CIVIL JET AIRCRAFT DESIGN

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PREFACE
APPENDICES
CASE STUDIES
ABOUT THE AUTHORS
AIRCRAFT LINKS




 

 

Data A : Aircraft Data File

Table 1 : Airbus Aircraft

Notes

Manufacturer

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

Type

A300-

A310-

A319-

A320-

A321-

A330-

A330-

A340-

A340-

A340-

A340-

A3XX-

Model

600R

300

100

200

200

200

300

200

300

500

600

100

Initial service date

1974

1983

1995

1988

1993

1998

1994

1993

1994

2002

2002

2004

In service (ordered)
Africa

28

11

2(1)

27(6)

4

--->

-

--->

8(1)

--->

(2)

-

Middle East/Asia/Pacific

205(5)

69(5)

(4)

162(47)

17(32)

--->

59(47)

--->

54(10)

--->

(6)

-

Europe & CIS

83

87(1)

48(82)

244(105)

84(68)

--->

17(42)

--->

69(15)

--->

(27)

-

North & South America

72(37)

57

57(264)

237(146)

-

--->

4(42)

--->

9(8)

--->

(5)

-

Total aircraft

388(42)

224(6)

107(351)

670(304)

105(102)

--->

80(131)

--->

140(34)

--->

(40)

-

Engine Manufacturer

P&W

P&W

CFMI

CFMI

CFMI

GE

GE

CFMI

CFMI

R-R

R-R

R-R/GE/PW

Model / Type

4158

4152

CFM56-5A4

CFM56-5A3

CFM56-5B3

CF6-80E1A4

CF6-80E1A2

CFM-56-5C2

CFM-56-5C4

Trent 553

Trent 556

Options

No. of engines

2

2

2

2

2

2

2

4

4

4

4

4

Static thrust (kN)

257.0

231.0

99.7

111.2

142.0

310.0

300.0

139.0

151.0

235.8

249.1

294.0

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

375

280

153

179

220

380

440

440

440

440

475

850

Two class seating

266

218

124

150

186

293

335

303

335

350

440

Three class seating

228

187

-

-

-

253

295

262

295

313

380

555

No. abreast

9

9

6

6

6

9

9

9

9

9

9

10+8

Hold volume (m)

