CIVIL JET AIRCRAFT DESIGN

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Data A : Aircraft Data File

Table 7 : Russian Manufacturers

Notes

Manufacturer

ILYUSHIN

ILYUSHIN

ILYUSHIN

ILYUSHIN

TUPOLEV

TUPOLEV

TUPOLEV

TUPOLEV

Type

Tu-204

Model

Il-62M/MK

Il-86

Il-96-300

Il-96M

Tu-134

Tu-154M

-200

Tu-334

Initial service date

1974

1980

1994

1996

1972

1997

200?

In service (ordered)

Asia

2

-

-

-

1

1

2

-

Europe

4

3

-

-

11

60

-

-

Mid. East; Africa

109(2)

92

9 (9)

(23)

353

521

8

-

N. & S. America

9

-

-

-

-

6

-

-

Total aircraft

124(2)

95

9(9)

(23)

365

580

10

-

Engine Manufacturer

Soloviev

Kuznetsov

Soloviev

P&W

Soloviev

Aviadvigatel

Soloviev

Lotarev

Model / Type

D-30KU

KKBM NK-86

PS-90A

2337

D-30 Srs II

D-30KU-154-II

PS-90A

D-436T1

No. of engines

4

4

4

4

2

3

2

2

Static Thrust (kN)

107.9

127.5

156.9

164.6

66.7

104.0

157.0

73.6

Operational Items:

Accomodation:

Max. seats (single class)

174

350

300

375

84

180

214

102

Two class seating

140

234

335

68

154

196

85

Three class seating

-

-

235

312

-

-

190

-

No. abreast

6

9

9

9

4

6

6

6

Hold volume (m3)

48.00

71.52

115.90

143.04

14.5

43.00

26.40

Volume per passenger

0.28

0.20

0.39

0.38

0.17

0.24

0.12

0.00

Mass (Weight) (kg):

Ramp

47200

100450

111750

46700

Max. take-off

165000

208000

216000

270000

47000

100000

110750

46500

Max. landing

105000

175000

175000

175158

43000

80000

89500

43404

Zero-fuel

94600

157000

190423

37250

74000

84200

41050

Max. payload

23000

42000

40000

58000

8200

18000

25200

11000

Max. fuel payload

9160

0

17290

3550

11660

18999.6

6910

Design payload

13300

22230

22325

29640

6460

14630

18620

9690

Design fuel load

80100

185770

76675

107960

11490

30070

33130

6760

Operational empty

71600

117000

132400

29050

55300

59000

30050

Weight Ratios:

Ops empty/Max. T/O

0.434

0.542

0.490

0.618

0.553

0.533

0.646

Max. payload/Max. T/O

0.139

0.202

0.185

0.215

0.174

0.180

0.228

0.237

Max. fuel/Max. T/O

0.504

0.433

0.550

0.440

0.303

0.326

0.292

0.203

Max. landing/Max. T/O

0.636

0.841

0.810

0.649

0.915

0.800

0.808

0.933

Fuel (litres):

Standard

105300

114000

150387

150387

18000

41300

40938

11925

Optional

47000

Manufacturer

ILYUSHIN

ILYUSHIN

ILYUSHIN

ILYUSHIN

TUPOLEV

TUPOLEV

TUPOLEV

TUPOLEV

Type

Tu-204

Model

Il-62M/MK

Il-86

Il-96-300

Il-96M

Tu-134

Tu-154M

-200

Tu-334

DIMENSIONS

Fuselage:

Length (m)

49.00

56.10

51.15

60.50

33.20

43.50

46.70

25.90

Height (m)

4.30

6.08

6.08

6.08

2.90

3.80

3.80

4.05

Width (m)

4.30

6.08

6.08

6.08

2.90

3.80

4.10

4.05

Finess Ratio

11.40

9.23

8.41

9.95

11.45

11.45

11.39

6.40

Wing:

Area (m)

279.55

320.00

391.60

391.60

127.30

201.45

182.40

83.23

Span (m)

43.20

48.06

55.57

55.57

29.00

37.55

40.30

28.00

MAC (m)

7.47

7.69

8.04

8.04

5.13

6.25

5.40

3.53

Aspect Ratio

6.68

7.22

7.89

7.89

6.61

7.00

8.90

9.42

Taper Ratio

0.254

0.265

0.279

0.279

0.255

0.267

0.228

0.228

Average (t/c) %

1/4 Chord Sweep ()

32.50

35.00

30.00

30.00

35.00

35.00

28.00

24.00

High Lift Devices:

Trailing Edge Flaps Type

S2

S2

S2

S2

S2

S3

S2

S2

Flap Span/Wing Span

0.720

0.740

0.790

0.790

0.605

0.750

0.770

0.670

Area (m2)

43.48

22.5

Leading Edge Flaps Type

none

slats

slats

slats

none

slats

slats

slats

Area (m)

