AIRPORT PLANNING MANUAL
|
|
- Betty Letitia Hunter
- 6 years ago
- Views:
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 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.
2
3 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) May 11/7 List of Tables * 1 (rev)... 2 Blank... Aug 15/5 List of Figures * 1 (rev) Oct 31/ May 11/7 4 Blank... Aug 15/5 Section Jan 9/ Oct 6/ Oct 6/ 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
4 * 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) (del)... Dec 18/6 7-2 (del)... Dec 18/ (del)... Dec 18/ (del)... Dec 18/ (del)... Dec 18/ 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
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 Lengths Landing Fields Lengths 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 EFFECTIVITY: ALL TABLE OF CONTENTS Page 1
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, US 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 19 DERIVATIVE AIRCRAFT 8. Possible EMBRAER 19 Derivative Aircraft Not Applicable SECTION 9 - SCALED DRAWINGS 9. Scaled Drawings General EFFECTIVITY: ALL 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. EFFECTIVITY: ALL Section 1 Page 1-1 Jan 9/6
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 EFFECTIVITY: ALL 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 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
10
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 ( 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
12 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 4795 kg (15712 lb) 546 kg ( lb) 5196 kg ( lb) MTOW 4779 kg (15359 lb) 53 kg (11892 lb) 518 kg ( 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] m 3 ( 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.) GENERAL AIRCRAFT DIMENSIONS External Dimensions Span over winglets m (94 ft 3 in.) Height (maximum) m (34 ft 7 in.) Overall length m (118 ft 11 in.) Wing Reference area m 2 (996 ft 2 ) Reference aspect ratio Section 2 Page 2-2
13 Fuselage Total Length m (118 ft 11 in.) Length of pressurized section m (95 ft 5 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
14 6.82 m (45 ft 4 in.) m (8 ft 1 in.) 1.57 m (34 ft 8 in.) 4.13 m (13 ft 6 in.) m (45 ft 4 in.) 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.) m (94 ft 3 in.) EM17APM211B.DGN General Aircraft Dimensions Figure 2.1 Section 2 Page 2-4
15 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
16 WEIGHT 4795 kg lb 4795 kg lb 4779 kg lb 4779 kg lb 43 kg lb 43 kg lb 48 kg lb 48 kg lb CG (%MAC) FUS ANGLE (DEG) (A) NOSE (B) 2.7 m 6ft9in m 7ft 2.5 m 6ft9in m 7ft 2.6 m 6ft9in m 7ft 2.6 m 6ft9in m 7ft FOR- WARD SERVICE DOOR (C) 2.58 m 8ft5in m 8ft7in m 8ft5in m 8ft7in m 8ft6in m 8ft8in m 8ft6in m 8ft8in. Table 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 m 8ft8in m 8ft6in m 5ft2in m 5ft3in 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 m 1 ft 8 in m 1 ft 8 in m 1 ft 8 in m 6ft5in m 6ft4in m 6ft6in. 3.3 m 9ft9in m 8ft8in. 3.3 m 9ft11in m 8ft8in m 5ft3in..5 m 1ft8in. 5.6 m 16 ft 7 in m 1 ft 8 in m 6ft4in m 9ft8in. 2.6 m 8ft6in m 5ft2in..5 m 1ft8in m 16 ft 9 in m 1 ft 8 in. 2.m 6ft7in. 3.6 m 9ft12in m 8ft9in m 5ft4in..51 m 1ft8in. 5.8 m 16 ft 8 in m 1 ft 8 in m 6ft5in m 9ft9in. 2.6 m 8ft6in m 5ft3in..51 m 1ft8in m 16 ft 1 in m 1 ft 9 in. 2.2 m 6ft7in. 3.7 m 1 ft 2.66 m 8ft9in m 5ft5in..52 m 1ft9in. 5.9 m 16 ft 8 in m 1 ft 9 in m 6ft5in. 3. m 9ft1in. AFT PASSEN- GER DOOR (L) 3.3 m 9ft9in m 8ft8in. 3.3 m 9ft11in m 9ft8in. 3.6 m 9ft12in m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. VERTI- CAL TAIL (M) 1.4 m 34 ft 2 in m 33 ft 9 in m 34 ft 2 in m 33 ft 1 in m 34 ft 3 in m 33 ft 1 in m 34 ft 4 in m 33 ft 11 in. TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (N) Section 2 Page 2-6
17 WEIGHT 546 kg lb 546kg lb 53kg 11892lb 53kg lb 43 kg lb 43 kg lb 48 kg lb 48 kg lb CG (%MAC) FUS ANGLE (DEG) (A) NOSE (B) 2.6 m 6ft9in m 7ft 2.6 m 6ft9in m 7ft 2.6 m 6ft9in m 7ft 2.6 m 6ft9in m 7ft2in. Table 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 m 8ft8in m 8ft5in m 8ft8in m 8ft6in m 8ft5in m 8ft7in m 8ft5in m 8ft7in. 2.6 m 8ft6in m 5ft2in. 1.6m 5ft4in m 5ft2in. 1.6 m 5ft4in 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 m 16 ft 9 in m 1 ft 7 in m 1 ft 7 in m 1 ft 7 in m 1 ft 7 in m 1 ft 8 in m 6ft5in. 1.94m 6ft4in m 6ft5in m 6ft4in. 2. m 6ft7in m 8ft8in m 8ft9in m 5ft4in..51 m 1ft8in. 5.8 m 16 ft 8 in m 1 ft 8 in m 6ft5in m 8ft6in. 2.6 m 8ft6in m 5ft3in..51 m 1ft8in m 16 ft 1 in m 1 ft 9 in. 2.2 m 6ft7in m 8ft8in m 8ft9in m 5ft5in..52 m 1ft9in. 5.9 m 16 ft 8 in m 1 ft 9 in m 6ft5in. AFT SERVICE DOOR (K) 3.2 m 9ft1in m 9ft8in. 3.2 m 9ft1in m 9ft8in. 3.6 m 9ft12in m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. AFT PASSEN- GER DOOR (L) 3.2 m 9ft1in m 9ft8in. 3.2 m 9ft1in m 9ft8in. 3.6 m 9ft12in m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. VERTI- CAL TAIL (M) 1.4 m 34 ft 1 in m 33 ft 9 in. 1.4 m 34 ft 1in m 33 ft 9 in m 34 ft 3 in m 33 ft 1 in m 34 ft 4 in m 33 ft 11 in. TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (N) Section 2 Page 2-7