116.00

79.90

27.00

38.76

51.76

136.00

162.90

136.00

162.90

134.10

187.74

Volume per passenger

0.31

0.29

0.18

0.22

0.24

0.36

0.37

0.31

0.37

0.30

0.40

Mass (Weight) (kg):
Ramp

171400

150900

64400

73900

89400

230900

217900

257900

271900

365900

365900

540900

Max. take-off

170500

150000

64000

73500

89000

230000

217000

257000

271000

365000

365000

540000

Max. landing

140000

123000

61000

64500

73500

177150

179000

181000

190000

236000

254000

381000

Zero-fuel

130000

113000

57000

60500

71500

165142

169000

172000

178000

222000

240000

356000

Max. payload

41100

33300

17390

19190

22780

36400

48400

49400

48150

51635

63000

85000

Max. fuel payload

27100

21500

5360

13500

19060

0

18600

21220

33160

31450

29311

15400

Design payload

25270

20710

11780

14250

17670

24035

28025

24890

28025

29735

36100

52725

Design fuel load

56330

49624

13020

17940

23330

85765

70786

111882

113125

164875

151890

216275

Operational empty

88900

79666

39200

41310

48000

120200

118189

120228

129850

170390

177010

271000

Weight Ratios:
Ops empty/Max. T/O

0.521

0.531

0.613

0.562

0.539

0.523

0.545

0.468

0.479

0.467

0.485

0.502

Max. payload/Max. T/O

0.241

0.222

0.272

0.261

0.256

0.158

0.223

0.192

0.178

0.141

0.173

0.157

Max. fuel/Max. T/O

0.316

0.322

0.295

0.256

0.210

0.478

0.358

0.430

0.412

0.423

0.423

0.464

Max. landing/Max. T/O

0.821

0.820

0.953

0.878

0.826

0.770

0.825

0.704

0.701

0.647

0.696

0.706

Fuel (litres):
Standard

68150

61100

23860

23860

23700

139090

98250

140000

141500

195620

195620

317000

Optional

75350

68300

26600

148700

213120

Manufacturer AIRBUS AIRBUS AIRBUS AIRBUS AIRBUS AIRBUS AIRBUS AIRBUS AIRBUS AIRBUS AIRBUS AIRBUS
Type A300- A310- A319- A320- A321- A330- A330- A340- A340- A340- A340- A3XX-
Model 600R 300 100 200 200 200 300 200 300 500 600 100
DIMENSIONS
Fuselage:
Length (m) 53.30 45.13 33.84 37.57 44.51 57.77 62.47 58.21 62.47 65.60 69.57 67.46
Height (m) 5.64 5.64 4.14 4.14 4.14 5.64 5.64 5.64 5.64 5.64 5.64 8.50
Width (m) 5.64 5.64 3.95 3.95 3.95 5.64 5.64 5.64 5.64 5.64 5.64 7.02
Finess Ratio 9.45 8.00 8.57 9.51 11.27 10.24 11.08 10.32 11.08 11.63 12.34 9.61
Wing:
Area (m) 260.00 219.00 122.40 122.40 122.40 363.10 363.10 363.10 363.10 437.30 437.30 817.00
Span (m) 44.84 43.89 33.91 33.91 33.91 58.00 58.00 58.00 58.00 61.20 61.20 79.80
M.A.C.(m) 6.44 5.89 4.29 4.29 4.29 7.26 7.26 7.26 7.26 8.35 8.35 12.02
Aspect Ratio 7.73 8.80 9.39 9.39 9.39 9.26 9.26 9.26 9.26 8.56 8.56 7.79
Taper Ratio 0.300 0.283 0.240 0.240 0.240 0.251 0.251 0.251 0.251 0.220 0.220 0.213
Average (t/c) % 10.50 11.80
1/4 Chord Sweep () 28.00 28.00 25.00 25.00 25.00 29.70 29.70 29.70 29.70 31.10 31.10 30.00
High Lift Devices:
Trailing Edge Flaps Type F2 F1 F1 F1 F2 S2 S2 S2 S2 S2 S2 S2
Flap Span/Wing Span 0.800 0.840 0.780 0.780 0.780 0.665 0.665 0.665 0.665 0.625 0.625 0.737
Area (m) 47.3 36.68 21.1 21.1 21.1
Leading Edge Flaps Type slats slats slats slats slats slats slats slats slats slats slats slats
Area (m) 30.3 28.54 12.64 12.64 12.64
Vertical Tail:
Area (m) 45.20 45.20 21.50 21.50 21.50 47.65 45.20 45.20 45.20 47.65 47.65 134.20
Height (m) 8.60 8.10 6.26 6.26 6.26 9.44 8.45 8.45 8.45 9.44 9.44 13.66
Aspect Ratio 1.64 1.45 1.82 1.82 1.82 1.87 1.58 1.58 1.58 1.87 1.87 1.39
Taper Ratio 0.365 0.395 0.303 0.303 0.303 0.350 0.350 0.350 0.350 0.350 0.350 0.424
1/4 Chord Sweep () 40.00 40.00 34.00 34.00 34.00 45.00 45.00 45.00 45.00 45.00 45.00
Tail Arm (m) 24.90 20.20 10.67 12.53 15.20 25.20 27.50 25.50 27.50 27.50 27.50 28.99
Sv/S 0.174 0.206 0.176 0.176 0.176 0.131 0.124 0.124 0.124 0.109 0.109 0.164
SvLv/Sb 0.097 0.095 0.055 0.065 0.079 0.057 0.059 0.055 0.059 0.049 0.049 0.060
Horizontal Tail:
Area (m) 69.45 64.00 31.00 31.00 31.00 31.00 72.90 72.90 72.90 93.00 93.00 222.57
Span (m) 16.26 16.26 12.45 12.45 12.45 12.45 19.06 19.06 19.06 21.50 21.50 31.29
Aspect Ratio 3.81 4.13 5.00 5.00 5.00 5.00 4.98 4.98 4.98 4.97 4.97 4.40
Taper Ratio 0.420 0.417 0.256 0.256 0.256 0.256 0.360 0.360 0.360 0.360 0.360 0.383
1/4 Chord Sweep () 34.00 34.00 29.00 29.00 29.00 29.00 30.00 30.00 30.00 30.00 30.00
Tail Arm (m) 25.60 22.50 11.67 13.53 16.20 16.20 28.60 26.50 28.60 28.60 28.60 31.29
Sh/S 0.267 0.292 0.253 0.253 0.253 0.253 0.201 0.201 0.201 0.213 0.213 0.272
ShLh/Sc 1.062 1.116 0.689 0.799 0.957 0.957 0.791 0.733 0.791 0.729 0.729 0.709
Undercarriage:
Track (m) 9.60 9.60 7.60 7.60 7.60 7.60 10.70 10.70 10.70 10.70 10.70 13.47
Wheelbase (m) 18.60 15.21 12.60 12.63 16.90 16.90 25.40 23.20 25.40 28.53 32.50 27.60
Turning radius (m) 34.00 31.40 20.60 21.90 29.00 29.00 41.40 40.60
No. of wheels (nose;main) 2;8 2;8 2;4 2;4 2;4 2;8 2;8 2;10 2;10 2;12 2;12 2;22
Main Wheel Diameter (m) 1.245 1.168 1.143 1.143 1.270
Main Wheel Width (m) 0.483 0.406 0.406 0.406 0.455
Nacelle:
Length (m) 6.70 6.30 4.44 4.44 4.44 7.00 7.00 4.95 4.95 6.10 6.10 7.30
Max Width (m) 2.70 2.70 2.37 2.37 2.37 3.10 3.10 2.37 2.37 3.05 3.05 3.20
Spanwise Location 0.359 0.352 0.338 0.338 0.338 0.312 0.312 0.312/0.672 0.312/0.672 0.296/0.625 0.296/0.625 0.348/0.678
Manufacturer

