EMBRAER S.A - P.O. BOX 85 12227-91 SAO JOSE DOS CAMPOS - S.P. BRAZIL PHONE: ++55123927-7517 FAX:++55123927-7546 http://www.embraer.com e-mail: distrib@embraer.com.br AIRPORT PLANNING MANUAL APM-191 15 AUGUST 25 REVISION 1-18 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.
Title TRList 1... Oct 22/7 2 Blank... Oct 22/7 SBList 1... Jan 9/6 2 Blank... Aug 15/5 List of Effective Pages * 1 (rev)... * 2 (rev)... Table of Contents * 1 (rev)... 2... May 11/7 List of Tables * 1 (rev)... 2 Blank... Aug 15/5 List of Figures * 1 (rev)... 2... Oct 31/12 3... May 11/7 4 Blank... Aug 15/5 Section 1 1-1... Jan 9/6 1-2... Oct 6/11 1-3... Oct 6/11 1-4 Blank... Aug 15/5 Section 2 * 2-1 (rev)... * 2-2 (rev)... * 2-3 (rev)... * 2-4 (rev)... * 2-5 (rev)... * 2-6 (rev)... * 2-7 (rev)... * 2-8 (rev)... * 2-9 (rev)... * 2-1 (rev)... * 2-11 (rev)... * 2-12 (rev)... * 2-13 (rev)... * 2-14 (rev)... * 2-15 (add)... * 2-16 Blank (add)... Section 3 * 3-1 (rev)... * 3-2 (rev)... * 3-3 (rev)... * 3-4 (rev)... * 3-5 (rev)... * 3-6 (rev)... * 3-7 (rev)... * 3-8 (rev)... * 3-9 (rev)... * 3-1 (rev)... * 3-11 (rev)... * 3-12 (rev)... * 3-13 (rev)... * 3-14 (rev)... * 3-15 (rev)... * 3-16 (rev)... * 3-17 (rev)... * 3-18 (rev)... * 3-19 (rev)... * 3-2 (rev)... * 3-21 (rev)... * 3-22 (rev)... * 3-23 (rev)... * 3-24 (rev)... * 3-25 (rev)... * 3-26 (rev)... * 3-27 (del)... * 3-28 (del)... Section 4 * 4-1 (rev)... * 4-2 (rev)... * 4-3 (rev)... * 4-4 (rev)... * 4-5 (rev)... * 4-6 (rev)... * 4-7 (rev)... * 4-8 (rev)... * 4-9 (rev)... * 4-1 Blank (rev)... Section 5 * 5-1 (rev)... * 5-2 (rev)... * 5-3 (rev)... * 5-4 (rev)... * 5-5 (rev)... * 5-6 (rev)... * 5-7 (rev)... * 5-8 (rev)... * 5-9 (rev)... * 5-1 (rev)... * 5-11 (rev)... * 5-12 (rev)... 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. 1 Page 1
* 5-13 (rev)... * 5-14 Blank (rev)... Section 6 * 6-1 (rev)... * 6-2 (rev)... * 6-3 (rev)... * 6-4 (rev)... * 6-5 (rev)... * 6-6 (rev)... * 6-7 (rev)... * 6-8 (rev)... * 6-9 (rev)... * 6-1 (rev)... * 6-11 (rev)... * 6-12 Blank (rev)... Section 7 * 7-1 (rev)... * 7-2 (rev)... * 7-3 (rev)... * 7-4 (rev)... * 7-5 (rev)... * 7-6 (rev)... * 7-7 (rev)... * 7-8 (rev)... * 7-9 (rev)... * 7-1 (rev)... * 7-11 (rev)... * 7-12 (rev)... * 7-13 (rev)... * 7-14 (rev)... * 7-15 (rev)... * 7-16 (rev)... * 7-17 (rev)... * 7-18 Blank (rev)... 7-19 (del)... Dec 18/6 7-2 (del)... Dec 18/6 7-21 (del)... Dec 18/6 7-22 (del)... Dec 18/6 7-23 (del)... Dec 18/6 7-24 Blank (del)... Dec 18/6 Section 8 * 8-1 (rev)... * 8-2 Blank (rev)... Section 9 * 9-1 (rev)... * 9-2 (rev)... * 9-3 (rev)... * 9-4 (rev)... * 9-5 (rev)... * 9-6 (rev)... 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. 1 Page 2
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... 2-5 2.4. Interior Arrangements... 2-9 2.5. Passenger Cabin Cross Section... 2-12 2.6. Lower Compartment Containers... 2-14 2.7. Door Clearances... 2-15 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... 3-18 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... 4-9 SECTION 5 - 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... 5-1 5.7. Preconditioned Airflow Requirements... 5-11 5.8. Ground Towing Requirements... 5-13 EFFECTIVITY: ALL TABLE OF CONTENTS Page 1
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... 6-1 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... 7-11 7.9. ACN - PCN System - Flexible and Rigid Pavements... 7-15 SECTION 8 - POSSIBLE EMBRAER 19 DERIVATIVE AIRCRAFT 8. Possible EMBRAER 19 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 11/7
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. 1.2. 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 1.1 - 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. EFFECTIVITY: ALL Section 1 Page 1-1 Jan 9/6
