Oct 06/11 w-apm1346 AIRPORT PLANNING MANUAL

5.7. PRECONDITIONED AIRFLOW REQUIREMENTS

This subsection presents the following information: • The air conditioning requirements for heating and cooling using ground conditioned air. The curves show airflow requirements to heat or cool the aircraft at ambient conditions within a given time. • The air conditioning heating and cooling requirements to maintain a constant cabin air temperature using low-pressure conditioned air. This conditioned air is supplied through a ground air connection directly to the passenger cabin, bypassing the air cycle machines.

Section 5 EFFECTIVITY: ALL Page 5-11 Oct 06/11 w-apm1346 AIRPORT PLANNING MANUAL

PRE−CONDITIONED AIRFLOW REQUIREMENTS [lbm/min] 150 [kg/min] 1 55 140 60 2 16 120

50 4 12 100 10 3 5 40 6 80

TOTAL AIRFLOW 30 5 60

20 40 1

10 20 PRESSURE AT GROUND CONNECTION (INCHES OF WATER) 0 0 −5 0 5 10 15 20 25 30 35 40 45 50 55 [°C] [°F] 30 50 70 90 110 120

AIR SUPPLY TEMPERATURE LEGEND:

1 CABIN AT 24°C (74°F), 97 OCCUPANTS, NOTES: BRIGHT DAY (SOLAR IRRADIATION), MAXIMUM ALLOWABLE TEMPERATURE 88°C (190°F) 39°C (103°F) DAY. (UPPER LIMIT DURING PULL UP OPERATION).

2 SAME AS 1 EXCEPT CABIN 27°C (81°F) MAXIMUM ALLOWABLE PRESSURE AT GROUND CONNECTION 203mmH20 (8 INCHES OF WATER).

3 SAME AS 1 EXCEPT CABIN 24°C (74°F), NO CABIN OCCUPANTS, FOUR CREWS MEMBERS ONLY.

4 CABIN AT 24°C (74°F), NO CABIN OCCUPANTS, FOUR CREW MEMBERS ONLY, OVERCAST DAY (NO SOLAR IRRADIATION), −40°C (−40°F) DAY.

5 SAME AS 4 EXCEPT −29°C (−20°F) DAY.

6 SAME AS 4 EXCEPT −18°C (−0°F) DAY. EM170MFEP040069B.DGN

Preconditioned Airflow Requirements Figure 5.8

Section 5 EFFECTIVITY: ALL Page 5-12 Oct 06/11 w-apm1346 AIRPORT PLANNING MANUAL

5.8. GROUND TOWING REQUIREMENTS

32000 (70547) 32000 34000 (74957) 34000

36000 (79366) 36000

28000 (61729) 28000

24000 (52910) 24000 26000 (57320) 26000

22000 (48501) 22000

20000 (44092) 20000 38000 (83775) 38000 30000 (66138) 30000 4

3 AIRCRAFT GROSS WEIGHT − kg (lb) kg − WEIGHT GROSS AIRCRAFT 2 PERCENT SLOPE (%) 1

0 REFERENCE LINE REFERENCE 2 1 ENGINES NUMBER OF IDLE THRUST BACKING AGAINST 0 5000

(11023)

ICE =0.05 ICE

GROUND TOWING REQUIREMENTS

WET ASPHALT =0.75 ASPHALT WET 4000

(8818)

WET CONCRETE =0.57 CONCRETE WET

SNOW CHAINS =0.45 CHAINS SNOW

ASPHALT =0.8 ASPHALT HARD SNOW =0.2 SNOW HARD DRY CONCRETE OR CONCRETE DRY 3000 (6614) (DRAWBAR PULL) 2000 (4409) TOTAL TRACTION WHEEL − kg (lb) 1000 (2204) − STRAIGHT−LINE TOW − UNUSUAL BREAKAWAY CONDITIONS NOT SHOWN − COEFFICIENTS OF FRICTION ( ) ARE ESTIMATED FOR RUBBER−TIRED TOW VEHICLES NOTES: 0 0 3000 2000 1000 (6614) (4409) (2204)

TOWBAR PULL − kg (lb) EM170APM050004A.DGN

Ground Towing Requirements Figure 5.9 Section 5 EFFECTIVITY: ALL Page 5-13 / 14 Oct 06/11 w-apm1346

AIRPORT PLANNING MANUAL

6. OPERATING CONDITIONS

This section provides the following information: • The jet engine exhaust velocities and temperatures. • The airport and community noise levels. • The hazard areas.

Section 6 EFFECTIVITY: ALL Page 6-1 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

6.1. ENGINE EXHAUST VELOCITIES AND TEMPERATURES

TAKEOFF POWER, SEA LEVEL, Tamb = ISA +16.7°C, FNIN1 = 63685 N (14317 lbf)

5 16 A 14 4 B 12 3 10 C 8 2 Meters 6 D F E 1 4 2 0 0 0 4 8 12162024283236404448525660 DISTANCE FROM CORE NOZZLE EXIT, Feet HEIGHT ABOVE GROUND PLANE, Feet 024681012141618 Meters

24 A 7 B 20 6 C

5 16 D 4 F E 12

Meters 3 8 2 4 1

0 0

DISTANCE FROM AIRPLANE CL − Feet 0 4 8 12162024283236404448525660 DISTANCE FROM CORE NOZZLE EXIT, Feet

024681012141618 Meters VELOCITY m/s (ft/s) MAX = 482.5 (1583) A 15.2 (50) B 30.5 (100) C 60.9 (200) D 121.9 (400) E 243.8 (800) F 457.2 (1500) NOTE:

EXHAUST VELOCITY CONTOURS INCLUDE WORST CASE 20 kn HEADWIND WITH GROUND EFFECTS. EM170MFEP010005.DGN

Jet Wake Velocity Profile - Takeoff Power Figure 6.1 Section 6 EFFECTIVITY: ALL Page 6-2 Dec 08/03 b-apm1346 b-apm1346 EXHAUST TEMPERATURECONTOURS INCLUDEWORSTCASE20knHEADWIND. NOTE: FETVT:ALL EFFECTIVITY:

Meters Meters 0 1 2 3 4 5 6 7 0 1 2 3 4 5

DISTANCE FROM AIRPLANE CL − Feet HEIGHT ABOVE GROUND PLANE − Feet MAX =689°C(1273°F) TOTAL TEMPERATURE 12 16 20 24 10 12 14 16 E D C B A 0 4 8 0 2 4 6 8 024681012141618 12162024283236404448525660 8 4 0 024 12162024283236404448525660 8 4 0 TAKEOFF POWER,SEALEVEL,Tamb=ISA+16.7°C,FNIN163685N(14317lbf) 582 204 93 66 38 °C 900 400 200 150 100 °F e aeTmeauePoie-TkofPower Takeoff - Profile Temperature Wake Jet DISTANCE FROMCORENOZZLEEXIT−Feet DISTANCE FROMCORENOZZLEEXIT−Feet 6

