expressly disclaims any warranty of merchantability or

In connection with the use of this document, Embraer does not provide any express or implied warranties andexpressly disclaims any warranty of merchantability or fitness for a particular purpose. This document contains trade secrets, confidential, proprietary information of Embraer and technical datasubject to U.S. Export Administration Regulation(″EAR″) and other countries export control laws and regula-tions. Diversion contrary to the EAR and other laws and regulations is strictly forbidden. The aboverestrictions may apply to data on all pages of this document.

RECORD OF REVISIONSREVNo.

ISSUEDATE

DATEINSERTED

BYREVNo.

ISSUEDATE

DATEINSERTED

BY

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

AIRPORTPLANNING MANUAL

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DATEINSERTED

DATEREMOVED

PAGENUMBER

REV.No.

DATEINSERTED

DATEREMOVED

PAGENUMBER


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SERVICE BULLETIN LIST

SERVICE BULLETIN MANUAL

NUMBERREV.No.

REV.No.

ISSUEDATE

SERVICE BULLETIN MANUAL

NUMBERREV.No.

REV.No.

ISSUEDATE


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1. INTRODUCTION ............................................................................................................... 1-11.1 Purpose ................................................................................................................... 1-11.2 Scope ...................................................................................................................... 1-1

2. AIRPLANE DESCRIPTION ............................................................................................... 2-12.1 General Airplane Characteristics ............................................................................. 2-12.2 Airplane Dimensions ............................................................................................... 2-32.3 Ground Clearances ................................................................................................. 2-52.4 Interior Arrangements .............................................................................................. 2-72.5 Passenger Cabin Cross-Section ............................................................................. 2-122.6 Lower Compartment Containers .............................................................................. 2-132.7 Door Clearances ..................................................................................................... 2-14

3. AIRPLANE PERFORMANCE ........................................................................................... 3-13.1 General Information ................................................................................................. 3-13.2 Payload x Range ..................................................................................................... 3-23.3 FAR Takeoff Runway Length Requirements ............................................................ 3-4

4. GROUND MANEUVERING ............................................................................................... 4-14.1 General Information ................................................................................................. 4-14.2 Turning Radii - No Slip Angle .................................................................................. 4-24.3 Minimum Turning Radii ........................................................................................... 4-34.4 Visibility from Cockpit in Static Position ................................................................... 4-44.5 Runway and Taxiway Turn Paths ............................................................................ 4-54.6 Runway Holding Bay ............................................................................................... 4-8

5. TERMINAL SERVICING ................................................................................................... 5-15.1 General Information ................................................................................................. 5-15.2 Airplane Servicing Arrangement .............................................................................. 5-25.3 Ground Servicing Connections ................................................................................ 5-35.4 Engine Starting Pneumatic Requirements ............................................................... 5-55.5 Ground Pneumatic Power Requirements ................................................................ 5-75.6 Conditioned Air Requirements ................................................................................. 5-85.7 Ground Towing Requirements ................................................................................. 5-9

6. OPERATING CONDITIONS .............................................................................................. 6-16.1 Engine Exhaust Velocities and Temperatures .......................................................... 6-26.2 Airport and Community Noise ................................................................................. 6-66.3 Hazard Areas .......................................................................................................... 6-9

7. PAVEMENT DATA ............................................................................................................ 7-17.1 General Information ................................................................................................. 7-17.2 Footprint .................................................................................................................. 7-47.3 Maximum Pavement Loads ..................................................................................... 7-57.4 Landing Gear Loading on Pavement ....................................................................... 7-67.5 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method . 7-87.6 Flexible Pavement Requirements - LCN Method .................................................... 7-11

TABLE OF CONTENTS

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7.7 Rigid Pavement Requirements - Portland Cement Association Design Method ...... 7-147.8 Rigid Pavement Requirements - LCN Method ........................................................ 7-177.9 ACN/PCN Reporting System, Flexible and Rigid Pavements .................................. 7-24

8. POSSIBLE EMB-135 DERIVATIVE AIRPLANES ............................................................. 8-1

9. EMB-135 SCALE DRAWINGS ......................................................................................... 9-19.1 EMB-135 Scale: 1 Inch Equals 32 Feet .................................................................. 9-19.2 EMB-135 Scale: 1 Inch Equals 50 Feet .................................................................. 9-39.3 EMB-135 Scale: 1 Inch Equals 100 Feet ................................................................ 9-49.4 EMB-135 Scale: 1 to 500 ........................................................................................ 9-59.5 EMB-135 Scale: 1 to 1000 ...................................................................................... 9-6

TABLE OF CONTENTS

Section Page


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Embraer - Empresa Brasileira de Aeronáutica S.A.

TECHNICAL PUBLICATIONS

STATUS REPORT – TEMPORARY REVISIONS

CURRENT STATUS OF EFFECTIVE TEMPORARY REVISIONS

APM-1343 Revision 8 - August 27/19

Currently there is no effective Temporary Revision intended for this manual. The latest revision to it has incorporated any and all preceding Temporary Revisions issued (if any).

Latest update: August 27/2019.

1. INTRODUCTION

1.1 Purpose

This document provides airplane characteristics data for general airport planning. Since the operationalpractices vary from one airline to the other, specific data should be coordinated with the using airlinesbefore the facility design is made.

EMBRAER should be contacted for any additional information required.

1.2 Scope

This document complies with NAS3601, revision 6.

It provides characteristics of the EMB-135BJ aircraft model for airport operators, airlines, and engineer-ing consultant organizations. Since the airplane changes and the available options may have differentinformation, the data presented herein must be regarded as subject to change.

