EMBRAER S.A 12227-901 SAO JOSE DOS CAMPOS - S.P. BRAZIL PHONE: + 55 12 3927-7517 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-1901 15 AUGUST 2005 REVISION 19 - 27 AUGUST 2021
Copyright © 2021 by EMBRAER S.A. All rights reserved.
EMBRAER S.A. AV. BRIGADEIRO FARIA LIMA, 2.170 - PHONE: + 55 12 3927-7517 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-1901 - ″AIRPORT PLANNING MANUAL″.
FRONT MATTER - REVISION No. 19 DATED AUGUST 27/2021
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 Aug 27/21
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-apm1901
AIRPORT PLANNING MANUAL
RECORD OF TEMPORARY REVISIONS
Temporary Page Issued Date By By Rev. No. Number Date Removed w-apm1901
AIRPORT PLANNING MANUAL
TEMPORARY REVISION STATUS REPORT
S* INDICATES TR HAS BEEN SUPERSEDED BY THE TR REFERRED TO.
EFFECTIVITY: ALL TR STATUS REPORT Page 1 / 2
w-apm1901 Aug 27/21
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 corre- sponds to the last digits of the highest aircraft designation number to indicate the end of the effectivity.
LIST OF SERVICE BULLETINS Page 1 / 2 Jan 09/06 w-apm1901
AIRPORT PLANNING MANUAL
Title 3-2 ...... Oct 07/13 BLOCK PAGE REVISION3-3 ...... Oct 07/13 TRList 3-4 ...... Oct 07/13 * 1 (rev) ...... Aug 27/21 3-5 ...... Oct 07/13 2 Blank ...... Oct 22/07 3-6 ...... Oct 07/13 SBList 3-7 ...... Oct 07/13 1 ...... Jan 09/06 3-8 ...... Oct 07/13 2 Blank ...... Aug 15/05 3-9 ...... Oct 07/13 List of Effective Pages 3-10 ...... Oct 07/14 * 1 (rev) ...... Aug 27/21 3-11 ...... Oct 07/14 * 2 (rev) ...... Aug 27/21 3-12 ...... Oct 07/14 Table of Contents 3-13 ...... Oct 07/14 1 ...... May 22/20 3-14 ...... Oct 07/14 2 ...... May 21/21 3-15 ...... Oct 07/14 List of Tables 3-16 ...... Oct 07/14 1 ...... May 21/21 3-17 ...... Oct 07/14 2 Blank ...... Aug 15/05 3-18 ...... Oct 07/14 List of Figures 3-19 ...... Oct 07/14 1 ...... May 22/20 3-20 ...... Oct 07/14 2 ...... May 22/20 3-21 ...... Oct 07/14 3 ...... May 21/21 3-22 ...... Oct 07/14 4 Blank ...... Aug 15/05 3-23 ...... Oct 07/14 Section 1 3-24 ...... Oct 07/14 1-1 ...... Jan 09/06 3-25 ...... Oct 07/14 1-2 ...... Aug 09/19 3-26 ...... Oct 07/14 1-3 ...... Oct 06/11 3-27 ...... Oct 07/14 1-4 Blank ...... Aug 15/05 3-28 ...... Oct 07/14 Section 2 Section 4 2-1 ...... Oct 07/13 4-1 ...... Oct 07/13 2-2 ...... Oct 07/13 4-2 ...... Oct 07/13 2-3 ...... Oct 07/13 4-3 ...... Oct 07/13 2-4 ...... May 21/21 4-4 ...... Oct 07/13 2-5 ...... May 22/20 4-5 ...... Sep 27/19 2-6 ...... May 22/20 4-6 ...... May 25/18 2-7 ...... May 22/20 4-7 ...... May 25/18 2-8 ...... May 22/20 4-8 ...... May 25/18 2-9 ...... May 22/20 4-9 ...... May 25/18 2-10 ...... May 22/20 4-10 ...... May 25/18 2-11 ...... May 22/20 4-11 ...... May 25/18 2-12 ...... May 22/20 4-12 ...... May 25/18 2-13 ...... May 22/20 4-13 ...... May 25/18 * 2-14 (rev) ...... Aug 27/21 4-14 Blank ...... May 25/18 2-15 ...... May 22/20 Section 5 2-16 ...... May 22/20 5-1 ...... Oct 07/13 2-17 ...... May 22/20 5-2 ...... Oct 07/13 2-18 ...... May 22/20 5-3 ...... May 22/20 Section 3 5-4 ...... Oct 07/13 3-1 ...... Oct 07/13 5-5 ...... Oct 07/13
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).
EFFECTIVITY: ALL LIST OF EFFECTIVE PAGES REV. 19 Page 1 Aug 27/21 w-apm1901 AIRPORT PLANNING MANUAL
5-6 ...... Oct 07/13 8-1 ...... Oct 07/13 5-7 ...... Oct 07/13 8-2 Blank ...... Oct 07/13 5-8 ...... Oct 07/13 Section 9 5-9 ...... May 25/18 9-1 ...... Oct 07/13 5-10 ...... Oct 07/13 9-2 ...... Oct 07/13 5-11 ...... Oct 07/13 9-3 ...... Oct 07/13 5-12 ...... Oct 07/13 9-4 ...... Oct 07/13 5-13 ...... May 22/20 9-5 ...... Oct 07/13 5-14 Blank ...... Oct 07/13 9-6 ...... Oct 07/13 Section 6 6-1 ...... Oct 07/13 6-2 ...... Oct 07/13 6-3 ...... Oct 07/13 6-4 ...... Oct 07/13 6-5 ...... Oct 07/13 6-6 ...... Oct 07/13 6-7 ...... Oct 07/13 6-8 ...... Oct 07/13 6-9 ...... Oct 07/13 6-10 ...... Oct 07/13 6-11 ...... Oct 07/13 6-12 Blank ...... Oct 07/13 Section 7 7-1 ...... Oct 07/13 7-2 ...... May 21/21 7-3 ...... Oct 07/13 7-4 ...... Oct 07/13 7-5 ...... Oct 07/13 7-6 ...... May 21/21 7-7 ...... Oct 07/13 7-8 ...... May 21/21 7-9 ...... May 21/21 7-10 ...... May 21/21 7-11 ...... May 21/21 7-12 ...... May 21/21 7-13 ...... May 21/21 7-14 ...... May 21/21 7-15 ...... May 21/21 7-16 ...... May 21/21 7-17 ...... May 21/21 * 7-18 (rev) ...... Aug 27/21 * 7-19 (rev) ...... Aug 27/21 * 7-20 (rev) ...... Aug 27/21 * 7-21 (rev) ...... Aug 27/21 7-22 Blank ...... May 21/21 7-23 (del) ...... Dec 18/06 7-24 Blank (del) ...... Dec 18/06 Section 8
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).
EFFECTIVITY: ALL LIST OF EFFECTIVE PAGES REV. 19 Page 2 Aug 27/21 w-apm1901 AIRPORT PLANNING MANUAL
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 ...... 2-2 2.3. Ground Clearances ...... 2-8 2.4. Interior Arrangements ...... 2-12 2.5. Passenger Cabin Cross Section ...... 2-15 2.6. Lower Compartment Containers ...... 2-17 2.7. Door Clearances ...... 2-18
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 ...... 3-9 3.4. Landing Fields Lengths ...... 3-20
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 Apron ...... 4-12
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
EFFECTIVITY: ALL TABLE OF CONTENTS Page 1 May 22/20 w-apm1901 AIRPORT PLANNING MANUAL
SECTION 6 - OPERATING CONDITIONS
6. Operating Conditions ...... 6-1 6.1. Engine Exhaust Velocities and Temperatures ...... 6-2 6.2. Airport and Community Noise ...... 6-9 6.3. Hazard Areas ...... 6-10
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, US Corps of Engineers Design Method ...... 7-5 7.6. Flexible Pavement Requirements, LCN Method ...... 7-7 7.7. Rigid Pavement Requirements, Portland Cement Association Design Method ...... 7-9 7.8. Rigid Pavement Requirements, LCN Method ...... 7-12 7.9. ACN - PCN System - Flexible and Rigid Pavements ...... 7-17
SECTION 8 - POSSIBLE EMBRAER 190 DERIVATIVE AIRCRAFT
8. Possible EMBRAER 190 Derivative Aircraft ...... 8-1 8.1. Not Applicable ...... 8-1
SECTION 9 - SCALED DRAWINGS
9. Scaled Drawings ...... 9-1 9.1. General ...... 9-1
EFFECTIVITY: ALL TABLE OF CONTENTS Page 2 May 21/21 w-apm1901 AIRPORT PLANNING MANUAL
LIST OF TABLES
TABLE TITLE SECTION PAGE
1.1 APM Arrangement ...... 01 1
2.1 Aircraft General Characteristics ...... 02 2
2.2 Ground Clearance - STD Aircraft Model ...... 02 9
2.3 Ground Clearance - LR Aircraft Model...... 02 10
2.4 Ground Clearance - AR Aircraft Model ...... 02 11
2.5 Capacity for the Cargo Compartment ...... 02 14
3.1 ISA ...... 03 1
4.1 Reference Codes...... 04 5
7.1 Pavement Evaluation...... 07 17
EFFECTIVITY: ALL LIST OF TABLES Page 1 / 2 May 21/21 w-apm1901
AIRPORT PLANNING MANUAL
LIST OF FIGURES
FIGURE TITLE SHEET SECTION PAGE
2.1 General Aircraft Dimensions ...... 02 4
2.2 Passenger and Service Doors Dimensions ...... 1 of 3 02 5
2.2 Passenger and Service Doors Dimensions ...... 2 of 3 02 6
2.2 Passenger and Service Doors Dimensions ...... 3 of 3 02 7
2.3 Aircraft Ground Clearances...... 02 8
2.4 Typical Interior Arrangements ...... 02 13
2.5 Economy Class Passenger Cabin Cross-Section...... 02 15
2.6 First Class Passenger Cabin Cross-Section...... 02 16
2.7 Door Dimensions...... 02 18
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 Payload x Range - ISA Conditions ...... 03 7
3.6 Payload x Range - ISA + 10 °C Conditions ...... 03 8
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 Takeoff Field Lengths - ISA Conditions ...... 03 16
3.14 Takeoff Field Lengths - ISA + 15 °C Conditions...... 03 17
3.15 Takeoff Field Lengths - ISA Conditions ...... 03 18
3.16 Takeoff Field Lengths - ISA + 15 °C Conditions...... 03 19
3.17 Landing Field Lengths - Flaps 5 ...... 03 21
3.18 Landing Field Lengths - Flaps Full ...... 03 22
3.19 Landing Field Lengths - Flaps 5 ...... 03 23
EFFECTIVITY: ALL LIST OF FIGURES Page 1 May 22/20 w-apm1901 AIRPORT PLANNING MANUAL
FIGURE TITLE SHEET SECTION PAGE
3.20 Landing Field Lengths - Flaps Full ...... 03 24
3.21 Landing Field Lengths - Flaps 5 ...... 03 25
3.22 Landing Field Lengths - Flaps Full ...... 03 26
3.23 Landing Field Lengths - Flaps 5 ...... 03 27
3.24 Landing Field Lengths - Flaps Full ...... 03 28
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 7
4.5 More than 90° Turn - Runway to Taxiway ...... 04 8
4.6 90° Turn - Runway to Taxiway...... 04 9
4.7 90° Turn - Runway to Taxiway...... 04 10
4.8 90° Turn - Taxiway to Taxiway ...... 04 11
4.9 Runway Holding Bay...... 04 12
4.10 Runway Holding Bay...... 04 13
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...... 1 of 2 06 6
6.5 Jet Wake Velocity Profile - Breakaway Power...... 2 of 2 06 7
EFFECTIVITY: ALL LIST OF FIGURES Page 2 May 22/20 w-apm1901 AIRPORT PLANNING MANUAL
FIGURE TITLE SHEET SECTION PAGE
6.6 Jet Wake Temperature Profile - Breakaway Power...... 06 8
6.7 Hazard Areas - Takeoff Power ...... 06 10
6.8 Hazard Areas - Ground Idle...... 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 - LCN Method ...... 07 8
7.6 Rigid Pavement Requirements - Portland Cement Associa- tion Design Method ...... 07 10
7.7 Rigid Pavement Requirements - Portland Cement Associa- tion Design Method ...... 07 11
7.8 Radius of Relative Stiffness ...... 07 13
7.9 Radius of Relative Stiffness (other values)...... 07 14
7.10 Rigid Pavement Requirements - LCN Method ...... 07 15
7.11 Rigid Pavement Requirements - LCN Method ...... 07 16
7.12 ACN For Flexible Pavement ...... 07 18
7.13 ACN For Flexible Pavement ...... 07 19
7.14 ACN For Rigid Pavement...... 07 20
7.15 ACN For Rigid Pavement...... 07 21
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
EFFECTIVITY: ALL LIST OF FIGURES Page 3 / 4 May 21/21 w-apm1901
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.
Section 1 EFFECTIVITY: ALL Page 1-1 Jan 09/06 w-apm1901 AIRPORT PLANNING MANUAL
• 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 CEP. 12.227-901- São José dos Campos - SP - Brazil Phone: (55 12) 3927-7517 http://www.embraer.com e-mail: [email protected] • For support regarding technical information contained in non-operational publication, please contact: Routine Issues: Contact Embraer Customer Support Service AOG Issues: Contact Embraer AOG group directly
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
Section 1 EFFECTIVITY: ALL Page 1-2 Aug 09/19 w-apm1901 AIRPORT PLANNING MANUAL
Table 1.2 - List of Acronyms and Abbreviations used in the APM
ACRONYMS AND ABBREVIATIONS DESCRIPTION APM Airport Planning Manual APU Auxiliary Power Unit AR Advanced Range 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
Section 1 EFFECTIVITY: ALL Page 1-3 / 4 Oct 06/11 w-apm1901
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 CF34-10 with 82.3 kN (18500 lbf) maximum takeoff thrust (Sea Level, Static Condition and ISA) installed under the wings. The aircraft has three versions, with different ranges as a function of the difference between the MTOWs: • The STD aircraft model - MTOW 47790 kg (105359 lb); • The LR aircraft model - MTOW 50300 kg (110892 lb); • The AR aircraft model - MTOW 51800 kg (114199 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 at which the aircraft may normally be landed.
