B787- Planeacion de Aeropuertos

8/18/2019 B787- Planeacion de Aeropuertos

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Copyright © 2015 Boeing. All rights reserved.

.

June 2015

For specific airport compatibility questions regarding Boeing commercial airplanes, please contact

Airport Compatibility Engineering at Ph:+1 562-797-1172 / Email: [email protected]

PRELIMINARY

mailto:[email protected]:[email protected]


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COPYRIGHT © 2015 THE BOEING COMPANY PRELIMINARY 2

Introduction

This brochure provides basic characteristics of the Boeing 787-10

Dreamliner airplane that have an impact on airport compatibility. This

information is intended solely for airport planning purposes. Information for

the 787-10 is preliminary, for reference only and subject to change during

development and testing. Detailed data for the 787-8 and 787-9 can be

found in the Boeing Airplane Characteristics for Airport Planning documentlocated at www.boeing.com/airports .

The 787-10 is the third, longest and newest member of the 787 Dreamliner

family of medium-sized, twin-engine airplanes.

Launched in 2013, the 787-10 is in development and on track for firstdelivery in 2018.


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787-10 General Arrangement

* static condition, MTOW, nominal CG


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787-10 Airplane Characteristics

CHARACTERISTICS UNITS 787-10

Max Design Taxi Weight LB 559,000

KG 253,558

Max Design Takeoff Weight LB 557,000

KG 252,657

Max Design Landing Weight LG 445,000

KG 201,848

Max Design Zero Fuel Weight LB 425,000

KG 192,777

Maximum Fuel Capacity USGALLON 33,384

LITER 126,372


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787-10 Airport Regulatory Compatibility

767-300

(FT/M)

787-8

(FT/M)

787-9

(FT/M)

787-10

(FT/M)

777-200

(FT/M)

Wing Span 156.1 / 47.6 197.3 / 60.1 197.3 / 60.1 197.3 / 60.1 199.9 / 60.9

ICAO Code Letter D E E E E

FAA Design Group IV V V V V

Overall Length 180.3 / 54.9 186.1 / 56.7 206.1 / 62.8 224.1 / 68.3 209.1 / 63.7

RFF Category (ICAO) 8 8 9 9 9

ARFF Index (FAA) D D E E E


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787-10 Interior Arrangement (typical)


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787-10 Lower Cargo Compartments

Forward Cargo Bay Aft Cargo BayBulk Cargo Bay

402 cu ft (11.4 cu m)



787-10 Door Locations

D1 D2 D3 D4 C1 C2 C3

787-1020FT 8IN

6.3M

70FT 3IN

21.4M

126FT 2IN

38.5M

180FT 10IN

55.1M

36FT 1IN

11.0M

152FT 1IN

46.4M

174FT 8IN

53.2M

* All models



787-10 Ground Servicing Layout

• POTABLE WATER, AIR CONDITIONING, OR GROUND

POWER MAY BE SUPPLIED FROM THE PASSENGER

BRIDGE IF SO EQUIPPED

• IF THE APU IS NOT AVAILABLE, A QTY OF (3) GROUND

POWER UNITS ARE RECOMMENDED DURING ENGINE

START TO MINIMIZE IMPACT TO RAMP OPERATIONS



787-10 Turning Radius- Comparable to Other Mid-Sized Aircraft

* Requires differential braking / thrust for U-turn on 150 ft . (45 m) wide runway

Model Effective Steering Angle Minimum Pavement Width

787-8 65 138 ft / 42 m

767-300 61 146 ft / 44 m

787-9 65 154 ft / 47 m*

777-200LR 64 157 ft / 48 m*

787-10 64 177 ft / 54 m*

777-300ER 64 186 ft / 57 m*



Cockpit over

taxiway centerline

787-10 Taxiway Turn Fillet Requirements- Comparable to Other Mid -Sized Aircraft

*Fillet design to accommodate 777-200, with 15 ft (4.5 m) pavement

edge clearance and 150 ft (45 m) taxiway centerline radius

15 ft

150 ft

85 ft*

787-8

787-9 777-200LR

Tire Edge to Turn Center

787-10 99 ft 30 m

777-200LR 100 ft 31 m

787-9 104 ft 32 m

747-400 104 ft 32 m

787-8 109 ft 33 m

787-10


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787-10 Landing Gear Configuration

787-10

Maximum Design Taxi Weight LB / KG 559,000 / 253,558

Nose Gear Tire Size IN 40x16.0 R16/26PR

Nose Gear Tire Pressure PSI / KG/CM2 183 / 12.9

Main Gear Tire Size IN 54x21.0 R23/38PR

Main Gear Tire Pressure PSI / KG/CM2 226 / 15.9

Wheelbase (A) FT-IN / M 94-9 / 28.9

MLG Truck Width (B) FT-IN / M 5-0 / 1.5

MLG Truck Length (C) FT-IN / M 5-0 / 1.5

MLG Track Width (D) FT-IN / M 32-2 / 9.8

MLG Maximum Width (E) FT-IN / M 38-11 / 11.9

787 10 Ai ft Cl ifi ti N b (ACN)


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787-10 Aircraft Classification Number (ACN)- Flexible Pavement

40

45

50

55

60

65

70

75

80

85

90

95

100

105

110

115

120

425 450 475 500 525 550 575

A I R C R A F T

C L A S S I F I C A T I O N

N U M B E R

( A C N ) - F L E X I B L E

P A V E M

E N T

787-10 AIRCRAFT GROSS WEIGHT (x 1,000 LB)

CODE D - CBR 3 (ULTRA LOW)

CODE C - CBR 6 (LOW)

CODE B - CBR 10 (MEDIUM)

CODE A - CBR 15 (HIGH)

NOTE: PERCENT WEIGHT ON MAIN LANDING GEAR = 93.7

787 10 Ai ft Cl ifi ti N b (ACN)



787-10 Aircraft Classification Number (ACN)- Rigid Pavement

40

45

50

55

60

65

70

75

80

85

90

95

100

105

110

115

120

425 450 475 500 525 550 575

A I R C R A F T

C L A S S I F I C A T I O N

N U M B E

R

( A C N ) - R I G I D

P A V E M E N

T

787-10 AIRCRAFT GROSS WEIGHT (x 1,000 LB)

CODE D - k=75 PCI (ULTRA LOW)

CODE C - k=150 PCI (LOW)

CODE B - k=300 PCI (MEDIUM)

CODE A - k=550 PCI (HIGH)

NOTE: PERCENT WEIGHT ON MAIN LANDING GEAR = 93.7

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B787- Planeacion de Aeropuertos