CIVIL JET AIRCRAFT DESIGN

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PREFACE
APPENDICES
CASE STUDIES
ABOUT THE AUTHORS
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Data A : Aircraft Data File

Table 5 : Douglas and Boeing (Douglas Products Division) Aircraft

Notes

Manufacturer

DOUG.

DOUG.

DOUG.

DOUG.

DOUG.

DOUG.

McDON.

McDON.

McDON.

McDON.

Type

/DOUG.

/DOUG.

/DOUG.

/DOUG.

Model

DC8-63

DC8-73

DC 9-10

DC 9-30

DC 9-40

DC 9-50

MD-81

MD-82

MD-83

MD-87

Initial service date

1959

1980

1965

1967

1968

1975

1980

1980

1980

1980

In service (ordered)

Africa

--->

11

-

10

-

2

--->

--->

--->

8

Middle East/Asia/Pacific

--->

-

-

10

-

-

--->

--->

--->

94

Europe & CIS

--->

7

2

38

22

18

--->

--->

--->

336

North & South America

--->

235

92

448

47

72

--->

--->

--->

706(29)

Total aircraft

--->

253

94

506

69

92

--->

--->

--->

1144(28)

Engine Manufacturer

PW

CFMI

PW

PW

PW

PW

P&W

P&W

P&W

P&W

Model / Type

JT3D-3B

CFM56-2C

JT8D-5

JT8D-7

JT8D-15A

JT8D-15A

JT8D-209

JT8D-217AC

JT8D-219

JT8D-217B/C

No. of engines

4

4

2

2

2

2

2

2

2

2

Static Thrust (kN)

80.1

98

54.5

62

68.9

68.9

85.6

92.7

96.5

92.7

Operational Items:

Accomodation:

Max. seats (single class)

259

259

90

119

125

139

172

172

172

130

Two class seating

189

189

68

97

105

122

155

155

155

114

Three class seating

-

-

-

-

-

-

-

-

-

-

No. abreast

5

5

5

5

5

5

5

5

5

5

Hold volume (m3)

70.8

70.8

17

25.3

28.9

28.4

35.20

35.20

28.70

26.60

Volume per passenger

0.27

0.27

0.19

0.21

0.23

0.20

0.20

0.20

0.17

0.20

Mass (Weight) (kg):

Ramp

160120

162000

35605

49500

52168

54700

63950

68270

73030

63950

Max. take-off

158760

161000

35245

49000

51710

54420

63500

67812

72580

63500

Max. landing

111130

117000

33565

45000

46265

49885

58000

58970

63280

58000

Zero-fuel

100458

104800

30120

39500

42184

44670

53500

55340

55340

53524

Max. payload

30719

29257

9570

14000

15510

15265

17953

18802

18721

17619

Max. fuel payload

15516.2

11988

3495

12484

12792

12600

10252

14620

14887

12728

Design payload

17955

17955

6460

9215

9975

11590

14725

14725

14725

10830

Design fuel load

71066

67545

8235

14385

13935

13530

13205

17457

21235

19417

Operational empty

69739

75500

20550

25400

27800

29300

35570

35630

36620

33253

Weight Ratios:

Ops empty/Max. T/O

0.439

0.469

0.583

0.518

0.538

0.538

0.560

0.525

0.505

0.524

Max. payload/Max. T/O

0.193

0.182

0.272

0.286

0.300

0.281

0.283

0.277

0.258

0.277

Max. fuel/Max. T/O

0.457

0.451

0.314

0.225

0.213

0.234

0.275

0.258

0.288

0.275

Max. landing/Max. T/O

0.700

0.727

0.952

0.918

0.895

0.917

0.913

0.870

0.872

0.913

Fuel (litres):

Standard

91881

91890

14000

13925

13925

16120

22106

22106

26495

22106

Optional

26384

26495

Manufacturer

DOUG.

DOUG.

DOUG.

DOUG.

DOUG.

DOUG.

McDON.

McDON.

McDON.

McDON.

Type

/DOUG.

/DOUG.

/DOUG.

/DOUG.