For further information, contact:

EMBRAER: Empresa Brasileira de Aeronáutica S/A

Av. Brigadeiro Faria Lima, 2170

P.O. Box 8050 - CEP 12227-901

São José dos Campos, SP - BRASIL

Att. Technical Publications

Phone: ++ 55 12 3927-7517

Fax: ++ 55 12 3927-7546

e-mail: [email protected]


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THIS PAGE LEFT BLANK INTENTIONALLY


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4.10 m13ft 5in

69ft 5in21.17m

7.55m24ft 9in

12.43m40ft 10in

24.39m80ft 0in

26.33m86ft 5in

6.76m22ft 2in

2.20m7ft 3in

145APM020261.MCE A

Figure 2.2.1 - EMB-135 BJ Airplane General Dimensions


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2.3 Ground Clearances

CG(%)

FUS.ANGLE

MAIN.DOOR

OPEN1ST.STEP

WINGTIP

BAGGAGEDOOR

TAILSKIDANGLE

TAILBOOM

22270(49097)

22270(49097)

22200(48943)

22200(48943)

18500(40785)

18500(40785)

16000(35274)

16000(35274)14500

(31967)

14000(30865)

13500(29762)

13000(28660)

3.727m12ft 2.7in

3.735m12ft 3.0in

3.727m12ft 2.7in

3.735m12ft 3.1in

3.745m12ft 3.5in

3.758m12ft 4.0in

3.763m12ft 4.2in

3.778m12ft 4.7in

3.777m12ft 4.7in

3.782m12ft 4.9in

3.805m12ft 5.8in

3.802m12ft 5.7in

1.304m4ft 3.3in

1.332m4ft 4.5in

1.304m4ft 3.4in

1.333m4ft 4.5in

1.301m4ft 3.2in

1.348m4ft 5.1in

1.305m4ft 3.4in

1.361m4ft 5.6in

1.309m4ft 3.5in

1.311m4ft 3.6in

1.379m4ft 6.3in

1.353m4ft 5.3in

1.488m4ft 10.6in

1.505m4ft 11.3in

1.488m4ft 10.6in

1.505m4ft 11.3in

1.496m4ft 10.9in

1.525m5ft 0.0in

1.507m4ft 11.3in

1.541m5ft 0.7in

1.516m4ft 11.7in

1.520m4ft 11.8in

1.564m5ft 1.6in

1.550m5ft 1.0in

0.295m11.6in

0.313m1ft 0.3in

0.295m11.6in

0.313m1ft 0.3in

0.304m1ft

0.332m1ft 1.1in

0.315m1ft 0.4in

0.349m1ft 1.7in

0.324m1ft 0.8in

0.328m1ft 0.9n

0.372m1ft 2.6in

0.358m1ft 2.1in

EMERG.EXIT

2.188m7ft 2.1in

2.188m7ft 2.1in)

2.188m7ft 2.1in

2.188m7ft 2.1in

2.215m7ft 3.2in

2.214m7ft 3.2in

2.238m7ft 4.1in

2.237m7ft 4.1in

2.255m7ft 4.8in

2.262m7ft 5.0in

2.266m7ft 5.2in

2.273m7ft 5.5in

MLGDOOR

0.331m1ft 1.0in

0.329m1ft 0.9in

0.332m1ft 1.1in

0.329m1ft 1.0in

0.361m1ft 2.2in

0.356m1ft 2.0in

0.387m1ft 3.2in

0.380m1ft 2.9in

0.405m1ft 3.9in

0.412m1ft 4.2in

0.410m1ft 4.1in

0.420m1ft 4.6in

3.413m11ft 2.4in

3.403m11ft 2.0in

3.414m11ft 2.4in

3.404m11ft 2.0in

3.450m11ft 3.8in

3.433m11ft 3.2in

3.480m11ft 5.0in

3.459m11ft 4.2in

3.502m11ft 5.9in

3.510m11ft 6.2in

3.493m11ft 5.5in

3.511m11ft 6.2in

2.319m7ft 7.3in

2.307m7ft 6.8in

2.320m7ft 7.3in

2.308m7ft 6.9in

2.359m7ft 8.9in

2.338m7ft 8.1in

2.391m7ft 10.1in

2.365m7ft 9.1in

2.414m7ft 11.0in

2.422m7ft 11.3in

2.399m7ft 10.5in

2.420m7ft 11.3in

1.674m5ft 5.9in

1.660m5ft 5.4in

1.674m5ft 5.9in

1.660m5ft 5.4in

1.715m5ft 7.5in

1.692m5ft 6.6in

1.748m5ft 8.8in

1.719m5ft 7.7in

1.772m5ft 9.8in

1.780m5ft 10.1in

1.754m5ft 9.0in

1.777m5ft 10.0in

6.675m21ft 10.8in

6.648m21ft 9.7in

6.675m21ft 10.8in

6.649m21ft 9.8in

6.730m22ft 0.9in

6.685m21ft 11.2in

6.771m22ft 2.6in

6.716m22ft 0.4in

6.801m22ft 3.7in

6.811m22ft 4.1in

6.756m22ft 2.0in

6.794m22ft 3.5in

APM020267A.MCE

FUS ANGLE

D F

H

K

ref. horiz.

38.0

19.3

38.0

16.6

38.0

15.0

WEIGHT

A

ANTENNA

B

(deg)(%mac)

C

NOSE

D E F G H I J

NACELLE

K L

26.9

38.0

30.0

38.0

15.0

26.9

15.88

15.64

15.96

15.88

15.33

15.66

15.08

14.95

14.79

14.96

14.80

15.36

G

L

I

C

BA

E J

(deg)kg (lb)

−1.46

−1.33

−1.46

−1.33

−1.59

−1.38

−1.68

−1.42

−1.74

−1.76

−1.47

−1.62

Figure 2.3.1 - EMB-135 BJ Ground Clearances (MTOW 22200kg)


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EM145APM020001A.DGN

CG(%)

FUS.ANGLE

MAIN.DOOR

OPEN1ST.STEP

WINGTIP

BAGGAGEDOOR

TAILSKIDANGLE

TAILBOOM

22570(49758)

22500(49604)

22500(49604)

18500(40785)

18500(40785)

16000(35274)

16000(35274)14500

(31967)

14000(30865)

13313(29350)

13000(28660)

