Fokker 100 Specs, Interior, Cockpit, and Price – Fokker 100 is a medium-sized aircraft that was developed and produced by the Fokker Aircraft Company (FAC), the Netherlands. Introduced in the 1980s, these aircraft have low operating costs and no competition and are best-sellers in the category of 100 seats in that period.
In 1983 the Fokker 100 design was announced as a replacement for the extended Fokker F28. The United States Federal Aviation Administration said the plane was a Fokker 28-0100, although many parts of the two designs were similar. The first prototype (PH-MKH) made its maiden flight in November 1986. The second prototype (PH-MKC) flew in February 1987. The first Fokker 100 was sent to its launch customer, SwissAir, in February 1988.
The airline crisis in the 1990s and competition from Bombardier CRJ200 and Embraer ERJ 145 adversely affected the sale of Fokker 100 and the company went bankrupt in 1996. Production ended in 1997. A total of 278 aircraft were produced. In 2009, 30 airlines operated 229 Fokker 100 aircraft.
The basic Fokker 100 aircraft has a maximum maximum ramp (MRW) of 44,680kg, maximum takeoff weight (MTOW) of 44,450kg and a maximum landing weight of 39,915kg. It has a maximum payload capacity of 11,240kg and a fuel tank capacity of 10,293 kg.
The expanded range version of Fokker 100 with an additional fuel tank was introduced in 1993. In 1994 the passenger / transport version, Fokker 100QC, was launched. The economical design life of the aircraft is 90,000 landings or flight hours. Most aircraft reach 3,500 flight hours per year.
The Tay 620 engine weighs 3.135lb and provides a maximum take-off boost of 13,850lb. The engine is 94.8in long and 44in fan diameter. In full passenger loads, the engine has a range of 2,020nm. The Tay 650 engine produces 15.100lb of thrust and weighs 3.340lb. Its length is 94.8in and has a fan diameter of 44.8in. In full passenger loads, the engine has a range of 1,680nm.
At a maximum payload of 11,240kg, the Fokker 100 can cross in the range of 1,600 nm. With MTOW 45,810kg and maximum payload capacity, this aircraft has a range of 2,200 nm.
In 1983 the Fokker 100 design was announced as a replacement for the extended Fokker F28. The United States Federal Aviation Administration said the plane was a Fokker 28-0100, although many parts of the two designs were similar. The first prototype (PH-MKH) made its maiden flight in November 1986. The second prototype (PH-MKC) flew in February 1987. The first Fokker 100 was sent to its launch customer, SwissAir, in February 1988.
The airline crisis in the 1990s and competition from Bombardier CRJ200 and Embraer ERJ 145 adversely affected the sale of Fokker 100 and the company went bankrupt in 1996. Production ended in 1997. A total of 278 aircraft were produced. In 2009, 30 airlines operated 229 Fokker 100 aircraft.
Fokker 100 Specs
Fokker 100 provides seating for 109 passengers. The standard aircraft is 8.5m high, 35.53m long and has a wingspan of 28m. It has a wing area of 93.5m², a 5m main wheel track and a 14m wheel base.The basic Fokker 100 aircraft has a maximum maximum ramp (MRW) of 44,680kg, maximum takeoff weight (MTOW) of 44,450kg and a maximum landing weight of 39,915kg. It has a maximum payload capacity of 11,240kg and a fuel tank capacity of 10,293 kg.
The expanded range version of Fokker 100 with an additional fuel tank was introduced in 1993. In 1994 the passenger / transport version, Fokker 100QC, was launched. The economical design life of the aircraft is 90,000 landings or flight hours. Most aircraft reach 3,500 flight hours per year.
Fokker 100 Engine
Fokker 100 uses the Rolls-Royce Tay 620 or Tay 650 engine. The first 36 aircraft are equipped with the Tay 620 engine and the aircraft built then runs with the Tay 650 engine. Both engines offer high fuel efficiency, performance, reliability and noise and emission levels. The low one.The Tay 620 engine weighs 3.135lb and provides a maximum take-off boost of 13,850lb. The engine is 94.8in long and 44in fan diameter. In full passenger loads, the engine has a range of 2,020nm. The Tay 650 engine produces 15.100lb of thrust and weighs 3.340lb. Its length is 94.8in and has a fan diameter of 44.8in. In full passenger loads, the engine has a range of 1,680nm.
At a maximum payload of 11,240kg, the Fokker 100 can cross in the range of 1,600 nm. With MTOW 45,810kg and maximum payload capacity, this aircraft has a range of 2,200 nm.
Fokker 100 Cabin and Interior
Fokker 100 has two cabin configurations. One of them is a 109-seat economy class layout with five consecutive seats and the other is a business class layout with four consecutive seats. The typical cabin layout has 107 seats on pitch 32in. The aircraft has a top deck compartment to both sides of the entrance that offers a higher carrying capacity. It also has a passenger door opening to the front or a downward opening door with integrated stairs.
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