Boeing 727
Summary
Category | Transport aircraft |
Origin country | πΊπΈ United States |
First flight | 9 February 1963 |
Year of introduction | 1964 |
Number produced | 1832 units |
Description
The Boeing 727 is a mid-sized, three-engine, narrow-body airliner that was developed by Boeing Commercial Airplanes in the late 1960s. Designed to serve as a short-haul and medium-range passenger aircraft, it was also utilized by some military organizations for various missions. The 727 was equipped with advanced features at the time, including a T-tail configuration, low wing design, and a retractable tricycle landing gear. It featured a spacious cabin capable of accommodating around 149 to 189 passengers, depending on the specific configuration. The aircraft was widely deployed by civil airlines around the world and served a vital role in their fleet for several decades.
Technical specifications
Version: 727-200 | |
---|---|
Wing area | 157.9 mΒ² (1699.9 sqft) |
Wingspan | 33 m (108.3 ft) |
Height | 10 m (32.8 ft) |
Length | 46.7 m (153.2 ft) |
Service ceiling | 12802 m (42001 ft) |
Empty weight | 45359 kg (99999 lbs) |
Max. takeoff weight | 95028 kg (209501 lbs) |
Takeoff distance | 1768 m (5801 ft) |
Powerplant | 3 Γ turbojets Pratt & Whitney JT8D-9A delivering 6577 kgp |
Current operating countries
Country | Units | ||
---|---|---|---|
Colombia | 1 | ||
π¨π© | Congo Democratic Republic | 1 | |
Ecuador | 1 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.
All operators
Belgium β’ Congo Democratic Republic β’ Colombia β’ Djibouti β’ Ecuador β’ Greece β’ Iran β’ Kuwait β’ Liberia β’ Mexico β’ Mauritania β’ Nigeria β’ New Zealand β’ Panama β’ Qatar β’ Senegal β’ Taiwan β’ United States β’ Yemen β’ Ex-Yugoslavia