E iue6.2 Figure 81012141618 Meters Meters LNIGMANUAL PLANNING AIRPORT

C e 08/03 Dec eto 6 Section ae6-3 Page

EM170MFEP010006.DGN EXHAUST VELOCITYCONTOURS INCLUDEWORSTCASE20knHEADWINDWITHGROUNDEFFECTS. NOTE: FETVT:ALL EFFECTIVITY:

MAX =89.0(292) VELOCITY m/s(ft/s) Meters Meters 0 1 2 3 4 5 6 7 D C B A 0 1 2 3 4 5 76.2 45.7 30.5 15.2 GROUND IDLE,SEALEVEL,Tamb=ISA+16.7°C,FNIN13785N(851lbf) DISTANCE FROM AIRPLANE CL − Feet HEIGHT ABOVE GROUND PLANE − Feet 12 16 20 24 10 12 14 16 (250) (150) (100) (50) 0 4 8 0 2 4 6 8 024681012141618 12162024283236404448525660 8 4 0 024681012141618 12162024283236404448525660 8 4 0 e aeVlct rfl rudIdle Ground - Profile Velocity Wake Jet DISTANCE FROMCORENOZZLEEXIT−Feet DISTANCE FROMCORENOZZLEEXIT−Feet iue6.3 Figure LNIGMANUAL PLANNING AIRPORT

D Meters Meters

A e 08/03 Dec eto 6 Section ae6-4 Page

EM170MFEP010007.DGN

b-apm1346 w-apm1346 EXHAUST TEMPERATURECONTOURS INCLUDEWORSTCASE20knHEADWIND. NOTE: FETVT:ALL EFFECTIVITY:

Meters Meters 0 1 2 3 4 5 6 7 MAX =519°C(966°F) TOTAL TEMPERATURE 0 1 2 3 4 5 E D C B A GROUND IDLE,SEALEVEL,Tamb=ISA+16.7°C,FNIN13785N(851lbf) 582 204 93 66 38 °C DISTANCE FROM AIRPLANE CL − Feet HEIGHT ABOVE GROUND PLANE − Feet 12 16 20 24 10 12 14 16 0 4 8 0 2 4 6 8 024681012141618 12162024283236404448525660 8 4 0 0246810121416180481 21 62 02 42 83 23 64 04 44 85 25 66 0 900 400 200 150 100 °F e aeTmeauePoie-Gon Idle Ground - Profile Temperature Wake Jet DISTANCE FROMCORENOZZLEEXIT−Feet

E iue6.4 Figure DISTANCE FROMCORENOZZLEEXIT−Feet LNIGMANUAL PLANNING AIRPORT

D Meters Meters

A e 08/03 Dec eto 6 Section ae6-5 Page

EM170MFEP010008.DGN AIRPORT PLANNING MANUAL

6 20 5

15 4 A B 3 10

Meters C 2 5 D 1

0 0 C 020406010 30 52 DISTANCE FROM CORE NOZZLE EXIT, Feet

0 2 4 6 8 1012141618 Meters 10

8 25

A 6 20 B

Meters 15 4 D

DISTANCE FROM AIRPLANE CL − Feet5 HEIGHT ABOVE GROUND PLANE, Feet

0 0 0410 15 20 25 30 35 40 45 50 55 60

VELOCITY m/s (ft/s) DISTANCE FROM CORE NOZZLE EXIT, Feet MAX = 230.8 (757.3) A 15.2 (50) 0 2 4 6 8 10 12 14 16 18 B 30.5 (100) C 60.9 (200) Meters D 121.9 (400)

NOTE:

EXHAUST VELOCITY CONTOURS INCLUDE WORST CASE 20 kn HEADWIND WITH GROUND EFFECTS. EM170APM060006A.DGN

Jet Wake Velocity Profile - Breakaway Power Figure 6.5

Section 6 EFFECTIVITY: ALL Page 6-6 Jan 09/06 w-apm1346 AIRPORT PLANNING MANUAL

6 20 FED 5

4 15 3 Meters C 2 10

1 5 BA 0 0 HEIGHT ABOVE GROUND PLANE − Feet 0 5 10 15 20 25 30 35 40 45 50 55 60

DISTANCE FROM CORE NOZZLE EXIT − Feet

0 2 4 6 8 10 12 14 16 18

Meters

F D C B 6 20

15 4 A

10 Meters 2 5

0 HEIGHT ABOVE GROUND PLANE − Feet 0 5 10 15 20 25 30 35 40 45 50 55 60

DISTANCE FROM CORE NOZZLE EXIT − Feet TOTAL TEMPERATURE MAX = 495 °C (923 °F) 0 2 4 6 8 10 12 14 16 18 °C °F Meters A 38 100 B 66 150 C 93 200 D 121 250 E 149 300 F 177 350

NOTE:

EXHAUST TEMPERATURE CONTOURS INCLUDE WORST CASE 20 kn HEADWIND WITH GROUND EFFECTS. EM170APM060007A.DGN

Jet Wake Temperature Profile - Breakaway Power Figure 6.6

Section 6 EFFECTIVITY: ALL Page 6-7 Jan 09/06 w-apm1346 AIRPORT PLANNING MANUAL

6.2. AIRPORT AND COMMUNITY NOISE

Aircraft noise is a major concern for the airport and community planner. The airport is a basic element in the community’s transportation system and, thus, is vital to its growth. However, the airport must also be a good neighbor, and this can only be accomplished with proper planning. Since aircraft noise extends beyond the boundaries of the airport, it is vital to consider the noise impact on the surrounding communities. Many means have been devised to provide the planner with a tool to estimate the impact of airport operations. 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 exercised to ensure that the contours, used correctly, estimate the noise resulting from aircraft operations conducted at an airport. The size and shape of the single-event contours, which are inputs into the cumulative noise contours, 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.

6.2.1. External Certification Noise Levels

The aircraft comply with the Stage 3 / Chapter 3 noise limits set forth in 14 CFR Part 36, ICAO Annex 16, Volume 1, Chapter 3, Amendment 7 and CTA RBHA 36.

6.2.2. Ramp Noise Levels

The ramp noise will not exceed 80 dBA (maximum) and 77 dBA (average) on the rectangular perimeter of 20 m (65 ft 7 in) from the aircraft centerline, nose and tail, 90 dBA on the service positions and 80 dBA on the passenger entrance positions resulting from operation of the APU (if fitted), ECS, equipment cooling fans and vent fans, in any combination.

Section 6 EFFECTIVITY: ALL Page 6-8 Dec 18/06 w-apm1346 AIRPORT PLANNING MANUAL

6.3. HAZARD AREAS

TAKEOFF POWER, SEA LEVEL, Tamb = ISA +16.7° C, FNIN1 = 63685 N (14317 lbf)

132 m (433 ft)

ENGINE EXHAUST HAZARD AREA VELOCITY = 65 mph OR GREATER = 29.0 m/s (95.3 ft/s)

2 1.8 m R=4.3 m (6 ft) (14 ft) NOTE: NO ACCESS TO ENGINE ACCESSORIES AT TAKEOFF POWER.