MTOW
It is the maximum allowed total loaded aircraft weight at the start of the takeoff run.
BOW
It is the weight of the structure, powerplant, instruments, flight controls, hydraulic, electronic, electrical, air conditioning, oxygen, anti-icing and pressurization systems, interior furnishings, portable and 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 tanks.
Section 2 EFFECTIVITY: ALL Page 2-1 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
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 AIRCRAFT MODELS DESIGN WEIGHTS[1] STD LR AR MRW 47950 kg (105712 lb) 50460 kg (111245 lb) 51960 kg (114552 lb) MTOW 47790 kg (105359 lb) 50300 kg (110892 lb) 51800 kg (114199 lb) MLW 43000 kg (94799 lb) 44000 kg (97003 lb) BOW [2] 27900 kg (61509 lb) MZFW 40800 kg (89949 lb) 40900 kg (90169 lb) Maximum Payload [2] 12900 kg (28440 lb) 13000 kg (28660 lb) Maximum Seating 106 passengers Capacity Maximum Cargo 22.63 m3 (799.18 ft3) Volume[3] Usable 13000 kg (28660 lb) Fuel [4] 16029 (4234 gal.)
1. Applicable for standard models. For further information, refer to AFM and AOM. 2. Typical standard configuration (weights may vary according to optional equipment installed or interior layouts). 3. Standard configuration (volume may vary according to optional equipment installed). 4. Adopted fuel density of 0.811 kg/ (6.77 lb/gal.).
2.2. GENERAL AIRCRAFT DIMENSIONS
2.2.1. External Dimensions • Span over winglets - 28.72 m (94 ft 3 in.) • Height (maximum) - 10.55 m (34 ft 7 in.) • Overall length - 36.24 m (118 ft 11 in.)
2.2.2. Wing • Reference area - 92.50 m2 (996 ft2) • Reference aspect ratio - 8.1
Section 2 EFFECTIVITY: ALL Page 2-2 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
2.2.3. Fuselage • Total Length - 36.24 m (118 ft 11 in.) • Length of pressurized section - 29.08 m (95 ft 5 in.)
2.2.4. Horizontal Tail • Span - 12.08 m (39 ft 8 in.) • Area - 26.00 m2 (280 ft2)
2.2.5. Vertical Tail • Reference area - 16.20 m2 (174 ft2 54 in2)
Section 2 EFFECTIVITY: ALL Page 2-3 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
24.57 m (80 ft 10 in.) 6.82 m (45 ft 4 in.) 10.57 m (34 ft 8 in.)
4.13 m 13.83 m (13 ft 6 in.) (45 ft 4 in.)
36.24 m (118 ft 11 in.)
27.60 m (90 ft 7 in.) 4.27 m (14 ft)
12.08 m (39 ft 8 in.)
4.71 m (15 ft 5.4in.) 27.60 m (90 ft 7 in.)
20.04 m (65 ft 9 in.)
5.94 m (19 ft 6 in.)
28.72 m (94 ft 3 in.) EM170APM020011C.IDR
General Aircraft Dimensions Figure 2.1
Section 2 EFFECTIVITY: ALL Page 2-4 May 21/21 w-apm1901 w-apm1901 FETVT:ALL EFFECTIVITY: (4 ft7.1 in) 1.40 m 1.40 asne n evc or Dimensions Doors Service and Passenger (5 ft0.7 in) 1.54 m 1.54 (2 ft6 in) 0.76 m 0.76 iue2.2 Figure he 1 Sheet LNIGMANUAL PLANNING AIRPORT (5 ft10 in) 1.78 m 1.78 (2 ft9.5 in) 0.85 m 0.85 (6 ft2.4 in) 1.89 m 1.89 a 22/20 May eto 2 Section ae2-5 Page
EM170APM020026A.IDR FETVT:ALL EFFECTIVITY: (4 ft10 in) 1.47 m 1.47 asne n evc or Dimensions Doors Service and Passenger (5 ft2.2 in) 1.58 m 1.58 (2 ft6.3 in) 0.77 m 0.77 iue2.2 Figure he 2 Sheet (2 ft6 in) 0.76 m 0.76 LNIGMANUAL PLANNING AIRPORT (5 ft1.8 in) 1.57 m 1.57 (6 ft2.4 in) 1.89 m 1.89 a 22/20 May eto 2 Section ae2-6 Page
EM170APM020027A.IDR
w-apm1901 w-apm1901 FETVT:ALL EFFECTIVITY: (1 ft7.7 in) 0.50 m 0.50 LIMIT CLEARENCE CRITICAL asne n evc or Dimensions Doors Service and Passenger (17 ft 0in) ft (17 5.18 m 5.18 LIMIT CLEARENCE CRITICAL iue2.2 Figure he 3 Sheet (5 ft2.2 in) 1.58 m 1.58 LNIGMANUAL PLANNING AIRPORT (5 ft0.7 in) 1.54 m 1.54 (2 ft6.3 in) 0.77 m 0.77 (2 ft6 in) 0.76 m 0.76 (2 ft5.2 in) 0.74 m 0.74 (2 ft6.3 in) 0.77 m 0.77 (6 ft4.4 in) 1.94 m 1.94 a 22/20 May eto 2 Section ae2-7 Page
EM170APM020028A.IDR AIRPORT PLANNING MANUAL
2.3. GROUND CLEARANCES
FUSLG ANGLE (REF.) A M
N B
C E H J K L D
G
F EM170MFEP020013B.DGN
Aircraft Ground Clearances Figure 2.3 Section 2 EFFECTIVITY: ALL Page 2-8 May 22/20 w-apm1901 w-apm1901
FETVT:ALL EFFECTIVITY: Table 2.2 - Ground Clearance - STD Aircraft Model TAIL FOR- SKID FOR- FOR- AFT FUS WARD EMER- AFT AFT VERTI- ANGU- WARD WARD NA- PASSEN- CG ANGLE NOSE PASSEN- WINGLET GENCY CARGO SERVICE CAL LAR WEIGHT SERVICE CARGO CELLE GER (%MAC) (DEG) (B) GER (G) EXIT DOOR DOOR TAIL CLEAR- DOOR DOOR (F) DOOR (A) DOOR (H) (J) (K) (M) ANCE (C) (E) (L) (D) (DEG) (N) 47950 kg 2.07 m 2.58 m 2.59 m 1.57 m 0.49 m 5.09 m 3.24 m 1.99 m 3.03 m 3.03 m 10.40 m 6.0 -1.1 12.7 105712 lb 6ft9in. 8ft5in. 8ft6in. 5ft2in. 1ft7in. 16 ft 8 in. 10 ft 8 in. 6ft5in. 9ft9in. 9ft9in. 34 ft 2 in. 47950 kg 2.13 m 2.63 m 2.64 m 1.61 m 0.50 m 5.05 m 3.24 m 1.94 m 2.97 m 2.97 m 10.33 m 28.7 -0.8 12.4 105712 lb 7ft 8ft7in. 8ft8in. 5ft3in. 1ft8in. 16 ft 7 in. 10 ft 8 in. 6ft4in. 8ft8in. 8ft8in. 33 ft 9 in. 47790 kg 2.05 m 2.58 m 2.59 m 1.57 m 0.49 m 5.09 m 3.24 m 1.99 m 3.03 m 3.03 m 10.43 m 6.0 -1.1 12.7 105359 lb 6ft9in. 8ft5in. 8ft6in. 5ft2in. 1ft7in. 16 ft 8 in. 10 ft 8 in. 6ft6in. 9ft11in. 9ft11in. 34 ft 2 in. 47790 kg 2.13 m 2.63 m 2.64 m 1.61 m 0.50 m 5.06 m 3.24 m 1.94 m 2.97 m 2.97 m 10.33 m 28.7 -0.8 12.3 105359 lb 7ft 8ft7in. 8ft8in. 5ft3in. 1ft8in. 16 ft 7 in. 10 ft 8 in. 6ft4in. 9ft8in. 9ft8in. 33 ft 10 in. 43000 kg 2.06 m 2.59 m 2.60 m 1.58 m 0.50 m 5.12 m 3.26 m 2.00m 3.06 m 3.06 m 10.45 m 6.0 -1.1 12.8 94799 lb 6ft9in. 8ft6in. 8ft6in. 5ft2in. 1ft8in. 16 ft 9 in. 10 ft 8 in. 6ft7in. 9ft12in. 9ft12in. 34 ft 3 in. 43000 kg 2.14 m 2.65 m 2.66 m 1.63 m 0.51 m 5.08 m 3.26 m 1.96 m 2.99 m 2.99 m 10.35 m 29.0 -0.8 12.4 94799 lb 7ft 8ft8in. 8ft9in. 5ft4in. 1ft8in. 16 ft 8 in. 10 ft 8 in. 6ft5in. 9ft9in. 9ft9in. 33 ft 10 in.
40800 kg 2.06 m 2.59 m 2.60 m 1.59 m 0.51 m 5.13 m 3.27 m 2.02 m 3.07 m 3.07 m 10.47 m MANUAL PLANNING AIRPORT 6.0 -1.1 12.9 89949 lb 6ft9in. 8ft6in. 8ft6in. 5ft3in. 1ft8in. 16 ft 10 in. 10 ft 9 in. 6ft7in. 10 ft 10 ft 34 ft 4 in. 40800 kg 2.15 m 2.65 m 2.66 m 1.64 m 0.52 m 5.09 m 3.27 m 1.98 m 3.00 m 3.00 m 10.36 m 29.0 -0.8 12.5 89949 lb 7ft 8ft8in. 8ft9in. 5ft5in. 1ft9in. 16 ft 8 in. 10 ft 9 in. 6ft5in. 9ft10in. 9ft10in. 33 ft 11 in. a 22/20 May eto 2 Section ae2-9 Page FETVT:ALL EFFECTIVITY: Table 2.3 - Ground Clearance - LR Aircraft Model TAIL FOR- SKID FOR- FOR- AFT FUS WARD EMER- AFT AFT VERTI- ANGU- WARD WARD NA- PASSEN- CG ANGLE NOSE PASSEN- WINGLET GENCY CARGO SERVICE CAL LAR WEIGHT SERVICE CARGO CELLE GER (%MAC) (DEG) (B) GER (G) EXIT DOOR DOOR TAIL CLEAR- DOOR DOOR (F) DOOR (A) DOOR (H) (J) (K) (M) ANCE (C) (E) (L) (D) (DEG) (N) 50460 kg 2.06 m 2.58 m 2.58 m 1.57 m 0.48 m 5.08 m 3.23 m 1.97 m 3.02 m 3.02 m 10.40 m 8.8 -1.1 12.6 111245lb 6ft9in. 8ft5in. 8ft5in. 5ft2in. 1ft7in. 16 ft 8 in. 10 ft 7 in. 6ft5in. 9ft10in. 9ft10in. 34 ft 1 in. 50460kg 2.12 m 2.62 m 2.63 m 1.60m 0.49 m 5.05 m 3.24 m 1.94m 2.97 m 2.97 m 10.33 m 27.6 -0.8 12.3 111245 lb 7ft 8ft8in. 8ft7in. 5ft4in. 1ft7in. 16 ft 7 in. 10 ft 7 in. 6ft4in. 9ft8in. 9ft8in. 33 ft 9 in. 50300kg 2.06 m 2.58 m 2.58 m 1.57 m 0.48 m 5.08 m 3.23 m 1.97 m 3.02 m 3.02 m 10.40 m 8.8 -1.1 12.6 110892lb 6ft9in. 8ft5in. 8ft5in. 5ft2in. 1ft7in. 16 ft 8 in. 10 ft 7 in. 6ft5in. 9ft10in. 9ft10in. 34 ft 1in. 50300kg 2.12 m 2.62 m 2.63 m 1.60 m 0.49 m 5.05 m 3.24 m 1.94 m 2.97 m 2.97 m 10.33 m 27.6 -0.8 12.3 110892 lb 7ft 8ft8in. 8ft7in. 5ft4in. 1 ft 7in. 16 ft 7 in. 10 ft 7 in. 6ft4in. 9ft8in. 9ft8in. 33 ft 9 in. 43000 kg 2.06 m 2.59 m 2.60 m 1.58 m 0.50 m 5.12 m 3.26 m 2.00 m 3.06 m 3.06 m 10.45 m 6.0 -1.1 12.8 94799 lb 6ft9in. 8ft6in. 8ft6in. 5ft2in. 1ft8in. 16 ft 9 in. 10 ft 8 in. 6ft7in. 9ft12in. 9ft12in. 34 ft 3 in. 43000 kg 2.14 m 2.65 m 2.66 m 1.63 m 0.51 m 5.08 m 3.26 m 1.96 m 2.99 m 2.99 m 10.35 m 29.0 -0.8 12.4 94799 lb 7ft 8ft8in. 8ft9in. 5ft4in. 1ft8in. 16 ft 8 in. 10 ft 8 in. 6ft5in. 9ft9in. 9ft9in. 33 ft 10 in.