3.716m12ft 2.3in

3.724m12ft 2.6in

3.716m12ft 2.3in

3.724m12ft 2.6in

3.736m12ft 3.1in

3.749m12ft 3.6in

3.754m12ft 3.8in

3.769m12ft 4.4in

3.767m12ft 4.3in

3.773m12ft 4.5in

3.799m12ft 5.6in

3.794m12ft 5.4in

1.286m4ft 2.6in

1.314m4ft 3.7in

1.287m4ft 2.7in

1.315m4ft 3.8in

1.283m4ft 2.5in

1.332m4ft 4.4in

1.287m4ft 2.7in

1.345m4ft 5.0in

1.291m4ft 2.8in

1.293m4ft 2.9in

1.367m4ft 5.8in

1.337m4ft 4.6in

1.473m4ft 10.0in

1.491m4ft 10.7in

1.474m4ft 10.0in

1.491m4ft 10.7in

1.482m4ft 10.3in

1.512m4ft 11.5in

1.494m4ft 10.8in

1.530m5ft 0.2in

1.503m4ft 11.2in

1.507m4ft 11.3in

1.556m5ft 1.3in

1.539m5ft 0.6in

0.281m11.0in

0.281m11.0in

0.320m1ft 2.0in

0.337m1ft 1.3in

0.311m1ft 0.2in

0.315m1ft 04.n

0.363m1ft 2.3in

0.346m1ft 1.6in

EMERG.EXIT

2.179m7ft 1.8in

2.179m7ft 1.8in)

2.179m7ft 1.8in

2.179m7ft 1.8in

2.208m7ft 2.9in

2.208m7ft 2.9in

2.232m7ft 3.9in

2.231m7ft 3.9in

2.249m7ft 4.5in

2.256m7ft 4.8in

2.263m7ft 5.1in

2.267m7ft 5.2in

MLGDOOR

0.323m1ft 0.7in

0.321m1ft 0.6in

0.324m1ft 0.7in

0.321m1ft 0.6in

0.356m1ft 2.0in

0.351m1ft 1.8in

0.382m1ft 3.0in

0.375m1ft 2.8in

0.400m1ft 3.7in

0.407m1ft 4.0in

0.408m1ft 4.1in

0.416m1ft 4.4in

2.612m8ft 6.8in

2.602m8ft 6.4in

2.612m8ft 6.8in

2.603m8ft 6.5in

2.652m8ft 8.4in

2.635m8ft 7.7in

2.682m8ft 9.5in

2.661m8ft 8.8in

2.704m8ft 10.5in

2.712m8ft 10.8in

2.697m8ft 10.2in

2.713m8ft 10.8in

2.314m7ft 7.1in

2.303m7ft 6.7in

2.315m7ft 7.1in

2.303m7ft 6.7in

2.358m7ft 8.8in

2.336m7ft 8.0in

2.390m7ft 10.1in

2.363m7ft 9.0in

2.413m7ft 11.0in

2.421m7ft 11.3in

2.401m7ft 10.5in

2.419m7ft 11.9in

1.669m5ft 5.7in

1.656m5ft 5.2in

1.670m5ft 5.7in

1.656m5ft 5.2in

1.715m5ft 7.5in

1.690m5ft 6.5in

1.748m5ft 8.8in

1.718m5ft 7.6in

1.772m5ft 9.8in

1.780m5ft 10.1in

1.755m5ft 9.1in

1.776m5ft 9.9in

6.675m21ft 10.8in

6.648m21ft 9.7in

6.675m21ft 10.8in

6.649m21ft 9.8in

6.734m22ft 1.1in

6.688m21ft 11.3in

6.776m22ft 2.8in

6.719m22ft 0.5in

6.805m22ft 3.9in

6.815m22ft 4.3in

6.762m22ft 2.2in

6.797m22ft 3.6in

FUS ANGLE

D F

H

K

ref. horiz.

38.0

19.3

38.0

16.6

38.0

15.0

WEIGHT

A

ANTENNA

B

(deg)(%mac)

C

NOSE

D E F G H I J

NACELLE

K L

27.5

38.0

30.0

38.0

15.0

27.5

14.83

14.60

14.91

14.84

14.27

14.62

14.03

13.88

13.72

13.89

13.73

14.31

G

L

I

C

BA

E J

kg (lb)

−1.50

−1.37

−1.50

−1.38

−1.65

−1.43

−1.73

−1.47

−1.79

−1.81

−1.52

−1.67

22570(49758)

0.298m11.4in

0.299m11.8in

0.290m11.4in

0.302m11.9in

(deg) [1]

[1] MEASURED FROM THE OIL DRAIN TUBE.

Figure 2.3.2 - EMB-135 BJ Ground Clearances (MTOW 22500kg)


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2.4 Interior Arrangements

2.4.1 Interior Arrangement

The interior arrangements provide accommodation for two pilots, one flight observer, one flight attendantand up to 13 passengers.

2.4.2 Cockpit

The ″quiet and dark″ cockpit is designed to accommodate the pilots with comfort during all flight phases,with minimum workload and maximum safety. The cockpit is provided with two pilot seats, a foldable flightobserver seat, control columns and pedals, control pedestal, left, right, and aft consoles, as well as main,overhead, circuit breaker, and glareshield panel. A sun shade is provided for each pilot and thecompartment is separated from the passenger cabin by a partition with a lockable door.

2.4.2.1 Panels

The main instrument panel displays the main navigation, engine, and system indications, through thePFD, MFD, and EICAS displays, permits the audio selection, and ELT reset, and has the landing gearand pedal electric adjustment controls. It also accommodates the standby instruments and displaysreversionary functions.

A glareshield panel is located over the main panel, including the master caution and master warninglights, flight control, display control, and lighting intensity controls. One of the different possibleconfigurations of the glareshield panel includes dual radar control panels.

An overhead panel provides the hydraulic, electrical, powerplant, APU, fire protection, environmental,and external and internal lighting controls.

The circuit breakers, in ordered and grouped positions, are placed on a panel aft of the overhead panel.

2.4.2.2 Left and Right Consoles

The left and right consoles accommodate ashtrays, holders for cups, headset and microphone, oxygenmasks and oxygen control, a waste container, and recesses for crew publication. The left console alsoaccommodates the nose wheel steering handle. A rechargeable flashlight is available on the rightconsole for the copilot and in the cockpit partition behind the seat for the pilot. The Airshow cockpitmonitor is installed on the right-hand sidewall panel left of the First Officer’s seat and below the cockpitwindow.

