AIRPORT PLANNING MANUAL

Transcription

1 EMBRAER S.A - P.O. BOX SAO JOSE DOS CAMPOS - S.P. BRAZIL PHONE: FAX: distrib@embraer.com.br AIRPORT PLANNING MANUAL APM JULY 26 REVISION 8-18 FEBRUARY 213 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. Copyright 213 by EMBRAER S.A. All rights reserved.

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3 Title TRList 1... Oct 22/7 2 Blank... Oct 22/7 SBList 1... Jul 28/6 2 Blank... Jul 28/6 List of Effective Pages * 1 (rev)... Feb 18/13 * 2 (rev)... Feb 18/13 Table of Contents 1... Oct 31/ May 11/7 List of Tables 1... Oct 7/8 2 Blank... Jul 28/6 List of Figures 1... Oct 31/ Oct 31/ Oct 31/12 4 Blank... Oct 31/12 Section Jul 28/ Oct 6/11 1-2A... Oct 6/11 1-2B Blank... Oct 6/ Oct 7/8 1-4 Blank... Jul 28/6 Section Oct 6/ Oct 6/ Oct 7/ Oct 7/ Oct 7/ Oct 7/ Oct 7/ Oct 7/ Oct 7/ Oct 7/ Oct 6/ Oct 7/ Oct 7/ Oct 7/ Oct 6/ Blank... Oct 7/8 Section Jul 28/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/ Oct 31/12 Section Oct 7/ Oct 7/ Oct 7/ May 11/ Oct 7/ Oct 7/ Oct 7/ Oct 7/ Oct 7/ Oct 7/8 Section Jul 28/ May 11/ May 11/ Jul 28/ May 11/ Jul 28/ May 11/ May 11/ Oct 6/ Oct 6/ Oct 6/ Oct 6/ Oct 6/ Blank... Oct 6/11 Section Jul 28/6 Pages revised or added by the current revision are indicated by an asterisk (*). Pages deleted by the current revision are indicated by * (del). Pages deleted by the previous revision are indicated by (del). LIST OF EFFECTIVE PAGES REV. 8 Page 1 Feb 18/13

4 May 11/ Oct 7/ May 11/ May 11/ May 11/ May 11/ May 11/ Oct 22/ May 11/ Oct 7/ Blank... May 11/7 Section May 11/ Oct 7/ Oct 7/ Oct 7/ May 11/ May 11/ May 11/ May 11/ May 11/ May 11/ May 11/ May 11/ May 11/ May 11/ May 11/ Oct 6/ Oct 6/ Oct 6/ Oct 6/ Blank... Oct 6/11 Section Jul 28/6 8-2 Blank... Jul 28/6 Section Jul 28/ May 11/ May 11/ May 11/ May 11/ May 11/7 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). LIST OF EFFECTIVE PAGES REV. 8 Page 2 Feb 18/13

5 TABLE OF CONTENTS SECTION 1 - SCOPE 1. Scope Purpose Introduction Abbreviations SECTION 2 - AIRCRAFT DESCRIPTION 2. Aircraft Description Aircraft Characteristics General Aircraft Dimensions Ground Clearances Interior Arrangements Passenger Cabin Cross Section Lower Compartment Containers Door Clearances SECTION 3 - AIRCRAFT PERFORMANCE 3. Aircraft Performance General Information Payload X Range Takeoff Field Lenghts Landing Fields Lenghts SECTION 4 - GROUND MANEUVERING 4. Ground Maneuvering General Information Turning Radii Minimum Turning Radii Visibility From Cockpit Runway and Taxiway Dimensions Runway Holding Apron SECTION 5 - TERMINAL SERVICING 5. Terminal Servicing Aircraft Servicing Arrangement Terminal Operations - Turnaround Station Terminal Operations - En Route Station Ground Servicing Connections Engine Starting Pneumatic Requirements Ground Pneumatic Power Requirements Preconditioned Airflow Requirements Ground Towing Requirements TABLE OF CONTENTS Page 1 Oct 31/12

6 SECTION 6 - OPERATING CONDITIONS 6. Operating Conditions Engine Exhaust Velocities and Temperatures Airport and Community Noise Hazard Areas SECTION 7 - PAVEMENT DATA 7. Pavement Data General Information Footprint Maximum Pavement Loads Landing Gear Loading on Pavement Flexible Pavement Requirements, U.S. Corps of Engineers Design Method Flexible Pavement Requirements, LCN Method Rigid Pavement Requirements, Portland Cement Association Design Method Rigid Pavement Requirements, LCN Method ACN - PCN System - Flexible and Rigid Pavements SECTION 8 - POSSIBLE EMBRAER 195 DERIVATIVE AIRCRAFT 8. Possible EMBRAER 195 Derivative Aircraft Not Applicable SECTION 9 - SCALED DRAWINGS 9. Scaled Drawings General TABLE OF CONTENTS Page 2 May 11/7

7 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 INTRODUCTION The APM has been prepared in accordance with NAS 361. It provides aircraft characteristics for general airport planning, airport operators, airlines, and engineering consultant organizations. The APM is arranged as shown in the table below: Manual Front Matter Section ARRANGEMENTS Table APM Arrangement CONTENTS Title Page Costumer Comment Form Highlights Record of Revision Sheet Temporary Revision Sheet List of Service Bulletins List of Effective Pages Table of Contents List of Tables List of Figures Scope Aircraft Description Aircraft Performance Ground Maneuvering Terminal Servicing Operating Conditions Pavement Data Possible Derivative Aircraft Scaled Drawings The front matter for the whole manual contains: 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 Page 1-1 Jul 28/6

8 List of Service Bulletins: Lists the Service Bulletins, including all issued revisions, which affect the manual as well as the affected section(s) (APM Section Number), the aircraft affected by the Service Bulletin, and the date of incorporation of the SB in the manual. Temporary Revision Sheet: Lists the temporary revision numbers, page number, issue date, person responsible for the insertion and insertion date. List of Effective Pages: Lists all sections and their list of effective pages with the latest issue dates. Queries concerning any printed material, including purchasing, copying, shipping and handling, complaints, or compliments may be addressed to: Technical Publications Distribution: Embraer S.A. Attention of: Technical Publications Department P.O. BOX 85 CEP São José dos Campos - SP - Brazil Phone: (55 12) FAX: (55 12) distrib@embraer.com.br For support regarding technical information contained in non-operational publication, please contact: Routine Issues: Contact Embraer Customer Support Service AOG Issues: Contact Embraer AOG group directly For Digital Technical Publications support: cdrom.support@embraer.com.br 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 ABBREVIATIONS This list gives all the abbreviations, acronyms and measurement units used in this manual with their definitions. Table 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 Page 1-2 Oct 6/11

