CIVIL JET AIRCRAFT DESIGN

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




 

 

Data A : Aircraft Data File

Table 2 : Boeing Aircraft

Notes

Manufacturer

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

Type

707-

717-

727-

737-

737-

737-

737-

737-

737-

737-

Model

320C

200

200Adv

200

300

400

500

600

700

800

Initial service date

1962

1999

1970

1967

1967

1967

1967

1998

1997

1998

In service (ordered)
Africa

53

-

58

85

14(1)

7

17

(7)

(2)

2(12)

Middle East/Asia/Pacific

31

-

52

114

194(19)

142(5)

49(2)

-

9(24)

7(45)

Europe & CIS

9

-

94

147

272(12)

216(4)

145(1)

6(49)

21(35)

20(110)

North & South America

25

(60)

799

532

573(11)

97(5)

165(1)

-

36(146)

13(211)

Total aircraft

120

(60)

1003

878

1053(43)

462(14)

376(4)

6(56)

66(207)

42(378)

Engine Manufacturer

P&W

BMW R-R

P&W

P&W

CFMI

CFMI

CFMI

CFMI

CFMI

CFMI

Model / Type

JT3D-7

715

JT8D-15A

JT8D-15A

CFM56-3-B1

CFM56-3B-2

CFM56-3-B1R

CFM56-7B18

CFM56-7B20

CFM56-7B24

No. of engines

4

2

3

2

2

2

2

2

2

2

Static thrust (kN)

84.5

97.9

71.2

71.2

89.0

97.9

82.3

82.0

89.0

107.0

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

219

110

189

130

149

170

130

132

149

189

Two class seating

147

106

136

115

128

146

108

108

128

160

Three class seating

-

-

-

-

-

-

-

-

-

-

No. abreast

6

5

6

6

6

6

6

6

6

6

Hold volume (m3)

50.27

25.00

43.10

24.78

30.20

38.90

23.30

23.30

30.2

47.1

Volume per passenger

0.23

0.23

0.23

0.19

0.20

0.23

0.18

0.18

0.20

0.25

Mass (Weight) (kg):
Ramp

152405

52110

95238

52615

56700

63050

52620

65310

69610

78460

Max. take-off

151315

51710

95028

52390

56470

62820

52390

65090

69400

78220

Max. landing

112037

46266

72575

46720

51710

54880

49900

54650

58060

65310

Zero-fuel

104330

43545

63318

43091

47630

51250

46490

51480

54650

61680

Max. payload

38100

12220

18597

15445

16030

17740

15530

9800

11610

14690

Max. fuel payload

12852

8921

24366

9118

8705

13366

5280

7831

10996

15921

Design payload

13965

10070

12920

10925

12160

13870

10260

10260

12160

15200

Design fuel load

71126

9965

35944

13819

12441

15580

11170

18390

19655

21540

Operational empty

66224

31675

46164

27646

31869

33370

30960

36440

37585

41480

Weight Ratios:
Ops empty/Max. T/O

0.438

0.613

0.486

0.528

0.564

0.531

0.591

0.560

0.542

0.530

Max. payload/Max. T/O

0.252

0.236

0.196

0.295

0.284

0.282

0.296

0.151

0.167

0.188

Max. fuel/Max. T/O

0.471

0.212

0.255

0.341

0.281

0.253

0.303

0.316

0.296

0.263

Max. landing/Max. T/O

0.740

0.895

0.764

0.892

0.916

0.874

0.952

0.840

0.837

0.835

Fuel (litres):
Standard

90299

13892

30622

19532

20105

20105

20105

26024

26024

26024

Optional

16065

40068

22598

23170

23170

23170

 

Manufacturer

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

BOEING

Type

707-

717-

727-

737-

737-

737-

737-

737-

737-

737-

Model

320C

200

200Adv

200

300

400

500

600

700

800

DIMENSIONS
Fuselage:
Length (m)

