| Wednesday, January 07, 2009 |
 |
Boeing 767
IOC: 1982
Total Production: 1,017
Total Program's Cost: USD$100 billion
Boeing 767-300
IOC: 1986
Origin
United States of America
Contractor/s
Boeing
Family Members
Boeing 767-200ER
Boeing 767-300ER
Boeing 767-300F
Boeing 767-400ER
Power plant:
CF6-80C2 (2)
PW4062 (2)
RB211-524G (2)
RB211-524H (2)
|
Description:
The Boeing 767 is a complete family of twin-engine aircraft suitable for medium and long range operations which can accommodate from 200 to 300 passengers as well as cargo in the 767 freighter variant. The first version, a 767-200, entered service in 1982 and its final delivery occurred in 1994. The 767 family has low fuel consumption and produces less pollutant per pound of fuel than other similar twin-engine aircraft.
The Boeing 767-300 is a stretched version of 767-200/ER to carry more passengers. The seating capacity ranges from 261 to 290 passengers in a two-class or one-class configurations respectively. The first -300 model entered service in 1986 with a Japanese airline.
Specifications
Accommodation: Crew 2, Passengers 290
Dimensions: Height 15.8 m, Length 54.9 m, Wingspan 47.6 m
Weights: Max Weight 160 t, Min Weight 86,100 kg (189,815 lb), Payload 40,230 kg (88,690 lb)
Engine/s Performance: Thrust 126,600 lb (57,426 kg)
Performance: Max Range 7,200 km (3,888 nm), Top Speed 266 mps (Mach 0.80)
Other: Number of Engines 2
|
|
Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)
Last Updated: Saturday, December 20, 2008
Leave Feedback >>
|
|
Copyright © 2003 - 2009 deagel.com. All Rights Reserved.
United States of America