 Data A : Aircraft Data File
 Table 6 : Douglas, Boeing (Douglas Products Division) &
Lockheed Aircraft
 Notes
Manufacturer |
McDON. |
DOUG. |
DOUG. |
McDON. |
McDON. |
McDON. |
LOCKHD |
Type |
/DOUG. |
|
|
/DOUG. |
/DOUG. |
/DOUG. |
|
Model |
MD-90-30 |
DC10-10 |
DC10-30 |
MD-11 |
MD-12LR |
MD-12HC |
L1011-100 |
Initial
service date |
1995 |
1971 |
1973 |
1990 |
- |
- |
1973 |
In
service (ordered) |
|
|
|
|
|
|
|
Africa |
2 |
---> |
5 |
- |
- |
- |
1 |
Middle
East/Asia/Pacific |
52(43) |
---> |
32 |
46(3) |
- |
- |
27 |
Europe & CIS |
10 |
---> |
51 |
55(10) |
- |
- |
17 |
North & South
America |
21 |
---> |
251 |
77(3) |
- |
- |
111 |
Total aircraft |
85(43) |
---> |
339 |
178(16) |
- |
- |
156 |
Engine
Manufacturer |
IAE |
GE |
GE |
GE |
R-R/GE/PW |
R-R/GE/PW |
R-R |
Model / Type |
V2525-D5 |
CF6-50C2B |
CF6-50C2B |
CF6-80C2 D1F |
Options |
Options |
RB211-22B |
No. of engines |
2 |
3 |
3 |
3 |
4 |
4 |
3 |
Static Thrust (kN) |
111.2 |
178.0 |
236.0 |
274.0 |
284.7 |
284.7 |
187 |
Operational
Items: |
|
|
|
|
|
|
|
Accomodation: |
|
|
|
|
|
|
|
Max. seats (single
class) |
182 |
380 |
380 |
405 |
660 |
660 |
400 |
Two class seating |
153 |
277 |
277 |
323 |
|
|
304 |
Three class seating |
- |
231 |
231 |
293 |
481 |
511 |
- |
No. abreast |
5 |
9 |
9 |
10 |
11/8 |
11/8 |
10 |
Hold volume (m3) |
38.03 |
132.20 |
132.20 |
194.00 |
126.40 |
126.40 |
110.40 |
Volume per
passenger |
0.21 |
0.35 |
0.35 |
0.48 |
0.19 |
0.19 |
0.276 |
Mass (Weight) (kg): |
|
|
|
|
|
|
|
Ramp |
71215 |
192218 |
265000 |
285081 |
|
|
212281 |
Max. take-off |
70760 |
190854 |
263636 |
283720 |
430846 |
430846 |
211374 |
Max. landing |
64410 |
164854 |
182798 |
207744 |
291468 |
291468 |
166922 |
Zero-fuel |
58965 |
151956 |
166922 |
195043 |
273308 |
273308 |
145150 |
Max. payload |
17350 |
48330 |
48330 |
55566 |
85489 |
78452 |
33355 |
Max. fuel
payload |
13659.4 |
32000 |
32000 |
30343 |
|
|
19138 |
Design payload |
14535 |
26315 |
26315 |
30685 |
45695 |
48545 |
28880 |
Design fuel
load |
16810 |
53195 |
115957 |
118954 |
197332 |
187445 |
70699 |
Operational
empty |
39415 |
111344 |
121364 |
134081 |
187819 |
194856 |
111795 |
Weight Ratios: |
|
|
|
|
|
|
|
Ops empty/Max.
T/O |
0.557 |
0.583 |
0.460 |
0.473 |
0.436 |
0.452 |
0.529 |
Max.
payload/Max. T/O |
0.245 |
0.253 |
0.183 |
0.196 |
|
|
0.158 |
Max. fuel/Max.
T/O |
0.247 |
0.572 |
0.414 |
0.424 |
|
|
0.374 |
Max.