44.35

33.00

41.51

29.54

32.30

35.30

29.90

29.88

32.18

38.08

Height (m)

3.76

3.61

3.76

3.73

3.73

3.73

3.73

3.73

3.73

3.73

Width (m)

3.76

3.61

3.76

3.73

3.73

3.73

3.73

3.73

3.73

3.73

Finess Ratio

7.30

4.30

7.00

7.40

7.40

7.40

7.40

7.40

7.40

7.40

Wing:
Area (m)

283.40

92.97

157.90

91.04

91.04

91.04

91.04

124.60

124.60

124.60

Span (m)

44.42

28.40

32.92

28.35

28.90

28.90

28.90

34.30

34.30

34.30

MAC (m)

7.36

3.88

5.46

3.80

3.73

3.73

3.73

4.17

4.17

4.17

Aspect Ratio

6.96

8.68

6.86

8.83

9.17

9.17

9.17

9.44

9.44

9.44

Taper Ratio

0.259

0.196

0.309

0.266

0.240

0.240

0.240

0.278

0.278

0.278

Average (t/c) %

10.00

11.60

11.00

12.89

12.89

12.89

12.89

1/4 Chord Sweep ()

35.00

24.50

32.00

25.00

25.00

25.00

25.00

25.00

25.00

25.00

High Lift Devices:
Trailing Edge Flaps Type

F1

S2

F3

F3

S3

S3

S3

S2

S2

S2

Flap Span/Wing Span

0.670

0.650

0.740

0.740

0.720

0.720

0.720

0.599

0.599

0.599

Area (m2)

44.22

36.04

Leading Edge Flaps Type

flaps

slats

slats/flaps

slats/flaps

slats/flaps

slats/flaps

slats/flaps

slats/flaps

slats/flaps

slats/flaps

Area (m)
Vertical Tail:
Area (m)

30.47

19.50

33.07

19.70

23.13

23.13

23.13

23.13

23.13

23.13

Height (m)

7.20

4.35

4.60

5.85

6.00

6.00

6.00

6.00

6.00

6.00

Aspect Ratio

1.70

0.97

0.64

1.74

1.56

1.56

1.56

1.56

1.56

1.56

Taper Ratio

0.410

0.780

0.780

0.288

0.310

0.310

0.310

0.310

0.310

0.310

1/4 Chord Sweep ()

30.00

45.00

53.00

35.00

35.00

35.00

35.00

35.00

35.0

35.0

Tail Arm (m)

21.00

12.80

14.20

12.10

13.68

14.90

12.90

13.55

14.7

17.7

Sv/S

0.108

0.210

0.209

0.216

0.254

0.254

0.254

0.186

0.186

0.186

SvLv/Sb

0.051

0.095

0.090

0.092

0.120

0.131

0.113

0.073

0.080

0.096

Horizontal Tail:
Area (m2)

58.06

24.20

34.93

31.31

31.31

31.31

31.31

32.40

32.40

32.40

Span (m)

13.95

10.80

10.90

12.70

12.70

12.70

12.70

13.40

13.40

13.40

Aspect Ratio

3.35

4.82

3.40

5.15

5.15

5.15

5.15

5.54

5.54

5.54

Taper Ratio

0.400

0.380

0.380

0.260

0.260

0.260

0.260

0.186

0.186

0.186

1/4 Chord Sweep ()

36.00

30.00

36.00

30.00

30.00

30.00

30.00

30.00

30.00

30.00

Tail Arm (m)

20.50

14.30

20.10

14.78

14.78

16.00

14.00

13.58

14.73

17.68

Sh/S

0.205

0.260

0.221

0.344

0.344

0.344

0.344

0.260

0.260

0.260

ShLh/Sc

0.571

0.959

0.814

1.338

1.363

1.475

1.291

0.847

0.919

1.102

Undercarriage:
Track (m)

6.73

4.88

5.72

5.23

5.25

5.25

5.25

5.70

5.7

5.7

Wheelbase (m)