1 EXHAUST HAZARD AREA − CONDITION: 20 kn HEADWIND WITH GROUND EFFECTS.

2 INLET HAZARD AREA − CONDITION: 20 kn HEADWIND/CROSSWIND BASED ON 12.2 m/s (40 ft/s) CRITICAL VELOCITY WITH 0.9 m (3 ft) CONTINGENCY FACTOR. EM170MFEP010001A.DGN

Hazard Areas - Takeoff Power Figure 6.7 Section 6 EFFECTIVITY: ALL Page 6-9 Jan 09/06 w-apm1346 AIRPORT PLANNING MANUAL

GROUND IDLE, SEA LEVEL, Tamb = ISA+16.7° C, FNIN1 = 3785 N (851 lbf)

ENGINE EXHAUST HAZARD AREA VELOCITY = 65 mph OR GREATER = 29.0 m/s (95.3 ft/s)

26 m (86 ft)

2.6 m R=2.5 m (8.6 ft) (8.3 ft)

1 INLET HAZARD AREA − CONDITION: 20 kn HEADWIND/CROSSWIND/TAILWIND BASED ON 12.2 m/s (40 ft/s) CRITICAL VELOCITY WITH 0.9 m (3 ft) CONTINGENCY FACTOR.

EXHAUST HAZARD AREA − CONDITION: 20 kn HEADWIND WITH GROUND EFFECTS. EM170MFEP010002A.DGN

Hazard Areas - Ground Idle Figure 6.8

Section 6 EFFECTIVITY: ALL Page 6-10 Oct 07/10 w-apm1346 AIRPORT PLANNING MANUAL

BREAKAWAY POWER, SEA LEVEL, Tamb = ISA +16.7° C, FNIN1 = 2328 DAN (5233 lbf)

121 m (397 ft) = 29.0 M/sec (95.3 ft/sec) Velocity = 65 MPH or greater Engine Exhaust Hazard Area

2 1.8 m (6.0 ft) R= 4.3 m (14.0 ft) NOTE: NO ACCESS TO ENGINE ACCESSORIES AT BREAKAWAY POWER.

1 EXHAUST HAZARD AREA − CONDITION: 20 knot HEADWIND WITH GROUND EFFECTS.

2 INLET HAZARD AREA − CONDITION: 20 knot HEADWIND/CROSSWIND BASED ON 40 ft/sec CRITICAL VELOCITY WITH 0.9 m (3 ft) CONTINGENCY FACTOR. EM170APM060011A.DGN

Hazard Areas - Breakaway Power Figure 6.9

Section 6 EFFECTIVITY: ALL Page 6-11 / 12 Oct 07/10 w-apm1346

AIRPORT PLANNING MANUAL

7. PAVEMENT DATA

7.1. GENERAL INFORMATION

Pavement is defined as a structure consisting of one or more layers of processed materials. The primary function of a pavement is to distribute concentrated loads so that the supporting capacity of the subgrade soil is not exceeded. The subgrade soil is defined as the material on which the pavement rests, whether embankment or excavation. Several methods for design of airport pavements have been developed that differ considerably in their approach. The design methods are derived from observation of pavements in service or experimental pavements. Thus, the reliability of any method is proportional to the amount of experimental verification behind the method, and all methods require a considerable amount of common sense and judgment on the part of the engineer who applies them. A brief description of the following pavement charts will be helpful in their use for airport planning. Each aircraft configuration is depicted with a minimum range of five loads imposed on the main landing gear to aid in the interpolation between the discrete values shown. The tire pressure used for the aircraft charts will produce the recommended tire deflection with the aircraft loaded to its maximum ramp weight and with center of gravity position. The tire pressure, where specifically designated in tables and charts, are values obtained under loaded conditions as certified for commercial use. This section is presented as follows: • The basic data on the landing gear footprint configuration, maximum design ramp loads, and tire sizes and pressures. • 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 on the pavement. Pavement requirements for commercial aircraft are customarily derived from the static analysis 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 Engineers Design Method and the LCN Method. • The rigid pavement design curves in accordance with the Portland Cement Association Design Method and the LCN Method. • The aircraft ACN values for flexible and rigid pavements.

Section 7 EFFECTIVITY: ALL Page 7-1 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

7.2. FOOTPRINT

AIRCRAFT MODELS STD LR, SU OR SE 36150 kg 37360 kg MAXIMUM RAMP WEIGHT (79697 lb) (82365 lb)

NOSE GEAR TIRE SIZE 24 x 7.7

7.24 ± 0.21 kg/cm ² NOSE GEAR TIRE PRESSURE (103 ± 3 psi)

MAIN GEAR TIRE SIZE H38 x 13−18

8.86 ± 0.7 kg/cm ² 9.14 ± 0.7 kg/cm ² MAIN GEAR TIRE PRESSURE (126 ± 10 psi) (130 ± 10 psi)

0.71 m (2 ft 4 in.)

10.62 m (34 ft 10 in.)

5.2 m (17 ft 1 in.) 0.40 m (1 ft 4 in.) EM170APM070002C.DGN

Footprint Figure 7.1 Section 7 EFFECTIVITY: ALL Page 7-2 Jul 01/05 w-apm1346 AIRPORT PLANNING MANUAL

7.3. MAXIMUM PAVEMENT LOADS

LEGEND: V =MAXIMUM VERTICAL NOSE GEAR GROUND LOAD AT MOST FORWARD C.G. NG V =MAXIMUM VERTICAL MAIN GEAR GROUND LOAD AT MOST FORWARD C.G. MG H=MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING

NOTE: ALL LOADS CALCULATED USING AIRCRAFT MAXIMUM RAMP WEIGHT

H V V NG MG

V (PER STRUT)H (PER STRUT) NG VMG MAXIMUM STEADY STEADY INSTANTANEOUS RAMP BRAKING BRAKING STATIC AT MOST STATIC AT MOST BRAKING MODEL WEIGHT WITH WITH FORWARD C.G. AFT C.G. (FRICTION DECELERATION OF DECELERATION OF COEF. OF 0.8) 3,0 m/sec2 3,0 m/sec2

LR, SU 37360 kg 4888 kg 6994 kg 17546 kg 5090 kg 11870 kg OR SE (82365 lb) (10776 lb) (15419 lb) (38682 lb) (11221 lb) (26169 lb)

36150 kg 4922 kg 6961 kg 16976 kg 4924 kg 11480 kg STD (79697 lb) (10851 lb) (15346 lb) (37426 lb) (10855 lb) (25309 lb) EM170APM070013C.DGN

