| Manufacturer |
Tupolev |
Boeing |
| Family |
|
737 MAX |
| Model |
|
737 MAX 8 |
| Description |
The Tupolev Tu-104 (NATO reporting name: Camel) is a medium-range, narrow-body, twin turbojet-powered Soviet airliner. |
|
| EASA TCDSN |
|
EASA.IM.A.120.6 |
| First Flight |
1955-06-17 |
|
| Entry Into service |
1956-09-15 |
|
| Production End |
1960-01-01 |
|
| Service End |
1981-01-01 |
|
| Designer |
Andrei Tupolev |
|
| Type |
Narrow-body jetliner |
|
| Length (m) |
40.06 |
39.52 |
| Height (m) |
11.9 |
12.45 |
| Line Logo |
|
737-8_line_drawing.jpg |
| White Logo |
|
737-8_white.jpg |
| Cockpit Crew |
7 |
2 |
| Max Seating |
115 |
189 |
| Two Class Typical Seating |
|
178 |
| Cargo Volume (m³) |
|
43.6 |
| Max Speed (km/h) |
950 |
|
| Max Ceiling (m) |
12000 |
12497 |
| Rate of Climb (m/s) |
10 |
|
| Capacity Description |
50–115 passengers |
|
| Number Built |
201 |
|
| Powerplant Description |
2 × Mikulin AM-3M-500 turbojet engines |
|
| Primary Users |
Aeroflot, ČSA |
|
| Status |
Retired |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Tupolev_Tu-104 |
en.wikipedia.org/wiki/Boeing_737_MAX |
| Flat Wing Span (m) |
34.54 |
35.92 |
| Flat Wing Area (m²) |
183 |
|
| Wing Sweepback (°) |
|
25 |
| Fuselage Diameter (m) |
|
3.76 |
| Aircraft Engine |
|
LEAP-1B28/28B1/28B2/28B3 |
| Number of Engines |
2 |
2 |