2.4.2.3 Control Pedestal

The control pedestal, located between the two pilots, presents the FMS control display units enginecontrol levers, the engine thrust rating panel, the speed brake lever, the emergency/parking brake lever,flight control switches (including flap selection), the pressurization control, the EICAS reversionary panel,clearance delivery control, HF control, ELT reset, aileron/elevator disconnect handles, A.P. control, SPS,T/O configuration switch, an FMS control display unit and Airshow cockpit controller. Aircraft equippedoptionally with 3rd VHF and printer have them installed in the control pedestal. CAT III approved aircraftalso have the Heading/Guidance System Control and the integrated 3rd VOR/VHF installed in the controlpedestal.


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2.4.2.4 Pilot Seat

The pilot seats are fixed to slide rails, which permit fore and aft adjustments. When the seats are in theiraftmost position, a lateral movement is also available, in order to facilitate crew access to the seat. Theseats are fitted with adjustable armrest, seat backs, thigh support and lumbar position, and can also beadjusted for height. Backrest inclination, thigh support and lumbar positions are hydromechanicallyadjusted. The armrest adjustment, and seat fore, aft, and lateral adjustments are made mechanically.The pilot and copilot seats are identical, except for the symmetrical arrangement of the controls.

2.4.2.5 Observer Seat

The flight observer seat is installed behind the copilot seat. When in use, it lies in front of the cockpit doorand, when stowed, it folds up and rotates away from the door area, stowing against the right side of thecockpit partition. The cockpit door can be opened/closed with the observer seat either in use or stowed.The observer seat is made up from machined parts combined with flat sandwich panels of graphite andNomex honeycomb core.

2.4.3 Passenger Cabin

The passenger cabin is 2.10 m (6 ft 11 in) wide with a flat floor for a 1.78 m (5 ft 8 in) height. The cabinlayout allows high flexibility with increased capacity for galley, closets, and cabinets.

2.4.3.1 Executive Seats and Divan

The passenger seats have a single lever control for base tracking, breadboard headrests, colorcoordinated seat belts, upholstered in leather per customer specification, thigh rest and lumbar supportadjustment, armrests, head rest, legrest and footrest. Each Executive Single Seat additionally has swivel& lateral movement, limited recline control on inside of inboard arm and life vest storage in each seatbase compartment. The Executive Double Seats have recline control on inside of inboard arm, life veststorage in each seat base compartment, breadboard headrests for each single seat, berthing capability(floor plan permitting), independent track and swivel for each seat position and single retractable armbetween seats. The Executive Divan (3 places) has three color coordinated seat belts, berthingcapabilities, one color coordinated sleeper belt, storage for life vests and passenger rafts included.

2.4.3.2 Entertainment Rack

The entertainment rack is installed in the forward cabin on the left side. It contains a video player, twoDVD players, an entertainment controller, storage for video/DVD/CD media, airshow genesys-datacommunications unit, SATCOM and the entrance control panel. A full-length fabric curtain can beprovided that extends across the main cabin door with attachments provided in the entertainment rack.

2.4.3.3 LH Forward Closet

The LH Forward Closet is offered for carry-on articles and full-length coats in the forward part of thepassenger cabin between the entertainment rack and the forward cabin partition on the left side. The LHForward Closet includes storage for a life raft, six umbrellas, emergency equipment, first-aid kit, crashaxe, crew walk-around oxygen bottle, extinguisher, smoke hood and flashlight, and a storage compart-ment (for electrical equipment cooling: VCP, DVD, CD players). It contains a coat rod, closet light, toe kickarea for heat/conditioned air and aisle lights, portable breathing equipment, floorlevel warm air outletsand ECS/ Decompression airflow outlets, and emergency light installations.


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2.4.3.4 Flight Attendant Station

The standard flight attendant station is positioned at the cockpit partition, close to the main door. The seatis of the foldaway type, to avoid interference with the door passageway. The attendant seats are madeup of machined parts combined with flat sandwich panels of graphite and Nomex honeycomb core.

2.4.3.5 Lavatory

The lavatory is spacious, accessible for handicapped, including wheelchair. It contains a washbasin withcool and hot water, soap dish or dispenser, dispensing for all lavatory amenities, waste container,ashtray, mirror, paper dispenser, automatic fire extinguisher, smoke detection system, and a recirculatingtoilet unit. A toilet shroud and a ventilation system, at the cabinet and waste tank, assure an odorlessenvironment.

2.4.3.6 Galley

The galley is installed in the forward cabin, on the right side. A full-height galley to match cabin contours,installed in the forward cabin area, has complete provisions for electric or microwave oven, coffee maker,trash container with fire extinguisher or flapper door, paper towel roll holder, cutting boards, storageprovisions for utensils and napkins, attendant call panel, flatware storage, ice compartment drawers,glassware storage, crystal and china storage and carrier, condiment storage, sink with hot water, bottleand can storage, juice can storage, liquor decanters or miniature storage, work table, working light,electrical circuit breaker panel, electrical control switch panel, miscellaneous storage, and in-line waterheaters and filters.

2.4.3.7 Amenity cabinets

There is a total of two closets installed next to the forward cabin partition on the RH/LH sides of theaircraft. These closets are offered for carry-on coats and miscellaneous items. They contain floorlevelwarm air outlets and ECS/Decompression airflowoutlets.

2.4.3.8 Divan Cabinets

The divan cabinets closes out the divan structure and is as heigh as the sideledge. Each divan cabinetcontains a miscellaneous storage, RH/LH passenger control unit at seats 11 and 13, modular cupholder/ash tray assembly, floorlevel warm air outlets, and ECS/Decompression airflow outlets.

2.4.3.9 Sideledges

The sideledges extend the full length of aircraft on the LH and RH sides of the cabin area between theforward cabin partition and the credenza, on the RH side between the credenza and the AFT Cabinpartition, and on the LH side between the forward cabin partition and the lavatory.