9 Table List of Acronyms and Abbreviations used in the APM ACRONYMS AND ABBREVIATIONS APM APU AR ATTCS BOW CBR ECS FAA FAR DESCRIPTION Airport Planning Manual Auxiliary Power Unit Advanced Range Automatic Takeoff-Thrust Control-System Basic Operating Weight California Bearing Ratio Environmental Control System Federal Aviation Administration Federal Aviation Regulations Section 1 Page 1-2A / 2B Oct 6/11

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11 Table List of Acronyms and Abbreviations used in the APM ACRONYMS AND ABBREVIATIONS FWD GEAE ICAO ISA JAR LCN LH LR MLW MRW MTOW MZFW N RBHA RH STD dba ft ft 2 ft 3 gal. in in 2 inhg kpa kg lb lb/in 3 lbf m m 2 m 3 min psi DESCRIPTION Forward General Electric Aircraft Engines International Civil Aviation Organization International Standard Atmosphere Joint Aviation Requirements Load Classification Number Left-Hand Long Range Maximum Landing Weight Maximum Ramp Weight Maximum Takeoff Weight Maximum Zero Fuel Weight Newton Requisitos Brasileiros de Homologação Aeronáutica Right-Hand Standard A-Weighted Decibel Foot Square Foot Cubic Foot Gallon Inch Square Inch Inch of Mercury Kilopascal Kilogram Pound Pound per Cubic Inch Pound Force Meter Square Meter Cubic Meter Minute Pounds per Square Inch Section 1 Page 1-3 / 4 Oct 7/8

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13 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 CF34-1 with 82.3 kn (185 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 4879 kg (17564 lb); The LR aircraft model - MTOW 579 kg ( lb); The AR aircraft model - MTOW 5229 kg (11528 lb) 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 emergency 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 Page 2-1 Oct 6/11

14 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 Aircraft General Characteristics DESIGN WEIGHTS [1] AIRCRAFT MODELS STD LR AR MRW 4895 kg (17916 lb) 595 kg ( lb) 5245 kg ( lb) MTOW 4879 kg (17564 lb) 579 kg ( lb) 5229 kg (11528 lb) MLW 45 kg (9928 lb) 458 kg (1972 lb) BOW [2] 287 kg (63273 lb) MZFW 425 kg (93696 lb) 426 kg (93917 lb) Maximum Payload [2] 138 kg (3424 lb) 139 kg (3644 lb) Maximum Seating Capacity 118 passengers Maximum Cargo Volume [3] 25.4 m 3 (897 ft 3 ) Usable Fuel [4] 131 kg (28881 lb) 1629 (4234 gal.) 1. Applicable for standard models. For further information, refer to AFM and AOM. 2. Standard configuration (weights may vary according to optional equipment installed or interior layouts). 3. Standard configuration (volume may vary according to optional equipment installed). 4. Adopted fuel density of.811 kg/ (6.77 lb/gal.) 2.2. GENERAL AIRCRAFT DIMENSIONS External Dimensions Span over winglets m (94 ft 3 in); Height (maximum) m (34 ft 7 in); Overall length m (126 ft 1 in). Section 2 Page 2-2 Oct 6/11

15 Wing Reference area m 2 (996 ft 2 ); Reference aspect ratio Fuselage Total Length m (126 ft 1 in); Length of pressurized section m (13 ft 4 in) Horizontal Tail Span m (39 ft 8 in); Area m 2 (28 ft 2 ) Vertical Tail Reference area m 2 (174 ft 2 54 in 2 ) Section 2 Page 2-3 Oct 7/8

16 6.82 m (45 ft 4 in) 26,98 m (88 ft 6 in) 1.57 m (34 ft 8 in.) m (48 ft) m (126 ft 1 in) 4.27 m (14 ft) 3.1 m (98 ft 5 in) 12.9 m (39 ft 8 in.) 4.71 m (15 ft 5.4in) 3.1 m (98 ft 5 in) 5.94 m (19 ft 6 in) m (94 ft 3 in.) EM17APM215B.DGN General Aircraft Dimensions Figure 2.1 Section 2 Page 2-4 Oct 7/8

17 2.3. GROUND CLEARANCES L A M B D G H J K C F E EM17APM219A.DGN Aircraft Ground Clearances Figure 2.2 Section 2 Page 2-5 Oct 7/8