Maximum Pavement Loads Figure 7.2 Section 7 EFFECTIVITY: ALL Page 7-3 Jul 01/05 w-apm1346 AIRPORT PLANNING MANUAL

7.4. LANDING GEAR LOADING ON PAVEMENT

7 % 11.3 % 27 % % CMA

90000 40000 90000 40000

80000 35000 80000 35000

70000

30000 70000

30000 60000 60000 25000 25000 50000 50000

20000 MOW 20000 40000 AIRCRAFT GROSS WEIGHT − (kg) WEIGHT ON MAIN LANDING GEAR (kg) WEIGHT ON MAIN LANDING GEAR (lb) 40000 WEIGHT ON MAIN LANDING GEAR (lb)

15000 15000 30000 30000

10000 20000 82 83 84 85 86 87 88 89 90 91 92 94 95 93 20000 PERCENT OF WEIGHT ON MAIN GEAR − (%)

LEGEND LR, SU OR SE AIRCRAFT MODELS STD AIRCRAFT MODEL EM170APM070014C.DGN

Landing Gear Loading on Pavement Figure 7.3 Section 7 EFFECTIVITY: ALL Page 7-4 Jul 01/05 w-apm1346 AIRPORT PLANNING MANUAL

7.5. FLEXIBLE PAVEMENT REQUIREMENTS, U.S. CORPS OF ENGINEERS DESIGN METHOD

The flexible pavement curves are based on the procedures set forth in Instruction Report No. S-77-1, “Procedures for Development of CBR Design Curves”, dated June 1977, and modified according to the methods described in FAA Advisory Circular 150/5320-6D, “Airport Pavement Design and Evaluation”, dated July 7, 1995. Instruction Report No. S-77-1 was prepared by the US Army Corps of Engineers Waterways Experiment Station, Soils and Pavements Laboratory, Vicksburg, Mississippi. The line showing 10,000 coverages is used to calculate ACN.

Section 7 EFFECTIVITY: ALL Page 7-5 Dec 08/03 b-apm1346 FETVT:EBAR10SDACFT STD 170 MODEL EMBRAER EFFECTIVITY: 3 3 89 10000 COVERAGES CALCULATIONS) (USED FORACN lxbePvmn eurmns-U ryCrso nier einMethod Design Engineers of Corps Army US - Requirements Pavement Flexible 10 4 4 NOTES: H38x13-18TIRESIZE-TIRESPRESSUREAT8.86kgf/cm(126psi) 5 5 678 6 FLEXIBLE PAVEMENTTHICKNESS(in.) FLEXIBLE PAVEMENTTHICKNESS(cm) SUBGRADE STRENGHT-CBR 78 20 WEIGHT ONMAIN LANDING GEAR 19398 (42765) 26892 (59287) 29336 (64675) 33064 (72894) 31400 (69225) DEPARTURES (kg) (lb) iue7.4 Figure 9 9

ANNUAL 25000 15000 6000 3000 1200 10 10 LNIGMANUAL PLANNING AIRPORT 30 40 2 50 20 030 20 60 70 e 08/03 Dec eto 7 Section 30 ae7-6 Page 80

EM170APM070017.DGN

b-apm1346 AIRPORT PLANNING MANUAL

2 NOTES: H38 X 13−18 TIRE SIZE − TIRES PRESSURE AT 9.14 kgf/cm (130 psi)

SUBGRADE STRENGHT − CBR

3 4 5 6 789 10 20 30

WEIGHT ON MAIN LANDING GEAR (kg) (lb) 34008 (74975) 32300 (71209) 29328 (64657) 27062 (59661) 19388 (42743)

10000 COVERAGES (USED FOR ACN CALCULATIONS)

ANNUAL DEPARTURES

1200

3000

6000

15000

25000

3 4 5 6789 10 20 30 FLEXIBLE PAVEMENT THICKNESS (in.) 8910 20 30 40 50 60 70 80 FLEXIBLE PAVEMENT THICKNESS (cm) EM170APM070001A.DGN

Flexible Pavement Requirements - US Army Corps of Engineers Design Method Figure 7.5

Section 7 EFFECTIVITY: EMBRAER 170 LR OR SU OR SE ACFT MODEL Page 7-7 Jul 01/05 w-apm1346 AIRPORT PLANNING MANUAL

7.6. FLEXIBLE PAVEMENT REQUIREMENTS, LCN METHOD

The LCN method presents curves for flexible pavements. They have been built using procedures and curves in the ICAO Aerodrome Design Manual, Part 3 - Pavements, Document 9157-AN/901, 1983. The same chart includes the data of equivalent single-wheel load versus pavement thickness.

Section 7 EFFECTIVITY: ALL Page 7-8 Dec 08/03 b-apm1346 b-apm1346

FETVT:EBAR10SDACFT STD 170 MODEL EMBRAER EFFECTIVITY: EQUIVALENT SINGLE WHEEL LOAD - (lb) 20000 10000 40000 30000 PART 2,PAR.4.1.3 IN ICAOAERODROMEMANUAL. ARE DERIVEDBYMETHODSSHOWN EQUIVALENT SINGLEWHEELLOADS NOTES: 3 TIRES H38x13-18AT8.86kg/cm(126psi) 4 WEIGHT ONMAIN LANDING GEAR FLEXIBLE PAVEMENTTHICKNESS-h(cm) 5 2 FLEXIBLE PAVEMENTTHICKNESS-h(in.) kg (lb) 6 7 34 8 9 10

19398 (42765) 26892 (59287) 29336 (64675) 31400 (69225) 33064 (72894) 5 lxbePvmn eurmns-LNMethod LCN - Requirements Pavement Flexible 6 2 7 20 89 10 30 40 iue7.6 Figure 50 030 20 60 70 LNIGMANUAL PLANNING AIRPORT 80 90 100 100 10 LCN -LOADCLASSIFICATIONNUMBER 20 30 e 08/03 Dec eto 7 Section ae7-9 Page 40 14000 10000 12000 16000 8000 6000

EM170APM070018.DGN EQUIVALENT SINGLE WHEEL LOAD - (kg) AIRPORT PLANNING MANUAL

2 TIRES H38x13−18 AT 9.14 kg/cm (130 psi)

40000 16000 WEIGHT ON MAIN 14000 30000 LANDING GEAR 32300 (71209) kg (lb) 12000

34008 (74975) 10000 20000 29328 (64657) 27062 (59661) 8000

19388 (42743) 6000

10000 4 5 6 7 8 9 10 20 30 40 50 60 70 8090 10 20 30 40 50 100 EQUIVALENT SINGLE WHEEL LOAD − (lb) FLEXIBLE PAVEMENT THICKNESS − h (cm) LCN − LOAD CLASSIFICATION NUMBER EQUIVALENT SINGLE WHEEL LOAD − (kg)

2 3 4 5 6 7 8 9 10 20 30 FLEXIBLE PAVEMENT THICKNESS − h (in.)