The sideledges contain interchangeable modules (cup holder, phone, and storage), and ashtrays,storage area for foldout executive tables, VIP control panel/headphone jack at seats, provisions forplug-in monitors to be located on the sideledge for each single seat, one phone at seat number 3 andanother located in front of the conference table, floorlevel warm air outlets, and ECS/Decompressionairflow outlets


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2.4.3.10 Executive and Conference Tables

The executive and conference tables are manually operated with hidden hinges, padded folding leavesand cup holders. Finish is veneered per customer-approved finish specification.

2.4.3.11 Credenza

The credenza is as heigh as the sideledge and installed on the LH side of the airplane near theconference table. It contains a soft storage, space provisions for 10.4″ pop-up LCD monitor, magazine,headphone and life raft storages, escape path lights, storage for printer/fax machine, with 110v outlet,and for miscellaneous items, floorlevel warm air outlets, and ECS/Decompression airflow outlets.

2.4.3.12 Headliner/Valance

A custom headliner/valance is provided manufactured and installed throughout the main cabin area of theaircraft. These panels contain speakers, lighting, and passenger service units as required.

2.4.4 Baggage Compartment

The standard baggage compartment complies with ″Class C″ compartment classification as per theFAR-25 requirements. The available volume is 6.8 m3 (240 cu.ft), and the standard allowed load is 454kg (1000 lb). A baggage compartment door located on the left side of the rear fuselage is 1.11 m (43.7in) high and 1.00 m (39.4 in) wide. A protective plate (in composite material) is installed in the cargo doorsill area to prevent small damage to the fuselage during loading services. The floor is designed foruniformly distributed loading, and is provided with anchor plates for high-density load tie-down. Thebaggage compartment may be accessed externally or internally. It contains an approved smoke detectorsystem with warning indication in the cockpit; a built-in fire extinguishing system which is controllablefrom the cockpit; and a ventilation system which allows for a partial control of the compartmenttemperature. The baggage compartment bulkheads are flat sandwich panel constructions, with Nomexhoneycomb core faced with graphite fabric. Local stiffeners are bonded to the flat panels to improvestiffness. The baggage compartment lining is a hand lay-up solid laminate construction, with fiberglassfabric facing the inner side and Kevlar facing the outer side. Nomex honeycomb core is used in someareas to work as local stiffeners. The compartment liners comply with flame penetration resistance tests,as required by FAR-25.


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Figure 2.4.1 - EMB-135 BJ Interior Arrangements-Configuration


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2.5 Passenger Cabin Cross-Section

Figure 2.5.1 - EMB-135 BJ Passenger Cabin Cross-Section


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2.6 Lower Compartment Containers

The EMB-135 BJ aircraft does not have lower compartment containers.

2.7 Door Clearances


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Figure 2.7.1 - EMB-135 BJ Door ClearancesSheet 1


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Figure 2.7.1 - EMB-135 BJ Door ClearancesSheet 2


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3. AIRPLANE PERFORMANCE

3.1 General Information

Section 3.2 presents payload x range information for a specific long range, cruise altitude, and the fuelreserve condition shown.

Section 3.3 and 3.4 represent FAR takeoff and landing runway length requirements for FAA certification.Standard day temperatures for the altitudes shown are tabulated below:

Table 3.1.1 - Standard Day Temperatures x Elevation

ELEVATION STANDARD DAY TEMPft m oF oC

0 0 59 15

2000 610 51.9 11.6

4000 1220 44.7 7.1

6000 1830 37.6 3.1

8000 2440 30.5 -0.8

3.2 Payload x Range


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8 PAX − 90 kg EACH

NOTES:500

1500

2000

2500

3000

EM145APM030001A.DGN

PAYLOAD X RANGE

EMB−135 BJ

ISA

LONG RANGE

MAX. CRUISE

RANGE − nm

00

500 1000 1500 2000 2500 3000

1000

PA

YLO

AD

− k

g

1000

0

2000

3000

4000

5000

6000

PA

YLO

AD

− lb

FLIGHT LEVEL.............................390RESERVE.....................................200nm ALTERNATE+30min HOLDINGMAX TAKEOFF WEIGHT..............22200 kg MAX ZERO FUEL WEIGHT..........16000 kg BASIC OPERATING WEIGHT......14030 kg MAXIMUM USABLE FUEL..............8056 kg

AE3007 A1P ENGINES

Figure 3.2.1 - Payload x Range, Engine with Thrust ReverserSheet 1


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PAYLOAD X RANGE

ISA

EMB−135 BJ

00

1000

0

2000

3000

4000

5000

6000

PA

YLO

AD

− lb

PA

YLO

AD

− k

g

500

1500

2000

2500

3000

1000

LONG RANGE

MAX. CRUISE

8 PAX − 90 kg EACH

NOTES: FLIGHT LEVEL.............................410RESERVE.....................................200nm ALTERNATE+30min HOLDINGMAX TAKEOFF WEIGHT..............22500 kg MAX ZERO FUEL WEIGHT..........16000 kg BASIC OPERATING WEIGHT......13650 kg MAXIMUM USABLE FUEL..............8242 kg

500 1000 1500 2000 2500 3000 3500

EM145APM030002A.DGN

AE3007 A1E ENGINES

RANGE − nm

Figure 3.2.1 - Payload x Range, Engine with Thrust ReverserSheet 2


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3.3 FAR Takeoff Runway Length Requirements

EM145APM030003A.DGN

ZERO WIND, FLAPS 9°, ISA

4700043000 45000 49000

AIR

POR

T PR

ESSU

RE

ALTI

TUD

E

m (f

t)

TAKEOFF RUNWAY LENGTH

EMB−135 BJ

AE3007 A1P ENGINES

1829

(600

0)12

19 (4

000)

610

(200

0)

SEA LEVEL

12000

1000

14000 16000 18000 20000 22000

27000 29000 31000 33000 35000 37000 39000 41000

OPERATIONAL TAKEOFF WEIGHT − kg

OPERATIONAL TAKEOFF WEIGHT − lb

FA

R T

AK

EO

FF

RU

NW

AY

LE

NG

TH

− ft

FA

R T

AK

EO

FF

RU

NW

AY

LE

NG

TH

− m

1200

1400

1600

1800

2000

2200

2400

3500

4000

4500

5000

5500

6000

6500

7000

7500

DRY AND LEVEL RUNWAY

Figure 3.3.1 - FAR Takeoff Runway Length RequirementsSheet 1


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ZERO WIND, FLAPS 9°, ISA

4700043000 45000 49000

AIR

POR

T PR

ESSU

RE

ALTI

TUD

E

m (f

t)