18 WEIGHT 4895 kg lb 4895 kg lb 4879 kg lb 4879 kg lb 45 kg 9928 lb 45 kg 9928 lb 425 kg lb 425 kg lb 295 kg 6536 lb CG (%MAC) NOSE (A) 2.7 m 6ft9in 2.16 m 7ft1in 2.6 m 6ft9in 2.16 m 7ft1in 2.7 m 6ft9in 2.17 m 7ft2in 2.8 m 6ft9in 2.18 m 7ft2in 2.15 m 7ft1in 2.58 m 8ft5in 2.65 m 8ft8in 2.58 m 8ft5in 2.65 m 8ft8in 2.59 m 8ft6in 2.66 m 8ft9in 2.59 m 8ft6in 2.67 m 8ft9in 2.66 m 8ft9in Table Ground Clearance STD Aircraft Model NACELLE (E) WINGLET (F) AFT CARGO DOOR (H) AFT SERVICE DOOR (J) 2.59 m 8ft6in 2.66 m 8ft9in 2.59 m 8ft6in 2.66 m 8ft9in 2.6 m 8ft6in 2.67 m 8ft9in 2.6 m 8ft9in 2.68 m 8ft1in 2.67 m 8ft9in 1.57 m 5ft2in 1.62 m 5ft4in 1.57 m 5ft2in 1.62 m 5ft4in 1.58 m 5ft2in 1.63 m 5ft4in 1.58 m 5ft2in 1.64 m 5ft5in 1.65 m 5ft5in.49 m 1ft7in.5 m 1ft8in.49 m 1ft8in.5 m 1ft8in.5 m 1ft8in.51 m 1ft8in.51 m 1ft9in.52 m 1ft8in.57 m 1ft11in 5.8 m 16 ft 8 in 5.4 m 16 ft 6 in 5.8 m 16 ft 8 in 5.4 m 16 ft 6 in 5.9 m 16 ft 8 in 5.5 m 16 ft 7 in 5.1 m 16 ft 9 in 5.6 m 16 ft 7 in 5.16 m 16 ft 11 in 3.24 m 1 ft 7 in 3.24 m 1 ft 7 in 3.24 m 1 ft 7 in 3.24 m 1 ft 7 in 3.25 m 1 ft 8 in 3.25 m 1 ft 8 in 3.26 m 1 ft 8 in 3.26 m 1 ft 8 in 3.32 m 1 ft 11 in 2. m 6ft7in 1.94 m 6ft4in 2. m 6ft7in 1.94 m 6ft4in 2.1 m 6ft7in 1.95 m 6ft5in 2.2 m 6ft8in 1.96 m 6ft5in 2.8 m 6ft1in 3.3 m 9ft11in 2.96 m 9ft9in 3.4 m 1 ft 2.96 m 9ft9in 3.5 m 9ft2in 2.97 m 9ft9in 3.6 m 1 ft 2.98 m 9ft9in 3.12 m 1 ft 3 in 3.3 m 9ft11in 2.96 m 9ft9in 3.4 m 1 ft 2.96 m 9ft9in 3.5 m 9ft2in 2.97 m 9ft9in 3.6 m 1 ft 2.98 m 9ft9in 3.12 m 1 ft 3 in FOR- WARD SERVICE DOOR (B) FOR- WARD PASSEN- GER DOOR (C) FOR- WARD CARGO DOOR (D) EMER- GENCY EXIT (G) AFT PASSEN- GER DOOR (K) VERTI- CAL TAIL (L) 1.41 m 34 ft 2 in 1.3 m 33 ft 1 in 1.41 m 34 ft 2 in 1.3 m 33 ft 1 in 1.43 m 34 ft 3 in 1.31m 33 ft 1 in 1.45 m 34 ft 3 in 1.32 m 33 ft 1 in 1.49 m 34 ft 5 in TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (M) Section 2 Page 2-6 Oct 7/8

19 WEIGHT 595 kg lb 595 kg lb 579 kg lb 579 kg lb 45 kg 9928 lb 45 kg 9928 lb 425 kg lb 425 kg lb 295 kg 6536 lb CG (%MAC) NOSE (A) 2.7 m 6ft9in 2.16 m 7ft1in 2.7 m 6ft9in 2.16 m 7ft1in 2.7 m 6ft9in 2.17 m 7ft2in 2.8 m 6ft9in 2.18 m 7ft2in 2.15 m 7ft1in 2.58 m 8ft5in 2.65 m 8ft8in 2.58 m 8ft5in 2.65 m 8ft8in 2.59 m 8ft6in 2.66 m 8ft9in 2.59 m 8ft6in 2.67 m 8ft9in 2.66 m 8ft9in Table Ground Clearance LR Aircraft Model NACELLE (E) WINGLET (F) AFT CARGO DOOR (H) 2.59 m 8ft6in 2.65 m 8ft8in 2.59 m 8ft6in 2.65 m 8ft8in 2.6 m 8ft6in 2.67 m 8ft9in 2.6 m 8ft9in 2.68 m 8ft1in 2.67 m 8ft9in 1.57 m 5 ft2 in 1.62 m 5 ft4 in 1.57 m 5ft2in 1.62 m 5ft4in 1.58 m 5ft2in 1.63 m 5ft4in 1.58 m 5ft2in 1.64 m 5ft5in 1.65 m 5ft5in.48 m 1ft7in.49 m 1ft7in.48 m 1ft7in.5 m 1ft8in.5 m 1ft8in.51 m 1ft8in.51 m 1ft9in.52 m 1ft8in.57 m 1ft11in 5.7 m 16 ft 8 in 5.3 m 16 ft 6 in 5.7 m 16 ft 8 in 5.3 m 16 ft 6 in 5.9 m 16 ft 8 in 5.5 m 16 ft 7 in 5.1 m 16 ft 9 in 5.6 m 16 ft 7 in 5.16 m 16 ft 11 in 3.23 m 1 ft 7 in 3.23 m 1 ft 7 in 3.23 m 1 ft 7 in 3.24 m 1 ft 7 in 3.25 m 1 ft 8 in 3.25 m 1 ft 8 in 3.26 m 1 ft 8 in 3.26 m 1 ft 8 in 3.32 m 1 ft 11 in 1.98 m 6ft6in 1.93 m 6ft4in 1.98 m 6ft6in 1.93 m 6ft4in 2.1 m 6ft7in 1.95 m 6ft5in 2.2 m 6ft8in 1.96 m 6ft5in 2.8 m 6ft1in AFT SERVICE DOOR (J) 3.2 m 9ft11in 2.95 m 9ft8in 3.2 m 9ft11in 2.95 m 9ft8in 3.5 m 9ft2in 2.97 m 9ft9in 3.6 m 1 ft 2.98 m 9ft9in 3.12 m 1 ft 3 in 3.2 m 9ft11in 2.95 m 9ft8in 3.2 m 9ft11in 2.95 m 9ft8in 3.5 m 9ft2in 2.97 m 9ft9in 3.6 m 1 ft 2.98 m 9ft9in 3.12 m 1 ft 3 in FOR- WARD SERVICE DOOR (B) FOR- WARD PASSEN- GER DOOR (C) FOR- WARD CARGO DOOR (D) EMER- GENCY EXIT (G) AFT PASSEN- GER DOOR (K) VERTI- CAL TAIL (L) 1.4 m 34 ft 2 in 1.29 m 33 ft 9 in 1.4 m 34 ft 2 in 1.29 m 33 ft 9 in 1.43 m 34 ft 3 in 1.31 m 33 ft 1 in 1.45 m 34 ft 3 in 1.32 m 33 ft 1 in 1.49 m 34 ft 5 in TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (M) Section 2 Page 2-7 Oct 7/8

