787 Brochure

BOEING is a trademark of Boeing Management Company.Copyright © 2009 Boeing. All rights reserved. PRELIMINARY

Airport Compatibility Brochure – 787

March 2011

Specific airport compatibility questions concerning Boeing commercial aircraft should be forwarded to:

Airport Technology(Seattle, WA)Voice: 1-425-237-1004Fax: 1-425-237-2665E-mail: [email protected]

mailto:[email protected]

COPYRIGHT © 2009 THE BOEING COMPANY

PRELIMINARY

Introduction

This brochure provides airport compatibility data for the 787 Models. This information is intended solely for airport planning purposes. All information in this brochure is preliminary and may change during development and testing.

The 787-8 is a medium-sized, twin-engine aircraft. The 787-9 is a stretched-body derivative of the 787-8.

The 787-8 is the base model of a family of airplanes and is scheduled to enter into service in 2011, followed by the 787-9 in 2013.


PRELIMINARY

Introduction (continued)

Detailed preliminary information for the 787-8 can be found in the Airplane Characteristics for Airport Planning manual located at

www.boeing.com/airports

Airplane Description

Ground Maneuvering

Terminal Servicing

Operating Conditions

Pavement Data


PRELIMINARY

787-8 General Arrangement

*

* static condition, MTOW, nominal CG


PRELIMINARY

787-9 General Arrangement

*

* static condition, MTOW, nominal CG


PRELIMINARY

Airplane Characteristics

CHARACTERISTICS Units 787-8 787-9Max Design lb 503,500 555,000 Taxi Weight kg 228,384 251,744Max Design lb 502,500 553,000 Takeoff Weight kg 227,930 250,837Max Design lb 380,000 425,000 Landing Weight kg 172,365 192,777Max Design lb 355,000 400,000 Zero Fuel Weight kg 161,025 181,437Maximum Fuel US gallons 33,528 33,384 Capacity liters 126,917 126,372


PRELIMINARY

787 is Compatible with Today’s Airports

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

767-300ft/m

787-8ft/m

787-9ft/m

777-200ft/m

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

ICAO Code Letter D E E E

FAA Design Group IV V V V

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

RFF Category (ICAO) 8 8 9 9

ARFF Index (FAA) D D E E


PRELIMINARY

787-8 Interior Arrangement (typical)


PRELIMINARY

787-9 Interior Arrangement (typical)


PRELIMINARY

787-8 Lower Lobe

Forward Cargo Bay Aft Cargo Bay Bulk Cargo Bay402 cu ft (11.4 cu m)

5 pallets(88 x 125)

4 pallets(88 x 125)

5 pallets(96 x 125)

3 pallets (96 x 125)+ 2 LD-3s

16 LD-3s 12 LD-3sForward cargo bay

Mixed cargo capacities(96x125 or 88x125 pallets

Aft cargo bayMixed cargo capacities

(96x125 or 88x125 pallets4 pallets + 2 LD-3s3 pallets + 6 LD-3s2 pallets + 8 LD-3s

1 pallets + 12 LD-3s

3 pallets + 2 LD-3s2 pallets + 4 LD-3s1 pallets + 8 LD-3s


PRELIMINARY

787-9 Lower Lobe

Forward Cargo Bay Aft Cargo Bay Bulk Cargo Bay402 cu ft (11.4 cu m)

6 pallets(88 x 125)

5 pallets(88 x 125)

6 pallets(96 x 125)

5 pallets (96 x 125)

20 LD-3s 16 LD-3sForward cargo bay

Mixed cargo capacities(96x125 or 88x125 pallets

Aft cargo bayMixed cargo capacities

(96x125 or 88x125 pallets5 pallets + 4 LD-3s4 pallets + 6 LD-3s



1 pallets + 12 LD-3s


PRELIMINARY

Ground Servicing for the 787-8

• 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


PRELIMINARY

Ground Servicing for the 787-9

• 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


PRELIMINARY

Takeoff Field Length Full Passenger, Sea Level Takeoff

Takeoff Field Length information to be updated upon availability of

787-8 Flight Test Data


PRELIMINARY

Landing Field Length Sea Level, Standard Day

Landing Field Length information to be updated upon availability of 787-

8 Flight Test Data


PRELIMINARY

Turning RadiusComparable to Other Mid -Sized Aircraft

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

EFFECTIVETURN ANGLE

NOSE GEAR

PATH

MINIMUMPAVEMENTWIDTH

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*

767-400ER 61 166 ft / 50 m*

MD-11 61 161 ft / 49 m*


PRELIMINARY

Cockpit over taxiway centerline

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

*Assumes 15 ft (4.5 m) pavement edge clearance and 150 ft (45 m) taxiway centerline radius**MD-11 requires the largest fillet among the mid-sized aircraft. MD-11 fillet is used for reference

MD-11 Fillet**

15 ft

150 ft

85 ft

+

787-8787-9 MD-11

Tire Edge to Turn Center

MD-11 100 ft 30.5 m

787-9 103 ft 31.4 m

747-400 106 ft 32.3 m

787-8 108 ft 32.9 m

767-300 111 ft 33.8 m


PRELIMINARY

Landing Gear Configuration

787-8 787-9

Maximum Design Taxi Weight LB 503,500 555,000

KG 228,384 251,744

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

Nose Gear Tire Pressure PSI 187 187

KG/CM2 13.15 13.15

Main Gear Tire Size IN 50x20.0 R22/34PR 54x21.0 R23/38PR

Main Gear Tire Pressure PSI 230 229

KG/CM2 16.17 16.10

787-8 74'-9" [22.79M]

787-9 84'-9"

[25.84M]

2'-5" [0.72M]

787-8 4'-3" [1.30M]

787-9 5'-0" [1.52M]

787-9 5'-0" [1.51M]

787-8 4'-10"

[1.46M]

32'-2" [9.80M]

787-8 38'-1" [11.61M] 787-9 38'-11"

[11.86M]

(10’ longer than -8)

(10” widerthan -8)


PRELIMINARY

787-8 Aircraft Classification Number (ACN)

Flexible = Rigid =

35

45

55

65

75

85

95

105

115

350 375 400 425 450 475 500

MTW (x 1,000 lb)

Airc

raft

Cla

ssifi

catio

n N

umbe

r (A

CN

)

CODE D - CBR 3 (ULTRA LOW)CODE C - CBR 6 (LOW)CODE B - CBR 10 (MEDIUM)CODE A - CBR 15 (HIGH)

NOTE: ACN VALUE DETERMINED AS REFERENCED IN AMENDMENT 35, ICAO ANNEX 14 "AERODROMES", 8TH EDITION, MARCH 1983. ALL ACN INFORMATION IS PRELIMINARY AND MAY CHANGE DURING DEVELOPMENT AND TESTING


PRELIMINARY

787-9 Aircraft Classification Number (ACN)

Flexible = Rigid =

40

60

80

100

120

400 425 450 475 500 525 550

MTW (x 1,000 lb)

Airc

raft

Cla

ssifi

catio

n N

umbe

r (A

CN

)

CODE D - CBR 3 (ULTRA LOW)CODE C - CBR 6 (LOW)CODE B - CBR 10 (MEDIUM)CODE A - CBR 15 (HIGH)

NOTE: ACN VALUE DETERMINED AS REFERENCED IN AMENDMENT 35, ICAO ANNEX 14 "AERODROMES", 8TH EDITION, MARCH 1983. ALL ACN INFORMATION IS PRELIMINARY AND MAY CHANGE DURING DEVELOPMENT AND TESTING

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787 Brochure