 Data A : Aircraft Data File
 Table 4 : Boeing Aircraft
 Notes
| Manufacturer |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
| Type |
777- |
777- |
777- |
777- |
777- |
777- |
777- |
| Model |
100X1 |
100X2 |
200 |
200IGW |
200X1 |
200X2 |
300 |
| Initial
service date |
2000 |
2000 |
1995 |
1995 |
2000 |
2000 |
1998 |
| In service (ordered) |
|
|
|
|
|
|
|
| Africa |
- |
- |
---> |
3(4) |
- |
- |
- |
| Middle East/Asia/Pacific |
- |
- |
---> |
90(74) |
- |
- |
11(37) |
| Europe & CIS |
- |
- |
---> |
26(39) |
- |
- |
- |
| North & South America |
- |
- |
---> |
38(78) |
- |
- |
- |
| Total aircraft |
- |
- |
---> |
157(195) |
- |
- |
11(37) |
| Engine Manufacturer |
R-R/GE/PW |
R-R/GE/PW |
R-R/GE/PW |
R-R/GE/PW |
R-R/GE/PW |
R-R/GE/PW |
R-R |
| Model / Type |
Options |
Options |
Options |
Options |
Options |
Options |
Trent 895 |
| No. of engines |
2 |
2 |
2 |
2 |
2 |
2 |
2 |
| Static Thrust (kN) |
400.0 |
400.0 |
342.5 |
373.7 |
413.8 |
436.0 |
423.0 |
| Operational Items: |
|
|
|
|
|
|
|
| Accomodation: |
|
|
|
|
|
|
|
| Max. seats (single class) |
330 |
330 |
440 |
440 |
440 |
440 |
550 |
| Two class seating |
|
|
375 |
375 |
375 |
375 |
479 |
| Three class seating |
271 |
250 |
310 |
310 |
298 |
298 |
394 |
| No. abreast |
|
|
10 |
10 |
10 |
10 |
10 |
| Hold volume (m3) |
|
|
160.00 |
160.00 |
160.00 |
160.00 |
200.50 |
| Volume per passenger |
|
|
0.36 |
0.36 |
0.36 |
0.36 |
0.36 |
| Mass (Weight) (kg): |
|
|
|
|
|
|
|
| Ramp |
|
|
243577 |
287804 |
|
|
299600 |
| Max. take-off |
286621 |
299320 |
242670 |
286897 |
299320 |
312925 |
299370 |
| Max. landing |
|
|
201850 |
208652 |
|
|
237685 |
| Zero-fuel |
|
|
190510 |
195045 |
|
|
224530 |
| Max. payload |
|
|
54635 |
56925 |
|
|
68570 |
| Max. fuel payload |
|
|
|
|
|
|
|
| Design payload |
25745 |
23750 |
35625 |
29450 |
|
|
|
| Design fuel load |
|
|
71170 |
119327 |
|
|
|
| Operational empty |
|
|
135875 |
138120 |
|
|
155960 |
| Weight Ratios: |
|
|
|
|
|
|
|
| Ops empty/Max. T/O |
|
|
0.560 |
0.481 |
|
|
0.521 |
| Max. payload/Max. T/O |
|
|
0.225 |
0.198 |
|
|
0.229 |
| Max. fuel/Max. T/O |
|
|
0.382 |
0.466 |
|
|
0.452 |
| Max. landing/Max. T/O |
|
|
0.832 |
0.727 |
|
|
0.794 |
| Fuel (litres): |
|
|
|
|
|
|
|
| Standard |
|
|
117348 |
169208 |
174735 |
174735 |
171170 |
| Optional |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
| Manufacturer |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
| Type |
777- |
777- |
777- |
777- |