landing/Max. T/O |
0.910 |
0.864 |
0.693 |
0.732 |
0.677 |
0.677 |
0.790 |
Fuel (litres): |
|
|
|
|
|
|
|
Standard |
22107 |
138165 |
138165 |
152108 |
|
|
100000 |
Optional |
|
|
153434 |
161226 |
|
|
|
|
|
|
|
|
|
|
|
| Manufacturer |
McDON. |
DOUG. |
DOUG. |
McDON. |
McDON. |
McDON. |
LOCKHD |
| Type |
/DOUG. |
|
|
/DOUG. |
/DOUG. |
/DOUG. |
|
| Model |
MD-90-30 |
DC10-10 |
DC10-30 |
MD-11 |
MD-12LR |
MD-12HC |
L1011-100 |
| DIMENSIONS |
|
|
|
|
|
|
|
| Fuselage: |
|
|
|
|
|
|
|
| Length (m) |
43.00 |
51.97 |
51.97 |
58.65 |
58.82 |
58.82 |
54.20 |
| Height (m) |
3.61 |
6.02 |
6.02 |
6.02 |
8.51 |
8.51 |
6.06 |
| Width (m) |
3.61 |
6.02 |
6.02 |
6.02 |
7.47 |
7.47 |
6.06 |
| Finess Ratio |
11.91 |
8.63 |
8.63 |
9.74 |
7.87 |
7.87 |
8.94 |
| Wing: |
|
|
|
|
|
|
|
| Area (m²) |
112.30 |
367.70 |
367.70 |
338.90 |
543.00 |
543.00 |
321.50 |
| Span (m) |
32.87 |
50.40 |
50.40 |
51.77 |
64.92 |
64.92 |
47.35 |
| MAC (m) |
4.08 |
8.59 |
8.59 |
7.68 |
9.80 |
9.80 |
7.90 |
| Aspect Ratio |
9.62 |
6.91 |
6.91 |
7.91 |
7.76 |
7.76 |
6.97 |
| Taper Ratio |
0.195 |
0.22 |
0.22 |
0.239 |
0.215 |
0.215 |
0.259 |
| Average (t/c) % |
11.00 |
11.00 |
11.00 |
9.350 |
|
|
10.700 |
| 1/4 Chord Sweep (º) |
24.50 |
35.00 |
35.00 |
35.00 |
35.00 |
35.00 |
35.00 |
| High Lift Devices: |
|
|
|
|
|
|
|
| Trailing Edge Flaps Type |
S2 |
S2 |
S2 |
S2 |
S2 |
S2 |
S2 |
| Flap Span/Wing Span |
0.630 |
0.680 |
0.680 |
0.700 |
|
|
0.77 |
| Area (m2) |
|
62.1 |
62.1 |
|
|
|
49.8 |
| Leading Edge Flaps Type |
slats |
slats |
slats |
slats |
slats |
slats |
slats |
| Area (m2) |
|
43.84 |
43.84 |
|
|
|
33.45 |
| Vertical Tail: |
|
|
|
|
|
|
|
| Area (m²) |
21.40 |
56.21 |
56.21 |
56.20 |
96.10 |
96.10 |
51.10 |
| Height (m) |
4.70 |
11.16 |
11.16 |
11.16 |
12.90 |
12.90 |
9.90 |
| Aspect Ratio |
1.03 |
2.22 |
2.22 |
2.22 |
1.73 |
1.73 |
1.92 |
| Taper Ratio |
0.770 |
0.475 |
0.475 |
0.369 |
0.345 |
0.345 |
0.290 |
| 1/4 Chord Sweep (º) |
43.00 |
40.00 |
40.00 |
40.00 |
40.00 |
40.00 |
35.00 |
| Tail Arm (m) |
15.60 |
20.65 |
20.65 |
20.92 |
24.50 |
24.50 |
20.60 |
| Sv/S |
0.191 |
0.153 |
0.153 |
0.166 |
0.177 |
0.177 |
0.159 |
| SvLv/Sb |
0.090 |
0.063 |
0.063 |
0.067 |
0.067 |
0.067 |
0.069 |
| Horizontal Tail: |
|
|
|
|
|
|
|
| Area (m2) |
33.00 |
124.30 |
124.30 |
85.50 |
113.80 |
113.80 |
119.10 |
| Span (m) |
12.24 |
21.69 |
21.69 |
18.03 |
22.55 |
22.55 |
21.90 |
| Aspect Ratio |
4.54 |
3.78 |
3.78 |
3.80 |
4.47 |
4.47 |
4.03 |
| Taper Ratio |
0.360 |
0.344 |
0.344 |
0.383 |
0.326 |
0.326 |
0.310 |
| 1/4 Chord Sweep (º) |
30.00 |
35.00 |
35.00 |
35.00 |
35.00 |
35.00 |
35.00 |
| Tail Arm (m) |
18.60 |
19.80 |
19.80 |
20.92 |
24.67 |
24.67 |
17.70 |
| Sh/S |
0.294 |
0.338 |
0.338 |
0.252 |
0.210 |
0.210 |
0.370 |
| ShLh/Sc |
1.340 |
0.780 |
0.780 |
0.687 |
0.528 |
0.528 |
0.830 |
| Undercarriage: |
|
|
|
|