20 WEIGHT 5245 kg lb 5245 kg lb 5229 kg lb 5229 kg lb 458 kg 1972 lb 458 kg 1972 lb 426 kg lb 426 kg lb 295 kg 6536 lb CG (%MAC) NOSE (A) 2.7 m 6ft9in 2.15 m 7ft1in 2.7 m 6ft9in 2.15 m 7ft1in 2.7 m 6ft9in 2.17 m 7ft2in 2.8 m 6ft9in 2.18 m 7ft2in 2.15 m 7ft1in 2.58 m 8ft5in 2.64 m 8ft8in 2.58 m 8ft5in 2.64 m 8ft8in 2.59 m 8ft6in 2.65 m 8ft8in 2.59 m 8ft6in 2.67 m 8ft9in 2.66 m 8ft9in Table Ground Clearance AR Aircraft Model NACELLE (E) WINGLET (F) AFT CARGO DOOR (H) 2.59 m 8ft6in 2.65 m 8ft8in 2.59 m 8ft6in 2.65 m 8ft8in 2.59 m 8ft6in 2.67 m 8ft9in 2.6 m 8ft9in 2.67 m 8 ft9 in 2.67 m 8ft9in 1.57 m 5 ft2 in 1.62 m 5ft4in 1.57 m 5ft2in 1.61 m 5ft3in 1.58 m 5ft2in 1.63 m 5ft4in 1.58 m 5ft2in 1.64 m 5ft5in 1.65 m 5ft5in.48 m 1ft7in.49 m 1ft7in.48 m 1ft7in.49 m 1ft7in.5 m 1ft8in.51 m 1ft8in.51 m 1ft8in.52 m 1ft8in.57 m 1ft11in 5.6 m 16 ft 7 in 5.3 m 16 ft 6 in 5.6 m 16 ft 7 in 5.3 m 16 ft 6 in 5.9 m 16 ft 8 in 5.5 m 16 ft 7 in 5.1 m 16 ft 9 in 5.6 m 16 ft 7 in 5.16 m 16 ft 11 in 3.23 m 1 ft 7 in 3.23 m 1 ft 7 in 3.23 m 1 ft 7 in 3.23 m 1 ft 7 in 3.25 m 1 ft 8 in 3.25 m 1 ft 8 in 3.26 m 1 ft 8 in 3.26 m 1 ft 8 in 3.32 m 1 ft 11 in 1.98 m 6ft6in 1.93 m 6ft4in 1.98 m 6ft6in 1.93 m 6ft4in 2. m 6ft7in 1.95 m 6ft5in 2.2 m 6ft8in 1.96 m 6ft5in 2.8 m 6ft1in AFT SERVICE DOOR (J) 3.1 m 9ft11in 2.95 m 9ft8in 3.1 m 9ft11in 2.95 m 9ft8in 3.5 m 1 ft 2.97 m 9ft9in 3.6 m 1 ft 2.98 m 9ft9in 3.12 m 1 ft 3 in 3.1 m 9ft11in 2.95 m 9ft8in 3.1 m 9ft11in 2.95 m 9ft8in 3.5 m 1 ft 2.97 m 9ft9in 3.6 m 1 ft 2.98 m 9ft9in 3.12 m 1 ft 3 in FOR- WARD SERVICE DOOR (B) FOR- WARD PASSEN- GER DOOR (C) FOR- WARD CARGO DOOR (D) EMER- GENCY EXIT (G) AFT PASSEN- GER DOOR (K) VERTI- CAL TAIL (L) 1.38 m 34 ft 1 in 1.28 m 33 ft 9 in 1.38 m 34 ft 1 in 1.28 m 33 ft 9 in 1.43 m 34 ft 3 in 1.31 m 33 ft 1 in 1.45 m 34 ft 3 in 1.32 m 33 ft 1 in 1.49 m 34 ft 5 in TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (M) Section 2 Page 2-8 Oct 7/8

21 2.4. INTERIOR ARRANGEMENTS The interior arrangement provides accommodation for two pilots, one observer, three flight attendants, and 18 passengers in 32 in pitch standard configuration. One additional flight attendant seat is available as an option. Section 2 Page 2-9 Oct 7/8

22 m (2 ft 11.4 in.) m (2 ft 1 in.).78 m (2 ft 6.7 in.) 1.82 m (5 ft 11 in.) 5.72 m (18 ft 9.2 in.) 8.64 m (28 ft 4.16 in.) 5.95 m (19 ft 6.3 in.) 8.8 m (28 ft 1.5 in.) 1.86 m (6 ft 4 in.) 32.5 m (15 ft 1.8 in) m (2 ft 7.1 in.) m (3 ft 11.6 in.) FLIGHT ATTENDANT SEAT 2 FWD RH LAVATORY 3 FWD RH G1 GALLEY 4 FWD RH G2 GALLEY 5 AFT RH GALLEY 6 AIRSTAIRS WARDROBE 7 AFT LAVATORY 8 CARGO COMPARTMENT 9 OVERHEAD BIN 1 PASSENGER SEAT CARGO/BAGGAGE VOLUME 3 3 CARGO COMPARTMENT m (96.17 ft ) 3 3 OVERHEAD BIN.6 m / pax (2. ft / pax) 3 3 UNDERSEAT VOLUME.4 m / pax (1.4 ft / pax) EM17APM22B.DGN Interior Arrangements Figure 2.3 Section 2 Page 2-1 Oct 7/8

23 Passenger Cabin The passenger cabin accommodates 18 passengers in 27 double seats on both sides. 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. m (6 ft 7 in) Width m (9 ft) Aisle wide -.49 m (1 ft 7 in) Pitch -.82 m (32 in) 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 classification. The table below contain the capacity for the cargo compartment: Table Capacity for the Cargo Compartment CARGO COMPARTMENT LOADING VOLUME FWD [1] 19 kg (4189 lb) 12.7 m 3 ( ft 3 ) Aft 18 kg (3968 lb) 12.7 m 3 ( ft 3 ) Total 37 kg (8157 lb) 25.4 m 3 (897.7 ft 3 ) 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 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 Page 2-11 Oct 6/11

24 2.5. PASSENGER CABIN CROSS SECTION.78 m (2 ft 7 in.) 2. m (6 ft 7 in.).46 m (1 ft 6 in.).5 m (2. in.) 1.44 m (4 ft 9 in.) 3.35 m (11 ft in.).49 m (1 ft 7 in.).94 m (3 ft 1 in.).45 m (1 ft 6 in.) 1.66 m (5 ft 5 in.) 2.72 m (8 ft 11 in.).75 m (2 ft 5 in.) 2.74 m (9 ft) 3.1 m (9 ft 11 in.) EM17APM21A.DGN Economy Class Passenger Cabin Cross-Section Figure 2.4 Section 2 Page 2-12 Oct 7/8