40800 kg 2.06 m 2.59 m 2.60 m 1.59 m 0.51 m 5.13 m 3.27 m 2.02 m 3.07 m 3.07 m 10.47 m MANUAL PLANNING AIRPORT 6.0 -1.1 12.9 89949 lb 6ft9in. 8ft6in. 8ft6in. 5ft3in. 1ft8in. 16 ft 10 in. 10 ft 9 in. 6ft7in. 10 ft 10 ft 34 ft 4 in. 40800 kg 2.15 m 2.65 m 2.66 m 1.64 m 0.52 m 5.09 m 3.27 m 1.98 m 3.00 m 3.00 m 10.36 m 29.0 -0.8 12.5 89949 lb 7ft2in. 8ft8in. 8ft9in. 5ft5in. 1ft9in. 16 ft 8 in. 10 ft 9 in. 6ft5in. 9ft10in. 9ft10in. 33 ft 11 in. a 22/20 May 2-10 Page eto 2 Section
w-apm1901 w-apm1901
FETVT:ALL EFFECTIVITY: Table 2.4 - Ground Clearance - AR Aircraft Model TAIL FOR- SKID FOR- FOR- AFT FUS WARD EMER- AFT AFT VERTI- ANGU- WARD WARD NA- PASSEN- CG ANGLE NOSE PASSEN- WINGLET GENCY CARGO SERVICE CAL LAR WEIGHT SERVICE CARGO CELLE GER (%MAC) (DEG) (B) GER (G) EXIT DOOR DOOR TAIL CLEAR- DOOR DOOR (F) DOOR (A) DOOR (H) (J) (K) (M) ANCE (C) (E) (L) (D) (DEG) (N) 51960 kg 2.06 m 2.58 m 2.59 m 1.57 m 0.48 m 5.08 m 3.23 m 1.97 m 3.01 m 3.01 m 10.40 m 10.7 -1.1 12.6 114552lb 6ft9in. 8ft5in. 8ft6in. 5ft2in. 1ft7in. 16 ft 8 in. 10 ft 7 in. 6ft5in. 9ft10in. 9ft10in. 34 ft 1 in. 51960 kg 2.12 m 2.62 m 2.63 m 1.60 m 0.49 m 5.05 m 3.23 m 1.93 m 2.96 m 2.96 m 10.32 m 27.0 -0.8 12.3 114552lb 7ft 8ft8in. 8ft7in. 5ft4in. 1ft7in. 16 ft 7 in. 10 ft 7 in. 6ft4in. 9ft8in. 9ft8in. 33 ft 9 in. 51800kg 2.06 m 2.58 m 2.59 m 1.57 m 0.48 m 5.08 m 3.23 m 1.97 m 3.01 m 3.01 m 10.40 m 10.7 -1.1 12.6 11499lb 6ft9in. 8ft5in. 8ft6in. 5ft2in. 1ft7in. 16 ft 8 in. 10 ft 7 in. 6ft5in. 9ft10in. 9ft10in. 34 ft 1in. 51800kg 2.12m 2.62 m 2.63 m 1.60 m 0.49 m 5.05 m 3.23 m 1.93 m 2.96 m 2.96 m 10.33 m 27.0 -0.8 12.3 11499lb 7ft 8ft8in. 8ft7in. 5ft4in. 1ft7in. 16 ft 7 in. 10 ft 7 in. 6ft4in. 9ft8in. 9ft8in. 33 ft 9 in. 44000 kg 2.06 m 2.59 m 2.60 m 1.58 m 0.50 m 5.11 m 3.26 m 2.00 m 3.03 m 3.03 m 10.45 m 6.0 -1.1 12.8 97003 lb 6ft9in. 8ft6in. 8ft6in. 5ft2in. 1ft8in. 16 ft 9 in. 10 ft 8 in. 6ft7in. 9ft12in. 9ft12in. 34 ft 3 in. 44000 kg 2.14 m 2.64 m 2.65 m 1.63 m 0.51 m 5.07 m 3.26 m 1.96 m 2.99 m 2.99 m 10.34 m 29.0 -0.8 12.4 97003 lb 7ft 8ft8in. 8ft8in. 5ft4in. 1ft8in. 16 ft 8 in. 10 ft 8 in. 6ft5in. 9ft9in. 9ft9in. 33 ft 10 in.
40900 kg 2.06 m 2.59 m 2.60 m 1.59 m 0.51 m 5.13 m 3.27 m 2.02 m 3.07 m 3.07 m 10.47 m MANUAL PLANNING AIRPORT 6.0 -1.1 12.9 90169 lb 6ft9in. 8ft6in. 8ft6in. 5ft3in. 1ft8in. 16 ft 10 in. 10 ft 9 in. 6ft7in. 10 ft 10 ft 34 ft 4 in. 40900 kg 2.15 m 2.65 m 2.66 m 1.63 m 0.52 m 5.09 m 3.27 m 1.97 m 3.00 m 3.00 m 10.36 m 29.0 -0.8 12.5 90169 lb 7ft2in. 8ft8in. 8ft9in. 5ft4in. 1ft9in. 16 ft 8 in. 10 ft 9 in. 6ft5in. 9ft10in. 9ft10in. 33 ft 11 in. a 22/20 May ae2-11 Page eto 2 Section AIRPORT PLANNING MANUAL
2.4. INTERIOR ARRANGEMENTS
The interior arrangement provides accommodation for two pilots, one observer, three flight attendants, and 98 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 98 passengers in 24 double seats on both sides, in 32 in pitch standard configuration. As an option, the passenger cabin is also provided with some double first-class seats on the RH side and some single first-class seats on the LH side. The main dimensions of passenger cabin are presented below: • Height - 2.00 m (6 ft 7 in.) • Width - 2.74 m (9 ft) • Aisle wide - 0.49 m (1 ft 7 in.) • Pitch - 0.82 m (32 in.)
Section 2 EFFECTIVITY: ALL Page 2-12 May 22/20 w-apm1901 AIRPORT PLANNING MANUAL
3 4 9 5
0.90 m 0.88 m 0.78 m (2 ft 11.4 in.) 8 8 (2 ft 10.6 in.) (2 ft 6.7 in.) 1.82 m 4.82 m 4.17 m 1.85 m (5 ft 11.7 in.) (15 ft 9.8 in.) (13 ft 8.2 in.) (6 ft 0.8 in.) 7.82 7.16 (25 ft 7.9 in.) (23 ft 5.9 in.)
25.91 m (85 ft)
0.81 m 3 4 2 10 (2 ft 8 in.) 5
6 1 2 1.48 m 17 (4 ft 10 in.)
1 − FLIGHT ATTENDANT SEAT 6 − FWD LAVATORY 2 − WARDROBE 7 − AFT LAVATORY
3 − FWD RH G1 GALLEY 8 − CARGO COMPARTMENT 4 − FWD RH G2 GALLEY 9 − OVERHEAD BIN 5 − AFT RH GALLEY 10 − PASSENGER SEAT
CARGO/BAGGAGE VOLUME
3 3 CARGO COMPARTMENT 22.63 m (799.18 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) EM170APM020013C.DGN
Typical Interior Arrangements Figure 2.4
Section 2 EFFECTIVITY: ALL Page 2-13 May 22/20 w-apm1901 AIRPORT PLANNING MANUAL
2.4.2. Cargo Compartments
Two cargo compartments are available, located underfloor, one forward of the wing, and another aft of the wing. The cargo compartments comply with the FAR-25/JAR-25/RBHA-25 “class C” compartment classifica- tion. The table below contain the capacity for the cargo compartment:
Table 2.5 - Capacity for the Cargo Compartment CARGO COMPARTMENT LOADING VOLUME FWD [1] 1850 kg (4078 lb) 10.84 m3 (382.81 ft3) Aft 1440 kg (3175 lb) 7.60 m3 (268.39 ft3) Total 3290 kg (7253 lb) 18.44 m3 (651.20 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 - to avoid damage due to cargo shifting (two for each cargo compartments). Also, there are provisions for two extra vertical nets in the forward cargo compartment and one in the aft cargo compartment; • 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, which avoids harm to the flight crew. The cockpit is separated from the passenger cabin by a bulkhead with a lockable door. The cockpit door is provided with lockable means operable only from the cockpit side, spy hole and escape mechanism on the cockpit side.
Section 2 EFFECTIVITY: ALL Page 2-14 Aug 27/21 w-apm1901 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 2.5 Section 2 EFFECTIVITY: ALL Page 2-15 May 22/20 w-apm1901 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 2.6
Section 2 EFFECTIVITY: ALL Page 2-16 May 22/20 w-apm1901 AIRPORT PLANNING MANUAL
2.6. LOWER COMPARTMENT CONTAINERS
Not Applicable
Section 2 EFFECTIVITY: ALL Page 2-17 May 22/20 w-apm1901 AIRPORT PLANNING MANUAL
2.7. DOOR CLEARANCES
1.71 m (5 ft 7.3 in.) 1.36 m 1.82 m 0.98 m (4 ft 5.5 in.) (5 ft 11.6 in.) (3 ft 2.6 in.) 1.37 m (4 ft 5.9 in.)
SEE FIGURE 2.2 FOR HEIGHT ABOVE 0.78 m GROUND 0.87 m (2 ft 6.7 in.) 0.90 m (2 ft 10 in.) (2 ft 11.4 in.)
1.10 m 0.99 m (3 ft 7.3 in.) (3 ft 3 in.)
0.61 m 0.53 m 0.63 m (2 ft) (1 ft 8.9 in.) (2 ft 0.8 in.)
0.75 m 0.53 m 0.63 m (2 ft 6.7 in.) (1 ft 8.9 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. EM170APM020014C.DGN
Door Dimensions Figure 2.7 Section 2 EFFECTIVITY: ALL Page 2-18 May 22/20 w-apm1901 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 pro- nounced 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 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
3.2. PAYLOAD X RANGE
The Payload x Range charts are based on the following conditions: • CF34 - 10E 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 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
PAYLOAD VS RANGE CF34 −10E5A, −10E5A1, −10E6A, −10E6A1 & −10E7 ENGINES FLIGHT LEVEL 370 ISA RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 47790 kg (105359 lb)
14000 30000
13000 28000
12000 26000
11000 108 PAX @ 100 kg 24000
22000 10000
20000 9000
18000 8000
16000 7000
14000 PAYLOAD − kg PAYLOAD − lb 6000
12000 5000 10000
4000 8000
3000 6000 LONG RANGE
2000 MAX CRUISE 4000 0.78 MACH
2000 1000
0 0 0 500 1000 1500 2000 2500 3000 NOTES: RANGE − nm MAX TAKEOFF WEIGHT 47790 kg (105359 lb) MAX ZERO FUEL WEIGHT 40800 kg (89948 lb) BASIC OPERATING WEIGHT 27900 kg (61509 lb)
MAX USABLE FUEL 13100 kg (28880 lb) EM170APM030030E.DGN
Payload x Range - ISA Conditions Figure 3.1
Section 3 EFFECTIVITY: EMBRAER 190 STD ACFT MODEL Page 3-3 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
PAYLOAD VS RANGE CF34 −10E5A, −10E5A1, −10E6A, −10E6A1 & −10E7 ENGINES FLIGHT LEVEL 370 ISA + 10°C RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 47790 kg (105359 lb)
14000 30000
13000 28000
12000 26000
11000 108 PAX @ 100 kg 24000
22000 10000
20000 9000
18000 8000
16000 7000
14000 PAYLOAD − lb PAYLOAD − kg 6000
12000 5000 10000
4000 8000
3000 LONG RANGE 6000 MAX CRUISE
2000 0.78 MACH 4000
2000 1000
0 0 0 500 1000 1500 2000 2500 3000 RANGE − nm NOTES: MAX TAKEOFF WEIGHT 47790 kg (105359 lb) MAX ZERO FUEL WEIGHT 40800 kg (89948 lb) BASIC OPERATING WEIGHT 27900 kg (61509 lb)
MAX USABLE FUEL 13100 kg (28880 lb) EM170APM030031E.DGN
Payload x Range - ISA + 10 °C Conditions Figure 3.2
Section 3 EFFECTIVITY: EMBRAER 190 STD ACFT MODEL Page 3-4 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
PAYLOAD VS RANGE CF34 −10E5A, −10E5A1, −10E6A, −10E6A1 & −10E7 ENGINES FLIGHT LEVEL 370 ISA RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 50300 kg (110893 lb)
14000 30000
13000 28000
12000 26000
11000 108 PAX @ 100 kg 24000
22000 10000
20000 9000
18000 8000
16000 7000
14000 PAYLOAD − lb PAYLOAD − kg 6000
12000 5000 10000
LONG RANGE 4000 8000 MAX CRUISE
3000 0.78 MACH 6000
2000 4000
2000 1000
0 0 0 500 1000 1500 2000 2500 3000 RANGE − nm NOTES: MAX TAKEOFF WEIGHT 50300 kg (110893 lb) MAX ZERO FUEL WEIGHT 40800 kg (89949 lb) BASIC OPERATING WEIGHT 27900 kg (61509 lb)
MAX USABLE FUEL 13100 kg (28880 lb) EM170APM030032D.DGN
Payload x Range - ISA Conditions Figure 3.3
Section 3 EFFECTIVITY: EMBRAER 190 LR ACFT MODEL Page 3-5 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
PAYLOAD VS RANGE CF34 −10E5A, −10E5A1, −10E6A, −10E6A1 & −10E7 ENGINES FLIGHT LEVEL 370 ISA + 10°C RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 50300 kg (110893 lb)
14000 30000
13000 28000
12000 26000
11000 108 PAX @ 100 kg 24000
22000 10000
20000 9000
18000 8000
16000 7000
14000 PAYLOAD − lb PAYLOAD − kg 6000
12000 5000 10000
4000 LONG RANGE 8000
MAX CRUISE
3000 6000 0.78 MACH
2000 4000
2000 1000
0 0 0 500 1000 1500 2000 2500 3000 RANGE − nm NOTES: MAX TAKEOFF WEIGHT 50300 kg (110893 lb) MAX ZERO FUEL WEIGHT 40800 kg (89949 lb) BASIC OPERATING WEIGHT 27900 kg (61509 lb)
MAX USABLE FUEL 13100 kg (28880 lb) EM170APM030033D.DGN
Payload x Range - ISA + 10 °C Conditions Figure 3.4
Section 3 EFFECTIVITY: EMBRAER 190 LR ACFT MODEL Page 3-6 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
PAYLOAD VS RANGE CF34 −10E5A, −10E5A1, −10E6A, −10E6A1 & −10E7 ENGINES FLIGHT LEVEL 370 ISA RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 51800 kg (114199 lb)
14000 30000
13000 28000
12000 26000
11000 108 PAX @ 100 kg 24000
22000 10000
20000 9000
18000 8000
16000 7000
14000 PAYLOAD − kg PAYLOAD − lb 6000
12000 5000 10000
4000 LONG RANGE 8000
3000 MAX CRUISE 6000
2000 4000 0.78 MACH
2000 1000
0 0 0 500 1000 1500 2000 2500 3000 RANGE − nm NOTES: MAX TAKEOFF WEIGHT 51800 kg (114199 lb) MAX ZERO FUEL WEIGHT 40900 kg (90169 lb) BASIC OPERATING WEIGHT 27900 kg (61509 lb)
MAX USABLE FUEL 13100 kg (28880 lb) EM170APM030060C.DGN
Payload x Range - ISA Conditions Figure 3.5
Section 3 EFFECTIVITY: EMBRAER 190 AR ACFT MODEL Page 3-7 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
PAYLOAD VS RANGE CF34 −10E5A, −10E5A1, −10E6A, −10E6A1 & −10E7 ENGINES FLIGHT LEVEL 370 ISA+10 RESERVE : 100 nm ALTERNATE + 45 min FLIGHT MTOW = 51800 kg (114199 lb)
14000 30000
13000 28000
12000 26000
11000 108 PAX @ 100 kg 24000
22000 10000
20000 9000
18000 8000
16000 7000
14000 PAYLOAD − kg PAYLOAD − lb 6000
12000 5000 10000
4000 LONG RANGE 8000
MAX CRUISE 3000 6000
0.78 MACH
2000 4000
2000 1000
0 0 0 500 1000 1500 2000 2500 3000 NOTES: RANGE − nm MAX TAKEOFF WEIGHT 51800 kg (114199 lb) MAX ZERO FUEL WEIGHT 40900 kg (90169 lb) BASIC OPERATING WEIGHT 27900 kg (61509 lb)
MAX USABLE FUEL 13100 kg (28880 lb) EM170APM030061C.DGN
Payload x Range - ISA + 10 °C Conditions Figure 3.6
Section 3 EFFECTIVITY: EMBRAER 190 AR ACFT MODEL Page 3-8 Oct 07/13 w-apm1901 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 lengths 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 - 10E 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 + 10 °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 3-9 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF 34−10E5 & −10E6 ENGINE@T/O−1 MODE ATTCS OFF / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA
4400 AIRPORT PRESSURE 14000 ALTITUDE m (ft) 4200
13000 4000
3800 12000 3600
3400 11000
3200
10000 3000 4268 3658 (14000) (12000) 2800 609 9000 3048 FLAP 1 2438 (2000) (10000) 1829 (8000) 2600 (6000) 1219 (4000) SEA LEVEL 8000 2400 FLAP 2
2200 7000 −570 (−1870)
FIELD LENGTH − ft 2000 FIELD LENGTH − m FLAP 3
6000 1800
1600 5000 FLAP 4 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000
WEIGHT − lb EM170APM030036E.DGN
Takeoff Field Lengths - ISA Conditions Figure 3.7