EMB−135 BJ

AE3007 A1E ENGINES

1829

(600

0)

1219

(400

0)

610

(200

0)SEA L

EVEL

12000

1000

14000 16000 18000 20000 22000

27000 29000 31000 33000 35000 37000 39000 41000



FA

R T

AK

EO

FF

RU

NW

AY

LE

NG

TH

− ft

FA

R T

AK

EO

FF

RU

NW

AY

LE

NG

TH

− m

1200

1400

1600

1800

2000

2200

2400

EM145APM030004A.DGN

3500

4000

4500

5000

5500

6000

6500

7000

7500




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4700043000 45000 49000

AIR

POR

T PR

ESSU

RE

ALTI

TUD

E

m (f

t)


EMB−135 BJ

AE3007 A1P ENGINES

1829

(600

0)12

19 (4

000)

610

(200

0)

SEA LEVEL

12000

1000

14000 16000 18000 20000 22000

27000 29000 31000 33000 35000 37000 39000 41000



FA

R T

AK

EO

FF

RU

NW

AY

LE

NG

TH

− ft

FA

R T

AK

EO

FF

RU

NW

AY

LE

NG

TH

− m

1200

1400

1600

1800

2000

2200

2400

ZERO WIND, FLAPS 9°, ISA +10°C

EM145APM030006A.DGN

3500

4000

4500

5000

5500

6000

6500

7000

7500




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EM145APM030007A.DGN

4700043000 45000 49000


FA

R T

AK

EO

FF

RU

NW

AY

LE

NG

TH

− ft

FA

R T

AK

EO

FF

RU

NW

AY

LE

NG

TH

− m


1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

12000 14000 16000 18000 20000 22000

EMB−135 BJ

1000

1100

AIRPORT P

RESSURE ALT

ITUDE

m (f

t)

1219 (4000)

610 (2000)

AE3007 A1E ENGINES

27000 29000 31000 33000 35000 37000 39000 41000


SEA LEVEL18

29 (6

000)

3500

4000

4500

5000

5500

6000

6500

7000

7500

8000

8500

9000

9500

DRY AND LEVEL RUNWAYZERO WIND, FLAPS 9°, ISA +10°C



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FLAPS 45°

2200

2300

2400

16000 18000 20000 22000 24000

PRESSURE ALTITUDE (ft

)

10000

80009000

7000

6000

5000

4000

3000

2000

1000

−1000

4700043000 45000 49000

EM145APM030008A.DGN

LANDING RUNWAY LENGTH

14000

FA

R L

AN

DIN

G R

UN

NW

AY

LE

NG

TH

− ft

EMB−135 BJ

SEA LEVEL

1100

1200

1300

1400

1500

1600

1700

1800

1900

12000

5000

4500

4000

3500

FAR

LA

ND

ING

RU

NN

WA

Y L

EN

GTH

− m

2000

2100

AE3007 A1P ENGINES

27000 29000 31000 33000 35000 37000 39000 41000



5500

6000

6500

7000

7500

DRY AND LEVEL RUNWAYZERO WIND, ISA

Figure 3.3.2 - FAR Landing Runway Length RequirementsSheet 1


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2200

2300

2400

16000 18000 20000 22000 24000

PRESSURE ALTITUDE (ft

)

10000

80009000

7000

6000

5000

4000

3000

2000

1000

−1000

4700043000 45000 49000

14000

FA

R L

AN

DIN

G R

UN

NW

AY

LE

NG

TH

− ft

EMB−135 BJ

SEA LEVEL

1100

1200

1300

1400

1500

1600

1700

1800

1900

4500

4000

3500

FAR

LA

ND

ING

RU

NN

WA

Y L

EN

GTH

− m

2000

2100

AE3007 A1E ENGINES

27000 29000 31000 33000 35000 37000 39000 41000



FLAPS 45°

LANDING RUNWAY LENGTH

12000

EM145APM030009A.DGN

5000

5500

6000

6500

7000

7500

DRY AND LEVEL RUNWAYZERO WIND, ISA

Figure 3.3.2 - FAR Landing Runway Length RequirementsSheet 2


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4. GROUND MANEUVERING


This section provides the aircraft turning capability and maneuvering characteristics. For ease ofpresentation, these data have been determined from theoretical limits imposed by the geometry of theaircraft.

As such, they reflect the turning capability of the aircraft in favorable operating circumstances. Thesedata should be used only as guidelines for the method of determination of such parameters and for themaneuvering characteristics of the EMB-135 BJ.

In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary, as far as the performance is concerned, over a wide range of operatingcircumstances throughout the world.

Variations from standard aircraft operating patterns may be necessary to satisfy physical constants withinthe maneuvering area, such as adverse grades, limited area, or high risk of jet blast damage. For thesereasons, the ground maneuvering requirements should be coordinated with the using airline prior to thelayout planning.

Section 4.2 presents the turning radii for various nose gear steering angles.

Section 4.3 presents data on the minimum width of the pavement for 180o turn.

Section 4.4 presents the pilot’s visibility from the cockpit and the limits of ambinocular vision through thewindows. Ambinocular vision is defined as the total field of vision seen by both eyes at the same time.

Section 4.5 presents the performance of the EMB-135 BJ on runway-to-taxiway, and taxiway-to-taxiwayturn paths.

Section 4.6 presents the runway holding bay configuration.

