Design
The all-metal F26 design consisted of a low-wing layout with a 17-seat pressurized fuselage, a fully retractable gear and two Rolls-Royce Nene RB.41 series I jet engines. With a thrust of 2.3 kN (5,171 lbf) each, these engines were the most powerful engines available at the time. The aircraft was designed for a flight crew of three people.
The passenger cabin had a single aisle layout, with two seats abreast on the right and a single row on the left. The aft side had a toilet section and two cargo bays. The aircraft was to be flown by two pilots and one radio operator.
Based on design studies the F26 had an economical cruise speed of 800 km/h (497 mph) with a range of 1,000 km (621 mi).
Read more about this topic: Fokker F26
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