CIVIL JET AIRCRAFT DESIGN

ABOUT THE BOOK
PREFACE
APPENDICES
CASE STUDIES
ABOUT THE AUTHORS
AIRCRAFT LINKS




 

 

Data A : Aircraft Data File

Table 4 : Boeing Aircraft

Notes

Manufacturer

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

Type

777-

777-

777-

777-

777-

777-

777-

Model

100X1

100X2

200

200IGW

200X1

200X2

300

Initial service date

2000

2000

1995

1995

2000

2000

1998

In service (ordered)
Africa

-

-

--->

3(4)

-

-

-

Middle East/Asia/Pacific

-

-

--->

90(74)

-

-

11(37)

Europe & CIS

-

-

--->

26(39)

-

-

-

North & South America

-

-

--->

38(78)

-

-

-

Total aircraft

-

-

--->

157(195)

-

-

11(37)

Engine Manufacturer

R-R/GE/PW

R-R/GE/PW

R-R/GE/PW

R-R/GE/PW

R-R/GE/PW

R-R/GE/PW

R-R

Model / Type

Options

Options

Options

Options

Options

Options

Trent 895

No. of engines

2

2

2

2

2

2

2

Static Thrust (kN)

400.0

400.0

342.5

373.7

413.8

436.0

423.0

Operational Items:
Accomodation:
Max. seats (single class)

330

330

440

440

440

440

550

Two class seating

375

375

375

375

479

Three class seating

271

250

310

310

298

298

394

No. abreast

10

10

10

10

10

Hold volume (m3)

160.00

160.00

160.00

160.00

200.50

Volume per passenger

0.36

0.36

0.36

0.36

0.36

Mass (Weight) (kg):
Ramp

243577

287804

299600

Max. take-off

286621

299320

242670

286897

299320

312925

299370

Max. landing

201850

208652

237685

Zero-fuel

190510

195045

224530

Max. payload

54635

56925

68570

Max. fuel payload
Design payload

25745

23750

35625

29450

Design fuel load

71170

119327

Operational empty

135875

138120

155960

Weight Ratios:
Ops empty/Max. T/O

0.560

0.481

0.521

Max. payload/Max. T/O

0.225

0.198

0.229

Max. fuel/Max. T/O

0.382

0.466

0.452

Max. landing/Max. T/O

0.832

0.727

0.794

Fuel (litres):
Standard

117348

169208

174735

174735

171170

Optional
Manufacturer

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

Type

777-

777-

777-

777-

777-

777-

777-

Model

100X1

100X2

200

200IGW

200X1

200X2

300

DIMENSIONS
Fuselage:
Length (m)

56.40

59.60

62.78

62.78

62.78

62.78

72.88

Height (m)

6.20

6.20

6.20

6.20

6.20

6.20

6.20

Width (m)

6.20

6.20

6.20

6.20

6.20

6.20

6.20

Finess Ratio

9.10

9.61

10.13

10.13

10.13

10.13

11.75

Wing:
Area (m)

427.80

427.80

427.80

427.80

427.80

427.80

427.80

Span (m)

60.90

60.90

60.90

60.90

60.90

60.90

60.90

MAC (m)

8.75

8.75

8.75

8.75

8.75

8.75

8.75

Aspect Ratio

8.67

8.67

8.67

8.67

8.67

8.67

8.67

Taper Ratio

0.149

0.149

0.149

0.149

0.149

0.149

0.149

Average (t/c) %
1/4 Chord Sweep ()

31.60

31.60

31.60

31.60

31.60

31.60

31.60

High Lift Devices:
Trailing Edge Flaps Type

S2/S1

S2/S1

S2/S1

S2/S1

S2/S1

S2/S1

S2/S1

Flap Span/Wing Span

0.758

0.758

0.758

0.758

1.758

2.758

2.758

Area (m)
Leading Edge Flaps Type

slats

slats

slats

slats

slats

slats

slats

Area (m)
Vertical Tail:
Area (m)

53.23

53.23

53.23

53.23

53.23

53.23

53.23

Height (m)

