 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 (m²) |
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 (º) |
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 (m²) |
|
|
|
|
- |
|
|
|
Vertical Tail: |
|
|
|
|
|
|
|
|
Area (m²) |
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
(º) |
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 (º) |
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 +20ºC SL. |
|
|
|
|
|
2420 |
|
|
| ISA 5,000ft |
|
|
|
|
|
2500 |
|
|
| ISA +20ºC 5,000ft |
|
|
|
|
|
3240 |
|
|
| Landing
(m): |
| ISA sea level. |
2500 |
2300 |
1980 |
2250 |
2200 |
2060 |
2130 |
|
| ISA +20ºC SL. |
|
|
|
|
|
2210 |
|
|
| ISA 5,000ft |
|
|
|
|
|
2330 |
|
|
| ISA +20ºC 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 |
|
|
|