Section 3 EFFECTIVITY: ALL Page 3-10 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF34−10E5 & −10E6 Engines @ T/O−1 MODE ATTCS OFF / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15°C
4400 14000 4200 AIRPORT PRESSURE ALTITUDE m (ft)
13000 4000
3800 12000 3600
3400 11000
3200 4268 3658 10000 (14000) 3000 (12000) 3048 (10000) FLAP 1 2438 2800 1829 SEA LEVEL 9000 (8000) 1219 (6000) 609 (4000) 2600 (2000) FLAP 2 8000 2400 −570 2200 (−1870) 7000 FLAP 3
FIELD LENGTH − ft 2000 FIELD LENGTH − m
6000 1800 FLAP 4 1600 5000 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000
WEIGHT − lb EM170APM030037E.DGN
Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.8
Section 3 EFFECTIVITY: ALL Page 3-11 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF34−10E5 & −10E6 Engines @ T/O−1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA
4400 14000 4200 AIRPORT PRESSURE ALTITUDE m (ft) 13000 4000
3800 12000 3600
3400 11000
3200 1829 (6000) 1219 10000 (4000) 3000 3658 2438 4268 (12000) 3048 (8000) (14000) (10000) FLAP 1 2800 609 9000 FLAP 2 (2000) 2600
8000 2400 SEA LEVEL
2200 FLAP 3 7000
FIELD LENGTH − ft 2000 −570 FIELD LENGTH − m (−1870) 6000 1800
1600 FLAP 4 5000 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000
WEIGHT − lb EM170APM030038E.DGN
Takeoff Field Lengths - ISA Conditions Figure 3.9
Section 3 EFFECTIVITY: ALL Page 3-12 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF34−10E5 & −10E6 Engines @ T/O−1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15°C
4400 14000 4200 AIRPORT PRESSURE ALTITUDE m (ft) 13000 4000
3800 12000 3600
3400 1829 1219 11000 2438 (6000) (4000) (8000) 3200 3658 4268 (12000) 3048 10000 (10000) 3000 (14000) FLAP 1
609 2800 (2000) 9000 FLAP 2 2600 SEA LEVEL 8000 2400 FLAP 3 −570 2200 (−1870) 7000
FIELD LENGTH − ft 2000 FIELD LENGTH − m
6000 1800 FLAP 4 1600 5000 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000
WEIGHT − lb EM170APM030039E.DGN
Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.10
Section 3 EFFECTIVITY: ALL Page 3-13 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF34−10E5A1 & 10E6A1 ENGINES@T/O−1 MODE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA
4400 14000 AIRPORT PRESSURE 4200 ALTITUDE m (ft)
13000 4000
3800 12000 3600
3400 11000
3200
10000 1829 3000 (6000) 1219 3658 2438 4268 3048 (4000) 2800 (12000) (8000) 9000 (14000) (10000) FLAP 1 2600 609 FLAP 2 (2000) 8000 2400
2200 SEA LEVEL 7000 FLAP 3 −570
FIELD LENGTH − ft 2000 FIELD LENGTH − m (−1870) 6000 1800 FLAP 4 1600 5000 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000 WEIGHT − lb EM170APM030034D.DGN
Takeoff Field Lengths - ISA Conditions Figure 3.11
Section 3 EFFECTIVITY: ALL Page 3-14 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF34−10E5A1 & 10E6A1 ENGINES@T/O−1 MODE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15°C
4400 AIRPORT PRESSURE 14000 4200 ALTITUDE m (ft)
13000 4000
3800 12000 3600
3400 11000
1829 1219 3200 2438 (6000) (4000) 10000 3658 (8000) 3000 4268 (12000) 3048 (14000) (10000) FLAP 1 2800 9000 609 FLAP 2 (2000) 2600
8000 2400 FLAP 3 SEA LEVEL 2200 −570 7000 (−1870)
FIELD LENGTH − ft 2000 FIELD LENGTH − m
6000 1800 FLAP 4 1600 5000 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000
WEIGHT − lb EM170APM030035D.DGN
Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.12
Section 3 EFFECTIVITY: ALL Page 3-15 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF 34−10E7 ENGINE@T/O−1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA
4400 14000 4200
13000 4000 AIRPORT PRESSURE 3800 ALTITUDE m (ft) 12000 3600
3400 11000
3200 3048 10000 (10000) 2438 3000 (8000) 1829 FLAP 1 (6000) 2800 9000
2600 FLAP 2 1219 (4000) 8000 2400
2200 FLAP 3 7000 609 (2000) FIELD LENGTH − ft 2000 FIELD LENGTH − m
6000 1800 SEA LEVEL
1600 5000 −570 1400 FLAP 4 (−1870)
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000
WEIGHT − lb EM170APM030040D.DGN
Takeoff Field Lengths - ISA Conditions Figure 3.13
Section 3 EFFECTIVITY: ALL Page 3-16 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF 34−10E7 ENGINE@T/O−1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15°C
4400 14000 4200
13000 4000 AIRPORT PRESSURE 3800 ALTITUDE m (ft) 12000 3600 1829 (6000) 3400 11000 3048 3200 (10000) 2438 10000 (8000) 3000 1219 FLAP 1 (4000) 2800 9000 FLAP 2 2600
8000 2400 FLAP 3 2200 7000 609 (2000)
FIELD LENGTH − ft 2000 FIELD LENGTH − m
6000 SEA LEVEL 1800
1600 FLAP 4 5000 −570 (−1870) 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000 WEIGHT − lb EM170APM030041D.DGN
Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.14
Section 3 EFFECTIVITY: ALL Page 3-17 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF 34−10E7 ENGINE@T/O−1 MODE ATTCS OFF / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA
4400 AIRPORT PRESSURE 14000 4200 ALTITUDE m (ft)
13000 4000
3800 12000 3600
3400 11000
3200
10000 1829 1219 3000 (6000) (4000) 3048 2438 2800 (10000) (8000) 9000 FLAP 1 609 2600 (2000) FLAP 2 8000 2400 SEA LEVEL 2200 7000 FLAP 3
FIELD LENGTH − ft 2000 FIELD LENGTH − m −570 (−1870) 6000 1800
1600 5000 FLAP 4 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000
WEIGHT − lb EM170APM030105A.DGN
Takeoff Field Lengths - ISA Conditions Figure 3.15
Section 3 EFFECTIVITY: ALL Page 3-18 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF FIELD LENGTH CF 34−10E7 ENGINE@T/O−1 MODE ATTCS OFF / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA+15
4400 AIRPORT PRESSURE 14000 4200 ALTITUDE m (ft)
13000 4000
3800 12000 3600
3400 11000
3200 1219 2438 (4000) 10000 (8000) 3000 FLAP 1 1829 3048 (6000) 2800 609 9000 (10000) (2000) 2600 FLAP 2
8000 2400 FLAP 3 SEA LEVEL 2200 7000 −570 (−1870)
FIELD LENGTH − ft 2000 FIELD LENGTH − m
6000 1800
1600 5000 FLAP 4 1400
4000 1200
1000 3000 800
2000 600
400 1000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 47000 49000 51000 53000 WEIGHT − kg
60000 70000 80000 90000 100000 110000
WEIGHT − lb EM170APM030106A.DGN
Takeoff Field Lengths - ISA + 15 °C Conditions Figure 3.16
Section 3 EFFECTIVITY: ALL Page 3-19 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
3.4. LANDING FIELDS LENGTHS
The landing field lengths charts provide data about the maximum landing weights for compliance with the operating regulations relating to landing field lengths. Data is presented according to the following associated conditions: • Landing gear: down; • Flaps setting position: 5 or full; • Pavement conditions: dry, hard paved and level runway surface with no obstacles; • Zero wind and atmosphere according to ISA conditions; • Pack OFF: No engine bleed extraction for air conditioning packs was considered in the takeoff and landing charts.
Section 3 EFFECTIVITY: ALL Page 3-20 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
LANDING FIELD LENGTH CF 34−10E5−10E5A1−10E6 & −10E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA
6000
1800
1700 AIRPORT PRESSURE ALTITUDE m (ft) 10000
9000
1600 8000
7000 5000 6000 1500 5000 4000 3000 1400 2000 1000 0 −1000
FIELD LENGTH − ft 1300 LAND FIELD LENGTH − m 4000 1200
1100
1000
3000 900 25000 2700029000 31000 33000 35000 37000 39000 41000 43000 45000 WEIGHT − kg
60000 70000 80000 90000 100000 EM170APM030046C.DGN
Landing Field Lengths - Flaps 5 Figure 3.17
Section 3 EFFECTIVITY: EASA-CERTIFIED ACFT Page 3-21 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
LANDING FIELD LENGTH CF34−10E5−10E5A1−10E6 & −10E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA
6000
1800
1700
AIRPORT PRESSURE ALTITUDE m (ft)
1600 10000
5000 9000
1500 8000
7000 6000 1400 5000 4000 3000 1300 2000 FIELD LENGTH − ft 1000
LAND FIELD LENGTH − m 0 4000 −1000 1200 −1870
1100
1000
3000 900 2500027000 29000 31000 33000 35000 37000 39000 41000 43000 45000 WEIGHT − kg
60000 70000 80000 90000 100000 EM170APM030047C.DGN
Landing Field Lengths - Flaps Full Figure 3.18
Section 3 EFFECTIVITY: EASA-CERTIFIED ACFT Page 3-22 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
LANDING FIELD LENGTH CF 34−10E7 ENGINE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA 6000
1800
AIRPORT PRESSURE 1700 ALTITUDE m (ft) 10000
9000
8000 1600 7000 6000 5000 1500 5000 4000
3000 1400 2000 1000 0 −1000 1300 FIELD LENGTH − ft −1870 LAND FIELD LENGTH − m 4000 1200
1100
1000
3000 900 2500027000 29000 31000 33000 35000 37000 39000 41000 43000 45000 WEIGHT − kg
60000 70000 80000 90000 100000 EM170APM030062B.DGN
Landing Field Lengths - Flaps 5 Figure 3.19
Section 3 EFFECTIVITY: EASA-CERTIFIED ACFT Page 3-23 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
LANDING FIELD LENGTH CF 34−10E7 ENGINE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA
6000
1800
AIRPORT PRESSURE 1700 ALTITUDE m (ft)
1600 10000
5000 9000 1500 8000
7000 6000 1400 5000 4000 3000 1300 2000 FIELD LENGTH − ft 1000
LAND FIELD LENGTH − m 0 4000 −1000 1200 −1870
1100
1000
3000 900 2500027000 29000 31000 33000 35000 37000 39000 41000 43000 45000 WEIGHT − kg
60000 70000 80000 90000 100000 EM170APM030063B.DGN
Landing Field Lengths - Flaps Full Figure 3.20
Section 3 EFFECTIVITY: EASA-CERTIFIED ACFT Page 3-24 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
LANDING FIELD LENGTH CF 34−10E5−10E5A1−10E6 & −10E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA
2000
1900 AIRPORT PRESSURE 14000 ALTITUDE m (ft) 13000 6000 12000 1800 11000 10000 1700 9000 8000 7000 1600 6000 5000 5000 4000 1500 3000 2000 1000 1400 0 FIELD LENGTH − ft −1000 −1870 LAND FIELD LENGTH − m 1300
4000 1200
1100
1000
3000 900 25000 27000 29000 31000 33000 35000 37000 39000 41000 43000 45000 WEIGHT − kg
60000 70000 80000 90000 100000 EM170APM030017A.DGN
Landing Field Lengths - Flaps 5 Figure 3.21
Section 3 EFFECTIVITY: FAA-CERTIFIED ACFT Page 3-25 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
LANDING FIELD LENGTH CF 34−10E5−10E5A1−10E6 & −10E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA
2000
1900
6000 AIRPORT PRESSURE 1800 ALTITUDE m (ft)
1700 14000 13000
12000 1600 11000
5000 10000 1500 9000 8000 7000 1400 6000 FIELD LENGTH − ft 5000 4000 LAND FIELD LENGTH − m 3000 1300 2000 1000 4000 0 1200 −1000 −1870
1100
1000
3000 900 25000 27000 29000 31000 33000 35000 37000 39000 41000 43000 45000 WEIGHT − kg
60000 70000 80000 90000 100000 EM170APM030018A.DGN
Landing Field Lengths - Flaps Full Figure 3.22
Section 3 EFFECTIVITY: FAA-CERTIFIED ACFT Page 3-26 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
LANDING FIELD LENGTH CF 34−10E7 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA
2000
1900 AIRPORT PRESSURE 6000 ALTITUDE m (ft) 1800
10000 1700 9000 8000 7000 1600 6000 5000 5000 4000 1500 3000 2000 1000 1400 0 FIELD LENGTH − ft −1000
LAND FIELD LENGTH − m −1870 1300
4000 1200
1100
1000
3000 900 25000 27000 29000 31000 33000 35000 37000 39000 41000 43000 45000 WEIGHT − kg
60000 70000 80000 90000 100000 EM170APM030019A.DGN
Landing Field Lengths - Flaps 5 Figure 3.23
Section 3 EFFECTIVITY: FAA-CERTIFIED ACFT Page 3-27 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
LANDING FIELD LENGTH CF 34−10E7 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA
2000
1900
AIRPORT PRESSURE 6000 ALTITUDE m (ft) 1800
1700
1600
10000 5000 9000 1500 8000 7000
1400 6000 FIELD LENGTH − ft 5000 4000
LAND FIELD LENGTH − m 3000 1300 2000 1000 0 4000 −1000 1200 −1870
1100
1000
3000 900 25000 27000 29000 31000 33000 35000 37000 39000 41000 43000 45000 WEIGHT − kg
60000 70000 80000 90000 100000 EM170APM030020A.DGN
Landing Field Lengths - Flaps Full Figure 3.24
Section 3 EFFECTIVITY: FAA-CERTIFIED ACFT Page 3-28 Oct 07/14 w-apm1901 AIRPORT PLANNING MANUAL
4. GROUND MANEUVERING
4.1. GENERAL INFORMATION
This section provides the aircraft turning capability and maneuvering characteristics. To facilitate the presentation, these 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 guidelines 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 constants 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 using airline prior to the layout planning. This section is presented as follows: • The turning radii for nose landing gear steering angles. • The pilot’s visibility from the cockpit and the limits of ambinocular vision through 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 bays dimensions.