9.24

9.24

9.24

9.24

9.24

9.24

9.24

Aspect Ratio

1.60

1.60

1.60

1.60

1.60

1.60

1.60

Taper Ratio

0.290

0.290

0.290

0.290

0.290

0.290

0.290

1/4 Chord Sweep ()

46.00

46.00

46.00

46.00

46.00

46.00

46.00

Tail Arm (m)

23.41

25.01

26.60

26.60

26.60

26.60

31.65

Sv/S

0.124

0.124

0.124

0.124

0.124

0.124

0.124

SvLv/Sb

0.048

0.051

0.054

0.054

0.054

0.054

0.065

Horizontal Tail:
Area (m)

101.26

101.26

101.26

101.26

101.26

101.26

101.26

Span (m)

21.35

21.35

21.35

21.35

21.35

21.35

21.35

Aspect Ratio

4.50

4.50

4.50

4.50

4.50

4.50

4.50

Taper Ratio

0.300

0.300

0.300

0.300

0.300

0.300

0.300

1/4 Chord Sweep ()

35.00

35.00

35.00

35.00

35.00

35.00

35.00

Tail Arm (m)

24.71

26.31

27.90

27.90

27.90

27.90

32.95

Sh/S

0.237

0.237

0.237

0.237

0.237

0.237

0.237

ShLh/Sc

0.668

0.712

0.755

0.755

0.755

0.755

0.891

Undercarriage:
Track (m)

11.00

11.00

11.00

11.00

11.00

11.00

11.00

Wheelbase (m)

25.80

25.80

25.80

25.80

25.80

25.80

25.80

Turning radius (m)

41.00

41.00

41.00

41.00

41.00

41.00

41.00

No. of wheels (nose;main)

2;12

2;12

2;12

2;12

2;12

2;12

2;12

Main Wheel diameter (m)

1.118

1.118

1.118

1.118

1.118

1.118

1.118

Main Wheel width (m)

0.457

0.457

0.457

0.457

0.457

0.457

0.457

Nacelle:
Length (m)

7.30

7.30

7.30

7.30

7.30

7.30

7.30

Max. width (m)

3.20

3.20

3.20

3.20

3.20

3.20

3.20

Spanwise location 0.326 0.326

0.326

0.326

0.326

0.326

0.326

Manufacturer BOEING BOEING BOEING BOEING BOEING BOEING BOEING
Type 777- 777- 777- 777- 777- 777- 777-
Model 100X1 100X2 200 200IGW 200X1 200X2 300
PERFORMANCE
Loadings:
Max Power Load (kg/kN) 358.28 374.15 354.24 383.90 361.67 358.86 353.87
Max Wing Load (kg/m2) 669.99 699.67 567.25 670.63 699.67 731.47 699.79
Thrust/Weight Ratio 0.2845 0.2724 0.2878 0.2655 0.2818 0.2841 0.2881
Take-off (m):
ISA sea level 2135
ISA +20C SL. 2440 3050 3540
ISA 5,000ft
ISA +20C 5,000ft
Landing (m):
ISA sea level. 1585 1620 1860
ISA +20C SL. 1585 1620 1860
ISA 5,000ft 1875 1940
ISA +20C 5,000ft 1875 1940
Speeds (kt/Mach):
V2
Vapp 138 140
Vno/Mmo 330/M0.87 330/M0.87 330/M0.87
Vne/Mme
CLmax (T/O)
CLmax (L/D @ MLM) 2.53 2.55
Max cruise :
Speed (kt) 499 499
Altitude (ft) 39000 39000
Fuel consumption (kg/h)
Long range cruise:
Speed (kt) 476 476
Altitude (ft) 39000 39000
Fuel consumption (kg/h)
Range (nm):
Max payload
Design range 7625 8420 4820 7380 7455 7970 5604
Max fuel (+ payload)
Ferry range
Design Parameters:
W/SCLmax
W/aCLtoST
Fuel/pax/nm (kg)
Seats x Range (seats.nm)