18 WEIGHT 5196 kg lb 5196 kg lb 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) NOSE (B) 2.6 m 6ft9in m 7ft 2.6 m 6ft9in. 2.12m 7ft 2.6 m 6ft9in m 7ft 2.6 m 6ft9in m 7ft2in. Table 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 m 8ft8in m 8ft5in m 8ft8in m 8ft6in m 8ft6in m 8ft7in m 8ft6in m 8ft7in. 2.6 m 8ft6in m 5ft2in. 1.6 m 5ft4in m 5ft2in. 1.6 m 5ft4in 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 m 16 ft 9 in m 1 ft 7 in m 1 ft 7 in m 1 ft 7 in m 1 ft 7 in m 1 ft 8 in m 6ft5in m 6ft4in m 6ft5in m 6ft4in. 2. m 6ft7in m 8ft8in m 8ft8in m 5ft4in..51 m 1ft8in. 5.7 m 16 ft 8 in m 1 ft 8 in m 6ft5in m 8ft6in. 2.6 m 8ft6in m 5ft3in..51 m 1ft8in m 16 ft 1 in m 1 ft 9 in. 2.2 m 6ft7in m 8ft8in m 8ft9in m 5ft4in..52 m 1ft9in. 5.9 m 16 ft 8 in m 1 ft 9 in m 6ft5in. AFT SERVICE DOOR (K) 3.1 m 9ft1in m 9ft8in. 3.1 m 9ft1in m 9ft8in. 3.3 m 9ft12in m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. AFT PASSEN- GER DOOR (L) 3.1 m 9ft1in m 9ft8in. 3.1 m 9ft1in m 9ft8in. 3.3 m 9ft12in m 9ft9in. 3.7 m 1 ft 3. m 9ft1in. VERTI- CAL TAIL (M) 1.4 m 34 ft 1 in m 33 ft 9 in. 1.4 m 34 ft 1in m 33 ft 9 in m 34 ft 3 in m 33 ft 1 in m 34 ft 4 in m 33 ft 11 in. TAIL SKID ANGU- LAR CLEAR- ANCE (DEG) (N) Section 2 Page 2-8
19 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 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 m (9 ft) Aisle wide -.49 m (1 ft 7 in.) Pitch -.82 m (32 in.) Section 2 Page 2-9
20 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.) 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.) m (85 ft) m (2 ft 8 in.) m (4 ft 1 in.) 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 m ( 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
21 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] 185 kg (478 lb) m 3 ( ft 3 ) Aft 165 kg (3638 lb) 1.22 m 3 (36.92 ft 3 ) Total 35 kg (7716 lb) m 3 ( 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
22 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
23 .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
24 2.6. LOWER COMPARTMENT CONTAINERS Not Applicable Section 2 Page 2-14
25 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
26
27 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 ( 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, 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
28 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
29 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) kg PAYLOAD lb PAYLOAD kg 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 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
30 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) 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 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
31 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) kg PAYLOAD lb PAYLOAD kg LONG RANGE 6 3 MAX CRUISE MACH 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
32 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) 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 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
33 PAYLOAD VS RANGE CF34 1E5A, 1E5A1, 1E6A, 1E6A1 & 1E7 ENGINES FLIGHT LEVEL 37 ISA RESERVE : 1 nm ALTERNATE + 45 min FLIGHT MTOW = 518 kg ( 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 518 kg ( 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
34 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 ( lb) kg PAYLOAD lb PAYLOAD kg LONG RANGE MAX CRUISE.78 MACH RANGE nm NOTES: MAX TAKEOFF WEIGHT MAX ZERO FUEL WEIGHT BASIC OPERATING WEIGHT MAX USABLE FUEL 518 kg ( 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
35 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
36 TAKEOFF FIELD LENGTH CF 34 1E5 & 1E6 1 MODE ATTCS OFF / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA AIRPORT PRESSURE ALTITUDE m (ft) FLAP FLAP 3 6 FIELD LENGTH ft FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM336D.DGN Takeoff Field Lengths - ISA Conditions Figure 3.7 Section 3 Page 3-1
37 TAKEOFF FIELD LENGTH CF34 1E5 & 1E6 T/O 1 MODE ATTCS OFF / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15 C AIRPORT PRESSURE ALTITUDE m (ft) FLAP FLAP FIELD LENGTH ft FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM337D.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.8 Section 3 Page 3-11
38 TAKEOFF FIELD LENGTH CF34 1E5 & 1E6 T/O 1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA AIRPORT PRESSURE ALTITUDE m (ft) FLAP FLAP FIELD LENGTH ft FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM338D.DGN Takeoff Field Lengths - ISA Conditions Figure 3.9 Section 3 Page 3-12