-

Vertical Tail:

Area (m)

35.60

57.10

61.00

56.20

21.25

31.70

34.20

23.50

Height (m)

6.05

8.80

9.40

8.00

5.25

5.60

7.70

4.65

Aspect Ratio

1.03

1.36

1.45

1.14

1.30

0.99

1.73

0.92

Taper Ratio

0.540

0.330

0.280

0.400

0.560

0.650

0.340

0.830

1/4 Chord Sweep ()

40.00

44.00

45.00

45.00

40.00

45.00

36.00

37.50

Tail Arm (m)

16.60

24.90

23.55

25.90

13.20

14.40

21.80

10.20

Sv/S

0.127

0.178

0.156

0.144

0.167

0.157

0.188

0.282

SvLv/Sb

0.049

0.092

0.066

0.067

0.076

0.060

0.101

0.103

Horizontal Tail:

Area (m2)

50.50

90.90

96.50

96.50

30.68

42.20

44.60

22.30

Span (m)

12.23

20.57

20.57

20.57

11.80

13.40

15.10

10.70

Aspect Ratio

2.96

4.65

4.38

4.38

4.54

4.25

5.11

5.13

Taper Ratio

0.360

0.410

0.290

0.290

0.396

0.480

0.300

0.360

1/4 Chord Sweep ()

35.00

36.00

37.50

37.50

35.00

40.00

34.00

27.00

Tail Arm (m)

22.50

25.30

24.25

26.50

14.90

18.30

21.30

12.80

Sh/S

0.181

0.284

0.246

0.246

0.241

0.209

0.245

0.268

ShLh/Sc

0.544

0.935

0.743

0.812

0.700

0.613

0.964

0.972

Undercarriage:

Track (m)

6.80

11.15

10.40

10.40

10.50

11.50

7.82

4.70

Wheelbase (m)

24.49

21.34

20.07

27.35

15.80

18.92

17.00

11.25

Turning radius (m)

36.00

No. of wheels (nose;main)

2;8

2;8

2;8

2;8

2;8

2;12

2;8

2;4

Main Wheel diameter (m)

1.450

1.300

1.300

1.300

0.930

0.930

Main Wheel width (m)

0.450

0.480

0.480

0.480

0.305

0.305

Nacelle:

Length (m)

6.15

7.00

5.90

6.00

5.75

7.10

6.00

5.00

Max. width (m)

2.35

2.00

2.20

2.60

1.55

2.20

2.60

1.90

Spanwise location

0.41/0..69

0.37/0.58

0.37/0.58

-

-

0.330

-

Manufacturer ILYUSHIN ILYUSHIN ILYUSHIN ILYUSHIN TUPOLEV TUPOLEV TUPOLEV TUPOLEV
Type Tu-204
Model Il-62M/MK Il-86 Il-96-300 Il-96M Tu-134 Tu-154M -200 Tu-334
PERFORMANCE
Loadings:
Max Power Load (kg/kN) 382.30 407.84 344.17 410.09 352.32 320.51 352.71 316.11
Max Wing Load (kg/m2) 590.23 650.00 551.58 689.48 369.21 496.40 607.18 558.72
Thrust/Weight Ratio 0.267 0.250 0.296 0.249 0.289 0.318 0.289 0.322
Take-off (m):
ISA sea level 3300 2600 2760 3350 2400 2100 2500
ISA +20C SL. 2420
ISA 5,000ft 2500
ISA +20C 5,000ft 3240
Landing (m):
ISA sea level. 2500 2300 1980 2250 2200 2060 2130
ISA +20C SL. 2210
ISA 5,000ft 2330
ISA +20C 5,000ft 2600
Speeds (kt/Mach):
V2 145 138 151
Vapp 129 140 140 121
Vno/Mmo 486 0.86 310/M0.90 314/
Vne/Mme 340/
CLmax (T/O) 2.45 2.27 2.32
CLmax (L/D @ MLM) 2.31 2.85 2.33 2.77
Max cruise :
Speed (kt) 486 512 486 469 458 514 458 448
Altitude (ft) 33000 9000 10100 9000 32800 31000 40000
Fuel consumption (kg/h) 4600 3270
Long range cruise:
Speed (kt) 442 486 459 459 432 459
Altitude (ft) 39400 11000 12100 12000 36100 36000 36500
Fuel consumption (kg/h) 3650
Range (nm):
Max payload 4160 1944 4050 1020 2019 1565 1080
Design range 4860 6195 1550 2805
Max fuel (+ payload) 4963 2480 5940 3564 2079 1566
Ferry range
Design Parameters:
W/SCLmax 2508 2234 2320 1755.10
W/aCLtoST 3583 3406 2984 2102.53
Fuel/pax/nm (kg) 0.0520 0.1090 0.0696
Seats x Range (seats.nm) 2075325 105400 431970