Fokker F28 Mark 1000

Fokker

ICAOF28
Fokker F28 Mark 1000 aircraft
FokkerFokker F28 Fellowship

Photograph of the Fokker F28 Fellowship family. No photograph on Wikimedia Commons identifies this variant specifically.

Photo: Piergiuliano Chesi · CC BY 3.0 · Modified

About

The first Fellowship, approved in February 1969, seating 70. The certificate takes it from 25,720 kg at approval to 30,164 kg through six service bulletins, and this row carries the last of them. A 3,300-litre centre wing tank was optional on the Mark 1000 and on no other Mark; the fuel figure here is the wing tanks alone, which every Mark has. Dimensions are EUROCONTROL's figures for the F28 type code rather than the certificate's: EASA TCDS A.037 states no dimension for any Mark, and the source does not distinguish them.

Weightscompared to Airbus A318

MTOW (Maximum Takeoff Weight)

30,164kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

26,770kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

24,720kg
0
25k
53k

Capacitycompared to Airbus A318

Passenger Capacity

70passengers
0
100
132

53% of A318 maximum capacity

Dimensions

Length

27.4m

Wingspan

27.1m

Height

8.5m

Engine Specifications

Engine Count

2×

Engine Model

Rolls-Royce RB183 Mk 555-15, -15N or -15P

Thrust per Engine

43.8 kN(9847 lbf)

Fuel & Cargo

Fuel Capacity

9,740 L

Production & History

Production Status

Out of production

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