39 TAKEOFF FIELD LENGTH CF34 1E5 & 1E6 T/O 1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15 C AIRPORT PRESSURE ALTITUDE m (ft) FLAP FLAP FIELD LENGTH ft FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM339D.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.1 Section 3 Page 3-13
40 TAKEOFF FIELD LENGTH CF34 1E7 1 MODE ATTCS OFF CF34 1E5A1 & 1E6A1 1 MODE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA FLAP FLAP FIELD LENGTH ft FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM334C.DGN Takeoff Field Lengths - ISA Conditions Figure 3.11 Section 3 Page 3-14
41 TAKEOFF FIELD LENGTH CF34 1E7 1 MODE ATTCS OFF / ECS OFF CF34 1E5A1 & 1E6A1 ENGINES@T/O 1 MODE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15 C FLAP FLAP FIELD LENGTH ft FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM335C.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.12 Section 3 Page 3-15
42 TAKEOFF FIELD LENGTH CF 34 1E7 1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA AIRPORT PRESSURE ALTITUDE m (ft) FLAP 3 FIELD LENGTH ft FLAP 4 2 SEA LEVEL WEIGHT kg WEIGHT lb EM17APM34C.DGN Takeoff Field Lengths - ISA Conditions Figure 3.13 Section 3 Page 3-16
43 TAKEOFF FIELD LENGTH CF 34 1E7 1 MODE ATTCS ON / ECS OFF DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY ISA + 15 C AIRPORT PRESSURE ALTITUDE m (ft) FLAP FIELD LENGTH ft FLAP SEA LEVEL WEIGHT kg WEIGHT lb EM17APM341C.DGN Takeoff Field Lengths - ISA + 15 C Conditions Figure 3.14 Section 3 Page 3-17
44 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
45 LANDING FIELD LENGTH CF 34 1E5 1E5A1 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft LAND FIELD LENGTH m WEIGHT kg EM17APM346C.DGN Landing Field Lengths - Flaps 5 Figure 3.15 EFFECTIVITY: EASA-CERTIFIED Section 3 Page 3-19
46 LANDING FIELD LENGTH CF34 1E5 1E5A1 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft 4 LAND FIELD LENGTH m WEIGHT kg EM17APM347C.DGN Landing Field Lengths - Flaps Full Figure 3.16 EFFECTIVITY: EASA-CERTIFIED Section 3 Page 3-2
47 6 LANDING FIELD LENGTH CF 34 1E7 ENGINE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft LAND FIELD LENGTH m WEIGHT kg EM17APM362B.DGN Landing Field Lengths - Flaps 5 Figure 3.17 EFFECTIVITY: EASA-CERTIFIED Section 3 Page 3-21
48 LANDING FIELD LENGTH CF 34 1E7 ENGINE DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft 4 LAND FIELD LENGTH m WEIGHT kg EM17APM363B.DGN Landing Field Lengths - Flaps Full Figure 3.18 EFFECTIVITY: EASA-CERTIFIED Section 3 Page 3-22
49 LANDING FIELD LENGTH CF 34 1E5 1E5A1 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft 5 LAND FIELD LENGTH m WEIGHT kg EM17APM317A.DGN Landing Field Lengths - Flaps 5 Figure 3.19 EFFECTIVITY: FAA-CERTIFIED Section 3 Page 3-23
50 LANDING FIELD LENGTH CF 34 1E5 1E5A1 1E6 & 1E6A1 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft 5 4 LAND FIELD LENGTH m WEIGHT kg EM17APM318A.DGN Landing Field Lengths - Flaps Full Figure 3.2 EFFECTIVITY: FAA-CERTIFIED Section 3 Page 3-24
51 LANDING FIELD LENGTH CF 34 1E7 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP 5 ISA AIRPORT PRESSURE ALTITUDE m (ft) FIELD LENGTH ft 5 LAND FIELD LENGTH m WEIGHT kg EM17APM319A.DGN Landing Field Lengths - Flaps 5 Figure 3.21 EFFECTIVITY: FAA-CERTIFIED Section 3 Page 3-25
52 LANDING FIELD LENGTH CF 34 1E7 ENGINES DRY, SMOOTH, HARD PAVED AND LEVEL RUNWAY FLAP FULL ISA AIRPORT PRESSURE ALTITUDE m (ft) 17 FIELD LENGTH ft 5 4 LAND FIELD LENGTH m WEIGHT kg EM17APM32A.DGN Landing Field Lengths - Flaps Full Figure 3.22 EFFECTIVITY: FAA-CERTIFIED Section 3 Page 3-26
53 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 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
54 R5 R6 R3 R6.44 m 21ft 2 in 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 m m 22.5 m m 2.24 m m m m 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 R m m m m m 16.7 m m m 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 R m 2.3 m m m m 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 R m 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 R m m m m m m 21.3 m m 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 R m m 26.9 m m 24.2 m m 22.5 m 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
55 4.3. MINIMUM TURNING RADII R5 R6 R6.44 m 21 ft 1 in 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 R m 59 ft 5 in m 47 ft 1 in 7.4 m 23 ft 1 in.17 m 7 in 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
56 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
57 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 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
58 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 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
59 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
60 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. EM17APM413.DGN 9 Turn - Taxiway to Taxiway Figure 4.6 Section 4 Page 4-8