25 .86 m (3 ft) 2. m (6 ft 7 in.).6 m (1 ft 1 in.).69 m (2 ft 3 in.) 3.35 m (11 ft in.) 1.44 m (4 ft 9 in.).2 m (8 in.).51 m (1 ft 8 in.).7 m (3 in.).61 m (2 ft) 1.1 m (3 ft 8 in.).94 m (3 ft 1 in.).45 m (1 ft 6 in.) 1.66 m (5 ft 5 in.) 2.72 m (8 ft 11 in.).75 m (2 ft 5 in.) 2.74 m (9 ft) 3.1 m (9 ft 11 in.) EM17APM22A.DGN First Class Passenger Cabin Cross-Section Figure 2.5 Section 2 Page 2-13 Oct 7/8

26 2.6. LOWER COMPARTMENT CONTAINERS Not Applicable Section 2 Page 2-14 Oct 7/8

27 2.7. DOOR CLEARANCES 1.36 m (4 ft 5.5 in.) 1.82 m (5 ft 11.6 in.).98 m (3 ft 2.6 in.) 1.37 m (4 ft 5.9 in.) 1.71 m (5 ft 7.3 in.).9 m (2 ft 11.4 in.).87 m (2 ft 1 in.).78 m (2 ft 6.7 in.) SEE FIGURE 2.2 FOR HEIGHT ABOVE GROUND 1.1 m (3 ft 7.3 in.).99 m (3 ft 3 in.).61 m (2 ft).53 m (1 ft 8.9 in.).63 m (2 ft.8 in.).75 m (2 ft 6.7 in.).53 m (1 ft 8.9 in.).63 m (2 ft.8 in.) NOTE: FOR DIMENSIONS OF ALL DOORS, CONSIDER THAT AIRCRAFT IS IN OPERATION, THAT IS, EQUIPPED WITH DOOR LININGS AND DOOR SURROUNDS. EM17APM214C.DGN Door Dimensions Figure 2.6 Section 2 Page 2-15 / 16 Oct 6/11

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29 3. AIRCRAFT PERFORMANCE 3.1. GENERAL INFORMATION The performance of the aircraft and engine depends on the generation of forces by the interaction between the aircraft or engine and the air mass through which it flies. The atmosphere has a pronounced effect on the temperature, pressure and density of the air. The ICAO estabilishes 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 ( K) Standard Pressure Po = 11.3 kpa (29.92 inhg) Standard Density ρo =.2377 slug per cubic feet 2. ISA Table ISA ALTITUDE TEMPERATURE m ft C F NOTE: NOTE: The performance data shown in this section must not be used for operations. 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, landing field lengths and/or takeoff field lengths with conditions different from those presented in this section, Embraer should be contacted so that these charts can be obtained. Section 3 Page 3-1 Jul 28/6

30 3.2. PAYLOAD X RANGE The Payload x Range charts are based on the following conditions: CF34-1E engine models; Aircraft carrying passengers at 1 kg (22 lb) each one; Flight level 35, that represents the cruising altitude equal to 1668 m (35 ft); Atmosphere acording to ISA and ISA + 1 C conditions; MTOW. Section 3 Page 3-2 Oct 31/12

31 PAYLOAD VS RANGE CF34 1E7, 1E6A1, 1E6A, 1E5A1 & 1E5A ENGINES FLIGHT LEVEL 35 ISA RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 4879 kg (17564 lb) kg PAYLOAD lb PAYLOAD kg MAX CRUISE.78 MACH LONG RANGE RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 4879 kg (17564 lb) 425 kg (93696 lb) 287 kg (63273 lb) 131 kg (2888 lb) EM17APM348B.DGN Payload x Range - ISA Conditions Figure 3.1 EFFECTIVITY: EMBRAER 195 STD ACFT MODEL Section 3 Page 3-3 Oct 31/12

32 PAYLOAD VS RANGE CF34 1E7, 1E6A1, 1E6A, 1E5A1 & 1E5A ENGINES FLIGHT LEVEL 35 ISA + 1 C RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 4879 kg (17564 lb) kg PAYLOAD lb PAYLOAD kg MAX CRUISE.78 MACH LONG RANGE RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 4879 kg (17564 lb) 425 kg (93696 lb) 287 kg (63273 lb) 131 kg (2888 lb) EM17APM349B.DGN Payload x Range - ISA + 1 C Conditions Figure 3.2 EFFECTIVITY: EMBRAER 195 STD ACFT MODEL Section 3 Page 3-4 Oct 31/12

33 PAYLOAD VS RANGE CF34 1E7, 1E6A1, 1E6A, 1E5A1 & 1E5A ENGINES FLIGHT LEVEL 35 ISA RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 579 kg ( lb) kg PAYLOAD lb PAYLOAD kg MAX CRUISE.78 MACH LONG RANGE RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 579 kg ( lb) 425 kg (93696 lb) 287 kg (63273 lb) 131 kg (2888 lb) EM17APM35B.DGN Payload x Range - ISA Conditions Figure 3.3 EFFECTIVITY: EMBRAER 195 LR ACFT MODEL Section 3 Page 3-5 Oct 31/12

34 PAYLOAD VS RANGE CF34 1E7, 1E6A1, 1E6A, 1E5A1 & 1E5A ENGINES FLIGHT LEVEL 35 ISA + 1 C RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 579 kg ( lb) kg PAYLOAD lb PAYLOAD kg MAX CRUISE.78 MACH LONG RANGE RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 579 kg ( lb) 425 kg (93696 lb) 287 kg (63273 lb) 131 kg (2888 lb) EM17APM351B.DGN Payload x Range - ISA + 1 C Conditions Figure 3.4 EFFECTIVITY: EMBRAER 195 LR ACFT MODEL Section 3 Page 3-6 Oct 31/12

35 PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 5229 kg (11528 lb) kg PAYLOAD lb PAYLOAD kg MAX CRUISE.78 MACH LONG RANGE RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 5229 kg (11528 lb) 426 kg (93917 lb) 287 kg (63273 lb) 131 kg (28881 lb) EM17APM321A.DGN Payload x Range - ISA Conditions Figure 3.5 EFFECTIVITY: EMBRAER 195 AR ACFT MODEL Section 3 Page 3-7 Oct 31/12

