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Boeing

Boeing 767-300ER

Out of Production
Boeing 767-300ER

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.

AIRCRAFT DATA

PASSENGERS

210-350

RANGE

6,879 mi

SPEED

529 mph

FIRST FLIGHT

1986

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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