61 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
62
63 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
64 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 AIR CONDITIONING 9 PNEUMATIC STARTER EM17APM511A.DGN Aircraft Servicing Arrangement With Passenger Stairs Figure 5.1 Section 5 Page 5-2
65 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 EM17APM512.DGN Aircraft Servicing Arrangement With Passenger Bridge Figure 5.2 Section 5 Page 5-3
66 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
67 ELAPSED TIME (MINUTES) 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, 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, 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
68 5.3. TERMINAL OPERATIONS - EN ROUTE STATION Not Applicable Section 5 Page 5-6
69 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) = 295 kg (CG FWD 4.% CMA) COORD. Z (mm) HEIGHT ABOVE GROUND (mm) EXTERNAL POWER SUPPLY 115 VAC EM17APM514E.DGN Ground Servicing Connections Figure 5.4 Section 5 Page 5-7
AIRPORT PLANNING MANUAL
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-1997 28
More information@AIRBUS A /-600 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
@AIRBUS A340-500/-600 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More information@AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More information@AIRBUS A320 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A320 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More information@AIRBUS A319 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A319 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More information@AIRBUS A321 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A321 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More informationAIRPORT PLANNING MANUAL TRANSMITTAL LETTER REVISION 9
TRANSMITTAL LETTER REVISION 9 This package contains the CRJ1000 Aircraft Airport Planning Manual, CSP D 020, Revision 9, dated Dec 20/2016. TRANSMITTAL LETTER Page 1 Dec 20/2016 THIS PAGE INTENTIONALLY
More information@AIRBUS A319 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A319 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More informationEuropean Aviation Safety Agency
TCDS No.: EASA.IM.A.526 EMB-550 Page 1 of 11 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. EASA.IM.A.526 for EMB-550 Type Certificate Holder: Embraer S.A. Av. Brigadeiro Faria Lima,2170.
More informationAIRPORT PLANNING MANUAL
AIRPORT PLANNING MANUAL Technical Publications Manual Change Request B TO: MCR FOCAL, TECHNICAL PUBLICATIONS BOMBARDIER AEROSPACE 123 GARRATT BLVD. TORONTO, ONTARIO, CANADA, M3K 1Y5 MAIL STOP: N42 25
More information@AIRBUS A321 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A321 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More information5.2 Terminal Operations - Turnaround Station. 5.3 Terminal Operations - En Route Station. 5.4 Ground Servicing Connections
5. TERMINAL SERVICING 5.1 Airplane Servicing Arrangement Typical Turnaround 5.2 Terminal Operations Turnaround Station 5.3 Terminal Operations En Route Station 5.4 Ground Servicing Connections 5.5 Engine
More information4.1 General Information. 4.2 Turning Radii. 4.3 Clearance Radii. 4.4 Visibility From Cockpit in Static Position. 4.5 Runway and Taxiway Turn Paths
4.0 GROUND MANEUVERING 4.1 General Information 4.2 Turning Radii 4.3 Clearance Radii 4.4 Visibility From Cockpit in Static Position 4.5 Runway and Taxiway Turn Paths 4.6 Runway Holding Bay DECEMBER 2002
More informationTYPE-CERTIFICATE DATA SHEET
TCDS No.:EASA.IM.A.013 Gulfstream 200 / Galaxy Issue: 03 Date: 03 July 2017 TYPE-CERTIFICATE DATA SHEET EASA.IM.A.013 for GULFSTREAM 200 / GALAXY Type Certificate Holder GULFSTREAM AEROSPACE LP (GALP P.O.
More informationTypical Reserve Policy
Three View Drawing Payload Range Length Height Wingspan 29.94 m / 98.2 ft.28 m /.7 ft 27.80 m / 91.21 ft Flight Techniques: Climb: 20Kts/280Kts/M 0.78 Cruise: M 0.78 / FL 70 Descent: 0.78/280Kts/20Kts
More information5.2 Terminal Operations - Turnaround Station. 5.3 Terminal Operations - En Route Station. 5.4 Ground Servicing Connections
5.0 TERMINAL SERVICING 5.1 Airplane Servicing Arrangement Typical Turnaround 5.2 Terminal Operations Turnaround Station 5.3 Terminal Operations En Route Station 5.4 Ground Servicing Connections 5.5 Engine
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.073 for Beechcraft 390 (PREMIER I and IA) Type Certificate Holder: Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 USA For Models: Model 390 1
More informationEuropean Aviation Safety Agency
TCDS IM.A.080 BD100-1A10 (Challenger 300) Page 1/11 Issue 3.0, 26 October 2010 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET IM.A.080 CHALLENGER 300 Manufacturer: BOMBARDIER INC. P.