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. 12.227-91- São José dos Campos - SP - Brazil Phone: (55 12) 3927-7517 FAX: (55 12) 3927-7546 http://www.embraer.com e-mail: 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 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 EFFECTIVITY: ALL Section 1 Page 1-2 Oct 6/11
Table 1.2 - List of Acronyms and Abbreviations used in the APM ACRONYMS AND ABBREVIATIONS APM APU AR ATTCS BOW CBR ECS FAA FAR 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 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 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 EFFECTIVITY: ALL Section 1 Page 1-3 / 4 Oct 6/11
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 4779 kg (15359 lb); The LR aircraft model - MTOW 53 kg (11892 lb); The AR aircraft model - MTOW 518 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 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
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 DESIGN WEIGHTS [1] AIRCRAFT MODELS STD LR AR MRW 4795 kg (15712 lb) 546 kg (111245 lb) 5196 kg (114552 lb) MTOW 4779 kg (15359 lb) 53 kg (11892 lb) 518 kg (114199 lb) MLW 43 kg (94799 lb) 44 kg (973 lb) BOW [2] 279 kg (6159 lb) MZFW 48 kg (89949 lb) 49 kg (9169 lb) Maximum Payload [2] 129 kg (2844 lb) 13 kg (2866 lb) Maximum Seating Capacity 16 passengers Maximum Cargo Volume [3] 22.63 m 3 (799.18 ft 3 ) Usable Fuel [4] 13 kg (2866 lb) 1629 (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.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) - 1.55 m (34 ft 7 in.) Overall length - 36.24 m (118 ft 11 in.) 2.2.2. Wing Reference area - 92.5 m 2 (996 ft 2 ) Reference aspect ratio - 8.1 Section 2 Page 2-2
2.2.3. Fuselage Total Length - 36.24 m (118 ft 11 in.) Length of pressurized section - 29.8 m (95 ft 5 in.) 2.2.4. Horizontal Tail Span - 12.8 m (39 ft 8 in.) Area - 26. m 2 (28 ft 2 ) 2.2.5. Vertical Tail Reference area - 16.2 m 2 (174 ft 2 54 in 2 ) Section 2 Page 2-3
6.82 m (45 ft 4 in.) 24.57 m (8 ft 1 in.) 1.57 m (34 ft 8 in.) 4.13 m (13 ft 6 in.) 13.81 m (45 ft 4 in.) 36.24 m (118 ft 11 in.) 4.27 m (14 ft) 27.6 m (9 ft 7 in.) 12.8 m (39 ft 8 in.) 4.71 m (15 ft 5.4in.) 27.6 m (9 ft 7 in.) 2.4 m (65 ft 9 in.) 5.94 m (19 ft 6 in.) 28.72 m (94 ft 3 in.) EM17APM211B.DGN General Aircraft Dimensions Figure 2.1 Section 2 Page 2-4
2.3. GROUND CLEARANCES FUSLG ANGLE (REF.) A M B N C E H J K L D G F EM17MFEP213B.DGN Aircraft Ground Clearances Figure 2.2 Section 2 Page 2-5
WEIGHT 4795 kg 15712 lb 4795 kg 15712 lb 4779 kg 15359 lb 4779 kg 15359 lb 43 kg 94799 lb 43 kg 94799 lb 48 kg 89949 lb 48 kg 89949 lb CG (%MAC) FUS ANGLE (DEG) (A) 6. -1.1 28.7 -.8 6. -1.1 28.7 -.8 6. -1.1 29. -.8 6. -1.1 29. -.8 NOSE (B) 2.7 m 6ft9in. 2.13 m 7ft 2.5 m 6ft9in. 2.13 m 7ft 2.6 m 6ft9in. 2.14 m 7ft 2.6 m 6ft9in. 2.15 m 7ft FOR- WARD SERVICE DOOR (C) 2.58 m 8ft5in. 2.63 m 8ft7in. 2.58 m 8ft5in. 2.63 m 8ft7in. 2.59 m 8ft6in. 2.65 m 8ft8in. 2.59 m 8ft6in. 2.65 m 8ft8in. Table 2.2 - Ground Clearance - STD Aircraft Model WINGLET (G) FOR- WARD PASSEN- GER DOOR (D) FOR- WARD CARGO DOOR (E) NA- CELLE (F) EMER- GENCY EXIT (H) AFT CARGO DOOR (J) AFT SERVICE DOOR (K) 2.59 m 8ft6in. 2.64 m 8ft8in. 2.59 m 8ft6in. 1.57 m 5ft2in. 1.61 m 5ft3in. 1.57 m 5ft2in..49 m 1ft7in..5 m 1ft8in..49 m 1ft7in. 5.9 m 16 ft 8 in. 5.5 m 16 ft 7 in. 5.9 m 16 ft 8 in. 3.24 m 1 ft 8 in. 3.24 m 1 ft 8 in. 3.24 m 1 ft 8 in. 1.99 m 6ft5in. 1.94 m 6ft4in. 1.99 m 6ft6in. 3.3 m 9ft9in. 2.97 m 8ft8in. 3.3 m 9ft11in. 2.64 m 8ft8in. 1.61 m 5ft3in..5 m 1ft8in. 5.6 m 16 ft 7 in. 3.24 m 1 ft 8 in. 1.94 m 6ft4in. 2.97 m 9ft8in. 2.6 m 8ft6in. 1.58 m 5ft2in..5 m 1ft8in. 5.12 m 16 ft 9 in. 3.26 m 1 ft 8 in. 2.m 6ft7in. 3.6 m 9ft12in. 2.66 m 8ft9in. 1.63 m 5ft4in..51 m 1ft8in. 5.8 m 16 ft 8 in. 3.26 m 1 ft 8 in. 1.96 m 6ft5in. 2.99 m 9ft9in. 2.6 m 8ft6in. 1.59 m 5ft3in..51 m 1ft8in. 5.13 m 16 ft 1 in. 3.27 m 1 ft 9 in. 2.2 m 6ft7in. 3.7 m 1 ft 2.66 m 8ft9in. 1.64 m 5ft5in..52 m 1ft9in. 5.9 m 16 ft 8 in. 3.27 m 1 ft 9 in. 1.98 m 6ft5in. 3. m 9ft1in. AFT PASSEN- GER DOOR (L) 3.3 m 9ft9in. 2.97 m 8ft8in. 3.3 m 9ft11in. 2.97 m 9ft8in. 3.6 m 9ft12in. 2.99 m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. VERTI- CAL TAIL (M) 1.4 m 34 ft 2 in. 1.33 m 33 ft 9 in. 1.43 m 34 ft 2 in. 1.33 m 33 ft 1 in. 1.45 m 34 ft 3 in. 1.35 m 33 ft 1 in. 1.47 m 34 ft 4 in. 1.36 m 33 ft 11 in. TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (N) 12.7 12.4 12.7 12.3 12.8 12.4 12.9 12.5 Section 2 Page 2-6