4.2. TURNING RADII
This subsection presents the following information: • The turning radii for various nose landing gear steering angles. The minimum turning radius is determined, considering that the maximum nose landing gear steering angle is 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 07/13 w-apm1901 AIRPORT PLANNING MANUAL
R5
R6
R6.44 m 21ft 2 in R3
76° 70° 65° 60° R4 55° 50° 45° 40° 35° R14.07m 46ft 2 in
R2 R1
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.
STEERING NOSE NOSE GEAR OUTBOARD GEAR INBOARD GEAR RIGHT WINGLET RIGHT TAILTIP STEEL R1 R2 R3 R4 R5 R6 35° 26.53 m 87 ft 24.16 m 79 ft 3 in 23.28 m 76 ft 5 in 16.08 m 52 ft 9 in 34.35 m 112 ft 8 in 31.50 m 103 ft 4 in 40° 24.21 m 79 ft 5 in 21.58 m 70 ft 10 in 20.03 m 65 ft 9 in 12.82 m 42 ft 1 in 31.13 m 102 ft 2 in 28.91 m 94 ft 10 in 45° 22.50 m 73 ft 10 in 19.64 m 64 ft 5 in 17.38 m 57 ft 10.18 m 35 ft 5 in 28.52 m 93 ft 7 in 26.90 m 88 ft 3 in 50° 21.22 m 69 ft 7 in 18.14 m 59 ft 6 in 15.17 m 49 ft 9 in 7.96 m 26 ft 1 in 26.33 m 86 ft 5 in 25.32 m 83 ft 1 in 55° 20.24 m 66 ft 5 in 16.98 m 55 ft 9 in 13.25 m 43 ft 6 in 6.05 m 19 ft 10 in 24.45 m 80 ft 3 in 24.02 m 78 ft 10 in 60° 19.49 m 63 ft 11 in 16.07 m 52 ft 9 in 11.56 m 37 ft 11 in 4.35 m 14 ft 3 in 22.79 m 74 ft 9 in 22.95 m 75 ft 4 in 65° 18.91 m 63 ft 15.36 m 50 ft 5 in 10.03 m 32 ft 11 in 2.82 m 9 ft 3 in 21.30 m 69 ft 10 in 22.05 m 72 ft 4 in 70° 18.48 m 60 ft 8 in 14.82 m 48 ft 7 in 8.62 m 28 ft 3 in 1.41 m 4 ft 8 in 19.93 m 65 ft 5 in 21.29 m 69 ft 10 in
76° 18.12 m 59 ft 5 in 14.36 m 47 ft 1 in 7.04 m 23 ft 1 in 0.17 m 7 in 18.39 m 60 ft 4 in 20.51 m 67 ft 3 in EM170APM040008B.DGN
Turning Radii - No Slip Angle Figure 4.1
Section 4 EFFECTIVITY: ALL Page 4-2 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
4.3. MINIMUM TURNING RADII
R5
R6
R6.44 m 21 ft 1 in
76°
R1 R3 1 R14. 07 m 46 ft 2 in 21.40 m 70ft 3 in (RUNWAY MINIMUM WIDTH)
R14.36 m 47 ft 1 in
NOTE: ACTUAL OPERATING DATA MAY BE GREATER THAN VALUES SHOWN SINCE TIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS.
STEERING NOSE NOSE GEAR OUTBOARD GEAR INBOARD GEAR RIGHT WINGLET RIGHT TAILTIP STEEL R1 R2 R3 R4 R5 R6 76° 18.12 m 59 ft 5 in14.36 m 47 ft 1 in 7.04 m 23 ft 1 in 0.17 m 7 in 18.39 m 60 ft 4 in 20.51 m 67 ft 3 in
1 THEORETICAL CENTER OF TURN FOR MINIMUN RADIUS. SHOWS CONTINUOUS TURNING WITH ENGINE THRUST AS REQUIRED.
NO DIFFERENTIAL BRAKING. EM170APM040009B.DGN
Minimum Turning Radius Figure 4.2 Section 4 EFFECTIVITY: ALL Page 4-3 Oct 07/13 w-apm1901 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° EM170APM040010.DGN
Visibility from Cockpit in Static Position Figure 4.3 Section 4 EFFECTIVITY: ALL Page 4-4 Oct 07/13 w-apm1901 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 5_ E 65 m (213 ft 3 in) 14 m (45 ft 11 in)
In accordance with the table, the reference code is 3C for EMBRAER 190STD, EMBRAER 190LR and EMBRAER 190AR.
NOTE: • This classification may change depending on aircraft engine model and takeoff weight. • For further information, refer to AOM.
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 be not less than 30 m (98 ft 5 in); • The width of a taxiway should be not 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 centre 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
Section 4 EFFECTIVITY: ALL Page 4-5 Sep 27/19 w-apm1901 AIRPORT PLANNING MANUAL
not be less than 15 m (49 ft 2 in).
For reference code 4C the limits are: • The width of a runway should be not less than 30 m (147 ft 7.6 in); • The width of a taxiway should be not 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 centre 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 2 in).
Section 4 EFFECTIVITY: ALL Page 4-6 May 25/18 w-apm1901 w-apm1901 FETVT:EBAR10SDACFT STD 190 MODEL EMBRAER 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 a 25/18 May eto 4 Section ae4-7 Page
EM170APM040002.DGN AIRPORT PLANNING MANUAL
45 m (147 ft 7.6 in.)
NOTE: COORDINATE WITH AIRLINE OPERATOR FOR THE SPECIFIC PLANNED OPERATING PROCEDURE.
NOSE LANDING GEAR STEERING ANGLE IS 45° APPROXIMATELY 15.
15 m 100 ft RADIUS (49 ft 2 in.) (30 m)
PATH OF MAIN LANDING GEAR TIRE EDGE EM170APM040011A.DGN
More than 90° Turn - Runway to Taxiway Figure 4.5
Section 4 EFFECTIVITY: EMBRAER ACFT 190 LR OR AR MODEL Page 4-8 May 25/18 w-apm1901 w-apm1901 FETVT:EBAR10SDACFT STD 190 MODEL EMBRAER EFFECTIVITY: (98 ft5in.) 30 m 90° 0 un-Rna oTaxiway to Runway - Turn 90° iue4.6 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.) a 25/18 May eto 4 Section 15 m ae4-9 Page
EM170APM040003.DGN AIRPORT PLANNING MANUAL
NOTE: COORDINATE WITH AIRLINE OPERATOR 45 m FOR THE SPECIFIC PLANNED OPERATING (147 ft 7.6 in.) PROCEDURE.
NOSE LANDING GEAR STEERING ANGLE IS APPROXIMATELY 30.
100 ft RADIUS (30 m)
90°
15 m (49 ft 2 in.)
100 ft RADIUS (30 m)
PATH OF MAIN LANDING GEAR TIRE EDGE. EM170APM040012A.DGN
90° Turn - Runway to Taxiway Figure 4.7
Section 4 EFFECTIVITY: EMBRAER ACFT 190 LR OR AR MODEL Page 4-10 May 25/18 w-apm1901 AIRPORT PLANNING MANUAL
15 m NOTE: (49 ft 2 in.) COORDINATE WITH AIRLINE OPERATOR FOR THE SPECIFIC PLANNED OPERATING PROCEDURE.
NOSE LANDING GEAR STEERING ANGLE IS APPROXIMATELY 28.
90°
15 m (49 ft 2 in.)
100 ft Radius (30 m)
3 m (9 ft 10 in.)
PATH OF MAIN LANDING GEAR TIRE EDGE. EM170APM040013.DGN
90° Turn - Taxiway to Taxiway Figure 4.8
Section 4 EFFECTIVITY: ALL Page 4-11 May 25/18 w-apm1901 AIRPORT PLANNING MANUAL
4.6. RUNWAY HOLDING APRON
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.)
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 4.9 Section 4 EFFECTIVITY: EMBRAER 190 STD ACFT MODEL Page 4-12 May 25/18 w-apm1901 AIRPORT PLANNING MANUAL
RUNWAY 45 m (147 ft 7.6 in.)
MINIMUM CLEARENCES 15 m 75 m (49 ft 2 in.) (246 ft)
3 m (9 ft 10 in.)
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. EM170APM040014A.DGN
Runway Holding Bay Figure 4.10
Section 4 EFFECTIVITY: EMBRAER ACFT 190 LR OR AR MODEL Page 4-13 / 14 May 25/18 w-apm1901
AIRPORT PLANNING MANUAL
5. TERMINAL SERVICING
During turnaround at the air terminal, certain services must be performed on 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 equipments 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 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
5.1. AIRCRAFT SERVICING ARRANGEMENT
5 3 110 7 3 100 30
90
25 80 4 4 2 2
70 20
60
50
LENGTH − ft 15 LENGTH − m
40
10 30 1 1 20 5 9 6 10 8
0 0 0 510152025303540 45 LENGTH − m
0 102030405060708090100110120130 140 LENGTH − ft
SERVICING ARRANGEMENT 01 − PASSENGER STAIRS 02 − BAGGAGE LOADER 03 − BAGGAGE / CARGO 04 − GALLEY SERVICE 05 − FUEL SERVICE 06 − POTABLE WATER 07 − LAVATORY SERVICE 08 − AIR CONDITIONING 09 − PNEUMATIC STARTER EM170APM050011A.DGN
Aircraft Servicing Arrangement With Passenger Stairs Figure 5.1 Section 5 EFFECTIVITY: ALL Page 5-2 Oct 07/13 w-apm1901 w-apm1901 100 110 FETVT:ALL EFFECTIVITY: 1 30 10 20 40 LENGTH50 60 - ft 70 80 90 09 - GROUNDPOWER UNIT - 09 PASSENGER BRIDGE 08 - LAVATORY SERVICE 07 - POTABLE WATER06 - FUELSERVICE 05 - GALLEY SERVICE 04 - CARGO / BAGGAGE - 03 LOADER BAGGAGE - 02 PASSENGER STAIRS 01 - SERVICING ARRANGEMENT SERVICING 0 THE CABLEEXTENSION. AND THEGROUNDCONNECTION CONSIDERING GPUCANBEMOVEDTHE POSITION BETTER TO 25 30
LENGTH - m 20 10 15 0 5 01 02 035 30 25 20 15 10 5 1020304050607080901001101200 0 9 1 4 3 5 icatSriigArneetWt asne Bridge Passenger With Arrangement Servicing Aircraft 8 2 iue5.2 Figure LENGTH m - LENGTH -ft LNIGMANUAL PLANNING AIRPORT 1 2 3 4 7 3 140 130 40 a 22/20 May eto 5 Section ae5-3 Page 6 45 EM170APM050012A.IDR 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 performing servicing on the aircraft within a given time. The time of each service in the chart was calculated taking the following into consideration: • Load factor - 100%; • Passenger deplane - 24 pax/min; • Passenger enplane - 16 pax/min; • Baggages checked per passenger - 1,2; • Refuel (fuel quantity) - 80%; • Flow - 290 gpm; • Potable water - 70% to be refilled (56 ); • 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 Oct 07/13 w-apm1901 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 4.1
GALLEY SERVICING−FWD 7,0
PAX GALLEY SERVICING−AFT 7,0 SERVICES AIRPLANE INTERIOR SERVICES 6.1
PASSENGERS ENPLANE 6.1
BRIDGE / STAIRS REMOVAL 1,0
PUSH BACK / ENGINES START 2,0
FWD BAGGAGE / CARGO UNLOAD 4.3
REAR BAGGAGE / CARGO UNLOAD 3.5
BAGGAGE TIME BETWEEN UNLOADING / LOADING 0,5 & CARGO FWD BAGGAGE/CARGO LOAD 7.1
AFT BAGGAGE/CARGO LOAD 5.8
FUEL SERVICE 11.7
AIRCRAFT POTABLE WATER SERVICE 3,0 SERVICING TOILET SERVICE 5,0
LEGEND:
TRUCK POSITIONING/REMOVAL/SETTINGS
NOTE:
THIS DATA ILUSTRATES THE GENERAL SCOPE AND TASKS INVOLVING AIRPORT TERMINAL OPERATIONS. AIRLINE PARTICULAR PRACTICES AND OPERATING EXPERIENCE WILL
RESULT IN DIFFERENT SEQUENCES AND INTERVALS. EM170APM050013A.DGN
Air Terminal Operation - Turnaround Station Figure 5.3
Section 5 EFFECTIVITY: ALL Page 5-5 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
5.3. TERMINAL OPERATIONS - EN ROUTE STATION
Not Applicable
Section 5 EFFECTIVITY: ALL Page 5-6 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
5.4. GROUND SERVICING CONNECTIONS
1 2 7 8
6 22 5 4 11
3 9 10 12 13
14 15 16
19 18 17 21 20
HEIGHT COORD. Y ABOVE ITEM DESCRIPTION COORD. X COORD. Z (mm) (mm) (mm) GROUND (mm) 1 PRESSURE REFUELING PANEL 17316.95 7803.78 −543.75 2862.76 2 GRAVITY REFUELING PORT (RH) 17695.04 7774.46 −310.92 3104.19 3 GRAVITY REFUELING PORT (LH) 17932.67 −7646.75 −308.24 3112.32 4 FORWARD RAMP HEADSET 4164.44 −936.13 −1262.71 1842.51 5 STEERING SWITCH DISENGAGE 4136.97 −951.46 −1279.29 1825.31 6 WHEEL JACK POINT − NLG 4125.32 0.00 −2854.38 250.36 7 AIR COND. GROUND CONNECTION 13268.52 0.00 −1979.71 1334.39 8 ENGINE AIR STARTING (LOW PRESSURE UNIT) 13629.01 57.25 −1952.83 1369.51 9 GROUNDING POINT (ELECTRICAL) 18052.28 2930.25 −1744.67 1679.01 10 WHEEL JACK POINT− MLG (RH) 18078.03 2970.00 −2988.86 435.73 11 WHEEL JACK POINT− MLG (LH) 18078.03 −2970.00 −2988.86 435.73 12 HYD. SYS # 1 SERVICE PANEL 20139.16 −808.01 −1602.04 1869.43 13 WATER SERVICING PANEL 27861.83 −329.37 −1178.74 2469.64 14 EXTERNAL POWER SUPPLY 28 VDC / 400A 30421.65 −471.73 −605.30 3101.60 15 AFT RAMP HEADSET 30562.26 −449.47 −585.54 3124.58 16 OXYGEN SERVICING PANEL / BOTTLE 6562.14 1159.87 −961.05 2109.06 17 FUEL TANK DRAIN VALVE (LH) 16444.90 −691.60 −1611.45 1775.35 18 FUEL TANK DRAIN VALVE (RH) 16476.65 526.50 −1611.45 1776.08 19 HYD. SYS # 2 SERVICE PANEL 20139.16 808.01 −1602.04 1869.43 20 WASTE SERVICING PANEL 28784.01 349.20 −991.80 2677.66 21 HYD. SYS # 3 SERVICE PANEL 30398.86 519.15 −590.09 3116.29 22 EXTERNAL POWER SUPPLY 115 VAC 4146.90 −810.70 −1339.53 1765.31 NOTE: THE GROUND CLEARANCES IN THE TABLE REFER TO THE AIRCRAFT WITH THE MINIMUM OPERATING WEIGHT (MOW) = 29500 kg (CG FWD 4.0% CMA) EM170APM050014E.DGN
