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Boeing

Boeing 767-300ER

Out of Production

A versatile twin-aisle aircraft that pioneered transoceanic twin-engine operations. Its 2-3-2 economy seating means no middle seat is more than one seat from the aisle, making it a passenger favorite.

Passengers

210-350

Range

6,879 mi

Cruise Speed

529 mph

First Flight

1986

Did You Know?

The 767 was the first twin-engine aircraft certified for extended overwater operations (ETOPS), opening up transoceanic routes to more efficient twins.

History & Timeline

Key Milestones

1988

Entry into Service

American Airlines became the first operator of the 767-300ER in 1988, using it to expand transatlantic service with better economics than larger widebodies.

Development Story

Program Launch

The 767-300ER was developed as an extended-range version of the stretched 767-300, featuring additional fuel capacity and higher takeoff weights for transatlantic operations.

Comfortable 2-3-2 Layout

The 767s 2-3-2 economy configuration meant no passenger was ever more than one seat from the aisle, making it more comfortable than competing aircraft with middle seats in every row.

Interesting Facts

Best-Selling 767

The 767-300ER became the best-selling variant of the 767 family with over 580 delivered, proving the market demand for efficient medium-sized widebodies.

Records & Achievements

ETOPS-180 Approval

The 767-300ER with GE CF6 engines became one of the first aircraft to receive ETOPS-180 approval in 1989, allowing it to fly up to 180 minutes from the nearest airfield.

1989

Legacy & Impact

Freighter Conversion

Many retired 767-300ERs have found new life as converted freighters, with companies like Amazon and FedEx building large fleets of 767 cargo aircraft.

Technical Specifications

Performance

Range
11,070 km (6,879 mi)
Cruise Speed
851 km/h (529 mph)
Service Ceiling
13,137 m (43,100 ft)

Dimensions

Length
54.9 m (180 ft)
Wingspan
47.6 m (156 ft)

Capacity

Passengers
210-350
Cargo Volume
138 m³

Engines

Engine Count
2x PW4060 or GE CF6-80C2
Manufacturer
General Electric / Pratt & Whitney
Thrust (each)
266.9 kN

Weights

Max Takeoff (MTOW)
187,000 kg (412,264 lbs)
Fuel Capacity
90,774 L (23,980 gal)

Takeoff / Landing

Takeoff Distance
2,700 m (8,858 ft)
Landing Distance
1,700 m (5,577 ft)

Commercial

Total Orders
583
Delivered
583
List Price
$216.2M

History

First Flight
January 1, 1986
Status
Out of Production

Sources

Data compiled from the following sources:

M Manufacturer D Aviation Database N News