More informationTYPE-CERTIFICATE DATA SHEET
SF340A, 340B TYPE-CERTIFICATE DATA SHEET No. EASA.A.068 for SF340A, 340B Type Certificate Holder: Saab AB 581 88 Linköping SWEDEN For Models: SF340A, 340B TE.CERT.00051-001 European Aviation Safety Agency,
More informationMD-11 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
REPORT MDC K0388 REVISION E ISSUED: 1996 MD-11 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING OCTOBER 1990 To Whom It May Concern: This document is intended for airport planning purposes. Specific aircraft
More informationEuropean Aviation Safety Agency
TCDS EASA.A.109 ASI AVIATION Page 1 of 10 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.109 F 406 Type Certificate Holder : ASI AVIATION 14 allée René Fonck 51100 REIMS France
More informationEuropean Aviation Safety Agency
TCDS EASA.IM.A.162 Page 1/9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Tupolev TU 204-120CE Manufacturer: Tupolev PSC 17, Tupolev Embankment 111250 Moscow Russia For model: TU 204-120CE
More informationTYPE-CERTIFICATE DATA SHEET
TCDS No.: EASA.IM.A.207 Issue: 04 Date: 28 August 2018 TYPE-CERTIFICATE DATA SHEET No. EASA.IM.A.207 for CESSNA 500, 550, S550, 560, 560XL Type Certificate Holder: Textron Aviation Inc. One Cessna Boulevard
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.003 for Type Certificate Holder Erickson Incorporated, DBA Erickson Air-Crane 3100 Willow Springs Road P.O. Box 3247 Central Point, Oregon, 97502-0010 U.S.A. For
More informationA300 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING HIGHLIGHTS REVISION 22 DEC 01/09
A300 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING HIGHLIGHTS REVISION 22 DEC 01/09 This revision concerns introduction of new pages and corrections of pages. Description of change. SECTION PAGE(s) REASON
More information@AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More informationLCN ACN-PCN
7.0 PAVEMENT DATA 7.1 General Information 7.2 Footprint 7.3 Maximum Pavement Loads 7.4 Landing Gear Loading on Pavement 7.5 Flexible Pavement Requirements 7.6 Flexible Pavement Requirements, LCN Conversion
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A33EU
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A33EU Revision 2 DASSAULT-BREGUET Falcon 10 September 3, 1987 TYPE CERTIFICATE DATA SHEET NO. A33EU This data sheet which is a part of Type
More informationHawker Beechcraft Corporation on March 26, 2007
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00010WI Revision 8 Hawker Beechcraft 390 March 26, 2007 TYPE CERTIFICATE DATA SHEET NO. A00010WI This data sheet, which is part of Type Certificate
More informationSECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST
SECTION 6 WEIGHT AND BALANCE / EQUIPMENT LIST TABLE OF CONTENTS Page Introduction... 6-3 Airplane Weighing Procedures... 6-4 Airplane Weighing Form... 6-5 Sample Weight and Balance Record... 6-8 Loading
More informationTYPE-CERTIFICATE DATA SHEET
Issue: 03 Date: 25/07/2018 TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.636 for Model 3000 Type Certificate Holder Textron Aviation Defense LLC 9709 East Central 67206 Wichita, Kansas United States of America
More informationPage 1 of 7 01-Mar-2013 EASA.IM.A.341. Company. Be-103. Issue 2 EASA. Taganrog, BE-103. For models: general
Page 1 of 7 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.IM.A.341 BE-103 Type Certificate Holder: Berievv Aircraft Company 1,, Aviatorovv square Taganrog, 347923 RUSSIA For models:
More informationTYPE-CERTIFICATE DATA SHEET
TCDS No.: EASA.A.069 SAAB 2000 TYPE-CERTIFICATE DATA SHEET No. EASA.A.069 for SAAB 2000 Type Certificate Holder: Saab AB 581 88 Linköping SWEDEN For Models: SAAB 2000 TE.CERT.00051-001 European Aviation
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.A.607 for BS 115 Type Certificate Holder BLACKSHAPE S.P.A. Strada Statale 16 KM 841+900 70043 Monopoli (BA) ITALY For models: BS 115 TE.CERT.00048-001 European Aviation
More informationAIRCRAFT DESIGN SUBSONIC JET TRANSPORT
AIRCRAFT DESIGN SUBSONIC JET TRANSPORT Analyzed by: Jin Mok Professor: Dr. R.H. Liebeck Date: June 6, 2014 1 Abstract The purpose of this report is to design the results of a given specification and to
More informationSECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST
SECTION 6 WEIGHT AND BALANCE / EQUIPMENT LIST TABLE OF CONTENTS Page Introduction... 6-3 Airplane Weighing Procedures... 6-4 Airplane Weighing Form... 6-5 Weight and Balance... 6-7 Sample Weight and Balance
More informationThis Flight Planning Guide is published for the purpose of providing specific information for evaluating the performance of the Cessna Corvalis TT.