NOTES: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL. PART 2, PAR. 4.1.3 EM170APM070012A.DGN

Flexible Pavement Requirements - LCN Method Figure 7.7

Section 7 EFFECTIVITY: EMBRAER 170 LR OR SU OR SE ACFT MODEL Page 7-10 Jul 01/05 w-apm1346 AIRPORT PLANNING MANUAL

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 general accordance with the procedures outlined in the 1955 edition of “Design of Concrete Airport Pavement” 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 following procedure is used to develop rigid pavement design curves such as those shown in the chart: • Once the scale for the pavement thickness to the left and the scale for allowable working stress to the right have been established, an arbitrary load line is drawn representing the main 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 then established on the basis of the curve for k=300, already established.

Section 7 EFFECTIVITY: ALL Page 7-11 Dec 08/03 b-apm1346 FETVT:EBAR10SDACFT STD 170 MODEL EMBRAER EFFECTIVITY: RIGID PAVEMENT REQUIREMENTS

NOTES: TIRES H38 x 13-18 2 TIRE PRESSURE 8.86 kgf/cm (126 psi) (UNLOADED) ii aeetRqieet otadCmn soito einMethod Design Association Cement Portland - Requirements Pavement Rigid

60 60 850

22 800 55 55

33064 (72894) 750 20 50 50 31400 (69225) 700 29336 (64675) 18 45 650 45 26892 (59287)

2 600 16 40 40 550

iue7.8 Figure 14 WEIGHT ON MAIN LANDING GEAR - kg (lb) 35 19398 (42765) 35 500 450 12 30 30 400 MANUAL PLANNING AIRPORT 10 25 25 350

300 8 20 20 250 k= 300 lb/in k= 150 lb/in k= 75 lb/in3 3 3 6 15 k= 550 lb/in 15 MAXIMUM POSSIBLE MAIN-GEAR 3 200 LOAD ATWEIGHT MAXIMUM AND DESIGN AFT C.G. RAMP PAVEMENT THICKNESS (cm) PAVEMENT THICKNESS (in.) 4 10 10 150 ALLOWABLE WORKING STRESS - psi ALLOWABLE WORKING STRESS - kgf/cm 100 2 5 5 50

0 0 0 0

NOTE: THE VALUES OBTAINED BY USING THE ae7-12 Page e 08/03 Dec eto 7 Section MAXIMUM LOAD REFERENCE LINE AND ANY VALUE OF "K" ARE EXACT. FOR LOADS LESS THAN MAXIMUM, THE CURVES ARE EXACT FOR K=300 BUT DEVIATE SLIGHTLY FOR OTHER VALUES OF "K". EM170APM070020.DGN

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u 01/05 Jul

CTMODEL ACFT ae7-13 Page

FETVT:EBAR10L RS RSE OR SU OR LR 170 EMBRAER EFFECTIVITY:

eto 7 Section

iue7.9 Figure ii aeetRqieet otadCmn soito einMethod Design Association Cement Portland - Requirements Pavement Rigid NOTE: 16 20 22 14 12 18 PAVEMENT THICKNESS10 (in.) 6 8 2 4 0

PAVEMENT THICKNESS (cm) 50 40 25 60 55 10 35 45 20 15 30 SLIGHTLY FOROTHERVALUES OF"K". ARE EXACTFOR K=300BUTDEVIATE LOADS LESSTHAN MAXIMUM,THECURVES ANY VALUEOF"K" AREEXACT.FOR MAXIMUM LOAD REFERENCELINEAND THE VALUESOBTAINED BYUSINGTHE 5 0

MAXIMUM POSSIBLE MAIN-GEAR LOAD AT MAXIMUM DESIGN RAMP

WEIGHT AND AFT C.G. NOTES: RIGID PAVEMENTREQUIREMENTS TIRE PRESSURE9.14kgf/cm(130psi)(UNLOADED) TIRES H38x13-18

WEIGHT ON MAIN LANDING GEAR - kg (lb)

k= 550 lb/in 550 k=

k= 300 lb/in 300 k=

k= 150 lb/in 150 k= 3

19388 (42743) 27062 (59661)29328 (64657)32300 (71209)34008 (74975)

k= 75 lb/in 75 k= 3 15 10 60 55 50 40 25 0 35 45 20 30 5 2 ALLOWABLE WORKING STRESS (kgf/cm ) 100 150 200 250 300 350 400 450 500 550 600 650 700 850 750 800 50 0

EM170APM070010.DGN ALLOWABLE WORKING STRESS (psi)

LNIGMANUAL PLANNING AIRPORT AIRPORT PLANNING MANUAL

7.8. RIGID PAVEMENT REQUIREMENTS, LCN METHOD

This LCN Method presents curves for rigid pavements. They have been built using procedures and curves in ICAO Aerodrome Design Manual, Part 3 - Pavements, Document 9157-AN/901, 1983. The same 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 of relative stiffness values 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. For example, to find an RRS value based on an E of 3,000,000 psi, the “E” factor of 0.931 is multiplied by the RRS value found in figure 7.6.3. The effect of the variations of µ on the RRS value is treated in a similar manner.