4.2 Turning Radii - No Slip Angle


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Figure 4.2.1 - EMB-135 BJ Turning Radii - No Slip Angle


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4.3 Minimum Turning Radii

Figure 4.3.1 - EMB-135 BJ Minimum Turning Radii


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4.4 Visibility from Cockpit in Static Position

VISUAL ANGLES IN PLANEPARALLEL TO LONGITUDINALAXIS THROUGH PILOT’S EYEPOSITION

2.86 m9ft 5in

PILOT’S EYE POSITION23°

15,6°

0.61 m2ft

3.53 m11ft 7in

10.22 m33ft 6in

MAXIMUM AFT VISIONWITH HEAD ROTATEDABOUT SPINAL COLUMN

PILOT’S EYE POSITION

0.41 m1ft 4in

124°

VISUAL ANGLE IN PLANEPERPENDICULAR TO LONGITUDINALAXIS THROUGH PILOT’S EYE POSITION

0.45 m1ft 6in

PILOT’S EYE POSITION

15°

33°

EM145APM040457A.DGN

Figure 4.4.1 - Visibility from Cockpit in Static Position


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4.5 Runway and Taxiway Turn Paths

Figure 4.5.1 - More than 90o Turn - Runway to Taxiway


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Figure 4.5.2 - 90o Turn - Runway to Taxiway


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Figure 4.5.3 - 90o Turn - Taxiway to Taxiway


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4.6 Runway Holding Bay

Figure 4.6.1 - Runway Holding Bay


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5. TERMINAL SERVICING


During turnaround at the air terminal, certain services must be performed on aircraft, usually within agiven time to meet flight schedules. This section shows servicing vehicle arrangements, schedules,locations of servicing points, and typical servicing requirements. The data presented herein reflect idealconditions for a single airplane. Servicing requirements may vary according to the airplane condition andairline procedure.

This section provides the following information:

– Typical arrangements of ground support equipment during turnaround.

– The locations of ground servicing connections in graphic and tabular forms. Typical capacities andservicing requirements are shown in the figures. Services with requirements that vary with conditionsare described in the subsequent figures.

– Air conditioning requirements for heating and cooling the airplane, using low-pressure conditioned air.This conditioned air is supplied through an 8-inch GAC directly to the air distribution system,bypassing the air-cycle machines. Normally, a 36000 BTU/h source would be sufficient to meet the airconditioning requirements.

– Ground towing requirements for various towing conditions. Drawbar pull and total traction wheel loadmay be determined by considering airplane weight, pavement slope, coefficient of friction, and engineidle thrust.

5.2 Airplane Servicing Arrangement


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Figure 5.2.1 - EMB-135 BJ Airplane Servicing Arrangement


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5.3 Ground Servicing Connections

Figure 5.3.1 - EMB-135 BJ Ground Servicing Connections


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Table 5.3.1 - Ground Servicing Connection Data

SYSTEM

DISTANCE AFTOF NOSE

DISTANCE FROM AIRPLANECENTERLINE

HEIGHT ABOVEGROUND

ft-in mRIGHT SIDE LEFT SIDE MAXIMUM

ft-in m ft-in m ft-in m

5.4.1 Hydraulic Power SystemThree Servicing Connections:

A. Nose Servicing Panel ............................... . 6-3 1.90 2-8 0.81 - - 5-7 1.69

B. LH and RH Servicing Panels .................... 56-2 17.26 1-9 0.53 1-9 0.53 5-4 1.63

5.4.2 Electrical Power SystemOne External Power Supply Connection 230 VAC 50-60 Hz/28 V DC - 300 A or 1600 A ...

7-5 2.26 - - 3-1 0.94 5-7 1.71

5.4.3 Oxygen SystemOne Servicing Panel ..................................... 12-11 3.93 2-8 0.81 - - 5-1 1.74

5.4.4 Fuel System

A. Gravity Fuel Filler Port ............................. 45-10 13.99 17-10 5.43 17-10 5.43 6-.5 1.84

B. Fuel Magnetic Stick ................................... 43-1 13.14 8-11 2.73 8-11 2.73 4-3 1.31

C. Fuel Magnetic Stick ................................... 45-10 13.98 16-4 4.98 16-4 4.98 5-6 1.57

D. Fuel Magnetic Stick ................................... 40-9 12.43 1-1 0.35 1-1 0.35 3-6 1.06

E. Fuel Drain Valve ....................................... 42-4 12.90 3.6 1.06 3-6 1.06 4-6 1.37

F. Fuel Drain Valve ....................................... 42-7 12.97 1-4 0.41 1-4 0.41 3-6 1.06

G. Fuel Drain Valve ...................................... 32-3 9.78 0-3 .097 - - 4-5 1.36

H. Fuel Drain Valve ...................................... 32-3 9.78 - - 0-3 .097 4-5 1.36

I. Fuel Drain Valve ........................................ 66-2 20.19 0-0.5 0.15 - - 5-11 1.82

J. Fuel Drain Valve ....................................... 66-8 20.33 0-0.5 0.15 - - 6-0.8 1.85

G. Fuel Dump Valve ..................................... 40-9 12.43 2-2 0.68 2-2 0.68 3-6 1.06

H. Pressure Refueling/Defueling Panel ........ 32-5 10.21 3-5 1.04 - - 6-0.6 2.05

5.4.5 Air Conditioning System

33-4 10.17 2-5 0.73 - - 5-6 1.68One Pressurization Ground Test Connection........................................................................

One Air Conditioning Ground Connection .... 29-0 8.86 1-6 0.46 - - 5-7 1.72

5.4.6 Portable Water System 57-1 17.67 2-3 0.69 - - 6-5 1.97

One Servicing Panel ...................................... 58-11 17.67 0-2 0.69 - - 5-12 1.97

5.4.7 Lavatory SystemWaste Servicing Panel .................................. 58-7 17.87 0-4 0.40 - - 5-3 1.86

5.4.8 PowerplantTwo Engine Oil Supply/Level Check Panels

A. LH Panel .................................................... 62-11 19.20 - - 6-0.5 1.84 10-0.5 3.06

B. RH Panel ................................................... 62-11 19.20 7-8 2.35 - - 10-0.5 3.06

Ground Connection for Engine Air Starting . 65-3 19.88 0-11 0.27 - - 5-7 1.57


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5.4 Engine Starting Pneumatic Requirements

Figure 5.4.1 - Engine Starting Pneumatic Requirements - Airflow x Temperature


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Figure 5.4.2 - Engine Starting Pneumatic Requirements - Pressure x Temperature


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5.5 Ground Pneumatic Power Requirements

Figure 5.5.1 - Ground Pneumatic Power Requirements (APU Mode)


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5.6 Conditioned Air Requirements

Figure 5.6.1 - Pre-conditioned Airflow Requirements


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5.7 Ground Towing Requirements

Figure 5.7.1 - Ground Towing Requirements


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6. OPERATING CONDITIONS

This section presents graphics concerning:

– the EMB-135 BJ aircraft Jet Engine Exhaust velocities and temperatures,

– the Airport and Community Noise levels and Hazard Areas.