May 2010 TABLE OF CONTENTS This Flight Planning Guide is published for the purpose of providing specific information for evaluating the performance of the Cessna Corvalis TT. This guide is developed from
More informationEuropean Aviation Safety Agency
Page 1/8 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Cirrus Design SF50 Type Certificate Holder: Cirrus Design Corporation 4515 Taylor Circle Duluth, Minnesota 55811 United States
More information787-8 LAN AIRLINES S.A. WEIGHT AND BALANCE CONTROL AND LOADING MANUAL
LAN AIRLINES S.A. WEIGHT AND BALANCE Export controlled by ECCN 9E991 No License is required for the dissemination of the commercial information contained herein to foreign persons other than those from
More informationEuropean Aviation Safety Agency
TCDS No.: EASA.IM.A.212 Learjet M60 Page 1 of 15 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET No. EASA.IM.A.212 for LEARJET Model 60 Type Certificate Holder: Learjet Inc. One Learjet
More informationChapter 3: Aircraft Construction
Chapter 3: Aircraft Construction p. 1-3 1. Aircraft Design, Certification, and Airworthiness 1.1. Replace the letters A, B, C, and D by the appropriate name of aircraft component A: B: C: D: E: 1.2. What
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.120 for Type Certificate Holder Robinson Helicopter Company 2901 Airport Drive Torrance, CA 90505 U.S.A. For Models:, Alpha, Beta, Mariner TE.CERT.00049-001 European
More informationEuropean Aviation Safety Agency
TCDS EASA.A.191 Page 1/15 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Jetstream 3100 / 3200 Series Type Certificate Holder: BAE SYSTEMS (OPERATIONS) LTD Prestwick International Airport
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A18SW. San Antonio, Texas
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A18SW Revision 2 Fairchild Aircraft, Inc. SA227-CC SA227-DC (C-26B) November 14, 1996 TYPE CERTIFICATE DATA SHEET A18SW Type Certificate Holder:
More informationMALAYSIAN AIRLINE SYSTEM BERHAD WEIGHT AND BALANCE CONTROL AND LOADING MANUAL
MALAYSIAN AIRLINE SYSTEM BERHAD WEIGHT AND BALANCE Export controlled by ECCN 9E991 No License is required for the dissemination of the commercial information contained herein to foreign persons other than
More information7.0 PAVEMENT DATA. 7.1 General Information. 7.2 Landing Gear Footprint. 7.3 Maximum Pavement Loads
7.0 PAVEMENT DATA 7.1 General Information 7.2 Landing Gear Footprint 7.3 Maximum Pavement Loads 7.4 Landing Gear Loading on Pavement 7.5 Flexible Pavement Requirements - U.S. Army Corps of Engineers Method
More informationEuropean Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET EASA.A.155 FALCON 7X. DASSAULT AVIATION 9 Rond Point Marcel Dassault PARIS
TCDS A.155 Page 1/11 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET EASA.A.155 FALCON 7X DASSAULT AVIATION 9 Rond Point Marcel Dassault 75008 PARIS For models: FALCON 7X Issue 4.0: 20
More informationAircraft Design Conceptual Design
Université de Liège Département d Aérospatiale et de Mécanique Aircraft Design Conceptual Design Ludovic Noels Computational & Multiscale Mechanics of Materials CM3 http://www.ltas-cm3.ulg.ac.be/ Chemin
More informationLiberty Aerospace, Inc. Section 1 SECTION 1 GENERAL TABLE OF CONTENTS
Liberty Aerospace, Inc. Section 1 SECTION 1 TABLE OF CONTENTS Introduction... 1-3 Airplane Three Views... 1-4 Descriptive Data... 1-5 Engine... 1-5 Propeller... 1-5 Fuel... 1-5 Oil... 1-5 Maximum Certificated
More informationEuropean Aviation Safety Agency
TCDS A.004 Page 1/36 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.004 AIRBUS A330 AIRBUS 1 Rond-point Maurice Bellonte 31707 Blagnac France For models: A330-201 A330-223 A330-301
More informationCessna Citation Model Stats
Cessna Citation Model Stats Cessna Citation Sovereign - Dimensions Length 63 ft 6 in (19.35 m) Height 20 ft 4 in (6.20 m) Wingspan 72 ft 4 in (22.04 m) Wing Wing Area Wing Sweep Wheelbase Tread 516 sq
More informationEuropean Aviation Safety Agency
TCDS IM.A.226 Cessna Aircraft Company Page 1 of 20 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Cessna Model 208 Type Certificate Holder: Cessna Aircraft Company P.O. Box 7704 Wichita,
More informationLCN ACN-PCN
7.0 PAVEMENT DATA 7.1 General Information 7.2 Footprint 7.3 Maximum Pavement Loads 7.4 Landing Gear Loading on Pavement 7.5 Flexible Pavement Requirements 7.6 Flexible Pavement Requirements, LCN Conversion
More informationEuropean Aviation Safety Agency
Page 1 of 17 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.011 Extra Flugzeugproduktions- und Vertriebs GmbH Schwarze Heide 21 D-46569, Hünxe Germany For models: -500 Issue 24
More informationERF LOADAIR CARGO WEIGHT AND BALANCE CONTROL AND LOADING MANUAL. Export controlled by EAR99
LOADAIR CARGO WEIGHT AND BALANCE Export controlled by EAR99 Boeing Commercial Airplane Group Weight Engineering Organization P.O. Box 3707 Seattle, Washington 98124 Boeing Document No. INTRODUCTION The
More informationAIR TRACTOR, INC. OLNEY, TEXAS
TABLE OF CONTENTS LOG OF REVISIONS... 2 DESCRIPTION... 4 SECTION 1 LIMITATIONS... 5 SECTION 2 NORMAL PROCEDURES... 8 SECTION 3 EMERGENCY PROCEDURES... 8 SECTION 4 MANUFACTURER'S SECTION - PERFORMANCE...
