| Manufacturer |
Boeing |
Ilyushin |
| Description |
The Boeing 747SP (for Special Performance) is a shortened version of the Boeing 747 wide-body airliner, designed for a longer range. |
The Ilyushin Il-106 () was a proposed 1990s Russian heavy military transport to replace the Il-76. |
| ICAO Code |
B74S |
|
| EASA TCDSN |
EASA.IM.A.196 |
|
| First Flight |
1975-07-04 |
|
| Entry Into service |
1976-04-25 |
|
| Production End |
1982-01-01 |
|
| Designer |
|
Ilyushin |
| Type |
Wide-body jet airliner |
|
| Length (m) |
55.85 |
57.6 |
| Height (m) |
20.06 |
19.93 |
| Cockpit Crew |
3 |
|
| Max Seating |
331 |
|
| Cruise Speed (km/h) |
|
850 |
| Max Ceiling (m) |
13746.48 |
14000 |
| Capacity Description |
331 or 343 passengers (three-class), 3,900 cu ft (110 m3) of cargo, 83,730 lb (37,970 kg) total payload |
|
| Max Mach (Mach) |
0.92 |
|
| National Origin |
United States of America |
Russia |
| Number Built |
45 |
|
| Powerplant Description |
4 × Pratt & Whitney JT9D-7J high bypass turbofan |
4 × Kuznetsov NK-92 or D-100 turbofans, 176.53 kN thrust each |
| Primary Users |
Pan Am (historical), United Airlines (historical), South African Airways (historical), Iran Air (historical) |
|
| Status |
Two in service with Pratt & Whitney Canada |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Boeing_747SP |
en.wikipedia.org/wiki/Ilyushin_Il-106 |
| Flat Wing Span (m) |
59.64 |
58.5 |
| Flat Wing Area (m²) |
|
370 |
| Wake Category |
H |
|
| Aircraft Engine |
Pratt & Whitney JT9D |
|
| Number of Engines |
4 |
4 |