WEIGHT 546 kg 111245lb 546kg 111245 lb 53kg 11892lb 53kg 11892 lb 43 kg 94799 lb 43 kg 94799 lb 48 kg 89949 lb 48 kg 89949 lb CG (%MAC) FUS ANGLE (DEG) (A) 8.8-1.1 27.6 -.8 8.8-1.1 27.6 -.8 6. -1.1 29. -.8 6. -1.1 29. -.8 NOSE (B) 2.6 m 6ft9in. 2.12 m 7ft 2.6 m 6ft9in. 2.12 m 7ft 2.6 m 6ft9in. 2.14 m 7ft 2.6 m 6ft9in. 2.15 m 7ft2in. Table 2.3 - Ground Clearance - LR Aircraft Model WINGLET (G) FOR- WARD SERVICE DOOR (C) FOR- WARD PASSEN- GER DOOR (D) FOR- WARD CARGO DOOR (E) NA- CELLE (F) EMER- GENCY EXIT (H) AFT CARGO DOOR (J) 2.58 m 8ft5in. 2.62 m 8ft8in. 2.58 m 8ft5in. 2.62 m 8ft8in. 2.59 m 8ft6in. 2.58 m 8ft5in. 2.63 m 8ft7in. 2.58 m 8ft5in. 2.63 m 8ft7in. 2.6 m 8ft6in. 1.57 m 5ft2in. 1.6m 5ft4in. 1.57 m 5ft2in. 1.6 m 5ft4in. 1.58 m 5ft2in..48 m 1ft7in..49 m 1ft7in..48 m 1ft7in..49 m 1 ft 7in..5 m 1ft8in. 5.8 m 16 ft 8 in. 5.5 m 16 ft 7 in. 5.8 m 16 ft 8 in. 5.5 m 16 ft 7 in. 5.12 m 16 ft 9 in. 3.23 m 1 ft 7 in. 3.24 m 1 ft 7 in. 3.23 m 1 ft 7 in. 3.24 m 1 ft 7 in. 3.26 m 1 ft 8 in. 1.97 m 6ft5in. 1.94m 6ft4in. 1.97 m 6ft5in. 1.94 m 6ft4in. 2. m 6ft7in. 2.65 m 8ft8in. 2.66 m 8ft9in. 1.63 m 5ft4in..51 m 1ft8in. 5.8 m 16 ft 8 in. 3.26 m 1 ft 8 in. 1.96 m 6ft5in. 2.59 m 8ft6in. 2.6 m 8ft6in. 1.59 m 5ft3in..51 m 1ft8in. 5.13 m 16 ft 1 in. 3.27 m 1 ft 9 in. 2.2 m 6ft7in. 2.65 m 8ft8in. 2.66 m 8ft9in. 1.64 m 5ft5in..52 m 1ft9in. 5.9 m 16 ft 8 in. 3.27 m 1 ft 9 in. 1.98 m 6ft5in. AFT SERVICE DOOR (K) 3.2 m 9ft1in. 2.97 m 9ft8in. 3.2 m 9ft1in. 2.97 m 9ft8in. 3.6 m 9ft12in. 2.99 m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. AFT PASSEN- GER DOOR (L) 3.2 m 9ft1in. 2.97 m 9ft8in. 3.2 m 9ft1in. 2.97 m 9ft8in. 3.6 m 9ft12in. 2.99 m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. VERTI- CAL TAIL (M) 1.4 m 34 ft 1 in. 1.33 m 33 ft 9 in. 1.4 m 34 ft 1in. 1.33 m 33 ft 9 in. 1.45 m 34 ft 3 in. 1.35 m 33 ft 1 in. 1.47 m 34 ft 4 in. 1.36 m 33 ft 11 in. TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (N) 12.6 12.3 12.6 12.3 12.8 12.4 12.9 12.5 Section 2 Page 2-7
WEIGHT 5196 kg 114552lb 5196 kg 114552lb 518kg 11499lb 518kg 11499lb 44 kg 973 lb 44 kg 973 lb 49 kg 9169 lb 49 kg 9169 lb CG (%MAC) FUS ANGLE (DEG) (A) 1.7-1.1 27. -.8 1.7-1.1 27. -.8 6. -1.1 29. -.8 6. -1.1 29. -.8 NOSE (B) 2.6 m 6ft9in. 2.12 m 7ft 2.6 m 6ft9in. 2.12m 7ft 2.6 m 6ft9in. 2.14 m 7ft 2.6 m 6ft9in. 2.15 m 7ft2in. Table 2.4 - Ground Clearance - AR Aircraft Model WINGLET (G) FOR- WARD SERVICE DOOR (C) FOR- WARD PASSEN- GER DOOR (D) FOR- WARD CARGO DOOR (E) NA- CELLE (F) EMER- GENCY EXIT (H) AFT CARGO DOOR (J) 2.58 m 8ft5in. 2.62 m 8ft8in. 2.58 m 8ft5in. 2.62 m 8ft8in. 2.59 m 8ft6in. 2.59 m 8ft6in. 2.63 m 8ft7in. 2.59 m 8ft6in. 2.63 m 8ft7in. 2.6 m 8ft6in. 1.57 m 5ft2in. 1.6 m 5ft4in. 1.57 m 5ft2in. 1.6 m 5ft4in. 1.58 m 5ft2in..48 m 1ft7in..49 m 1ft7in..48 m 1ft7in..49 m 1ft7in..5 m 1ft8in. 5.8 m 16 ft 8 in. 5.5 m 16 ft 7 in. 5.8 m 16 ft 8 in. 5.5 m 16 ft 7 in. 5.11 m 16 ft 9 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. 3.26 m 1 ft 8 in. 1.97 m 6ft5in. 1.93 m 6ft4in. 1.97 m 6ft5in. 1.93 m 6ft4in. 2. m 6ft7in. 2.64 m 8ft8in. 2.65 m 8ft8in. 1.63 m 5ft4in..51 m 1ft8in. 5.7 m 16 ft 8 in. 3.26 m 1 ft 8 in. 1.96 m 6ft5in. 2.59 m 8ft6in. 2.6 m 8ft6in. 1.59 m 5ft3in..51 m 1ft8in. 5.13 m 16 ft 1 in. 3.27 m 1 ft 9 in. 2.2 m 6ft7in. 2.65 m 8ft8in. 2.66 m 8ft9in. 1.63 m 5ft4in..52 m 1ft9in. 5.9 m 16 ft 8 in. 3.27 m 1 ft 9 in. 1.97 m 6ft5in. AFT SERVICE DOOR (K) 3.1 m 9ft1in. 2.96 m 9ft8in. 3.1 m 9ft1in. 2.96 m 9ft8in. 3.3 m 9ft12in. 2.99 m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. AFT PASSEN- GER DOOR (L) 3.1 m 9ft1in. 2.96 m 9ft8in. 3.1 m 9ft1in. 2.96 m 9ft8in. 3.3 m 9ft12in. 2.99 m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. VERTI- CAL TAIL (M) 1.4 m 34 ft 1 in. 1.32 m 33 ft 9 in. 1.4 m 34 ft 1in. 1.33 m 33 ft 9 in. 1.45 m 34 ft 3 in. 1.34 m 33 ft 1 in. 1.47 m 34 ft 4 in. 1.36 m 33 ft 11 in. TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (N) 12.6 12.3 12.6 12.3 12.8 12.4 12.9 12.5 Section 2 Page 2-8