Ground Servicing Connections Figure 5.4 Section 5 EFFECTIVITY: ALL Page 5-7 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
1 2 7 8
6 22 5 4 11
3 9 10 12 13
14 15 16
19 18 17 21 20
HEIGHT COORD. Y ABOVE ITEM DESCRIPTION COORD. X COORD. Z (mm) (mm) (mm) GROUND (mm) 1 PRESSURE REFUELING PANEL 17316.95 7803.78 −543.75 2849.66 2 GRAVITY REFUELING PORT (RH) 17695.04 7774.46 −310.92 3088.37 3 GRAVITY REFUELING PORT (LH) 17932.67 −7646.75 −308.24 3094.78 4 FORWARD RAMP HEADSET 4146.44 −936.13 −1262.71 1924.92 5 STEERING SWITCH DISENGAGE 4136.97 −951.46 −1279.29 1907.92 6 WHEEL JACK POINT − NLG 4125.32 0.00 −2854.38 250.48 7 AIR COND. GROUND CONNECTION 13268.52 0.00 −1979.71 1350.51 8 ENGINE AIR STARTING (LOW PRESSURE UNIT) 13629.01 57.25 −1952.83 1383.02 9 GROUNDING POINT (ELECTRICAL) 18052.28 2930.25 −1744.67 1660.39 10 WHEEL JACK POINT− MLG (RH) 18077.02 2970.00 −2969.64 428.34 11 WHEEL JACK POINT− MLG (LH) 18077.02 −2970.00 −2969.64 428.34 12 HYD. SYS # 1 SERVICE PANEL 20139.16 −808.01 −1602.04 1835.66 13 WATER SERVICING PANEL 27861.83 −329.37 −1178.74 2379.79 14 EXTERNAL POWER SUPPLY 28 VDC / 400A 30421.65 −471.73 −605.30 2993.22 15 AFT RAMP HEADSET 30562.26 −449.47 −585.54 3015.18 16 OXYGEN SERVICING PANEL / BOTTLE 6562.14 1159.87 −961.05 2264.08 17 FUEL TANK DRAIN VALVE (LH) 16444.90 −691.60 −1611.45 1768.43 18 FUEL TANK DRAIN VALVE (RH) 16476.65 526.50 −1611.45 1768.43 19 HYD. SYS # 2 SERVICE PANEL 20139.16 808.01 −1602.04 1835.66 20 WASTE SERVICING PANEL 28784.01 349.20 −991.80 2581.13 21 HYD. SYS # 3 SERVICE PANEL 30398.86 519.15 −590.09 3008.07 22 EXTERNAL POWER SUPPLY 115 VAC 4146.90 −810.70 −1339.53 1847.84 NOTE: THE GROUND CLEARANCES IN THE TABLE REFER TO THE AIRCRAFT WITH THE MINIMUM OPERATING WEIGHT (MOW) = 29500 kg (CG REAR 29.0% CMA) EM170APM050024.DGN
Ground Servicing Connections Figure 5.5
Section 5 EFFECTIVITY: ALL Page 5-8 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
5.5. ENGINE STARTING PNEUMATIC REQUIREMENTS
TABLE 1 − PNEUMATIC ENGINE START REQUIREMENTS
Ambient Temp Minimum Minimum Altitude ft °C (°F) Pressure psia Flow lb/min SL −40 (− 40) 48.0 95.1 SL 15 (59) 43.7 82.0 SL 49 (120) 40.7 73.7 9000 −40 (− 40) 37.7 74.5 9000 − 5 (23) 30.0 57.3 9000 13 (86) 28.9 53.4 13,000 −40 (− 40) 36.0 71.3 13,000 −11 (12) 27.2 52.2 13,000 21.7 (71) 26.7 49.6 15,000 −40 (− 40) 32.9 66.6 15,000 −15 (5) 25.3 49.0 15,000 15 (59) 24.4 46.1 EM170APM050030B.DGN
Engine Starting Pneumatic Requirements Figure 5.6 Section 5 EFFECTIVITY: ALL Page 5-9 May 25/18 w-apm1901 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 07/13 w-apm1901 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 within a given time at ambient conditions. • The air conditioning requirements for heating and cooling to maintain a constant cabin air tempera- ture 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 07/13 w-apm1901 AIRPORT PLANNING MANUAL
PRE−CONDITIONED AIRFLOW REQUIREMENTS [lbm/min] 150 [kg/min] 1 4 55 140 60 2 16 120 6 5 50 12 3 100 10
40 80
30 5
TOTAL AIRFLOW 60
20 40 1
10 20 PRESSURE AT GROUND CONNECTION (INCHES OF WATER)
0 0 −5 0510 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 406mmH20 (16 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. EM170MFEP040070B.DGN
Preconditioned Airflow Requirements Figure 5.8
Section 5 EFFECTIVITY: ALL Page 5-12 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
5.8. GROUND TOWING REQUIREMENTS
5
50 (121254) 55000 45000 (99208) 45000
30 (116845) 53000
43000 (94799) 43000
10 (112436) 51000 41000 (90390) 41000
90 (108027) 49000
39000 (85980) 39000 37000 (81571) 37000
47000 (103617) 47000 35000 (77162) 35000
33000 (72753) 33000 31000 (68343) 31000 29000 (63934) 29000 4 3
2 AIRCRAFT GROSS WEIGHT - kg (lb) kg - WEIGHT GROSS AIRCRAFT PERCENT SLOPE (%) PERCENT SLOPE 1
0 REFERENCE LINE REFERENCE 2 1 ENGINES NUMBER OF NUMBER IDLE THRUST BACKING AGAINST 0 7000 (15432)
6000
ICE =0.05 ICE (13227)
WET ASPHALT =0.75 ASPHALT WET
ASPHALT =0.8 ASPHALT
WET CONCRETE =0.57 CONCRETE WET
SNOW CHAINS =0.45 CHAINS SNOW DRY CONCRETE OR CONCRETE DRY HARD SNOW =0.2 SNOW HARD 5000 (11023) GROUND PUSHBACK / TOWING REQUIREMENTS 4000 (8818) 3000 (6614) (DRAWBAR PUSH / PULL) 2000 (4409) TOTAL TRACTION WHEEL - kg TRACTION WHEEL (lb)TOTAL - STRAIGHT-LINE TOW - UNUSUAL BREAKAWAY CONDITIONS NOT SHOWN - COEFFICIENTS OF ( ) ARE FRICTION ESTIMATED FOR RUBBER-TIRED TOW VEHICLES NOTES: 1000 (2204) 0 0 5000 4000 3000 2000 1000
(8818) (6614) (4409) (2204) (11023) (lb) kg - PULL / PUSH TOWBAR EM170MFEP040066C.IDR
Ground Towing Requirements Figure 5.9 Section 5 EFFECTIVITY: ALL Page 5-13 / 14 May 22/20 w-apm1901
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 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
6.1. ENGINE EXHAUST VELOCITIES AND TEMPERATURES
TAKEOFF POWER, SEA LEVEL, Tamb = ISA +20°C, FNIN1 = 84347 N (18962 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 396.2 (1300) NOTE:
EXHAUST VELOCITY CONTOURS INCLUDE WORST CASE 20 kn HEADWIND WITH GROUND EFFECTS. EM170MFEP020014A.DGN
Jet Wake Velocity Profile - Takeoff Power Figure 6.1 Section 6 EFFECTIVITY: ALL Page 6-2 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
TAKEOFF POWER, SEA LEVEL, Tamb = ISA +20°C, FNIN1 = 84347 N (18962 lbf)
A 5 16 4 14 12 3 10 8 B 2 Meters 6 C E D 1 4 2 0 0 0 4 8 12162024283236404448525660 DISTANCE FROM CORE NOZZLE EXIT − Feet HEIGHT ABOVE GROUND PLANE − Feet
0246 81012141618 Meters
24 7 A 6 20 B 5 16
4 E D 12 C
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 TOTAL TEMPERATURE MAX = 689°C (1273°F) °C °F A 38 100 B 66 150 C 93 200 D 204 400 E 582 900 NOTE:
EXHAUST TEMPERATURE CONTOURS INCLUDE WORST CASE 20 kn HEADWIND. EM170MFEP020016B.DGN
Jet Wake Temperature Profile - Takeoff Power Figure 6.2
Section 6 EFFECTIVITY: ALL Page 6-3 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
GROUND IDLE, SEA LEVEL, Tamb = ISA +15°C, FNIN1 = 2558 N (575 lbf)
5 16 4 14 12 3 10 A 8 2 Meters 6 D C B 1 4 2 0 0 0 4 8 12162024283236404448525660 DISTANCE FROM CORE NOZZLE EXIT − Feet HEIGHT ABOVE GROUND PLANE − Feet
024681012141618 Meters
24 7 A 6 20
5 16 C B 4 D 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 = 89.0 (292) A 15.2 (50) B 30.5 (100) C 45.7 (150) D 57.9 (190)
NOTE:
EXHAUST VELOCITY CONTOURS INCLUDE WORST CASE 20 kn HEADWIND WITH GROUND EFFECTS. EM170MFEP020015A.DGN
Jet Wake Velocity Profile - Ground Idle Figure 6.3
Section 6 EFFECTIVITY: ALL Page 6-4 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
GROUND IDLE, SEA LEVEL, Tamb = ISA +15°C, FNIN1 = 2558 N (575 lbf)
5 16 4 14 12 A 3 10 8 2 Meters 6 E D C B 1 4 2 0 0 04812162024283236404448525660 DISTANCE FROM CORE NOZZLE EXIT − Feet HEIGHT ABOVE GROUND PLANE − Feet 024681012141618 Meters
24 7
6 20 A
5 16 4 D C B 12
Meters 3 8 E 2 4 1
0 0
DISTANCE FROM AIRPLANE CL − Feet 0 4 8 12162024283236404448525660 DISTANCE FROM CORE NOZZLE EXIT − Feet
024681012141618 Meters TOTAL TEMPERATURE MAX = 519°C (966°F) °C °F A 38 100 B 66 150 C 93 200 D 204 400 E 582 900
NOTE:
EXHAUST TEMPERATURE CONTOURS INCLUDE WORST CASE 20 kn HEADWIND. EM170MFEP020017A.DGN
Jet Wake Temperature Profile - Ground Idle Figure 6.4
Section 6 EFFECTIVITY: ALL Page 6-5 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
BREAKAWAY POWER, SEA LEVEL, Tamb = ISA +0°C, FNIN1 = 40660 N (9139 lbf)
5 16 14 4 A 12 3 10 B 8 Meters 2 6 4 E D C 1 2 0 0 0 4 8 12162024283236404448525660
HEIGHT ABOVE GROUND PLANE, Feet DISTANCE FROM CORE NOZZLE EXIT, Feet
024681012141618 Meters
28 8 24 7 A
6 B
5 16 E D C 4 Meters 12 3 8 2
1 4 DISTANCE FROM AIRPLANE CL − Feet 0 0 0 4 8 12162024283236404448525660 DISTANCE FROM CORE NOZZLE EXIT, Feet VELOCITY (ft/sec) MAX = 497 024 6 8 10 12 14 16 18 A 50 Meters B 100 C 200 D 300 E 450
NOTE:
EXHAUST VELOCITY CONTOURS INCLUDE WORST CASE 20 knot HEADWIND WITH GROUND EFFECTS. EM170APM060008A.DGN
Jet Wake Velocity Profile - Breakaway Power Figure 6.5 Sheet 1
Section 6 EFFECTIVITY: ALL Page 6-6 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
BREAKAWAY POWER, SEA LEVEL, Tamb = ISA +0°C, FNIN1 = 40660 N (9139 lbf)
50 Meters
40 12
10 30 35 MPH 8
20 6 50 MPH
4 75 MPH 10 2 100 MPH
0 0 0 20 40 60 80 100 120 140 160180 200 220 240 Feet
HEIGHT ABOVE GROUND PLANE − Feet (Meters) 0 10203040506070
AXIAL DISTANCE BEHIND AIRPLANE
50
40 12 35 MPH 10 30 50 MPH 8 75 MPH 20 6 100 MPH 4 10 2 0 0 CL AIRPLANE −2 −10 −4
−20 −6 −8 DISTANCE FROM AIRPLANE CL − Feet −30 −10
−40 −12
−50 EM170APM060010A.DGN
Jet Wake Velocity Profile - Breakaway Power Figure 6.5 Sheet 2
Section 6 EFFECTIVITY: ALL Page 6-7 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
BREAKAWAY POWER, SEA LEVEL, Tamb = ISA +0°C, FNIN1 = 40660 N (9139 lbf)
5 16
14 4 12 3 10 8
Meters 2 6 A 4 B 1 2 E D C 0 0 0 4 8 12162024283236404448525660 HEIGHT ABOVE GROUND PLANE − Feet DISTANCE FROM CORE NOZZLE EXIT − Feet
024681012141618 Meters
28 8
24 7
6 20 A 5 16 B 4
Meters 12 E D C 3 8 2
4 1 DISTANCE FROM AIRPLANE CL − Feet 0 0 0 4 8 12162024283236404448525660 DISTANCE FROM CORE NOZZLE EXIT − Feet
024 6 8 10 12 14 16 18
TOTAL TEMPERATURE Meters MAX = 697 °F (369 °C) °F °C A 100 38 B 150 66 C 200 93 D 400 204 E 650 343
NOTE:
EXHAUST TEMPERATURE CONTOURS INCLUDE WORST CASE 20 knot HEADWIND. EM170APM060009A.DGN
Jet Wake Temperature Profile - Breakaway Power Figure 6.6
Section 6 EFFECTIVITY: ALL Page 6-8 Oct 07/13 w-apm1901 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 6-9 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
6.3. HAZARD AREAS
TAKEOFF POWER, SEA LEVEL, Tamb = ISA +15° C, FNIN1 = 91184 N (20499 lbf)
1
144 m (474 ft)
ENGINE EXHAUST HAZARD AREA VELOCITY = 65 mph OR GREATER = 29.0 m/s (95.3 ft/s)
2 1.9 m (6.2 ft) R= 5.23 m (17 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. EM170APM060004B.DGN
Hazard Areas - Takeoff Power Figure 6.7 Section 6 EFFECTIVITY: ALL Page 6-10 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
GROUND IDLE, SEA LEVEL, Tamb = ISA+15° C, FNIN1 = 3768 N (847 lbf)
ENGINE EXHAUST HAZARD AREA VELOCITY = 65 mph OR GREATER = 29.0 m/s (95.3 ft/s)
17 m (55 ft)
2
1.0 m R=2.6 m (3.3 ft) (8.5 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.