777- |
777- |
777- |
| Model |
100X1 |
100X2 |
200 |
200IGW |
200X1 |
200X2 |
300 |
| DIMENSIONS |
|
|
|
|
|
|
|
| Fuselage: |
|
|
|
|
|
|
|
| Length (m) |
56.40 |
59.60 |
62.78 |
62.78 |
62.78 |
62.78 |
72.88 |
| Height (m) |
6.20 |
6.20 |
6.20 |
6.20 |
6.20 |
6.20 |
6.20 |
| Width (m) |
6.20 |
6.20 |
6.20 |
6.20 |
6.20 |
6.20 |
6.20 |
| Finess Ratio |
9.10 |
9.61 |
10.13 |
10.13 |
10.13 |
10.13 |
11.75 |
| Wing: |
|
|
|
|
|
|
|
| Area (m²) |
427.80 |
427.80 |
427.80 |
427.80 |
427.80 |
427.80 |
427.80 |
| Span (m) |
60.90 |
60.90 |
60.90 |
60.90 |
60.90 |
60.90 |
60.90 |
| MAC (m) |
8.75 |
8.75 |
8.75 |
8.75 |
8.75 |
8.75 |
8.75 |
| Aspect Ratio |
8.67 |
8.67 |
8.67 |
8.67 |
8.67 |
8.67 |
8.67 |
| Taper Ratio |
0.149 |
0.149 |
0.149 |
0.149 |
0.149 |
0.149 |
0.149 |
| Average (t/c) % |
|
|
|
|
|
|
|
| 1/4 Chord Sweep (º) |
31.60 |
31.60 |
31.60 |
31.60 |
31.60 |
31.60 |
31.60 |
| High Lift Devices: |
|
|
|
|
|
|
|
| Trailing Edge Flaps Type |
S2/S1 |
S2/S1 |
S2/S1 |
S2/S1 |
S2/S1 |
S2/S1 |
S2/S1 |
| Flap Span/Wing Span |
0.758 |
0.758 |
0.758 |
0.758 |
1.758 |
2.758 |
2.758 |
| Area (m²) |
|
|
|
|
|
|
|
| Leading Edge Flaps Type |
slats |
slats |
slats |
slats |
slats |
slats |
slats |
| Area (m²) |
|
|
|
|
|
|
|
| Vertical Tail: |
|
|
|
|
|
|
|
| Area (m²) |
53.23 |
53.23 |
53.23 |
53.23 |
53.23 |
53.23 |
53.23 |
| Height (m) |
9.24 |
9.24 |
9.24 |
9.24 |
9.24 |
9.24 |
9.24 |
| Aspect Ratio |
1.60 |
1.60 |
1.60 |
1.60 |
1.60 |
1.60 |
1.60 |
| Taper Ratio |
0.290 |
0.290 |
0.290 |
0.290 |
0.290 |
0.290 |
0.290 |
| 1/4 Chord Sweep (º) |
46.00 |
46.00 |
46.00 |
46.00 |
46.00 |
46.00 |
46.00 |
| Tail Arm (m) |
23.41 |
25.01 |
26.60 |
26.60 |
26.60 |
26.60 |
31.65 |
| Sv/S |
0.124 |
0.124 |
0.124 |
0.124 |
0.124 |
0.124 |
0.124 |
| SvLv/Sb |
0.048 |
0.051 |
0.054 |
0.054 |
0.054 |
0.054 |
0.065 |
| Horizontal Tail: |
|
|
|
|
|
|
|
| Area (m²) |
101.26 |
101.26 |
101.26 |
101.26 |
101.26 |
101.26 |
101.26 |
| Span (m) |
21.35 |
21.35 |
21.35 |
21.35 |
21.35 |
21.35 |
21.35 |
| Aspect Ratio |
4.50 |
4.50 |
4.50 |
4.50 |
4.50 |
4.50 |
4.50 |
| Taper Ratio |
0.300 |
0.300 |
0.300 |
0.300 |
0.300 |
0.300 |
0.300 |
| 1/4 Chord Sweep (º) |
35.00 |
35.00 |
35.00 |
35.00 |
35.00 |
35.00 |
35.00 |
| Tail Arm (m) |
24.71 |
26.31 |
27.90 |
27.90 |
27.90 |
27.90 |
32.95 |
| Sh/S |
0.237 |
0.237 |
0.237 |
0.237 |
0.237 |
0.237 |
0.237 |
| ShLh/Sc |
0.668 |
0.712 |
0.755 |
0.755 |
0.755 |
0.755 |
0.891 |
| Undercarriage: |
|
|
|
|
|