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. m (6 ft 7 in.) Width - 2.74 m (9 ft) Aisle wide -.49 m (1 ft 7 in.) Pitch -.82 m (32 in.) Section 2 Page 2-9
3 4 9 5.9 m (2 ft 11.4 in.) 8 8.87 m (2 ft 1 in.).78 m (2 ft 6.7 in.) 1.82 m (5 ft 11 in.) 4.82 m (15 ft 1 in.) 7.77 (25 ft 6 in.) 4.17 m (13 ft 8 in.) 7.16 (23 ft 6 in.) 1.86 m (6 ft 4 in.) 25.91 m (85 ft) 3 4 2 1.81 m (2 ft 8 in.) 5 6 1 2 1.48 m (4 ft 1 in.) 1 7 1 FLIGHT ATTENDANT SEAT 6 FWD LAVATORY 2 WARDROBE 7 AFT LAVATORY 3 FWD RH G1 GALLEY 4 FWD RH G2 GALLEY 5 AFT RH GALLEY 8 CARGO COMPARTMENT 9 OVERHEAD BIN 1 PASSENGER SEAT CARGO/BAGGAGE VOLUME 3 3 CARGO COMPARTMENT 22.63 m (799.18 ft ) 3 3 OVERHEAD BIN.6 m / pax (2. ft / pax) 3 3 UNDERSEAT VOLUME.4 m / pax (1.4 ft / pax) EM17APM213B.DGN Typical Interior Arrangements Figure 2.3 Section 2 Page 2-1
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 classification. The table below contain the capacity for the cargo compartment: Table 2.5 - Capacity for the Cargo Compartment CARGO COMPARTMENT LOADING VOLUME FWD [1] 185 kg (478 lb) 12.41 m 3 (438.26 ft 3 ) Aft 165 kg (3638 lb) 1.22 m 3 (36.92 ft 3 ) Total 35 kg (7716 lb) 22.63 m 3 (799.18 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. 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 Page 2-11
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
.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
2.6. LOWER COMPARTMENT CONTAINERS Not Applicable Section 2 Page 2-14
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
3. AIRCRAFT PERFORMANCE 3.1. GENERAL INFORMATION The performance of the aircraft and engine depends on the generation of forces by the interaction between the aircraft or engine and the air mass through which it flies. The atmosphere has a pronounced effect on the temperature, pressure and density of the air. The ICAO establishes standard basics for estimating and comparing aircraft and engine performance. Some ICAO standard basics are shown below: 1. Sea level standard day: Standard Temperature To = 15 C (288.15 K) Standard Pressure Po = 11.3 kpa (29.92 inhg) Standard Density ρo =.2377 slug per cubic feet 2. ISA Table 3.1 - ISA ALTITUDE TEMPERATURE m ft C F 15. 59. 35 1 13. 55.4 61 2 11. 51.9 915 3 9.1 48.3 122 4 7.1 44.7 1524 5 5.1 41.2 349 1-4.8 23.3 4573 15-14.7 5.5 698 2-24.6-12.3 7622 25-34.5-3.2 9146 3-44.4-48. 113 3689-56.5-69.7 12195 4-56.5-69.7 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, 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 Page 3-1
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 according to ISA or ISA + 1 C conditions; MTOW. Section 3 Page 3-2
PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 4779 kg (15359 lb) 3 28 14 13 26 12 24 11 18 PAX @ 1 kg 22 1 2 9 PAYLOAD lb 18 16 14 PAYLOAD kg 8 7 6 12 1 8 5 4 6 3 4 2 LONG RANGE 2 1 MAX CRUISE.78 MACH 5 1 NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 15 RANGE nm 2 25 4779 kg (15359 lb) 48 kg (89948 lb) 279 kg (6159 lb) 131 kg (2888 lb) 3 EM17APM33E.DGN Payload x Range - ISA Conditions Figure 3.1 EFFECTIVITY: EMBRAER 19 STD MODEL Section 3 Page 3-3
PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA + 1 C RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 4779 kg (15359 lb) 3 28 26 14 13 12 24 11 18 PAX @ 1 kg 22 1 2 9 PAYLOAD lb 18 16 14 PAYLOAD kg 8 7 6 12 1 8 5 4 6 3 4 2 MAX CRUISE LONG RANGE 2 1.78 MACH 5 1 15 2 25 3 RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 4779 kg (15359 lb) 48 kg (89948 lb) 279 kg (6159 lb) 131 kg (2888 lb) EM17APM331E.DGN Payload x Range - ISA + 1 C Conditions Figure 3.2 EFFECTIVITY: EMBRAER 19 STD MODEL Section 3 Page 3-4
PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 53 kg (11893 lb) 3 28 26 14 13 12 24 11 18 PAX @ 1 kg 22 1 2 9 PAYLOAD lb 18 16 14 PAYLOAD kg 8 7 6 12 1 5 8 4 LONG RANGE 6 3 MAX CRUISE 4 2.78 MACH 2 1 5 1 15 2 25 3 NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL RANGE nm 53 kg (11893 lb) 48 kg (89949 lb) 279 kg (6159 lb) 131 kg (2888 lb) EM17APM332D.DGN Payload x Range - ISA Conditions Figure 3.3 EFFECTIVITY: EMBRAER 19 LR MODEL Section 3 Page 3-5
PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA + 1 C RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 53 kg (11893 lb) 3 28 26 14 13 12 24 11 18 PAX @ 1 kg 22 1 2 9 PAYLOAD lb 18 16 14 PAYLOAD kg 8 7 6 12 1 5 8 4 6 3 MAX CRUISE LONG RANGE 4 2.78 MACH 2 1 5 1 15 2 25 3 RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 53 kg (11893 lb) 48 kg (89949 lb) 279 kg (6159 lb) 131 kg (2888 lb) EM17APM333D.DGN Payload x Range - ISA + 1 C Conditions Figure 3.4 EFFECTIVITY: EMBRAER 19 LR MODEL Section 3 Page 3-6
PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 518 kg (114199 lb) 3 28 26 14 13 12 24 11 18 PAX @ 1 kg 22 1 2 9 PAYLOAD lb 18 16 14 PAYLOAD kg 8 7 6 12 1 5 8 4 6 3 4 2 MAX CRUISE LONG RANGE 2 1.78 MACH 5 1 15 2 25 3 RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 518 kg (114199 lb) 49 kg (9169 lb) 279 kg (6159 lb) 131 kg (2888 lb) EM17APM36C.DGN Payload x Range - ISA Conditions Figure 3.5 EFFECTIVITY: EMBRAER 19 AR MODEL Section 3 Page 3-7
PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA+1 RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 518 kg (114199 lb) 3 28 26 14 13 12 24 11 18 PAX @ 1 kg 22 1 2 9 PAYLOAD lb 18 16 14 PAYLOAD kg 8 7 6 12 1 5 8 4 LONG RANGE 6 3 4 2 MAX CRUISE.78 MACH 2 1 5 1 15 2 25 3 RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 518 kg (114199 lb) 49 kg (9169 lb) 279 kg (6159 lb) 131 kg (2888 lb) EM17APM361C.DGN Payload x Range - ISA + 1 C Conditions Figure 3.6 EFFECTIVITY: EMBRAER 19 AR MODEL Section 3 Page 3-8
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: CF34-1E 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 + 1 C conditions; Pack OFF: No engine bleed extraction for air conditioning packs was considered in the takeoff and landing charts. Section 3 Page 3-9
TAKEOFF FIELD LENGTH CF 34 1E5 & 1E6 ENGINE@T/O 1 MODE ATTCS OFF / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA 14 13 44 42 4 AIRPORT PRESSURE ALTITUDE m (ft) 12 38 36 FLAP 1 14 12 1 8 11 34 32 1 9 3 28 FLAP 3 6 FIELD LENGTH ft 8 7 26 24 22 2 FLAP 4 4 2 6 18 SEA LEVEL 187 5 16 14 4 12 3 1 8 2 6 1 4 27 29 31 33 35 37 39 41 43 45 47 49 51 53 WEIGHT kg 6 7 8 9 1 11 WEIGHT lb EM17APM336D.DGN Takeoff Field Lengths - ISA Conditions Figure 3.7 Section 3 Page 3-1
TAKEOFF FIELD LENGTH CF34 1E5 & 1E6 Engines @ T/O 1 MODE ATTCS OFF / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15 C 44 14 13 12 42 4 38 36 AIRPORT PRESSURE ALTITUDE m (ft) FLAP 1 14 12 1 8 11 34 32 1 3 FLAP 3 6 9 28 FIELD LENGTH ft 8 7 6 26 24 22 2 18 FLAP 4 4 2 SEA LEVEL 187 5 16 14 4 12 3 1 8 2 6 1 4 27 29 31 33 35 37 39 41 43 45 47 49 51 53 WEIGHT kg 6 7 8 9 1 11 WEIGHT lb EM17APM337D.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.8 Section 3 Page 3-11
TAKEOFF FIELD LENGTH CF34 1E5 & 1E6 Engines @ T/O 1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA 44 14 13 42 4 AIRPORT PRESSURE ALTITUDE m (ft) FLAP 1 14 12 38 12 36 1 11 34 32 FLAP 3 8 1 3 9 28 FIELD LENGTH ft 8 7 26 24 22 2 FLAP 4 6 4 2 6 5 18 16 SEA LEVEL 187 14 4 12 3 1 8 2 6 1 4 27 29 31 33 35 37 39 41 43 45 47 49 51 53 WEIGHT kg 6 7 8 9 1 11 WEIGHT lb EM17APM338D.DGN Takeoff Field Lengths - ISA Conditions Figure 3.9 Section 3 Page 3-12