2
EXHAUST HAZARD AREA − CONDITION: 20 kn HEADWIND WITH GROUND EFFECTS. EM170APM060005C.DGN
Hazard Areas - Ground Idle Figure 6.8
Section 6 EFFECTIVITY: ALL Page 6-11 / 12 Oct 07/13 w-apm1901
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 on charts, are values obtained under loaded conditions as certificated for commercial use. This section is presented as follows: • The basic data on the landing gear footprint configuration, maximum design ramp loads, 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 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
7.2. FOOTPRINT
AIRCRAFT MODELS STD LR AR 47950 kg 50460 kg 51960 kg MAXIMUM RAMP WEIGHT (105712 lb) (111245 lb) (114552 lb)
NOSE GEAR TIRE SIZE 24 x 7.7 16PR 9.21 - 0/+0.7 kg/cm ² NOSE GEAR TIRE PRESSURE (131 - 0/+10 psi)
MAIN GEAR TIRE SIZE H41 x 16-20 22PR 11.04 - 0/+0.7 kg/cm ² MAIN GEAR TIRE PRESSURE (157 - 0/+10 psi)
0.87 m (2 ft 10 in.)
13.83 m 0.40 m (45 ft 4 in.) (1 ft 4 in.)
5.94 m (19 ft 6 in.) EM170APM070027C.IDR
Footprint Figure 7.1 Section 7 EFFECTIVITY: ALL Page 7-2 May 21/21 w-apm1901 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
50460 kg 6424 kg 8917 kg 23301 kg 6814 kg 16138 kg LR (111245 lb) (14162 lb) (19659 lb) (51370 lb) (15022 lb) (35578 lb)
47950 kg 6470 kg 8820 kg 22213 kg 6494 kg 15376 kg STD (105712 lb) (14264 lb) (19445 lb) (48971 lb) (14317 lb) (33898 lb)
51960 kg 6347 kg 8927 kg 23952 kg 7005 kg 16593 kg AR (114552 lb) (13993 lb) (19681 lb) (52805 lb) (15443 lb) (36581 lb)
46150 kg 6229 kg 8498 kg 21181 kg 6255 kg 14807 kg SR (101743 lb) (13732 lb) (18735 lb) (46696 lb) (13790 lb) (32644 lb) EM170APM070028D.DGN
Maximum Pavement Loads Figure 7.2 Section 7 EFFECTIVITY: ALL Page 7-3 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
7.4. LANDING GEAR LOADING ON PAVEMENT
6.0 % 29.0 % %MAC
50000 110000 51960
50460 110000
47950 100000 45000
45000 100000
90000 42500 40000 90000 40000
80000 37500 35000 80000 35000
70000 32500 30000 AIRCRAFT GROSS WEIGHT − (kg) 70000 WEIGHT ON MAIN LANDING GEAR (lb) WEIGHT ON MAIN LANDING GEAR (lb) WEIGHT ON MAIN LANDING GEAR (kg) 29500 60000 60000 25000
50000 50000
20000 84 86 88 90 92 94 PERCENT OF WEIGHT ON MAIN GEAR − (%)
LEGEND AR AIRCRAFT MODEL LR AIRCRAFT MODEL STD AIRCRAFT MODEL EM170APM070029B.DGN
Landing Gear Loading on Pavement Figure 7.3 Section 7 EFFECTIVITY: ALL Page 7-4 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
7.5. FLEXIBLE PAVEMENT REQUIREMENTS, US CORPS OF ENGINEERS DESIGN METHOD
The flexible pavement curves that are based on procedures set forth in Instruction Report No. S-77-1, “Procedures for Development of CBR Design Curves”, dated June 1977, and as modified according to the methods described in FAA Advisory Circular 150/5320-6D, “Airport Pavement Design and Evalua- tion”, 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 Oct 07/13 w-apm1901 FETVT:EBAR10L CTMODEL ACFT LR 190 EMBRAER EFFECTIVITY: 3 3 10000 COVERAGES 8910 CALCULATIONS) (USED FOR ACN (USED lxbePvmn eurmns-U ryCrso nier einMethod Design Engineers of Corps Army US - Requirements Pavement Flexible 4 4 5 5 NOTES: SUBGRADE STRENGHT - CBRMODEL SUBGRADE STRENGHT- 6 6 FLEXIBLE PAVEMENT THICKNESS - cm - PAVEMENT THICKNESS FLEXIBLE FLEXIBLE PAVEMENT THICKNESS - in - PAVEMENT THICKNESS FLEXIBLE TIRE PRESSURE: 11.04 kgf/cm (157 psi) (157 kgf/cm PRESSURE:TIRE 11.04 22PR H41 x16-20 SIZE: TIRE 7 7 20 8 8 iue7.4 Figure 9 9 10 10 LNIGMANUAL PLANNING AIRPORT 040 30 2 DEPARTURES WEIGHT ON MAIN LANDING GEAR LANDING 46806 103190 26302 57986 37832 83405 39988 88158 44046 97105 ANNUAL 25000 15000 6000 3200 1200 (kg) (lb) (kg) 50 20 20 60 a 21/21 May eto 7 Section 70 ae7-6 Page 30 30
EM170APM070031B.IDR
w-apm1901 AIRPORT PLANNING MANUAL
7.6. FLEXIBLE PAVEMENT REQUIREMENTS, LCN METHOD
The LCN Method 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 7-7 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
NOTES: TIRE SIZE: H41x16-20 22PR 2 TIRE PRESSURE: 11.04 kgf/cm (157 psi)
50000
20000 19000 40000 WEIGHT ON MAIN 18000 LANDING GEAR kg (lb) 16000
14000 30000 46806 (103190) 44046 (97105) 12000 39988 (88158) 37832 (83405) 10000 20000
8000 26302 (57986) EQUIVALENT SINGLE WHEEL LOAD -EQUIVALENT LOAD SINGLE(lb) WHEEL EQUIVALENT SINGLE WHEEL LOAD -EQUIVALENT LOAD SINGLE(kg) WHEEL 6000
10000 6 7 8 9 10 20 30 40 50 60 70 8090 100 10 20 30 40 50 60 70 8090100
FLEXIBLE PAVEMENT THICKNESS - (cm) LCN - LOAD CLASSIFICATION NUMBER
3 5 10 20 30
FLEXIBLE PAVEMENT THICKNESS - (in.)
NOTES: EQUIVALENT SINGLE WHEEL LOADS ARE DERIVED BY METHODS SHOWN IN ICAO AERODROME MANUAL. PART 2, PAR. 4.1.3 EM170APM070033B.IDR
Flexible Pavement Requirements - LCN Method Figure 7.5
Section 7 EFFECTIVITY: EMBRAER 190 LR ACFT MODEL Page 7-8 May 21/21 w-apm1901 AIRPORT PLANNING MANUAL
7.7. RIGID PAVEMENT REQUIREMENTS, PORTLAND CEMENT ASSOCIATION DESIGN METHOD
This method has a chart that have 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 that 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 7-9 May 21/21 w-apm1901 FETVT:EBAR10SDACFT STD 190 MODEL EMBRAER EFFECTIVITY: PAVEMENT THICKNESS (in.) 16 20 22 24 26 28 30 14 12 18 10 6 8 2 4 0
PAVEMENT THICKNESS (cm) 10 20 30 40 50 60 70 80 0 NOTE: ii aeetRqieet otadCmn soito einMethod Design Association Cement Portland - Requirements Pavement Rigid SLIGHTLY FOROTHERVALUESOF"K". ARE EXACTFORK=300BUTDEVIATE LOADS LESSTHANMAXIMUM,THECURVES ANY VALUEOF"K"AREEXACT.FOR MAXIMUM LOADREFERENCELINEAND THE VALUESOBTAINEDBYUSING k=550 lb/in k=300 lb/in NOTES: RIGID PAVEMENTREQUIREMENTS k=150 lb/in k=75 lb/in WEIGHT ANDAFTC.G. LOAD ATMAXIMUMDESIGNRAMP MAXIMUM POSSIBLEMAIN−GEAR TIRE PRESSURE:10.34kgf/cm(147psi)(UNLOADED) TIRE SIZE:H41x16−2022PR
WEIGHT ON MAIN LANDING GEAR − kg (lb) iue7.6 Figure LNIGMANUAL PLANNING AIRPORT 2
26302 (57986) 44776 (98053) 41444 (91368) 3783239988 (85405) (88158) 10 20 30 40 50 60 70 80 0 a 21/21 May 7-10 Page eto 7 Section ALLOWABLE WORKING STRESS − kgf/cm2 100 200 300 400 500 600 700 800 900 1000 1100 0
EM170APM070034A.DGN ALLOWABLE WORKING STRESS − psi
w-apm1901 AIRPORT PLANNING MANUAL
RIGID PAVEMENT REQUIREMENTS
NOTES: TIRE SIZE: H41 x 16-20 22PR TIRE PRESSURE: 11.04 kgf/cm 2 (157 psi) (UNLOADED)
80 80 30 1100
28 70 70 1000 2 26 46806 (103190) 44046 (97105) 900 24 60 39988 (88158) 60 22 800 37832 (85405) 20 50 WEIGHT ON MAIN LANDING GEAR - kg (lb) 50 700 k=550 lb/in 18 k=300 lb/in 26302 (57986) 600 16 40 k=150 lb/in 40 14 k=75 lb/in 500
12 30 30 400 10 PAVEMENT THICKNESSPAVEMENT (in.) PAVEMENT THICKNESSPAVEMENT (cm) ALLOWABLE WORKING STRESS - WORKING psi ALLOWABLE
ALLOWABLE WORKING STRESS - WORKING kgf/cmALLOWABLE 300 8 20 20
6 200 MAXIMUM POSSIBLE MAIN-GEAR 4 10 LOAD AT MAXIMUM DESIGN RAMP 10 100 2 WEIGHT AND AFT C.G. 0 0 0 0
NOTE: THE VALUES OBTAINED BY USING THE 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". EM170APM070035B.IDR
Rigid Pavement Requirements - Portland Cement Association Design Method Figure 7.7
Section 7 EFFECTIVITY: EMBRAER 190 LR ACFT MODEL Page 7-11 May 21/21 w-apm1901 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 that are based on Young’s modulus (E) of 4,000,000 psi and Poisson’s ratio (µ) of 0.15. For convenience in finding this radius based on other values of E and µ, the curves are included. 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 7-12 May 21/21 w-apm1901 w-apm1901 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 iue7.8 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 a 21/21 May 7-13 Page 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 iue7.9 Figure , POISSON’SRATIO LNIGMANUAL PLANNING AIRPORT 6 a 21/21 May 7-14 Page eto 7 Section
EM170APM070008.DGN
w-apm1901 w-apm1901
FETVT:EBAR10SDACFT STD 190 MODEL EMBRAER EFFECTIVITY: EQUIVALENT SINGLE WHEEL LOAD − (lb) 50000 10000 20000 30000 40000 PART 2,PAR.4.1.3 IN ICAOAERODROMEMANUAL. ARE DERIVEDBYMETHODSSHOWN EQUIVALENT SINGLEWHEELLOADS NOTES: 40 30 50 WEIGHT ONMAIN LANDING GEAR RADIUS OFRELATIVESTIFFNESS−(in.) RADIUS OFRELATIVESTIFFNESS−(cm) 60 kg (lb) 70 50 80 90 100 NOTES: 4144444476 (91368) (98053) 39988 (88158) 26302 (57986) 37832 (83405) 0 200 100 ii aeetRqieet C Method LCN - Requirements Pavement Rigid 200 TIRE PRESSURE:10.34kgf/cm(147psi) TIRE SIZE:H41x16−2022PR 300 400 iue7.10 Figure LNIGMANUAL PLANNING AIRPORT 2 LCN −LOADCLASSIFICATIONNUMBER 03 40 30 10 20 50 60 70 80 90 a 21/21 May 7-15 Page 100 eto 7 Section 10000 19000 20000 12000 6000 18000 14000 16000 8000