36 PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA+1 RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 5229 kg (11528 lb) kg PAYLOAD lb PAYLOAD kg MAX CRUISE LONG RANGE MACH RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 5229 kg (11528 lb) 426 kg (93917 lb) 287 kg (63273 lb) 131 kg (28881 lb) EM17APM322A.DGN Payload x Range - ISA + 1 C Conditions Figure 3.6 EFFECTIVITY: EMBRAER 195 AR ACFT MODEL Section 3 Page 3-8 Oct 31/12

37 3.3. TAKEOFF FIELD LENGHTS 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 is presented according to the following associated conditions: CF34-1E engine models; Takeoff Mode: 1; ATTCS positioning: ON and OFF; Flaps setting position: 1, 2, 3 and 4; Pavement conditions: dry, hard paved and level runway surface with no obstacles; Zero wind and atmosphere according to ISA and ISA + 1 C conditions; Takeoff safety speed - V 2 equal to 1.2 Vs; Pack OFF: No engine bleed extraction for air conditioning packs was considered in the takeoff and landing charts. Section 3 Page 3-9 Oct 31/12

38 TAKEOFF FIELD LENGTH CF 34 1E5A1, 1E6A1 & 1E7 T/O 1 MODE ATTCS: OFF / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 4 ISA AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft FIELD LENGTH m FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM352B.DGN Takeoff Field Lengths - ISA Conditions Figure 3.7 Section 3 Page 3-1 Oct 31/12

39 TAKEOFF FIELD LENGTH CF 34 1E5A1, 1E6A1 & 1E7 T/O 1 MODE ATTCS: OFF / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 4 ISA + 15 C AIRPORT PRESSURE ALTITUDE m (ft) 1 FIELD LENGTH ft FIELD LENGTH m FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM353B.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.8 Section 3 Page 3-11 Oct 31/12

40 TAKEOFF FIELD LENGTH CF 34 1E5 & 1E6 T/O 1 MODE ATTCS: ON / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 4 ISA AIRPORT PRESSURE ALTITUDE m (ft) 1 8 FIELD LENGTH ft FIELD LENGTH m FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM354B.DGN Takeoff Field Lengths - ISA Conditions Figure 3.9 Section 3 Page 3-12 Oct 31/12

41 TAKEOFF FIELD LENGTH CF 34 1E5 & 1E6 T/O 1 MODE ATTCS: ON / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 4 ISA+15 C AIRPORT PRESSURE ALTITUDE m (ft) 1 8 FIELD LENGTH ft FIELD LENGTH m FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM355B.DGN Takeoff Field Lengths - ISA Conditions + 15 C Conditions Figure 3.1 Section 3 Page 3-13 Oct 31/12

42 TAKEOFF FIELD LENGTH CF34 1E5 & 1E6 T/O 1 MODE ATTCS: OFF / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 4 ISA AIRPORT PRESSURE ALTITUDE m (ft) 1 8 FIELD LENGTH ft FIELD LENGTH m FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM356B.DGN Takeoff Field Lengths - ISA Conditions Figure 3.11 Section 3 Page 3-14 Oct 31/12

43 TAKEOFF FIELD LENGTH CF 34 1E5 & 1E6 T/O 1 MODE ATTCS: OFF / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 4 ISA + 15 C AIRPORT PRESSURE ALTITUDE m (ft) 1 8 FIELD LENGTH ft FIELD LENGTH m FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM357C.DGN Takeoff Field Lengths - ISA Conditions + 15 C Conditions Figure 3.12 Section 3 Page 3-15 Oct 31/12

44 TAKEOFF FIELD LENGTH CF34 1E7 T/O 1 MODE ATTCS: ON / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 4 ISA AIRPORT PRESSURE ALTITUDE m (ft) 1 FIELD LENGTH ft FIELD LENGTH m FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM327A.DGN Takeoff Field Lengths - ISA Conditions Figure 3.13 Section 3 Page 3-16 Oct 31/12

45 TAKEOFF FIELD LENGTH CF 34 1E7 T/O 1 MODE ATTCS: ON / ECS: OFF DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 4 ISA+15 C AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft FIELD LENGTH m FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM312A.DGN Takeoff Field Lengths - ISA Conditions + 15 C Figure 3.14 Section 3 Page 3-17 Oct 31/12

46 3.4. LANDING FIELDS LENGHTS 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 and full; Pavement conditions: dry, hard paved and level runway surface with no obstacles; Zero wind and atmosphere according to ISA conditions; Bleed open; Pack OFF: No engine bleed extraction for air conditioning packs was considered in the takeoff and landing charts. Section 3 Page 3-18 Oct 31/12

47 LANDING FIELD LENGTH CF34 1E5, 1E5A1, 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 5 ISA 2 19 PRESSURE ALTITUDE (ft) LAND FIELD LENGTH ft 5 LAND FIELD LENGTH m WEIGHT kg WEIGHT lb EM17APM358B.DGN Landing Field Lengths - Flaps 5 Figure 3.15 Section 3 Page 3-19 Oct 31/12

48 LANDING FIELD LENGTH CF34 1E5, 1E5A1, 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP FULL ISA PRESSURE ALTITUDE (ft) LAND FIELD LENGTH ft LAND FIELD LENGTH m WEIGHT kg WEIGHT lb EM17APM359B.DGN Landing Field Lengths - Flaps Full Figure 3.16 Section 3 Page 3-2 Oct 31/12

49 LANDING FIELD LENGTH CF34 1E7 ENGINE DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP 5 ISA 2 19 PRESSURE ALTITUDE (ft) LAND FIELD LENGTH ft 5 LAND FIELD LENGTH m WEIGHT kg WEIGHT lb EM17APM313A.DGN Landing Field Lengths - Flaps 5 Figure 3.17 Section 3 Page 3-21 Oct 31/12

50 LANDING FIELD LENGTH CF34 1E7 ENGINE DRY, SMOOTH, HARD PAVED AND LEVELLED RUNWAY FLAP FULL ISA PRESSURE ALTITUDE m (ft) 16 1 LAND FIELD LENGTH ft 5 LAND FIELD LENGTH m WEIGHT kg WEIGHT lb EM17APM314A.DGN Landing Field Lengths - Flaps Full Figure 3.18 Section 3 Page 3-22 Oct 31/12