|
|
|
| Track (m) |
5.09 |
10.67 |
10.67 |
10.60 |
11.59 |
11.59 |
10.90 |
| Wheelbase (m) |
23.53 |
22.05 |
22.05 |
24.60 |
26.84 |
26.84 |
21.33 |
| Turning radius (m) |
39.00 |
39.00 |
41.00 |
|
|
43.00 |
| No. of wheels (nose;main) |
2;4 |
2;8 |
2;10 |
2;10 |
2;16 |
2;16 |
2;8 |
| Main Wheel diameter (m) |
|
|
|
|
|
|
| Main Wheel width (m) |
|
|
|
|
|
|
| Nacelle: |
|
|
|
|
|
|
|
| Length (m) |
5.75 |
6.50 |
6.50 |
6.50 |
7.27 |
7.27 |
6.3 |
| Max. width (m) |
1.55 |
2.70 |
2.70 |
2.70 |
3.10 |
3.10 |
2.75 |
| Spanwise location |
- |
0.343 |
0.343 |
0.308 |
0.370/0.630 |
0.370/0.630 |
0.436 |
|
|
|
|
|
|
|
|
| Manufacturer |
McDON. |
DOUG. |
DOUG. |
McDON. |
McDON. |
McDON. |
LOCKHD |
| Type |
/DOUG. |
|
|
/DOUG. |
/DOUG. |
/DOUG. |
|
| Model |
MD-90-30 |
DC10-10 |
DC10-30 |
MD-11 |
MD-12LR |
MD-12HC |
L 1011 |
| PERFORMANCE |
| Loadings: |
| Max Power Load (kg/kN) |
318.14 |
357.40 |
372.37 |
345.16 |
378.33 |
378.33 |
376.78 |
| Max Wing Load (kg/m²) |
630.10 |
519.05 |
716.99 |
837.18 |
793.45 |
793.45 |
657.46 |
| Thrust/Weight Ratio |
0.320 |
0.285 |
0.274 |
0.295 |
0.269 |
0.269 |
0.271 |
| Take-off
(m): |
| ISA sea level |
2135 |
2625 |
2996 |
2926 |
3080 |
3080 |
3292 |
| ISA +20ºC SL. |
|
3816 |
3194 |
3078 |
|
|
3475 |
| ISA 5,000ft |
|
4154 |
4340 |
3633 |
|
|
4115 |
| ISA +20ºC 5,000ft |
|
4135 |
4255 |
4031 |
|
|
3719 |
| Landing
(m): |
| ISA sea level. |
1564 |
1720 |
1820 |
1966 |
2577 |
2577 |
1768 |
| ISA +20ºC SL. |
|
1720 |
1820 |
1966 |
|
|
1768 |
| ISA 5,000ft |
|
2012 |
2063 |
2234 |
|
|
1996 |
| ISA +20ºC 5,000ft |
|
2012 |
2063 |
2234 |
|
|
1996 |
| Speeds
(kt/Mach): |
| V2 |
|
157 |
184 |
177 |
|
|
159 |
| Vapp |
|
140 |
147 |
148 |
|
|
143 |
| Vno/Mmo |
/M0.76 |
356/M0.88 |
356/M0.88 |
365/M0.87 |
/M0.85 |
/M0.85 |
375/M0.90 |
| Vne/Mme |
|
400/M0.95 |
400/M0.95 |
400/M0.92 |
|
|
435/M0.95 |
| CLmax (T/O) |
|
1.84 |
1.85 |
2.33 |
|
|
2.27 |
| CLmax (L/D @ MLM) |
|
2.34 |
2.35 |
2.86 |
|
|
2.60 |
| Max
cruise : |
| Speed (kt) |
|
475 |
530 |
M0.87 |
|
|
512 |
| Altitude (ft) |
|
31000 |
31000 |
31000 |
|
|
33000 |
| Fuel consumption (kg/h) |
|
9445 |
9743 |
8970 |
|
|
7938 |
| Long
range cruise: |
| Speed (kt) |
437 |
490 |
490 |
M0.81 |
|
|
483 |
| Altitude (ft) |
35000 |
31000 |
31000 |
31000 |
|
|
33000 |
| Fuel consumption (kg/h) |
|
6920 |
7313 |
7060 |
|
|
6895 |
| Range
(nm): |
| Max payload |
|
3300 |
4000 |
5994 |
8000 |
7200 |
|
| Design range |
2275 |
4000 |
5373 |
6787 |
|
|
3455 |
| Max fuel (+ payload) |
2267 |
5750 |
6400 |
8234 |
|
|
4685 |
| Ferry range |
|
|
|
|
|
|
|
| Design
Parameters: |
| W/SCLmax |
|
2176 |
2989 |
2869 |
|
|
2483 |
| W/aCLtoST |
|
2907 |
4160 |
3701 |
|
|
3497 |
| Fuel/pax/nm (kg) |
0.0483 |
0.0480 |
0.0779 |
0.0543 |
|
|
0.0673 |
| Seats x Range (seats.nm) |
348075 |
1108000 |
1488321 |
2192201 |
|
|
1050320 |
|