17.98

17.60

19.28

11.38

12.40

14.30

11.00

12.4

Turning radius (m)

25.00

19.50

19.5

No. of wheels (nose;main)

2;8

2;4

2;4

2;4

2;4

2;4

2;4

2;4

2;4

2;4

Main Wheel diameter (m)

1.117

1.245

1.016

1.016

1.016

1.016

1.016

1.016

Main Wheel width (m)

0.406

0.432

0.368

0.368

0.368

0.368

0.368

0.368

Nacelle:
Length (m)

6.00

6.10

7.00

7.00

4.70

4.70

4.70

4.70

4.70

4.70

Max. width (m)

1.60

1.75

1.50

1.50

2.00

2.00

2.00

2.06

2.06

2.06

Spanwise location

0.44/0.71

-

-

0.350

0.340

0.340

0.340

0.282

0.282

0.282

 

Manufacturer BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING
Type 707- 717- 727- 737- 737- 737- 737- 737- 737- 737-
Model 320C 200 200Adv 200 300 400 500 600 700 800
PERFORMANCE
Loadings:
Max Power Load (kg/kN) 447.47 264.10 444.89 367.91 317.25 320.84 318.29 396.89 389.89 365.51
Max Wing Load (kg/m2) 533.93 556.20 601.82 575.46 620.28 690.03 575.46 522.39 556.98 627.77
Thrust/Weight Ratio 0.2278 0.3860 0.2291 0.2771 0.3213 0.3177 0.3203 0.2568 0.2615 0.2789
Take-off (m):
ISA sea level 3054 3033 1829 1939 2222 1832
ISA +20C SL. 3658 1859 2109 2475 2003 1878 2042 2316
ISA 5,000ft 3962 2886 2432 2316
ISA +20C 5,000ft 4176 3292 2637 2649
Landing (m):
ISA sea level. 1905 1445 1494 1350 1396 1582 1362 1268 1356 1600
ISA +20C SL. 1494 1350 1396 1582 1362 1268 1356 1600
ISA 5,000ft 1661 1615 1576 1695 1533
ISA +20C 5,000ft 1661 1615 1576 1695 1533
Speeds (kt/Mach):
V2 150 166 147 148 159 142
Vapp 135 130 137 131 133 138 130
Vno/Mmo 383/M0.90 438/M0.76 390/M0.90 350/M0.84 340/M0.82 340/M0.82 340/M0.82 392/M0.84 392/M0.84 392/M0.84
Vne/Mme 425/M0.95 M0.95
CLmax (T/O) 2.15 1.90 2.32 2.47 2.38 2.49
CLmax (L/D @ MLM) 2.22 3.01 2.51 3.06 3.28 3.24 3.32
Max cruise :
Speed (kt) 521 530 488 491 492 492
Altitude (ft) 25000 25000 25000 26000 26000 26000 41000 41000 41000
Fuel consumption (kg/h) 4536 4005 3890 3307 3574
Long range cruise:
Speed (kt) 478 438 467 420 429 430 429 450 452 452
Altitude (ft) 35000 33000 35000 35000 35000 35000 39000 39000 39000
Fuel consumption (kg/h) 4309 2827 2250 2377 2100 1932 2070 2186.84
Range (nm):
Max payload 3150 2140 1549 1578 1950 1360
Design range 1375 2400 1900 2850 2700 1700 3191 3197 2897
Max fuel (+ payload) 5000 2887 3187 2830 3450 3229 3245 2927
Ferry range
Design Parameters:
W/SCLmax 2360.53 1811.43 2356.82 1845.48 1852.54 2090.56 1701.59
W/aCLtoST 3947.87 1788.04 3918.96 2537.71 2196.64 2506.93 2024.27
Fuel/pax/nm (kg) 0.0684 0.1101 0.0632 0.0341 0.0395 0.0608 0.0534 0.0480 0.0465
Seats x Range (seats.nm) 145750 326400 218500 364800 394200 183600 344628 409216 463520