51 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 determination of 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 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 18 turn. Section 4 Page 4-1 Oct 7/8

52 R = m (61 ft 1 in) R = 21.9 m (71 ft 1 in) R = 6.66 m (21 ft 1 in) 76 R = m (62 ft 9 in) R = 15.1 m (49 ft 7 in) R = 7.29 m (23 ft 11 in) m (74 ft 5 in) RUNWAY MINIMUM WIDTH R = m (5 ft 6 in) NOTE: ACTUAL OPERATING DATA MAY BE GREATER THAN VALUES SHOWN SINCE TIRE SLIPPAGE IS NOT CONSIDERED IN THESE CALCULATIONS. 1 THEORETICAL CENTER OF TURN FOR MINIMUN RADIUS. SHOWS CONTINUOUS TURNING WITH ENGINE THRUST AS REQUIRED. NO DIFFERENTIAL BRAKING. EM17APM415B.DGN Turning Radii - No Slip Angle Figure 4.1 Section 4 Page 4-2 Oct 7/8

53 4.3. MINIMUM TURNING RADII R 5 R 6 R = 6.66 m (21 ft 1 in) m (74 ft 5 in) RUNWAY MINIMUM WIDTH R = 15.1 m (49 ft 7 in) R 3 R 4 R 1 R 2 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 STEEL R 1 R 2 R 3 R 4 R m (92 ft 9 in) m (85 ft) m (81 ft 2 in) m (57 ft 6 in) m (117 ft 4 in) m (84 ft 6 in) m (75 ft 11 in) m (69 ft 8 in) 14.2 m (46 ft) m (16 ft) m (78 ft 5 in) 21.6 m (69 ft 1 in) 18.4 m (6 ft 4 in) m (36 ft 8 in) 29.5 m (96 ft 9 in) m (73 ft 1 in) m (63 ft 1 in) 16.2 m (52 ft 7 in) 8.8 m (28 ft 1 in) m (89 ft 1 in) m (7 ft 4 in) 18.2 m (59 ft 9 in) m (45 ft 1 in) 6.75 m (22 ft 2 in) m (82 ft 5 in) m (67 ft 8 in) m (56 ft 6 in) m (39 ft 1 in) 4.93 m (16 ft 2 in) m (76 ft 7 in) m (65 ft 7 in) m (54 ft) 1.5 m (34 ft 5 in) 3.29 m (1 ft 1 in) m (71 ft 4 in) m (64 ft 1 in) m (52 ft 2 in) 8.99 m (29 ft 6 in) 1.78 m (5 ft 1 in) 2.25 m (66 ft 5 in) m (62 ft 9 in) m (5 ft 6 in) 7.29 m (23 ft 11 in).8 m (3 in) m (61 ft 1 in) RIGHT TAILTIP R m (19 ft 11 in) 3.75 m (1 ft 11 in) m (93 ft 11 in) m (88 ft 5 in) m (83 ft 11 in) m (8 ft 3 in) m (77 ft 2 in) m (74 ft 6 in) 21.9 m (71 ft 1 in) EM17APM416B.DGN Minimum Turning Radius Figure 4.2 Section 4 Page 4-3 Oct 7/8

54 4.4. VISIBILITY FROM COCKPIT VISUAL ANGLE IN PLANE PARALLEL TO LONGITUDINAL AXIS THROUGH PILOT S EYE POSITION 3.91 m (12 ft 1 in.) CL FUS HOR PILOT S EYE POSITION.75 m (2 ft 6 in.) m (47 ft 1 in.) 2.92 m (9 ft 7 in.) REF. GROUND (BOW) MAXIMUM AFT VISION WITH HEAD ROTATED ABOUT SPINAL COLUMN PILOT S EYE POSITION.53 m (1 ft 9 in.) 12.6 VISUAL ANGLE IN PLANE PERPENDICULAR TO LONGITUDINAL AXIS THROUGH PILOT S EYE POSITION.53 m (1 ft 9 in.) PILOT S EYE POSITION EM17APM41.DGN Visibility from Cockpit in Static Position Figure 4.3 Section 4 Page 4-4 May 11/7

55 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 Reference Codes CODE ELEMENT 1 CODE ELEMENT 2 CODE AIRCRAFT REFERENCE CODE OUTER MAIN LANDING WING SPAN NUMBER FIELD LENGTH LETTER GEAR WHEEL SPAN 1 less than 8 m Up to 15 m Up to 4.5 m A (2624 ft 8 in) (49 ft 3 in) (14 ft 9 in) 2 8 m (2624 ft 8 in) up to 15 m (49 ft 3 in) to 4.5 m (14 ft 9 in) to B 12 m (3937 ft) 24 m (78 ft 9 in) 6 m (19 ft 8 in) 3 12 m (3937 ft) up to 24 m (78 ft 9 in) to 6 m (19 ft 8 in) to C 18 m (595 ft 6 in) 36m(118ft1in) 9 m (29 ft 6 in) 4 18 m 36m(118ft1in)to 9 m (29 ft 6 in) to D (595 ft 6 in) and over 52 m (17 ft 7 in) 14 m (45 ft 11 in) 5 _ E 52 m (17 ft 7 in) to 9 m (29 ft 6 in) to 65 m (213 ft 3 in) 14 m (45 ft 11 in) In accordance with the table, the reference code for the EMBRAER 195STD and 195LR is 3C and the reference code for the EMBRAER 195AR is 4C. NOTE: Classification considering CF34-1E7 engines. This classification may change depending on aircraft engine model and takeoff weight. With the reference code it is possible to obtain the limits of the runway and taxiway where the aircraft can be operated. For reference code 3C the limits are: The width of a runway should be not less than 3 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 than 3m(9ft1in); The clearance between a parked aircraft and one moving along the taxiway in a holding bay should not be less than 15 m (49 ft 3 in). For reference code 4C the limits are: The width of a runway should be not less than 45 m (147 ft 7.6 in); Section 4 Page 4-5 Oct 7/8

56 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 than 3m(9ft1in); The clearance between a parked aircraft and one moving along the taxiway in a holding bay should not be less than 15 m (49 ft 3 in). Section 4 Page 4-6 Oct 7/8