TAKEOFF FIELD LENGTH CF34 1E5 & 1E6 Engines @ T/O 1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15 C 14 13 44 42 4 AIRPORT PRESSURE ALTITUDE m (ft) FLAP 1 14 12 38 1 12 36 11 34 FLAP 3 8 32 1 3 FIELD LENGTH ft 9 8 7 6 28 26 24 22 2 18 FLAP 4 6 4 2 SEA LEVEL 187 5 16 14 4 12 3 1 8 2 6 1 4 27 29 31 33 35 37 39 41 43 45 47 49 51 53 WEIGHT kg 6 7 8 9 1 11 WEIGHT lb EM17APM339D.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.1 Section 3 Page 3-13
TAKEOFF FIELD LENGTH CF34 1E7 ENGINE@T/O 1 MODE ATTCS OFF CF34 1E5A1 & 1E6A1 ENGINES@T/O 1 MODE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA 44 14 42 13 12 4 38 36 FLAP 1 14 12 11 34 1 32 1 3 FLAP 3 8 9 28 FIELD LENGTH ft 8 7 26 24 22 2 FLAP 4 6 4 6 5 18 16 2 SEA LEVEL 187 14 4 12 3 1 8 2 6 1 4 27 29 31 33 35 37 39 41 43 45 47 49 51 53 WEIGHT kg 6 7 8 9 1 11 WEIGHT lb EM17APM334C.DGN Takeoff Field Lengths - ISA Conditions Figure 3.11 Section 3 Page 3-14
TAKEOFF FIELD LENGTH CF34 1E7 ENGINE@T/O 1 MODE ATTCS OFF / ECS OFF CF34 1E5A1 & 1E6A1 ENGINES@T/O 1 MODE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15 C 44 14 42 14 12 13 4 FLAP 1 38 12 36 1 11 1 34 32 3 FLAP 3 8 9 28 FIELD LENGTH ft 8 7 26 24 22 2 FLAP 4 6 4 2 6 18 SEA LEVEL 5 16 187 14 4 12 3 1 8 2 6 1 4 27 29 31 33 35 37 39 41 43 45 47 49 51 53 WEIGHT kg 6 7 8 9 1 11 WEIGHT lb EM17APM335C.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.12 Section 3 Page 3-15
TAKEOFF FIELD LENGTH CF 34 1E7 ENGINE@T/O 1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA 14 44 42 13 12 4 38 36 AIRPORT PRESSURE ALTITUDE m (ft) 11 34 1 1 32 3 FLAP 3 FIELD LENGTH ft 9 8 7 28 26 24 22 2 8 6 4 6 5 18 16 FLAP 4 2 SEA LEVEL 187 14 4 12 3 1 8 2 6 1 4 27 29 31 33 35 37 39 41 43 45 47 49 51 53 WEIGHT kg 6 7 8 9 1 11 WEIGHT lb EM17APM34C.DGN Takeoff Field Lengths - ISA Conditions Figure 3.13 Section 3 Page 3-16
TAKEOFF FIELD LENGTH CF 34 1E7 ENGINE@T/O 1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15 C 44 14 42 13 4 38 AIRPORT PRESSURE ALTITUDE m (ft) 12 36 1 11 1 34 32 3 FLAP 3 9 28 8 FIELD LENGTH ft 8 7 6 26 24 22 2 18 FLAP 4 6 4 2 SEA LEVEL 5 16 187 14 4 12 3 1 8 2 6 1 4 27 29 31 33 35 37 39 41 43 45 47 49 51 53 WEIGHT kg 6 7 8 9 1 11 WEIGHT lb EM17APM341C.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.14 Section 3 Page 3-17
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 Page 3-18
LANDING FIELD LENGTH CF 34 1E5 1E5A1 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA 6 18 17 16 AIRPORT PRESSURE ALTITUDE m (ft) 1 9 8 7 5 6 15 5 FIELD LENGTH ft LAND FIELD LENGTH m 14 13 4 3 2 1 1 4 12 11 1 3 9 25 27 29 31 33 35 37 39 41 43 45 WEIGHT kg 6 7 8 9 1 EM17APM346C.DGN Landing Field Lengths - Flaps 5 Figure 3.15 EFFECTIVITY: EASA-CERTIFIED Section 3 Page 3-19
LANDING FIELD LENGTH CF34 1E5 1E5A1 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA 6 18 17 AIRPORT PRESSURE ALTITUDE m (ft) 16 1 5 9 15 8 FIELD LENGTH ft 4 LAND FIELD LENGTH m 14 13 12 7 6 5 4 3 2 1 1 187 11 1 3 9 25 27 29 31 33 35 37 39 41 43 45 WEIGHT kg 6 7 8 9 1 EM17APM347C.DGN Landing Field Lengths - Flaps Full Figure 3.16 EFFECTIVITY: EASA-CERTIFIED Section 3 Page 3-2
6 LANDING FIELD LENGTH CF 34 1E7 ENGINE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA 18 17 AIRPORT PRESSURE ALTITUDE m (ft) 1 9 16 8 7 5 6 15 5 FIELD LENGTH ft LAND FIELD LENGTH m 14 13 4 3 2 1 1 187 4 12 11 1 3 9 25 27 29 31 33 35 37 39 41 43 45 WEIGHT kg 6 7 8 9 1 EM17APM362B.DGN Landing Field Lengths - Flaps 5 Figure 3.17 EFFECTIVITY: EASA-CERTIFIED Section 3 Page 3-21
LANDING FIELD LENGTH CF 34 1E7 ENGINE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA 6 18 17 AIRPORT PRESSURE ALTITUDE m (ft) 16 1 5 15 9 8 FIELD LENGTH ft 4 LAND FIELD LENGTH m 14 13 12 7 6 5 4 3 2 1 1 187 11 1 3 9 25 27 29 31 33 35 37 39 41 43 45 WEIGHT kg 6 7 8 9 1 EM17APM363B.DGN Landing Field Lengths - Flaps Full Figure 3.18 EFFECTIVITY: EASA-CERTIFIED Section 3 Page 3-22