EM170APM070036A.DGN EQUIVALENT SINGLE WHEEL LOAD − (kg) FETVT:EBAR10L CTMODEL ACFT LR 190 EMBRAER EFFECTIVITY: EQUIVALENT SINGLE WHEEL LOAD - (lb) 50000 10000 20000 30000 40000 PART 2, PAR. 4.1.3 PAR. PART 2, IN ICAO AERODROME MANUAL. BY METHODS SHOWNARE DERIVED WHEEL SINGLE LOADS EQUIVALENT NOTES: 40 WEIGHT ON MAIN 30 50 LANDING GEAR LANDING RADIUS OF RELATIVE STIFFNESS - (in.) - STIFFNESS OF RELATIVE RADIUS RADIUS OF RELATIVE STIFFNESS - (cm) - STIFFNESS OF RELATIVE RADIUS 60 kg (lb) 70 50 80 90 100 NOTES: 26302 (57985) 46806 (103190) 3783239988 (83405) (88158)44046 (97104) 0 200 100 ii aeetRqieet C Method LCN - Requirements Pavement Rigid 200 TIRE PRESSURE: 11.04 kgf/cm (157 psi) (157 kgf/cm PRESSURE:TIRE 11.04 22PR H41 x16-20 SIZE: TIRE 0 400 300 iue7.11 Figure LNIGMANUAL PLANNING AIRPORT 2 LCN - LOAD CLASSIFICATION NUMBER LOAD CLASSIFICATION LCN - 10 20 30 40 50 60 70 80 90 100 a 21/21 May 7-16 Page eto 7 Section 10000 19000 20000 12000 6000 18000 14000 16000 8000
EM170APM070037B.IDR EQUIVALENT SINGLE WHEEL LOAD - (kg)
w-apm1901 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 which an evaluation shows can be borne by the pavement when applied by a standard single wheel. The ACN 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 be 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 with the results of their evaluation 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 1.75 Mpa (254 psi) U – Using aircraft C – Low Y – to 1.25 Mpa (181 psi) D – Ultra Low Z – to 0.5 Mpa (73 psi) Report example: PCN 80/R/B/X/T, where: 80 = PCN R = Pavement Type: Rigid B = Subgrade Category: Medium X = Tire Pressure Category: Medium (limited to 1.5 Mpa) T = Evaluation Method: Technical
The flexible pavements have four subgrade categories: A. High Strength - 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 7-17 May 21/21 w-apm1901 AIRPORT PLANNING MANUAL
FLEXIBLE PAVEMENT SUBGRADE
NOTES: TIRE SIZE: H41 x 16-20 22PR TIRE PRESSURE: 10.34 kgf/cm 2 (157 psi) (UNLOADED)
35
SBGRADE STRENGTH 30 ULTRA LOW - CBR=3% LOW - CBR=6% MEDIUM-CBR=10% HIGH-CBR=15% 25
20 MAXIMUM RAMP WEIGHT
15 AIRCRAFT CLASSIFICATION NUMBER-ACN
10 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 29500 AIRCRAFT GROSS WEIGHT-kg 47950
64000 68000 72000 76000 80000 84000 88000 92000 96000 100000 104000 108000 AIRCRAFT GROSS WEIGHT-lb EM170APM070038B.IDR
ACN For Flexible Pavement Figure 7.12
Section 7 EFFECTIVITY: EMBRAER 190 STD ACFT MODEL Page 7-18 Aug 27/21 w-apm1901 w-apm1901
FETVT:EBAR10L CTMODEL ACFT LR 190 EMBRAER EFFECTIVITY: AIRCRAFT CLASSIFICATION NUMBER-ACN 35 20 25 30 10 15 28000 40 80 20 60 00 84000 80000 76000 72000 68000 64000 29500 30000 32000 NOTES: 34000 FLEXIBLE PAVEMENT SUBGRADE FLEXIBLE HIGH-CBR=15% MEDIUM-CBR=10% CBR=6% LOW - CBR=3% LOWULTRA - SBGRADE STRENGTH TIRE PRESSURE: 11.04 kgf/cm (157 psi) (UNLOADED) psi) (157 kgf/cm PRESSURE:TIRE 11.04 22PR H41 x16-20 SIZE: TIRE 36000 C o lxbePavement Flexible For ACN AIRCRAFT GROSSWEIGHT-kg AIRCRAFT AIRCRAFT GROSSWEIGHT-lb AIRCRAFT 38000 iue7.13 Figure 80 20 60 000140 000112000 108000 104000 100000 96000 92000 88000 00 20 40 46000 44000 42000 40000 LNIGMANUAL PLANNING AIRPORT 2 48000 50000 ae7-19 Page u 27/21 Aug eto 7 Section 50460 MAXIMUM RAMP WEIGHT 52000
EM170APM070039C.IDR FETVT:EBAR10SDACFT STD 190 MODEL EMBRAER EFFECTIVITY: AIRCRAFT CLASSIFICATION NUMBER-ACN 35 20 25 30 10 15 28000 40 80 20 60 00 84000 80000 76000 72000 68000 64000 ULTRA LOW-k=20 MN/m (75 lb/in ) ULTRA LOW-k=20 MN/m lb/in (75 29500 MEDIUM-k=80 MN/m (300 lb/in ) MEDIUM-k=80 MN/m lb/in (300 HIGH-k=150 MN/m (550 lb/in ) MN/mHIGH-k=150 lb/in (550 30000 LOW-k=40 MN/m (150 lb/in ) LOW-k=40 MN/m lb/in (150 32000 NOTES: 3 3 3 3 34000 RIGID PAVEMENT SUBGRADE RIGID 3 3 3 3 TIRE PRESSURE: 10.34 kgf/cm (157 psi) (UNLOADED) psi) (157 kgf/cm PRESSURE:TIRE 10.34 22PR H41 x16-20 SIZE: TIRE 36000 C o ii Pavement Rigid For ACN AIRCRAFT GROSSWEIGHT-kg AIRCRAFT AIRCRAFT GROSSWEIGHT-lb AIRCRAFT 38000 iue7.14 Figure 80 20 60 000140 000112000 108000 104000 100000 96000 92000 88000 00 20 40 46000 44000 42000 40000 LNIGMANUAL PLANNING AIRPORT 2 47950 MAXIMUM RAMP WEIGHT 48000 50000 ae7-20 Page u 27/21 Aug eto 7 Section 52000
EM170APM070040B.IDR
w-apm1901 w-apm1901
FETVT:EBAR10L CTMODEL ACFT LR 190 EMBRAER EFFECTIVITY: AIRCRAFT CLASSIFICATION NUMBER-ACN 35 20 25 30 10 15 28000 40 80 20 60 00 84000 80000 76000 72000 68000 64000 ULTRA LOW-k=20 MN/m (75 lb/in ) ULTRA LOW-k=20 MN/m lb/in (75 29500 MEDIUM-k=80 MN/m (300 lb/in ) MEDIUM-k=80 MN/m lb/in (300 HIGH-k=150 MN/m (550 lb/in ) MN/mHIGH-k=150 lb/in (550 30000 LOW-k=40 MN/m (150 lb/in ) LOW-k=40 MN/m lb/in (150 32000 NOTES: 3 3 3 3 34000 RIGID PAVEMENT SUBGRADE RIGID 3 3 3 3 TIRE PRESSURE: 11.04 kgf/cm (157 psi) (UNLOADED) psi) (157 kgf/cm PRESSURE:TIRE 11.04 22PR H41 x16-20 SIZE: TIRE 36000 C o ii Pavement Rigid For ACN AIRCRAFT GROSSWEIGHT-kg AIRCRAFT AIRCRAFT GROSSWEIGHT-lb AIRCRAFT 38000 iue7.15 Figure 80 20 60 000140 000112000 108000 104000 100000 96000 92000 88000 00 20 40 46000 44000 42000 40000 LNIGMANUAL PLANNING AIRPORT 2 48000 ae72 22 / 7-21 Page 50000 u 27/21 Aug eto 7 Section 50460 MAXIMUM RAMP WEIGHT 52000
EM170APM070041C.IDR
AIRPORT PLANNING MANUAL
8. POSSIBLE EMBRAER 190 DERIVATIVE AIRCRAFT
8.1. NOT APPLICABLE
Section 8 EFFECTIVITY: ALL Page 8-1 / 2 Oct 07/13 w-apm1901
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 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
1 14
7
10
3 4
9 8
11 11
6 10
13 14
5 2
0 5 10 15 20 25 m
0163248 64 80 ft
WING SPAN: 28.72 m (94 ft 3 in.)
ITEM DESCRIPTION ITEM DESCRIPTION 1 EXTERNAL POWER SUPPLY 115 VAC 8 PRESSURE REFUELING / DEFUELING 2 EXTERNAL POWER SUPPLY 28 VDC 9 GROUNDING POINT (RIGHT MLG) 3 ENGINE AIR STARTING 10 CARGO DOOR 4 AIR CONDITIONING LOW PRESSURE 11 MAIN LANDING GEAR 5 WASTE SERVICING PANEL 12 NOSE LANDING GEAR 6 POTABLE WATER SERVICING PANEL 13 PASSENGER DOOR 7 OXYGEN REFILL / REPLACE BOTTLE 14 SERVICE DOOR EM170APM090006.DGN
Scale: 1 Inch Equals 32 Feet Figure 9.1
Section 9 EFFECTIVITY: ALL Page 9-2 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
12
1 14 13 7 10
3 4
9 8
11 11 6 10 13 14
2 5
0 5 10 15 20 25 m
0163248 64 80 ft
WING SPAN: 28.72 m (94 ft 3 in.)
ITEM DESCRIPTION ITEM DESCRIPTION 1 EXTERNAL POWER SUPPLY 115 VAC 8 PRESSURE REFUELING / DEFUELING 2 EXTERNAL POWER SUPPLY 28 VDC 9 GROUNDING POINT (RIGHT MLG) 3 ENGINE AIR STARTING 10 CARGO DOOR 4 AIR CONDITIONING LOW PRESSURE 11 MAIN LANDING GEAR 5 WASTE SERVICING PANEL 12 NOSE LANDING GEAR 6 POTABLE WATER SERVICING PANEL 13 PASSENGER DOOR 7 OXYGEN REFILL / REPLACE BOTTLE 14 SERVICE DOOR EM170APM090007.DGN
Scale: 1 Inch Equals 50 Feet Figure 9.2
Section 9 EFFECTIVITY: ALL Page 9-3 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
12 1 14 13 7 10 3 4 9 11 8
6 10 11 13 14 2 5
0 5 10 15 20 25 m
0163248 64 80 ft
WING SPAN: 28.72 m (94 ft 3 in.)
ITEM DESCRIPTION ITEM DESCRIPTION 1 EXTERNAL POWER SUPPLY 115 VAC 8 PRESSURE REFUELING / DEFUELING 2 EXTERNAL POWER SUPPLY 28 VDC 9 GROUNDING POINT (RIGHT MLG) 3 ENGINE AIR STARTING 10 CARGO DOOR 4 AIR CONDITIONING LOW PRESSURE 11 MAIN LANDING GEAR 5 WASTE SERVICING PANEL 12 NOSE LANDING GEAR 6 POTABLE WATER SERVICING PANEL 13 PASSENGER DOOR 7 OXYGEN REFILL / REPLACE BOTTLE 14 SERVICE DOOR EM170APM090008.DGN
Scale: 1 Inch Equals 100 Feet Figure 9.3
Section 9 EFFECTIVITY: ALL Page 9-4 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
12
1 14 13 7 10
3 4
9 8
11 11
6 10
13 14
5 2
0 5 10 15 20 25 m
0326416 48 80 ft
WING SPAN: 28.72 m (94 ft 3 in.)
ITEM DESCRIPTION ITEM DESCRIPTION 1 EXTERNAL POWER SUPPLY 115 VAC 8 PRESSURE REFUELING / DEFUELING 2 EXTERNAL POWER SUPPLY 28 VDC 9 GROUNDING POINT (RIGHT MLG) 3 ENGINE AIR STARTING 10 CARGO DOOR 4 AIR CONDITIONING LOW PRESSURE 11 MAIN LANDING GEAR 5 WASTE SERVICING PANEL 12 NOSE LANDING GEAR 6 POTABLE WATER SERVICING PANEL 13 PASSENGER DOOR 7 OXYGEN REFILL / REPLACE BOTTLE 14 SERVICE DOOR EM170APM090009.DGN
Scale: 1 to 500 Figure 9.4
Section 9 EFFECTIVITY: ALL Page 9-5 Oct 07/13 w-apm1901 AIRPORT PLANNING MANUAL
12 1 14 13 7 10 3 4 11 9 8
11 6 10 13 14 2 5
0 5 10 15 20 25 50 m
0326416 48 80 ft
WING SPAN: 28.72 m (94 ft 3 in.)
ITEM DESCRIPTION ITEM DESCRIPTION 1 EXTERNAL POWER SUPPLY 115 VAC 8 PRESSURE REFUELING / DEFUELING 2 EXTERNAL POWER SUPPLY 28 VDC 9 GROUNDING POINT (RIGHT MLG) 3 ENGINE AIR STARTING 10 CARGO DOOR 4 AIR CONDITIONING LOW PRESSURE 11 MAIN LANDING GEAR 5 WASTE SERVICING PANEL 12 NOSE LANDING GEAR 6 POTABLE WATER SERVICING PANEL 13 PASSENGER DOOR 7 OXYGEN REFILL / REPLACE BOTTLE 14 SERVICE DOOR EM170APM090010.DGN
Scale: 1 to 1000 Figure 9.5
Section 9 EFFECTIVITY: ALL Page 9-6 Oct 07/13 w-apm1901