Section 7 EFFECTIVITY: ALL Page 7-14 Dec 08/03 b-apm1346 b-apm1346 FETVT:ALL EFFECTIVITY: d(in) 11.0 10.0 11.5 10.5 15.0 14.0 13.0 15.5 14.5 13.5 12.5 25.0 24.0 23.0 22.0 21.0 20.0 19.0 18.0 17.0 24.5 23.5 22.5 21.5 20.5 19.5 18.5 17.5 16.5 12.0 16.0 9.0 8.0 7.0 6.0 9.5 8.5 7.5 6.5 42.67 52.94 35.34 59.43 57.83 54.59 49.60 47.90 44.43 39.06 33.43 61.02 56.22 51.28 46.18 40.88 37.22 31.48 89.04 87.64 86.24 90.43 84.83 81.99 77.66 76.20 74.73 71.76 70.26 67.23 65.69 62.59 80.55 73.25 68.75 64.15 91.81 83.41 79.11 k=75 =0 =5 k=200 k=150 k=100 61.13 59.70 58.25 56.78 72.27 68.17 85.44 69.54 82.86 81.56 80.26 77.63 76.30 74.96 34.63 84.15 78.95 73.62 66.78 65.38 63.98 36.35 39.71 38.04 62.56 32.89 49.27 44.57 42.97 50.80 46.16 53.82 52.32 47.72 55.31 31.11 29.30 41.35 70.91 d=RIGID−PAVEMENTTHICKNESS.in. WHERE: E=YOUNG’SMODULUS4x10psi k=SUBGRADEMODULUS,lb/in. RADIUS OFRELATIVESTIFFNESS() = 34.37 38.83 37.36 31.29 47.27 44.52 43.12 40.28 35.88 32.85 29.72 48.63 45.90 74.87 49.98 76.04 71.34 77.20 73.70 72.52 70.14 68.94 67.74 62.84 60.34 65.30 61.60 66.52 64.08 55.24 53.94 56.53 52.63 26.47 59.08 41.71 51.31 28.11 57.81 =POISSON’SRATIO0.15 4 aiso eaieStiffness Relative of Radius 12( 1−)k VALUES ININCHES 70.76 71.84 60.77 34.77 30.57 36.14 63.04 59.63 53.80 50.20 45.26 43.99 41.43 40.13 33.39 31.99 26.16 24.63 68.59 67.49 64.16 58.48 57.32 56.15 54.98 48.98 47.75 42.72 37.48 29.12 27.65 69.68 66.38 65.28 52.61 51.41 46.51 38.81 61.91 Ed 3 2 iue7.10 Figure =24.1652 k=250 34.17 27.54 24.74 40.40 32.89 23.30 39.18 37.95 35.45 31.58 30.25 26.15 57.47 47.47 65.90 64.86 63.83 61.73 56.39 52.00 45.16 67.95 66.92 62.78 60.68 59.62 58.55 50.88 49.75 48.62 46.32 43.98 36.71 28.91 41.61 42.80 55.31 54.21 53.11 LNIGMANUAL PLANNING AIRPORT k=300 61.97 57.97 35.07 33.87 30.17 63.94 55.94 52.84 50.74 47.54 37.44 23.64 62.96 59.99 56.96 51.80 45.36 44.26 40.89 38.60 36.26 24.99 21.42 22.26 64.92 60.98 58.98 53.88 49.68 46.45 43.15 42.02 39.75 32.65 31.42 27.62 26.32 54.91 48.61 28.91 4 d k 3 3 6 k=350 46.77 58.68 57.72 24.04 22.74 50.84 49.84 45.74 43.64 40.44 37.14 30.23 29.03 47.80 44.70 34.89 32.59 31.42 26.58 25.32 48.82 42.58 39.35 38.25 36.02 33.75 62.46 59.63 61.52 60.58 52.84 51.84 53.83 56.75 55.78 27.81 41.51 54.81 =0 =0 k=550 k=500 k=400 34.84 49.17 57.67 50.14 45.24 44.24 38.06 36.99 52.06 51.10 48.20 46.23 43.23 41.19 59.50 58.59 54.89 35.92 40.15 47.22 56.75 55.82 53.95 22.00 69 25.44 26.90 25.70 24.49 23.25 20.72 33.74 32.64 29.24 30.39 39.11 53.01 42.21 60.41 31.52 28.08 37.97 33.97 30.87 53.67 57.14 41.84 54.54 50.13 49.23 48.33 36.99 35.99 34.99 52.79 45.59 44.66 56.28 51.02 47.42 43.72 42.78 40.88 39.92 38.95 32.95 26.55 28.74 27.65 55.41 51.91 46.51 29.81 31.91 23.16 21.99 19.13 20.80 19.59 24.31 21.47 39.92 29.11 48.07 24.84 23.74 22.61 28.06 27.00 25.93 55.79 50.69 47.19 46.30 42.70 53.26 54.95 51.55 49.82 48.95 41.78 40.85 20.31 33.17 32.17 35.14 30.14 34.16 31.16 38.03 37.08 36.12 38.98 45.41 44.51 43.61 54.11 52.41 ae7-15 Page e 08/03 Dec eto 7 Section

EM170APM070007.DGN FETVT:ALL EFFECTIVITY: E FACTOR FACTOR 1.010 1.000 1.015 1.005 0.995 1.10 1.00 0.90 0.80 1.05 0.95 0.85 0 0 .501 .502 0.25 0.20 0.15 0.10 0.05 0 012345 NOTE: BOTH CURVESONTHISPAGEAREUSEDTOADJUSTTHE−VALUES. aiso eaieSifes(te values) (other Stiffness Relative of Radius E, YOUNG’SMODULUS(10,PSI) EFFECT OFEON−VALUES EFFECT OFON−VALUES iue7.11 Figure , POISSON’SRATIO LNIGMANUAL PLANNING AIRPORT 6 ae7-16 Page e 08/03 Dec eto 7 Section

EM170APM070008.DGN

b-apm1346 AIRPORT PLANNING MANUAL

2 TIRES H38x13−18 AT 8.86 kg/cm (126 psi)

40000 17000

15000 WEIGHT ON MAIN 30000 LANDING GEAR 13000 kg (lb)

33064 (72894) 31400 (69225) 29336 (64675) 10000 26892 (59287) 20000 9000

8000

19398 (42765) 7000

6000 EQUIVALENT SINGLE WHEEL LOAD − (lb)

5000 EQUIVALENT SINGLE WHEEL LOAD − (kg) 10000 30 40 50 60 70 80 90 100 200 300 10 20 30 40

RADIUS OF RELATIVE STIFFNESS − (cm) LCN − LOAD CLASSIFICATION NUMBER

20 30 40 50 60 70 80 90 100

RADIUS OF RELATIVE STIFFNESS − (in.)

NOTES: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL. PART 2, PAR. 4.1.3 EM170APM070019A.DGN

Rigid Pavement Requirements - LCN Method Figure 7.12

Section 7 EFFECTIVITY: EMBRAER 170 STD ACFT MODEL Page 7-17 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

2 TIRES H38x13−18 AT 9.14 kg/cm (130 psi)

40000 WEIGHT ON MAIN LANDING GEAR 16000 kg (lb) 14000 30000

12000

34008 (74975) 10000 32300 (71209) 20000 29328 (64657) 27062 (59661) 8000

19388 (42743) 6000 EQUIVALENT SINGLE WHEEL LOAD − (lb) EQUIVALENT SINGLE WHEEL LOAD − (kg) 10000 40 50 60 70 80 90 100 200 300 10 20 30 40

RADIUS OF RELATIVE STIFFNESS − (cm) LCN − LOAD CLASSIFICATION NUMBER

20 30 40 50 60 7080 90 100

RADIUS OF RELATIVE STIFFNESS − (in.)