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

AIRBUS

Type

A300-

A310-

A319-

A320-

A321-

A330-

A330-

A340-

A340-

A340-

A340-

A3XX-

Model

600R

300

100

200

200

200

300

200

300

500

600

100

PERFORMANCE
Loadings:
Max. power load (kg/kN)

331.71

324.68

320.96

330.49

313.38

370.97

361.67

462.23

448.68

386.98

366.32

459.18

Max. wing load (kg/m2)

655.77

684.93

522.88

600.49

727.12

633.43

597.63

707.79

746.35

834.67

834.67

660.95

Thrust/Weight Ratio

0.3073

0.3140

0.3176

0.3084

0.3253

0.2748

0.2819

0.2205

0.2272

0.2634

0.2783

0.2220

Take-off (m):
ISA sea level

2280

2290

1750

2180

2000

2470

2320

2790

3000

3100

3100

ISA +20C SL.

3189

2450

2080

2590

2286

2590

2680

3260

3380

3550

3550

3350

ISA 5000ft

2950

2360

2950

3269

3900

3840

4320

4298

4250

4250

ISA +20C 5000ft

3660

2870

4390

Landing (m):
ISA sea level.

1489

1490

1350

1440

1580

1750

1600

1856

1964

2090

2240

ISA +20C SL.

1489

1490

1350

1440

1580

1750

1600

1856

1964

2090

2240

ISA 5000ft

1701

1686

1530

1645

1795

1970

1920

2094

2227

2390

ISA +20C 5000ft

1701

1686

1530

1645

1795

1970

1920

2094

2227

2390

Speeds (kt/Mach):
V2

153

156

133

143

143

158

144

154

158

Vapp

136

138

131

134

138

135

136

134

136

139

144

<150

Vno/Mmo

335/M0.82

360/M0.84

381/M0.89

350/M0.82

350/M0.82

330/M0.86

330/M0.86

330/M0.86

330/M0.86

330/M0.86

330/M0.86

Vne/Mme

395/M0.88

420/M0.90

350/M0.82

381/M0.89

TBD/M0.89

365/M0.93

365/M0.93

365/M0.93

365/M0.93

365/M0.93

365/M0.93

CLmax (T/O)

2.44

2.45

2.58

2.56

3.10

2.21

2.51

2.60

2.61

CLmax (L/D @ MLM)

2.98

3.02

2.97

3.00

3.23

2.74

2.73

2.84

2.89

2.86

2.87

Max. cruise :
Speed (kt)

480

484

487

487

487

500

500

500

507

Altitude (ft)

31000

35000

33000

28000

28000

33000

33000

33000

35000

Fuel consumption (kg/h)

5120

4690

3160

3200

3550

5000

7180

7300

Long range cruise:
Speed (kt)

456

458

446

448

450

470

465

475

475

Altitude (ft)

35000

37000

37000

37000

37000

39000

39000

39000

39000

Fuel consumption (kg/h)

4300

3730

1980

2100

2100

4700

5400

5700

Range (nm):
Max. payload

3283

3645

1355

637

1955

4210

3888

6393

6371

7050

5700

6200

Design range

4000

4300

1900

2700

2700

6370

4500

7350

7150

8500

7500

7650

Max. fuel (+ payload)

4698

5076

4158

3672

2602

7046

8834

8089

9000

7800

-

Ferry range

9800

8800

10300

Design Parameters:
W/SCLmax

2160.21

2227.23

1726.69

1962.27

2211.48

2269.21

2150.33

2445.04

2529.97

2865.71

2857.63

W/SCLtoST

2678.25

2702.77

2071.39

2423.85

2590.29

3146.34

2906.75

4224.13

4242.69

4144.91

3912.54

Fuel/pax/nm (kg)

0.0529

0.0529

0.0553

0.0443

0.0465

0.0460

0.0470

0.0502

0.0472

0.0554

0.0460

Seats x Range (seats.nm)

1064000

937400

235600

405000

502200

1866410

1507500

2227050

2395250

2975000

3300000