LANDING FIELD LENGTH CF 34 1E5 1E5A1 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA 2 6 19 18 AIRPORT PRESSURE ALTITUDE m (ft) 14 13 12 11 1 17 9 8 FIELD LENGTH ft 5 LAND FIELD LENGTH m 16 15 14 13 7 6 5 4 3 2 1 1 187 4 12 11 1 3 9 25 27 29 31 33 35 37 39 41 43 45 WEIGHT kg 6 7 8 9 1 EM17APM317A.DGN Landing Field Lengths - Flaps 5 Figure 3.19 EFFECTIVITY: FAA-CERTIFIED Section 3 Page 3-23
LANDING FIELD LENGTH CF 34 1E5 1E5A1 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA 2 19 6 18 AIRPORT PRESSURE ALTITUDE m (ft) 17 14 13 FIELD LENGTH ft 5 4 LAND FIELD LENGTH m 16 15 14 13 12 12 11 1 9 8 7 6 5 4 3 2 1 1 187 11 1 3 9 25 27 29 31 33 35 37 39 41 43 45 WEIGHT kg 6 7 8 9 1 EM17APM318A.DGN Landing Field Lengths - Flaps Full Figure 3.2 EFFECTIVITY: FAA-CERTIFIED Section 3 Page 3-24
LANDING FIELD LENGTH CF 34 1E7 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA 2 6 19 18 AIRPORT PRESSURE ALTITUDE m (ft) 1 17 9 8 FIELD LENGTH ft 5 LAND FIELD LENGTH m 16 15 14 13 7 6 5 4 3 2 1 1 187 4 12 11 1 3 9 25 27 29 31 33 35 37 39 41 43 45 6 7 WEIGHT kg 8 9 1 EM17APM319A.DGN Landing Field Lengths - Flaps 5 Figure 3.21 EFFECTIVITY: FAA-CERTIFIED Section 3 Page 3-25
LANDING FIELD LENGTH CF 34 1E7 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA 2 6 19 18 AIRPORT PRESSURE ALTITUDE m (ft) 17 FIELD LENGTH ft 5 4 LAND FIELD LENGTH m 16 15 14 13 12 1 9 8 7 6 5 4 3 2 1 1 187 11 1 3 9 25 27 29 31 33 35 37 39 41 43 45 6 7 WEIGHT kg 8 9 1 EM17APM32A.DGN Landing Field Lengths - Flaps Full Figure 3.22 EFFECTIVITY: FAA-CERTIFIED Section 3 Page 3-26
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 18 turn. Section 4 Page 4-1
R5 R6 R3 R6.44 m 21ft 2 in 76 7 65 6 55 5 45 4 35 R14.7m 46ft 2 in R4 R1 R2 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 STEEL 35 4 45 5 55 6 65 7 76 26.53 m 24.21 m 22.5 m 21.22 m 2.24 m 19.49 m 18.91 m 18.48 m 18.12 m NOSE R1 87 ft 79 ft 5 in 73 ft 1 in 69 ft 7 in 66 ft 5 in 63 ft 11 in 63 ft 6 ft 8 in 59 ft 5 in NOSE GEAR R2 24.16 m 21.58 m 19.64 m 18.14 m 16.98 m 16.7 m 15.36 m 14.82 m 14.36 m 79 ft 3 in 7 ft 1 in 64 ft 5 in 59 ft 6 in 55 ft 9 in 52 ft 9 in 5 ft 5 in 48 ft 7 in 47 ft 1 in OUTBOARD GEAR R3 23.28 m 2.3 m 17.38 m 15.17 m 13.25 m 11.56 m 1.3 m 8.62 m 7.4 m 76 ft 5 in 65 ft 9 in 57 ft 49 ft 9 in 43 ft 6 in 37 ft 11 in 32 ft 11 in 28 ft 3 in 23 ft 1 in INBOARD GEAR R4 16.8 m 12.82 m 1.18 m 7.96 m 6.5 m 4.35 m 2.82 m 1.41 m.17 m 52 ft 9 in 42 ft 1 in 35 ft 5 in 26 ft 1 in 19 ft 1 in 14 ft 3 in 9 ft 3 in 4 ft 8 in 7 in RIGHT WINGLET R5 34.35 m 31.13 m 28.52 m 26.33 m 24.45 m 22.79 m 21.3 m 19.93 m 18.39 m 112 ft 8 in 12 ft 2 in 93 ft 7 in 86 ft 5 in 8 ft 3 in 74 ft 9 in 69 ft 1 in 65 ft 5 in 6 ft 4 in RIGHT TAILTIP R6 31.5 m 28.91 m 26.9 m 25.32 m 24.2 m 22.95 m 22.5 m 21.29 m 2.51 m 13 ft 4 in 94 ft 1 in 88 ft 3 in 83 ft 1 in 78 ft 1 in 75 ft 4 in 72 ft 4 in 69 ft 1 in 67 ft 3 in EM17APM48B.DGN Turning Radii - No Slip Angle Figure 4.1 Section 4 Page 4-2
4.3. MINIMUM TURNING RADII R5 R6 R6.44 m 21 ft 1 in 76 21.4 m 7ft 3 in (RUNWAY MINIMUM WIDTH) R1 R14. 7 m 46 ft 2 in R3 1 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 STEEL NOSE R1 NOSE GEAR R2 OUTBOARD GEAR R3 INBOARD GEAR R4 RIGHT WINGLET R5 RIGHT TAILTIP R6 76 18.12 m 59 ft 5 in 14.36 m 47 ft 1 in 7.4 m 23 ft 1 in.17 m 7 in 18.39 m 6 ft 4 in 2.51 m 67 ft 3 in 1 THEORETICAL CENTER OF TURN FOR MINIMUN RADIUS. SHOWS CONTINUOUS TURNING WITH ENGINE THRUST AS REQUIRED. NO DIFFERENTIAL BRAKING. EM17APM49B.DGN Minimum Turning Radius Figure 4.2 Section 4 Page 4-3
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.) 15 27.8 CL FUS HOR PILOT S EYE POSITION.75 m (2 ft 6 in.) 14.58 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 28.1 27.5 EM17APM41.DGN Visibility from Cockpit in Static Position Figure 4.3 Section 4 Page 4-4
