JEROEN VOGELAAR: Aviation Photographs

767-200

Boeing 767

Boeing 767-300ER N647UA United Airlines

The Boeing 767 is a mid- to large-size, long-range, wide-body twin-engine jet airliner built by Boeing Commercial Airplanes. It was the manufacturer’s first wide-body twinjet and its first airliner with a two-crew glass cockpit.

  • Role: Wide-body jet airliner
  • National origin: United States
  • Manufacturer: Boeing Commercial Airplanes
  • First flight: 767-200ER September 26, 1981, 767-300ER December 9, 1986, 767-400ER October 9, 1999
  • Introduction: September 8, 1982 with United Airlines
  • Status: In service
  • Produced: 1981–present
  • Number built: 1,069 through January 2015

Military variants

  • 767 Airborne Surveillance Testbed – – the Airborne Optical Adjunct (AOA) was modified from the prototype 767-200 for a United States Army program
  • E-767 – the Airborne Early Warning and Control (AWACS) platform for the Japan Self-Defense Forces
  • KC-767 Advanced Tanker – the 767-200ER-based aerial tanker developed for the USAF KC-X tanker competition
  • KC-767 Tanker Transport – the 767-200ER-based aerial refueling platform operated by the Italian Air Force (Aeronautica Militare), and the Japan Self-Defense Forces
  • Tanker conversions – the 767 MMTT or Multi-Mission Tanker Transport is a 767-200ER-based aircraft operated by the Colombian Air Force

Specifications

General characteristics

Boeing 767-200ER

  • Cockpit crew: 2
  • Seating capacity: 255, optional 290 (1-class)
  • Overall length: 159 ft 2 in (48.5 m)
  • Wingspan: 156 ft 1 in (47.6 m)
  • Overall height: 15,85 m.
  • Fuselage width: 16 ft 6 in (5.03 m)
  • Fuselage Height: 17 ft 9 in (5.41 m)
  • Operating empty weight: 181,610 lb (82,380 kg)
  • Maximum take-off weight: 395,000 lb (179,170 kg)
  • Service ceiling: 11.887 m
  • Cruising speed: Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Maximum speed: Mach 0.86 (493 knots, 567 mph, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Range fully loaded: 6,385 nmi (7,348 mi; 11,825 km)
  • Engine (× 2): P&W PW4052, or 4056, GE CF6-80C2, RR RB211-524G or H
  • Thrust: PW: 63,300 lb (282 kN), GE: 62,100 lbf (276 kN)

Boeing 767-300ER

  • Cockpit crew: 2
  • Seating capacity: 290; optional 350 (1-class)
  • Overall length: 180 ft 3 in (54.9 m)
  • Wingspan: 156 ft 1 in (47.6 m)
  • Overall height: 15,85 m.
  • Fuselage width: 16 ft 6 in (5.03 m)
  • Fuselage Height: 17 ft 9 in (5.41 m)
  • Operating empty weight: 198,440 lb (90,010 kg)
  • Maximum take-off weight: 412,000 lb (186,880 kg)
  • Service ceiling: 11.887 m
  • Cruising speed: Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Maximum speed: Mach 0.86 (493 knots, 567 mph, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Range fully loaded: 6,310 nmi (7,260 mi; 11,690 km)
  • Engine (× 2): P&W PW4056, 4060, or 4062. GE CF6-80C2. RR RB211-524G, or H
  • Thrust: PW: 63,300 lbf (282 kN), GE: 62,100 lbf (276 kN), RR: 59,500 lbf (265 kN)

Boeing 767-400ER

  • Cockpit crew: 2
  • Seating capacity: 375 (1-class)
  • Overall length: 201 ft 4 in (61.4 m)
  • Wingspan: 170 ft 4 in (51.9 m)
  • Overall height: 15,85 m.
  • Fuselage width: 16 ft 6 in (5.03 m)
  • Fuselage Height: 17 ft 9 in (5.41 m)
  • Operating empty weight: 229,000 lb (103,870 kg)
  • Maximum take-off weight: 395,000 lb (179,170 kg)
  • Service ceiling: 11.887 m
  • Cruising speed: Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Maximum speed: Mach 0.86 (493 knots, 567 mph, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Range fully loaded: 5,625 nmi (6,473 mi; 10,418 km)
  • Engine (× 2): P&W PW4062 GE CF6-80C2
  • Thrust: PW: 63,300 lbf (282 kN) GE: 63,500 lbf (282 kN)