More informationEuropean Aviation Safety Agency
TCDS EASA IM.A.157 Page 1/9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Embraer EMB-500 Manufacturer: Embraer Embraer SA Av. Brig. Faria Lima. 2170 12227-901 São Jose dos Campos SP
More informationEuropean Aviation Safety Agency
Page 1 of 10 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.IM.A.158 EMBRAER Type Certificate Holder: Embraer Embraer S.A. Av. Brig. Faria Lima. 2170 12227-901 São Jose dos Campos
More informationAircraft Design in a Nutshell
Dieter Scholz Aircraft Design in a Nutshell Based on the Aircraft Design Lecture Notes 1 Introduction The task of aircraft design in the practical sense is to supply the "geometrical description of a new
More informationEuropean Aviation Safety Agency
TCDS No.: TCDS IM.A.020 Learjet 45 Page 1 of 35 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. TCDS IM.A.020 for LEARJET MODEL 45 Type Certificate Holder: Learjet Inc. One Learjet
More informationTYPE-CERTIFICATE DATA SHEET EASA.A.060. Ae 270
TCDS EASA.A.060 Ae 270 Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.060 Ae 270 Type Certificate Holder: AIRCRAFT INTEGRATED SOLUTIONS LTD International House 12 Constance
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. TYPE CERTIFICATE DATA SHEET No. A50NM
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A50NM Dassault Aviation Falcon 2000 December 19, 1995 TYPE CERTIFICATE DATA SHEET No. A50NM This data sheet which is part of Type Certificate
More information7.1 General Information. 7.2 Landing Gear Footprint. 7.3 Maximum Pavement Loads. 7.4 Landing Gear Loading on Pavement
7.0 PAVEMENT DATA 7.1 General Information 7.2 Landing Gear Footprint 7.3 Maximum Pavement Loads 7.4 Landing Gear Loading on Pavement 7.5 Flexible Pavement Requirements - U.S. Army Corps of Engineers Method
More informationEuropean Aviation Safety Agency
TCDS IM.A.228 Page 1/16 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET GULFSTREAM G150 Type Certificate Holder: GULFSTREAM AEROSPACE LP (GALP) P.O. Box 1036 Airport City 7019900, Israel
More informationEuropean Aviation Safety Agency
Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET APM 20 and APM 30 series Type Certificate Holder: BP 1 Manufacturer: BP 1 For variants: APM 20 APM 30 Issue 3 : 23 December
More informationCHAPTER 09 TOWING AND TAXIING LIST OF EFFECTIVE PAGES
09 - Effective Pages AIRCRAFT MAINTENANCE MANUAL - PART I CHAPTER 09 TOWING AND TAXIING LIST OF EFFECTIVE PAGES Ch-Se-Su Effectivity Page Date Ch-Se-Su Effectivity Page Date ALL 1 09 - Contents ALL 1 ALL
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.R.145 for Type Certificate Holder Hélicoptères Guimbal 1070, rue du Lieutenant Parayre Aérodrome d'aix-en-provence 13290 Les Milles France For Model: TE.CERT.00049-001
More informationTYPE-CERTIFICATE DATA SHEET
S205-S208 Page 1 TYPE-CERTIFICATE DATA SHEET No. EASA.A.587 S205 S208 Type Certificate Holder: LEONARDO S.p.A. Divisione Velivoli Piazza Monte Grappa, 4 00195 Rome Italy Airworthiness Category: Small Aeroplanes
More informationCHAPTER 1 AIRCRAFT GENERAL
CHAPTER 1 AIRCRAFT GENERAL INTRODUCTION This manual provides a description of the major airframe and engine systems in the Cessna Citation Mustang (Figure 1-1). This material does not supersede, nor is
More informationChapter 10 Miscellaneous topics - 2 Lecture 39 Topics
Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics 10.3 Presentation of results 10.3.1 Presentation of results of a student project 10.3.2 A typical brochure 10.3 Presentation of results At the end
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13 1A13 Revision 27 Revo, Inc. COLONIAL C-1 COLONIAL C-2 LAKE LA-4 LAKE LA-4A LAKE LA-4P LAKE LA-4-200 LAKE
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.121 for Type Certificate Holder Robinson Helicopter Company 2901 Airport Drive Torrance, CA 90505 U.S.A. For Models:, II TE.CERT.00049-001 European Aviation Safety
More informationEuropean Aviation Safety Agency
TCDS IM.A.211 Page 1/20 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA IM.A.211 MD-90-30, B717-200 McDonnell Douglas Corporation 3855 Lakewood Boulevard Long Beach, California 90846-0001
More informationF SAMPLE MANUAL WEIGHT AND BALANCE CONTROL AND LOADING MANUAL
SAMPLE MANUAL WEIGHT AND BALANCE Export controlled by ECCN 9E991 No License is required for the dissemination of the commercial information contained herein to foreign persons other than those from or
More informationEuropean Aviation Safety Agency
TCDS No.: EASA.IM.A.115 Boeing 787 Page 1 of 18 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. EASA.IM.A.115 for BOEING 787 Type Certificate Holder: The Boeing Company 1301 Second
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A16EA
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A16EA Revision 15 True Flight Holdings LLC AA-5, AA-5A, AA-5B AG-5B September 18, 2009 TYPE CERTIFICATE DATA SHEET NO. A16EA This data sheet,
More informationEuropean Aviation Safety Agency
TCDS A.185 P2006T Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.185 P2006T Type Certificate Holder Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli
More informationCAL Ramp Operations Safety Notes
CAL Ramp Operations Safety Notes Ramp Security & Safety 1. Persons who need to access the aircraft SHALL hold a valid identification badge on the front of the outer garment above the waist. 2. Smoking
More informationEuropean Aviation Safety Agency
EASA.IM.A.191 Bombardier DHC-8 Page 1 of 34 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.IM.A.191 DHC-8 Type Certificate Holder: Bombardier Inc. 123 Garratt Boulevard Toronto,
More informationB737 Performance. Takeoff & Landing. Last Rev: 02/06/2004
B737 Performance Takeoff & Landing Last Rev: 02/06/2004 Takeoff Performance Takeoff Performance Basics Definitions: Runway Takeoff Distances Definitions: Takeoff Speeds JAR 25 Requirements Engine failure
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency DECISION N o 2011/006/R OF THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY OF 19 AUGUST 2011 Amending Decision No. 2003/1/RM of the Executive Director of the
More informationI - Model CITATION (Transport Category), approved 09 October 1998.