Model

DC8-63

DC8-73

DC 9-10

DC 9-30

DC 9-40

DC 9-50

MD-81

MD-82

MD-83

MD-87

DIMENSIONS

Fuselage:

Length (m)

55.70

55.70

27.91

32.28

34.70

37.14

41.30

41.30

41.30

36.30

Height (m)

3.80

3.80

3.60

3.60

3.60

3.60

3.61

3.61

3.61

3.61

Width (m)

3.80

3.80

3.60

3.60

3.60

3.60

3.61

3.61

3.61

3.61

Finess Ratio

14.66

14.66

7.75

8.97

9.64

10.32

11.44

11.44

11.44

10.06

Wing:

Area (m²)

271.90

271.90

86.77

92.97

92.97

92.97

112.30

112.30

112.30

112.30

Span (m)

45.23

45.23

27.25

28.47

28.47

28.47

32.87

32.87

32.87

32.87

MAC (m)

7.10

7.10

3.67

3.73

3.73

3.73

4.08

4.08

4.08

4.08

Aspect Ratio

7.52

7.52

8.56

8.72

8.72

8.72

9.62

9.62

9.62

9.62

Taper Ratio

0.181

0.181

0.194

0.206

0.206

0.206

0.195

0.195

0.195

0.195

Average (t/c) %

11.00

11.00

11.65

11.60

11.60

11.60

11.00

11.00

11.00

11.00

Max. seats (single class)

30.00

30.00

24.00

24.00

24.00

24.00

24.50

24.50

24.50

24.50

High Lift Devices:

Trailing Edge Flaps Type

S2

S2

S2

S3

S3

S3

S2

S2

S2

S2

Flap Span/Wing Span

0.730

0.730

0.670

0.670

0.670

0.670

0.670

0.670

0.670

0.670

Area (m2)

19.58

19.58

19.58

19.58

Leading Edge Flaps Type

flaps

flaps

none

slats

slats

slats

slats

slats

slats

slats

Area (m²)

-

11.58

11.58

11.58

Vertical Tail:

Area (m²)

23.60

23.60

14.96

14.96

14.96

14.96

15.60

15.60

15.60

18.50

Height (m)

6.40

6.40

3.90

4.90

5.90

6.90

4.10

4.10

4.10

4.20

Aspect Ratio

1.74

1.74

1.02

1.60

2.33

3.18

1.08

1.08

1.08

0.95

Taper Ratio

0.333

0.333

0.750

0.750

0.750

0.750

0.707

0.707

0.707

0.750

1/4 Chord Sweep (º)

35.00

35.00

42.00

42.00

42.00

42.00

42.00

42.00

42.00

42.50

Tail Arm (m)

25.70

25.70

11.70

13.10

14.50

15.72

15.70

15.70

15.70

13.60

Sv/S

0.087

0.087

0.172

0.161

0.161

0.161

0.139

0.139

0.139

0.165

SvLv/Sb

0.049

0.049

0.074

0.074

0.082

0.089

0.066

0.066

0.066

0.068

Horizontal Tail:

Area (m2)

51.10

51.10

25.60

25.60

25.60

25.60

29.17

29.17

29.17

29.17

Span (m)

14.48

14.48

11.23

11.23

11.23

11.23

12.24

12.24

12.24

12.24

Aspect Ratio

4.10

4.10

4.93

4.93

4.93

4.93

5.14

5.14

5.14

5.14

Taper Ratio

0.341

0.341

0.318

0.318

0.318

0.318

0.330

0.330

0.330

0.400

1/4 Chord Sweep (º)

35.00

35.00

30.00

30.00

30.00

30.00

30.00

30.00

30.00

30.00

Tail Arm (m)

24.95

24.95

14.35

15.82

17.23

18.45

18.00

18.00

18.00

16.30

Sh/S

0.188

0.188

0.295

0.275

0.275

0.275

0.260

0.260

0.260

0.260

ShLh/Sc

0.660

0.660

1.154

1.168

1.272

1.362

1.146

1.146

1.146

1.038

Undercarriage:

Track (m)

5.03

5.03

5.03

5.03

5.08

5.08

5.08

5.08

Wheelbase (m)

23.60

23.60

13.32

16.22

17.10

18.60

22.07

22.07

22.07

19.18

Turning radius (m)