NOTES: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL. PART 2, PAR. 4.1.3 EM170APM070011A.DGN

Rigid Pavement Requirements - LCN Method Figure 7.13

Section 7 EFFECTIVITY: EMBRAER 170 LR OR SU OR SE ACFT MODEL Page 7-18 Jul 01/05 w-apm1346 AIRPORT PLANNING MANUAL

7.9. ACN - PCN SYSTEM - FLEXIBLE AND RIGID PAVEMENTS

The ACN/PCN system as referenced in Amendment 35 to ICAO Annex 14, “Aerodromes”, provides a standardized international aircraft/pavement rating system. The PCN is an index rating of the mass that according to evaluation can be borne by the pavement when applied by a standard single wheel. The ACN is established for the particular pavement type and subgrade category of the rated pavement, as well as for the particular aircraft mass and characteristics. An aircraft shall have an ACN equal to or less than the PCN to operate without restriction on the pavement. The method of pavement evaluation is left up to the airport, and the results of such evaluation are presented as follows:

Table 7.1 - Pavement Evaluation PAVEMENT SUBGRADE CATEGORY TIRE PRESSURE CATEGORY METHOD TYPE R – Rigid A – High W – No Limit T – Technical F – Flexible B – Medium X – to 1.5 Mpa (217 psi) U – Using aircraft C – Low Y – to 1.0 Mpa (145 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 - CBR 15. B. Medium Strength - CBR 10. C. Low Strength - CBR 6. D. Ultra Low Strength - CBR 3. The rigid pavements have four subgrade categories: A. High Strength - Subgrade k = 150 MN/m3 (550 lb/in3). B. Medium Strength - k = 80 MN/m3 (300 lb/in3). C. Low Strength - k = 40 MN/m3 (150 lb/in3). D. Ultra Low Strength - k = 20 MN/m3 (75 lb/in3).

Section 7 EFFECTIVITY: ALL Page 7-19 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

FLEXIBLE PAVEMENT SUBGRADE

NOTES: H38 x 13−18 TIRE SIZE 2 TIRE PRESSURE 8.86 kgf/cm (126 psi) (UNLOADED)

30 SBGRADE STRENGTH

ULTRA LOW − CBR=3% LOW − CBR=6% 25 MEDIUM−CBR=10% HIGH−CBR=15%

5 MAXIMUM RAMP WEIGHT AIRCRAFT CLASSIFICATION NUMBER−ACN

0 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 36150 AIRCRAFT GROSS WEIGHT−kg

44000 48000 52000 56000 60000 64000 68000 72000 76000 80000 84000 AIRCRAFT GROSS WEIGHT−lb EM170APM070016A.DGN

ACN For Flexible Pavement Figure 7.14

Section 7 EFFECTIVITY: EMBRAER 170 STD ACFT MODEL Page 7-20 Dec 08/03 b-apm1346 AIRPORT PLANNING MANUAL

FLEXIBLE PAVEMENT SUBGRADE

NOTES: H38 x 13−18 TIRE SIZE 2 TIRE PRESSURE 9.14 kgf/cm (130 psi) (UNLOADED)

40 SBGRADE STRENGTH

ULTRAQ LOW − CBR=3% 35 LOW − CBR=6% MEDIUM−CBR=10% HIGH−CBR=15% 25

AIRCRAFT CLASSIFICATION NUMBER−ACN 5 MAXIMUM RAMP WEIGHT 0 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 37360 AIRCRAFT GROSS WEIGHT−kg

44000 48000 52000 56000 60000 64000 68000 72000 76000 80000 84000 AIRCRAFT GROSS WEIGHT−lb EM170APM070004A.DGN

ACN For Flexible Pavement Figure 7.15

Section 7 EFFECTIVITY: EMBRAER 170 LR OR SU OR SE ACFT MODEL Page 7-21 Oct 06/11 w-apm1346 FETVT:EBAR10A CTMODEL ACFT AR 170 EMBRAER EFFECTIVITY: ACN − FLEXIBLE PAVEMENT 20000 20 25 35 40 45 10 15 44000 0 5 NOTES: FLEXIBLE PAVEMENTSUBGRADE 22000 48000 TIRE PRESSURE9.56kgf/cm(136psi)(UNLOADED) H38 x13−18TIRESIZE 20 60 00 40 80 20 60 00 84000 80000 76000 72000 68000 64000 60000 56000 52000 24000 26000 AIRCRAFT GROSSWEIGHT−kg C o lxbePavement Flexible For ACN AIRCRAFT GROSSWEIGHT−lb 28000 iue7.16 Figure 2 30000 LNIGMANUAL PLANNING AIRPORT 32000 HIGH−CBR=15% MEDIUM−CBR=10% LOW −CBR=6% ULTRAQ LOW−CBR=3% SBGRADE STRENGTH 34000 36000 38000 ae7-22 Page eto 7 Section c 06/11 Oct

38760 MAXIMUM RAMP WEIGHT 86000 39000

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RIGID PAVEMENT SUBGRADES

NOTES: H38 x 13−18 TIRE SIZE 2 TIRE PRESSURE 8.86 kgf/cm (126 psi) (UNLOADED)

10 3 3 ULTRA LOW−k=20 MN/m (75 lb/in ) 3 LOW−k=40 MN/m3 (150 lb/in ) 3 MEDIUM−k=80 MN/m3 (300 lb/in ) 3 3 5 HIGH−k=150 MN/m (550 lb/in ) MAXIMUM RAMP WEIGHT AIRCRAFT CLASSIFICATION NUMBER−ACN

0 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 36150 AIRCRAFT GROSS WEIGHT−kg 44000 48000 52000 56000 60000 64000 68000 72000 76000 80000 84000 AIRCRAFT GROSS WEIGHT−lb EM170APM070015A.DGN

ACN For Rigid Pavement Figure 7.17

Section 7 EFFECTIVITY: EMBRAER 170 STD ACFT MODEL Page 7-23 Oct 06/11 w-apm1346 AIRPORT PLANNING MANUAL

RIGID PAVEMENT SUBGRADES

NOTES: H38 x 13−18 TIRE SIZE 2 TIRE PRESSURE 9.14 kgf/cm (130 psi) (UNLOADED)

3 3 ULTRA LOW−k=20 MN/m (75 lb/in ) 10 3 3 LOW−k=40 MN/m (150 lb/in ) 3 3 MEDIUM−k=80 MN/m (300 lb/in ) 3 3 HIGH−k=150 MN/m (550 lb/in )

5 AIRCRAFT CLASSIFICATION NUMBER−ACN MAXIMUM RAMP WEIGHT

20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 37360 AIRCRAFT GROSS WEIGHT−kg

44000 48000 52000 56000 60000 64000 68000 72000 76000 80000 84000 AIRCRAFT GROSS WEIGHT−lb EM170APM070003A.DGN

ACN For Rigid Pavement Figure 7.18

Section 7 EFFECTIVITY: EMBRAER 170 LR OR SU OR SE ACFT MODEL Page 7-24 Oct 06/11 w-apm1346 AIRPORT PLANNING MANUAL

RIGID PAVEMENT SUBGRADES

NOTES: H38 x 13−18 TIRE SIZE 2 TIRE PRESSURE 9.56 kgf/cm (136 psi) (UNLOADED)

15 ACN − FLEXIBLE PAVEMENT 10 3 3 ULTRA LOW−k=20 MN/m (75 lb/in ) 3 LOW−k=40 MN/m3 (150 lb/in ) 3 MEDIUM−k=80 MN/m3 (300 lb/in ) 3 3 5 HIGH−k=150 MN/m (550 lb/in ) MAXIMUM RAMP WEIGHT 0 20000 22000 24000 26000 28000 30000 32000 34000 36000 38000 39000