|
|
| Track (m) |
11.00 |
11.00 |
11.00 |
11.00 |
11.00 |
11.00 |
11.00 |
| Wheelbase (m) |
25.80 |
25.80 |
25.80 |
25.80 |
25.80 |
25.80 |
25.80 |
| Turning radius (m) |
41.00 |
41.00 |
41.00 |
41.00 |
41.00 |
41.00 |
41.00 |
| No. of wheels (nose;main) |
2;12 |
2;12 |
2;12 |
2;12 |
2;12 |
2;12 |
2;12 |
| Main Wheel diameter (m) |
1.118 |
1.118 |
1.118 |
1.118 |
1.118 |
1.118 |
1.118 |
| Main Wheel width (m) |
0.457 |
0.457 |
0.457 |
0.457 |
0.457 |
0.457 |
0.457 |
| Nacelle: |
|
|
|
|
|
|
|
| Length (m) |
7.30 |
7.30 |
7.30 |
7.30 |
7.30 |
7.30 |
7.30 |
| Max. width (m) |
3.20 |
3.20 |
3.20 |
3.20 |
3.20 |
3.20 |
3.20 |
| Spanwise location |
0.326 |
0.326 |
0.326 |
0.326 |
0.326 |
0.326 |
0.326 |
|
|
|
|
|
|
|
|
| Manufacturer |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
BOEING |
| Type |
777- |
777- |
777- |
777- |
777- |
777- |
777- |
| Model |
100X1 |
100X2 |
200 |
200IGW |
200X1 |
200X2 |
300 |
| PERFORMANCE |
|
|
|
|
|
|
|
| Loadings: |
| Max Power Load (kg/kN) |
358.28 |
374.15 |
354.24 |
383.90 |
361.67 |
358.86 |
353.87 |
| Max Wing Load (kg/m2) |
669.99 |
699.67 |
567.25 |
670.63 |
699.67 |
731.47 |
699.79 |
| Thrust/Weight Ratio |
0.2845 |
0.2724 |
0.2878 |
0.2655 |
0.2818 |
0.2841 |
0.2881 |
| Take-off
(m): |
| ISA sea level |
|
|
2135 |
|
|
|
|
| ISA +20ºC SL. |
|
|
2440 |
3050 |
|
|
3540 |
| ISA 5,000ft |
|
|
|
|
|
|
|
| ISA +20ºC 5,000ft |
|
|
|
|
|
|
|
| Landing
(m): |
| ISA sea level. |
|
|
1585 |
1620 |
|
|
1860 |
| ISA +20ºC SL. |
|
|
1585 |
1620 |
|
|
1860 |
| ISA 5,000ft |
|
|
1875 |
1940 |
|
|
|
| ISA +20ºC 5,000ft |
|
|
1875 |
1940 |
|
|
|
| Speeds
(kt/Mach): |
| V2 |
|
|
|
|
|
|
|
| Vapp |
|
|
138 |
140 |
|
|
|
| Vno/Mmo |
|
|
330/M0.87 |
330/M0.87 |
|
|
330/M0.87 |
| Vne/Mme |
|
|
|
|
|
|
|
| CLmax (T/O) |
|
|
|
|
|
|
|
| CLmax (L/D @ MLM) |
|
|
2.53 |
2.55 |
|
|
|
| Max
cruise : |
| Speed (kt) |
|
|
499 |
499 |
|
|
|
| Altitude (ft) |
|
|
39000 |
39000 |
|
|
|
| Fuel consumption (kg/h) |
|
|
|
|
|
|
|
| Long
range cruise: |
| Speed (kt) |
|
|
476 |
476 |
|
|
|
| Altitude (ft) |
|
|
39000 |
39000 |
|
|
|
| Fuel consumption (kg/h) |
|
|
|
|
|
|
|
| Range
(nm): |
| Max payload |
|
|
|
|
|
|
|
| Design range |
7625 |
8420 |
4820 |
7380 |
7455 |
7970 |
5604 |
| Max fuel (+ payload) |
|
|
|
|
|
|
|
| Ferry range |
|
|
|
|
|
|
|
| Design
Parameters: |
| W/SCLmax |
|
|
|
|
|
|
|
| W/aCLtoST |
|
|
|
|
|
|
|
| Fuel/pax/nm (kg) |
|
|
|
|
|
|
|
| Seats x Range (seats.nm) |
|
|
|
|
|
|
|
|