6.1 Engine Exhaust Velocities and Temperatures


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Figure 6.1.1 - Jet Wake Velocity Profile (T/O-1 Thrust Mode)


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Figure 6.1.2 - Jet Wake Temperature Profile (T/O-1 Thrust Mode)


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Figure 6.1.3 - Jet Wake Velocity Profile (Idle Thrust Mode)


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Figure 6.1.4 - Jet Wake Temperature Profile (Idle Thrust Mode)


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6.2 Airport and Community Noise

Aircraft noise is a major concern for the airport and community planner. The airport is a basic element inthe community’s transportation system and, as such, is vital to its growth. However, the airport must alsobe a good neighbor, and this can be accomplished only with proper planning. Since aircraft noise extendsbeyond the boundaries of the airport, it is vital to consider the noise impact on the surroundingcommunities.

Many means have been devised to provide the planner with a tool to estimate the impact of airportoperations. Too often they oversimplify noise to the point where the results become erroneous. Noise isnot a simple matter; therefore, there are no simple answers.

The cumulative noise contour is an effective tool. However, care must be exercised to ensure that thecontours, used correctly, estimate the noise resulting from aircraft operations conducted at an airport.

The size and shape of the single-event contours, which are inputs into the cumulative noise contours, aredependent upon numerous factors. They include:

6.2.1 Operational Factors

6.2.1.1 Aircraft Weight

Aircraft weight is dependent on the distance to be traveled, en-route winds, payload, and anticipatedaircraft delay upon reaching the destination.

6.2.1.2 Engine Power Setting

The rates of ascent and descent and the noise levels emitted at the source are influenced by the powersetting used.

6.2.1.3 Airport Altitude

Higher airport altitude will affect the engine performance and thus can influence noise.

6.2.2 Atmospheric Conditions - Sound Propagation

6.2.2.1 Wind

With stronger headwinds, the aircraft can takeoff and climb more rapidly relative to the ground. Also,winds can influence the distribution of noise in the surrounding communities.

6.2.2.2 Temperature and Relative Humidity

The absorption of noise in the atmosphere along the transmission path between the aircraft and theground observer varies with both temperature and relative humidity.

6.2.3 Surface Condition - Shielding, Extra Ground Attenuation (EGA)

Terrain - If the ground slopes down after takeoff or up before landing, noise will be reduced since theaircraft will be at a higher altitude above the ground. Additionally, hills, shrubs, trees, and large buildingscan act as sound buffers.

All of these factors can alter the shape and size of the contours appreciably. To demonstrate the effectof some of these factors, estimated noise level contours for two different operating conditions are shown


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on figure 6.2.1. These contours reflect a given noise level upon a ground level plane at runway elevation.

As indicated from these data, the contour size varies substantially with operating and atmosphericconditions. Most aircraft operations are, of course, conducted at less than the maximum gross weightsbecause the average flight distances are much shorter than the maximum aircraft range capability andthe average load factors are less than 100%. Therefore, in developing cumulative contours for planningpurposes, it is recommended that the airlines serving a particular city be contacted to provide operationalinformation.

In addition, there are no universally accepted methods for developing aircraft noise contours for relatingthe acceptability of specific noise zones to specific land uses. It is therefore expected that the noisecontour data for a particular aircraft and the impact assessment methodology change. To ensure thatcurrently available information of this type is used in any planning study, it is recommended that it beobtained directly from the Office of Environmental Quality in the Federal Aviation Administration inWashington, D.C.

It should be noted that the contours shown herein are only for illustrating the impact of the operating andatmospheric conditions and do not represent the single-event contour of the family of aircraft describedin this document. It is expected that the cumulative contours be developed as required by the plannersusing the data and methodology applicable to their specific study.


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Figure 6.2.1 - Airport and Community Noise Levels


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6.3 Hazard Areas

ENGINE INLETINGESTIONDANGER AREA

ENGINEACCESSORIESCAUTION AREA

13,0 m

( 42,6 ft )

25,0 m

( 82,0 ft )

25,0 m

( 82,0 ft )

50,0 m

( 164,0 ft )

4.3 m

( 14,1 ft )

7,0 m

( 23,0 ft )

3,0 m( 9,8 ft )

3,0 m( 9,8 ft )

ENGINEEXHAUSTDANGER AREA AT IDLE THRUST

ENGINEEXHAUSTDANGER AREA

AT MAX. THRUST

AIRCRAFT STATIC − SEA LEVEL I.S.A − NO WIND

1 WITH THE ENGINE RUNNING, THE ACCESS TO THIS AREAIS PERMITTED JUST WITH THE ENGINE IN IDLE SPEEDOR LESS.

1

6,0 m( 19,7 ft )

2,0 m( 6,6 ft )

145APM060651B.MCE

APUDANGERAREA

Figure 6.3.1 - Hazard Areas


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Aug 27/19

8. POSSIBLE EMB-135 DERIVATIVE AIRPLANES

No derivative models of the EMB-135 are current planned.


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9. EMB-135 SCALE DRAWINGS

This section provides EMB-135 plan views to the following scales:

• English1 inch = 32 feet1 inch = 50 feet1 inch = 100 feet

• Metric1:5001:1000

9.1 EMB-135 Scale: 1 Inch Equals 32 Feet


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Figure 9.1.1 - EMB-135 Scale: 1 Inch Equals 32 Feet


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9.4 EMB-135 Scale: 1 to 500

Figure 9.4.1 - EMB-135 Scale: 1 to 500


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9.5 EMB-135 Scale: 1 to 1000

Figure 9.5.1 - EMB-135 Scale: 1 to 1000


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