TYPE CERTIFICATE DATA SHEET Nº EA-9810 Type Certificate Holder: CESSNA AIRCRAFT CO. P. O. Box 7704 Wichita, Kansas, 67277 USA EA-9810-02 Sheet 01 CESSNA CITATION 750 X 10 October 2011 This data sheet,
More informationEuropean Aviation Safety Agency
TCDS A.185 Tecnam P2006T Page 1 of 8 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET P2006T Type Certificate Holder: Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET EASA.IM.A.081 for Type Certificate Holder: PACIFIC AEROSPACE Ltd 333 Airport Road, Hamilton 3282, New Zealand For models: TE.CERT.00048-001 European Aviation Safety Agency,
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-684. Raytehon Aircraft Company on April 15, 1996
Type Certificate Holder: Type Certicate Holder Record: DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-684 Hawker Beechcraft Corporation 9709 E. Central Wichita,
More informationEuropean Aviation Safety Agency
TCDS A.412 Tecnam P92 Page 1 of 13 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.412 TECNAM P92 Type Certificate Holder: Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478
More informationSECTION VI WEIGHT AND BALANCE/ EQUIPMENT LIST TABLE OF CONTENTS
BEECHCRAFT Sundowner 180 SECTION VI WEIGHT AND BALANCE/ EQUIPMENT LIST TABLE OF CONTENTS SUBJECT PAGE Introduction To Weight And Balance 6-3 Weighing Instructions 6-4 Basic Weight And Balance Form 6-7
More informationEuropean Aviation Safety Agency
P2010 Page 1 of 10 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.576 P2010 Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli ITALIA Issue 01: 26 Sept 2014 Issue
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-804. Continental E165-2 (see Item 106 for optional engines)
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-804 Revision 14 LAND-AIR (TEMCO) (LUSCOMBE) 11A 11E April 6, 2005 AIRCRAFT SPECIFICATION NO. A-804 Type Certificate Holder Luscombe Aircraft
More informationTCDS NUMBER E00078NE U.S. DEPARTMENT OF TRANSPORTATION REVISION: 3 DATE: April 12, 2011
TCDS NUMBER E00078NE U.S. DEPARTMENT OF TRANSPORTATION REVISION: 3 DATE: April 12, 2011 FEDERAL AVIATION ADMINISTRATION GENERAL ELECTRIC COMPANY MODELS: TYPE CERTIFICATE DATA SHEET E00078NE GEnx-1B54 GEnx-1B58
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. IM.E.093 for PW1100G-JM Series Engines Type Certificate Holder 400 Main Street East Hartford, CT 06118 United States of America For Models: PW1133G-JM PW1133GA-JM PW1130G-JM
More informationAnswer Key. Page 1 of 10
Name: Answer Key Score: [1] When range and economy of operation are the principal goals, the pilot must ensure that the airplane will be operated at the recommended A. equivalent airspeed. B. specific
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.503 for (King Air) Type Certificate Holder Textron Aviation Inc. Once Cessna BoulevardWichita, KS 67215 USA For models: C90A C90GT C90GTi TE.CERT.00048-001 European
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET For Models: No. IM.E.102 for Engine GEnx Series Engines Type Certificate Holder GE Aviation One Neumann Way Cincinnati Ohio 45215 United States of America GEnx 1B GEnx 2B GEnx
More informationA Game of Two: Airbus vs Boeing. The Big Guys. by Valerio Viti. Valerio Viti, AOE4984, Project #1, March 22nd, 2001
A Game of Two: Airbus vs Boeing The Big Guys by Valerio Viti 1 Why do we Need More Airliners in the Next 20 Years? Both Boeing and Airbus agree that civil air transport will keep increasing at a steady
More informationEuropean Aviation Safety Agency
TCDS IM.A.071 Page 1/18 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Embraer ERJ 190 Manufacturer: Embraer Empresa Brasileira de Aeronáutica SA Av. Brig. Faria Lima. 2170 12227-901
More informationCHAPTER 4 AIRWORTHINESS LIMITATIONS
Section Title CHAPTER 4 AIRWORTHINESS LIMITATIONS 4-10 Airworthiness Limitations..................................... 4.1 4-20 Additional Limitations....................................... 4.3 4-21 Parts
More informationSmall Fixed Wing Aircraft Operational Weight and Balance Computations
Small Fixed Wing Aircraft Operational Weight and Balance Computations Chapter 4 Weight and balance data allows the pilot to determine the loaded weight of the aircraft and determine whether or not the
More information3. What is the total fuel capacity with normal tanks? Usable? 4. What is the total fuel capacity with long range tanks? Usable?
Pilot Name: Last, first, mi. Date: (mo/dy/yr) Instructor: Pass/Fail: Instructors Initials: 1. What is the engine Manufacturer: Model: Type: 2. What is the horsepower rating? 3. What is the total fuel capacity
More informationMODEL 510 MAINTENANCE MANUAL
1. Scope TOWING AND TAXIING - GENERAL A. This chapter gives the procedures used to tow and taxi the airplane. Obey the local tow and taxi procedures. Examples are the use of the correct ramp and the correct
More information