32.60

32.60

19.80

20.70

23.00

22.80

22.80

22.80

20.60

No. of wheels (nose;main)

2;8

2;8

2;4

2;4

2;4

2;4

2;4

2;4

2;4

2;4

Main Wheel diameter (m)

1.024

1.024

1.024

1.024

1.130

1.130

1.130

1.130

Main Wheel width (m)

0.358

0.358

0.358

0.358

0.508

0.508

0.508

0.508

Nacelle:

Length (m)

6.00

4.70

5.30

5.30

5.30

5.30

6.10

6.10

6.10

6.10

Max. width (m)

1.60

2.00

1.56

1.56

1.56

1.56

2.00

2.00

2.00

1.95

Spanwise location

-

-

-

-

-

-

-

-

Manufacturer DOUG. DOUG. DOUG. DOUG. DOUG. DOUG. McDON. McDON. McDON. McDON.
Type /DOUG. /DOUG. /DOUG. /DOUG.
Model DC8-63 DC8-73 DC 9-10 DC 9-30 DC 9-40 DC 9-50 MD-81 MD-82 MD-83 MD-87
PERFORMANCE
Loadings:
Max Power Load (kg/kN) 469.70 410.71 323.35 395.16 375.25 394.92 370.91 365.76 376.06 342.50
Max Wing Load (kg/m²) 583.89 592.13 406.19 527.05 556.20 585.35 565.45 603.85 646.30 565.45
Thrust/Weight Ratio 0.217 0.248 0.315 0.258 0.272 0.258 0.275 0.279 0.271 0.298
Take-off (m):
ISA sea level 3505 3048 1615 1777 2091 2362 2195 2274 2551 1865
ISA +20ºC SL. 3139 2000 2402 3130 2646 2612 3066 2161
ISA 5,000ft 3962 2940 3734 3680 2804 2804 2804 2643
ISA +20ºC 5,000ft 4023 3860 3831 3570 2987 2987 2987 2987
Landing (m):
ISA sea level. 1801 1981 1411 1317 1457 1439 1481 1500 1585 1451
ISA +20ºC SL. 1981 1310 1457 1439 1481 1500 1585 1451
ISA 5,000ft 2286 1485 1655 1580 1664 1682 1783 1614
ISA +20ºC 5,000ft 2286 1485 1655 1525 1664 1682 1783 1614
Speeds (kt/Mach):
V2 127 137 151 160 148 153 153 141
Vapp 115 126 131 132 133 134 139 133
Vno/Mmo 352/M0.88 352/M0.88 425 425 425 425 340/M0.84 340/M0.84 340/M0.84 340/0.84
Vne/Mme 406/M0.95 406/M0.95 350 350 350 350 395/M0.90 395/M0.90 395/M0.90 395/M0.90
CLmax (T/O) 2.20 2.45 2.13 1.99 2.25 2.25 2.41 2.48
CLmax (L/D @ MLM) 2.99 3.12 2.97 3.15 2.99 2.99 2.98 2.99
Max cruise :
Speed (kt) 479 501 503 501 501 499 499 499 499
Altitude (ft) 35000 25000 26000 27000 27000 27000 27000 27000 27000
Fuel consumption (kg/h) 4881 4050 3980 4525 4077 4077 4027 3924
Long range cruise:
Speed (kt) 431 431 440 441 439 439 439 439
Altitude (ft) 35000 35000 35000 35000 35000 35000 35000 35000
Fuel consumption (kg/h) 2100 2280 2650 2560 2560 2518 2458
Range (nm):
Max payload 4190 1546 1423 1361 1385 1860 2369 1863
Design range 3907 1311 1725 1685 1500 1564 2050 2502 2372
Max fuel (+ payload) 1922 1790 1914 2851 2668 3147 2958
Ferry range 6686
Design Parameters:
W/SCLmax 1332 1658 1839 1823 1857 1980 2125 1857
W/aCLtoST 1610 2449 2580 2691 2575 2707 2987 2378
Fuel/pax/nm (kg) 0.0962 0.0924 0.0860 0.0788 0.0739 0.0545 0.0549 0.0548 0.0718
Seats x Range (seats.nm) 738423 89148 167325 176925 183000 242420 317750 387810 270408
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