AIRCRAFT GROSS WEIGHT−kg 38760

44000 48000 52000 56000 60000 64000 68000 72000 76000 80000 84000 86000 AIRCRAFT GROSS WEIGHT−lb EM170APM070097A.DGN

ACN For Rigid Pavement Figure 7.19

Section 7 EFFECTIVITY: EMBRAER 170 AR ACFT MODEL Page 7-25 / 26 Oct 06/11 w-apm1346

AIRPORT PLANNING MANUAL

8. POSSIBLE EMBRAER 170 DERIVATIVE AIRCRAFT

8.1. NOT APPLICABLE

Section 8 EFFECTIVITY: ALL Page 8-1 / 2 Dec 08/03 w-apm1346

AIRPORT PLANNING MANUAL

9. SCALED DRAWINGS

9.1. GENERAL

This section provides plan 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

Section 9 EFFECTIVITY: ALL Page 9-1 Dec 08/03 w-apm1346 FETVT:ALL EFFECTIVITY: TMDESCRIPTION ITEM 1 7 4 6 5 2 3 EXTERNAL POWERSUPPLY115VAC POTABLE WATERSERVICINGPANEL AIR CONDITIONINGLOWPRESSURE OXYGEN REFILL/REPLACEBOTTLE EXTERNAL POWERSUPPLY28VDC WASTE SERVICINGPANEL ENGINE AIRSTARTING 0 01632 01 025m 20 15 10 5 cl:1Ic qas3 Feet 32 Equals Inch 1 Scale: 13 13 4 3 6 2 11 1 WING SPAN: iue9.1 Figure (85 ft3in.) 25.99 m 12 ITEM 48 14 13 10 12 11 LNIGMANUAL PLANNING AIRPORT 9 8 11 10 10 14 5 14 7 64 9 8 PRESSURE REFUELING/DEFUELING GROUNDING POINT(RIGHTMLG) 80 ft NOSE LANDINGGEAR MAIN LANDINGGEAR PASSENGER DOOR SERVICE DOOR CARGO DOOR DESCRIPTION e 08/03 Dec eto 9 Section ae9-2 Page

EM170APM090001.DGN

w-apm1346 w-apm1346 FETVT:ALL EFFECTIVITY: TMDESCRIPTION ITEM 1 7 4 6 5 2 3 EXTERNAL POWERSUPPLY115VAC POTABLE WATERSERVICINGPANEL AIR CONDITIONINGLOWPRESSURE OXYGEN REFILL/REPLACEBOTTLE EXTERNAL POWERSUPPLY28VDC WASTE SERVICINGPANEL ENGINE AIRSTARTING 0 01632 cl:1Ic qas5 Feet 50 Equals Inch 1 Scale: 01 025m 20 15 10 5 11 13 WING SPAN: 13 (85 ft3in.) 1 4 3 2 6 iue9.2 Figure 25.99 m 48 ITEM 14 13 10 12 10 11 12 LNIGMANUAL PLANNING AIRPORT 10 5 9 8 14 11 7 14 64 9 8 80 ft PRESSURE REFUELING/DEFUELING GROUNDING POINT(RIGHTMLG) NOSE LANDINGGEAR MAIN LANDINGGEAR PASSENGER DOOR SERVICE DOOR CARGO DOOR DESCRIPTION e 08/03 Dec eto 9 Section ae9-3 Page

EM170APM090002.DGN FETVT:ALL EFFECTIVITY: TMDESCRIPTION ITEM 1 7 4 6 5 2 3 EXTERNAL POWERSUPPLY115VAC POTABLE WATERSERVICINGPANEL AIR CONDITIONINGLOWPRESSURE OXYGEN REFILL/REPLACEBOTTLE EXTERNAL POWERSUPPLY28VDC WASTE SERVICINGPANEL ENGINE AIRSTARTING cl:1Ic qas10Feet 100 Equals Inch 1 Scale: 0 01632 13 11 WING SPAN: 01 025m 20 15 10 5 3 13 (85 ft3in.) 1 4 6 iue9.3 Figure 2 25.99 m 48 12 ITEM 10 10 64 7 14 5 13 10 12 11 9 8 LNIGMANUAL PLANNING AIRPORT 9 14 80 ft 14 11 8 PRESSURE REFUELING/DEFUELING GROUNDING POINT(RIGHTMLG) NOSE LANDINGGEAR MAIN LANDINGGEAR PASSENGER DOOR SERVICE DOOR CARGO DOOR DESCRIPTION e 08/03 Dec eto 9 Section ae9-4 Page

EM170APM090003.DGN

w-apm1346 w-apm1346 FETVT:ALL EFFECTIVITY: TMDESCRIPTION ITEM 1 7 4 6 5 2 3 EXTERNAL POWERSUPPLY115VAC POTABLE WATERSERVICINGPANEL AIR CONDITIONINGLOWPRESSURE OXYGEN REFILL/REPLACEBOTTLE EXTERNAL POWERSUPPLY28VDC WASTE SERVICINGPANEL ENGINE AIRSTARTING 0 01632 01 025m 20 15 10 5 11 13 cl:1t 500 to 1 Scale: 13 WING SPAN: 2 1 4 3 6 (85 ft3in.) iue9.4 Figure 25.99 m 48 ITEM 14 13 10 12 LNIGMANUAL PLANNING AIRPORT 11 9 8 10 12 10 14 7 5 11 14 64 9 8 PRESSURE REFUELING/DEFUELING 80 ft GROUNDING POINT(RIGHTMLG) NOSE LANDINGGEAR MAIN LANDINGGEAR PASSENGER DOOR SERVICE DOOR CARGO DOOR DESCRIPTION e 08/03 Dec eto 9 Section ae9-5 Page

EM170APM090004.DGN FETVT:ALL EFFECTIVITY: TMDESCRIPTION ITEM 1 7 4 6 5 2 3 EXTERNAL POWERSUPPLY115VAC POTABLE WATERSERVICINGPANEL AIR CONDITIONINGLOWPRESSURE OXYGEN REFILL/REPLACEBOTTLE EXTERNAL POWERSUPPLY28VDC WASTE SERVICINGPANEL ENGINE AIRSTARTING 0 01632 11 13 5101520 13 WING SPAN: cl:1t 1000 to 1 Scale: 4 1 3 (85 ft3in.) 2 6 25.99 m iue9.5 Figure 48 12 10 5 64 14 ITEM 10 7 14 13 10 12 14 11 9 8 11 9 LNIGMANUAL PLANNING AIRPORT 8 80 ft 25 PRESSURE REFUELING/DEFUELING GROUNDING POINT(RIGHTMLG) NOSE LANDINGGEAR MAIN LANDINGGEAR PASSENGER DOOR 50 m SERVICE DOOR CARGO DOOR DESCRIPTION e 08/03 Dec eto 9 Section ae9-6 Page

EM170APM090005.DGN

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