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 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 19STD, 19LR and 19AR is 3C. 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 2 in). Section 4 Page 4-5
45 m (147 ft 7.6 in.) NOTE: COORDINATE WITH AIRLINE OPERATOR FOR THE SPECIFIC PLANNED OPERATING PROCEDURE. 45 NOSE LANDING GEAR STEERING ANGLE IS APPROXIMATELY 15. 1 ft RADIUS (3 m) 15 m (49 ft 2 in.) PATH OF MAIN LANDING GEAR TIRE EDGE EM17APM411A.DGN More than 9 Turn - Runway to Taxiway Figure 4.4 Section 4 Page 4-6
45 m (147 ft 7.6 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. EM17APM412A.DGN 9 Turn - Runway to Taxiway Figure 4.5 Section 4 Page 4-7
15 m (49 ft 2 in.) NOTE: COORDINATE WITH AIRLINE OPERATOR FOR THE SPECIFIC PLANNED OPERATING PROCEDURE. NOSE LANDING GEAR STEERING ANGLE IS APPROXIMATELY 28. 9 15 m (49 ft 2 in.) 1 ft Radius (3 m) 3 m (9 ft 1 in.) PATH OF MAIN LANDING GEAR TIRE EDGE. EM17APM413.DGN 9 Turn - Taxiway to Taxiway Figure 4.6 Section 4 Page 4-8
4.6. RUNWAY HOLDING APRON RUNWAY 45 m (147 ft 7.6 in.) MINIMUM CLEARENCES 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 EM17APM414A.DGN Runway Holding Bay Figure 4.7 Section 4 Page 4-9 / 1
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
5.1. AIRCRAFT SERVICING ARRANGEMENT 11 3 5 3 7 1 3 9 8 25 4 2 2 4 7 2 LENGTH ft 6 5 LENGTH m 15 4 3 1 2 1 5 1 9 8 1 6 5 1 15 2 25 3 35 4 LENGTH m 45 1 2 3 4 5 6 7 8 9 1 11 12 LENGTH ft 13 14 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 EM17APM511A.DGN Aircraft Servicing Arrangement With Passenger Stairs Figure 5.1 Section 5 Page 5-2
11 3 5 3 7 1 3 9 8 25 4 2 2 4 7 2 LENGTH ft 6 5 LENGTH m 15 4 3 1 1 2 1 5 8 6 5 1 15 2 25 3 35 LENGTH m 4 45 1 2 3 4 5 6 7 8 9 1 11 12 LENGTH ft 13 14 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 EM17APM512.DGN Aircraft Servicing Arrangement With Passenger Bridge Figure 5.2 Section 5 Page 5-3
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
ELAPSED TIME (MINUTES) 1 2 3 4 5 6 7 8 9 1 11 1213 14 15 16 17 18 19 2 OPERATIONS min. BRIDGE / STAIRS POSITIONING 1, PASSENGERS DEPLANE 4.1 PAX SERVICES GALLEY SERVICING FWD GALLEY SERVICING AFT AIRPLANE INTERIOR SERVICES PASSENGERS ENPLANE 7, 7, 6.1 6.1 BRIDGE / STAIRS REMOVAL 1, PUSH BACK / ENGINES START 2, FWD BAGGAGE / CARGO UNLOAD 4.3 BAGGAGE & CARGO AIRCRAFT SERVICING REAR BAGGAGE / CARGO UNLOAD TIME BETWEEN UNLOADING / LOADING FWD BAGGAGE/CARGO LOAD AFT BAGGAGE/CARGO LOAD FUEL SERVICE POTABLE WATER SERVICE TOILET SERVICE 3.5,5 7.1 5.8 11.7 3, 5, LEGEND: NOTE: TRUCK POSITIONING/REMOVAL/SETTINGS 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. EM17APM513A.DGN Air Terminal Operation - Turnaround Station Figure 5.3 Section 5 Page 5-5
5.3. TERMINAL OPERATIONS - EN ROUTE STATION Not Applicable Section 5 Page 5-6
5.4. GROUND SERVICING CONNECTIONS 1 2 7 8 6 22 5 4 11 3 9 1 12 13 16 14 15 21 2 19 18 17 ITEM 1 2 3 4 5 6 7 8 9 1 11 12 13 14 15 16 17 18 19 2 21 22 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) 17316.95 17695.4 COORD. Y (mm) NOTE: THE GROUND CLEARANCES IN THE TABLE REFER TO THE AIRCRAFT WITH THE MINIMUM OPERATING WEIGHT (MOW) = 295 kg (CG FWD 4.% CMA) COORD. Z (mm) 783.78 543.75 7774.46 31.92 HEIGHT ABOVE GROUND (mm) 2862.76 314.19 17932.67 7646.75 38.24 3112.32 4164.44 936.13 1262.71 1842.51 4136.97 951.46 1279.29 1825.31 4125.32. 2854.38 25.36 13268.52. 1979.71 1334.39 13629.1 57.25 1952.83 1369.51 1852.28 293.25 1744.67 1679.1 1878.3 297. 2988.86 435.73 1878.3 297. 2988.86 435.73 2139.16 88.1 162.4 1869.43 27861.83 329.37 1178.74 2469.64 3421.65 471.73 65.3 311.6 3562.26 449.47 585.54 3124.58 6562.14 1159.87 961.5 219.6 16444.9 691.6 1611.45 1775.35 16476.65 526.5 1611.45 1776.8 2139.16 88.1 162.4 1869.43 28784.1 349.2 991.8 2677.66 3398.86 519.15 59.9 3116.29 EXTERNAL POWER SUPPLY 115 VAC 4146.9 81.7 1339.53 1765.31 EM17APM514E.DGN Ground Servicing Connections Figure 5.4 Section 5 Page 5-7