57 3 m (98 ft 5 in.) NOTE: COORDINATE WITH AIRLINE OPERATOR FOR THE SPECIFIC PLANNED OPERATING PROCEDURE. 45 NOSE LANDING GEAR STEERING ANGLE IS APPROXIMATELY ft RADIUS (3 m) 15 m (49 ft 2 in.) PATH OF MAIN LANDING GEAR TIRE EDGE EM17APM417A.DGN More than 9 Turn - Runway to Taxiway Figure 4.4 Section 4 Page 4-7 Oct 7/8

58 3 m (98 ft 5 in.) NOTE: COORDINATE WITH AIRLINE OPERATOR FOR THE SPECIFIC PLANNED OPERATING PROCEDURE. NOSE LANDING GEAR STEERING ANGLE IS APPROXIMATELY 3. 1 ft RADIUS (3 m) 9 15 m (49 ft 2 in.) 1 ft RADIUS (3 m) PATH OF MAIN LANDING GEAR TIRE EDGE. EM17APM418A.DGN 9 Turn - Runway to Taxiway Figure 4.5 Section 4 Page 4-8 Oct 7/8

59 15 m (49 ft 2 in.) NOTE: COORDINATE WITH AIRLINE OPERATOR FOR THE SPECIFIC PLANNED OPERATING PROCEDURE. NOSE LANDING GEAR STEERING ANGLE IS APPROXIMATELY m (49 ft 2 in.) 1 ft Radius (3 m) 3 m (9 ft 1 in.) PATH OF MAIN LANDING GEAR TIRE EDGE. EM17APM419A.DGN 9 Turn - Taxiway to Taxiway Figure 4.6 Section 4 Page 4-9 Oct 7/8

60 4.6. RUNWAY HOLDING APRON RUNWAY 3 m (98 ft 5 in.) MINIMUM CLEARANCES 15 m (49 ft 2 in.) 75 m (246 ft) 3 m (9 ft 1 in.) 3 m (9 ft 1 in.) PATH OF MAIN LANDING GEAR TIRE EDGE. PATH OF MAIN LANDING GEAR TIRE EDGE. 15 m (49 ft 2 in.) TAXIWAY EM17APM42A.DGN Runway Holding Bay Figure 4.7 Section 4 Page 4-1 Oct 7/8

61 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 Page 5-1 Jul 28/6

62 5.1. AIRCRAFT SERVICING ARRANGEMENT LENGTH ft 6 5 LENGTH m LENGTH m LENGTH ft SERVICING ARRANGEMENT 1 PASSENGER STAIRS 2 BAGGAGE LOADER 3 BAGGAGE / CARGO 4 GALLEY SERVICE 5 FUEL SERVICE 6 POTABLE WATER 7 LAVATORY SERVICE 8 PASSENGER BRIDGE EM17APM515A.DGN Aircraft Servicing Arrangement With Passenger Bridge Figure 5.1 Section 5 Page 5-2 May 11/7

63 LENGTH ft 6 5 LENGTH m LENGTH m LENGTH ft SERVICING ARRANGEMENT 1 PASSENGER STAIRS 2 BAGGAGE LOADER 3 BAGGAGE / CARGO 4 GALLEY SERVICE 5 FUEL SERVICE 6 POTABLE WATER 7 LAVATORY SERVICE 8 AIR CONDITIONING 9 PNEUMATIC STARTER EM17APM516A.DGN Aircraft Servicing Arrangement With Passenger Stairs Figure 5.2 Section 5 Page 5-3 May 11/7

64 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 - 1%; Passenger deplane - 24 pax/min; Passenger enplane - 16 pax/min; Baggages checked per passenger - 1,2; Refuel (fuel quantity) - 8%; Flow - 29 gpm; Potable water - 7% 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 Page 5-4 Jul 28/6

65 ELAPSED TIME (MINUTES) OPERATIONS min. BRIDGE / STAIRS POSITIONING 1, PASSENGERS DEPLANE 4.5 PAX SERVICES GALLEY SERVICING FWD GALLEY SERVICING AFT AIRPLANE INTERIOR SERVICES PASSENGERS ENPLANE 7, 7, BRIDGE / STAIRS REMOVAL 1, PUSH BACK / ENGINES START 2, FWD BAGGAGE / CARGO UNLOAD 4.4 BAGGAGE & CARGO REAR BAGGAGE / CARGO UNLOAD TIME BETWEEN UNLOADING / LOADING FWD BAGGAGE/CARGO LOAD AFT BAGGAGE/CARGO LOAD 4.2, AIRCRAFT SERVICING FUEL SERVICE POTABLE WATER SERVICE TOILET SERVICE , 5, 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. EM17APM517B.DGN Air Terminal Operation - Turnaround Station Figure 5.3 Section 5 Page 5-5 May 11/7

66 5.3. TERMINAL OPERATIONS - EN ROUTE STATION Not Applicable Section 5 Page 5-6 Jul 28/6

67 5.4. GROUND SERVICING CONNECTIONS ITEM DESCRIPTION PRESSURE REFUELING PANEL GRAVITY REFUELING PORT (RH) GRAVITY REFUELING PORT (LH) FORWARD RAMP HEADSET STEERING SWITCH DISENGAGE WHEEL JACK POINT NLG AIR COND. GROUND CONNECTION ENGINE AIR STARTING (LOW PRESSURE UNIT) GROUNDING POINT (ELECTRICAL) WHEEL JACK POINT MLG (RH) WHEEL JACK POINT MLG (LH) HYD. SYS # 1 SERVICE PANEL WATER SERVICING PANEL EXTERNAL POWER SUPPLY 28 VDC / 4A AFT RAMP HEADSET OXYGEN SERVICING PANEL / BOTTLE FUEL TANK DRAIN VALVE (LH) FUEL TANK DRAIN VALVE (RH) HYD. SYS # 2 SERVICE PANEL WASTE SERVICING PANEL HYD. SYS # 3 SERVICE PANEL COORD. X (mm) COORD. Y (mm) NOTE: THE GROUND CLEARANCES IN THE TABLE REFER TO THE AIRCRAFT WITH THE MINIMUM OPERATING WEIGHT (MOW) = 298 kg (CG FWD 4.% CMA) COORD. Z (mm) HEIGHT ABOVE GROUND (mm) EXTERNAL POWER SUPPLY 115 VAC EM17APM518E.DGN Ground Servicing Connections Figure 5.4 Section 5 Page 5-7 May 11/7