Boeing 767-200

The original twinjet widebody built for transcontinental efficiency.

Overview

Boeing United States ICAO: B762 1982–1994 Active $160.2 million

The Boeing 767-200 was the first variant of the 767 family. Designed to provide efficient twin-engine widebody service, it entered airline operations in the early 1980s. The aircraft helped establish extended-range twin-engine operations.

Live Fleet Activity (B762)

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Specifications

Units
Engine
2 × General Electric CF6-80C2, Pratt & Whitney JT9D
Engine type
Turbofan
Thrust
2 × 60,600 lbf · 270 kN
Avionics
—
Wing tips
No winglets
Seats
290 economy · 224 business · 181 first
Crew
—
Cabin width
15 ft 5 in  ·  4.70 m
Cabin height
6 ft 11 in  ·  2.10 m
Cabin length
111 ft 4 in  ·  33.93 m
Exterior length
159 ft 1 in  ·  48.50 m
Tail height
52 ft 11 in  ·  16.13 m
Fuselage diameter
16 ft 6 in  ·  5.03 m
Wing span
156 ft 2 in  ·  47.60 m
Baggage volume
3,069 ft³  ·  86.9 m³
Gross weight
—
Empty weight
—
Max takeoff weight
315,000 lb  ·  143,000 kg
Max landing weight
272,000 lb  ·  123,500 kg
Max payload
73,500 lb  ·  33,300 kg
Fuel capacity
16,700 gal · 63,200 L · 50,600 kg (Jet A)
Max cruise speed
493 kt  ·  567 mph  ·  913 km/h
Maximum speed
—
Cruise speed
—
Approach speed
135 kt  ·  155 mph  ·  250 km/h
Range
6,590 nm  ·  7,580 mi  ·  12,200 km
Fuel burn
0.27 nm/gal  ·  0.13 km/L
Ceiling
43,199 ft  ·  13,200 m
Rate of climb
2,000 ft/min  ·  10 m/s
Takeoff distance
5,600 ft  ·  1,710 m
Landing distance
4,000 ft  ·  1,220 m
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Omni Air International – Boeing 767-200

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Operational Context

Boeing 767-200 — early widebody twin-engine jet

The 767-200 first flew in 1981 and entered service in 1982. It was developed to serve medium and long-haul routes with improved fuel efficiency compared with earlier widebodies. The aircraft introduced advanced flight deck systems for its era.

Powered by two high-bypass turbofan engines producing approximately 48,000 to 52,000 pounds of thrust (213 to 231 kN) each depending on variant, the 767-200 cruises at around 460 knots (850 km/h). Maximum takeoff weight exceeds 315,000 pounds (143,000 kg). Seating typically ranges from 180 to 218 passengers.

The 767-200 established the foundation for subsequent 767 variants. It played a significant role in expanding transcontinental and transatlantic services. Many aircraft were later converted to cargo use.

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