Fokker 60 Utility

Fokker

ICAOFK60
Fokker 60 Utility aircraft
FokkerFokker 50

Photograph of the Fokker 50 family. No photograph on Wikimedia Commons identifies this variant specifically.

Photo: kitmasterbloke · CC BY 2.0 · Modified

About

The Fokker 60 Utility is a stretched military transport variant of the Fokker 50, developed specifically for the Royal Netherlands Air Force (RNLAF). Introduced in 1996, the Fokker 60 features a 1.62-meter fuselage extension (1.02m forward, 0.80m aft of wing) bringing the total length to 26.87 meters. It is equipped with more powerful Pratt & Whitney Canada PW127B engines and features a large cargo door on the right side behind the cockpit for loading equipment and cargo. The aircraft was designed for tactical transport operations, capable of carrying equipment, soldiers, and conducting paradrop operations. Only four examples were ever built, all delivered to the RNLAF 334 Squadron at Eindhoven. Two were later converted to maritime patrol aircraft. The Fokker 60 is a stretched version of the Fokker 50.

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

22,995kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

22,950kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

21,750kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

20,700kg
0
25k
53k

Empty Weight

13,500kg
0
25k
40k

Capacitycompared to Airbus A318

Passenger Capacity

60passengers
0
100
132

45% of A318 maximum capacity

Crew

Total
3
Cockpit
2
Cabin
1

Dimensions

Length

26.9m

Wingspan

29.0m

Height

8.4m

Wing Area

70.0m²

Engine Specifications

Engine Count

2×

Engine Model

Pratt & Whitney Canada PW127B

Fuel & Cargo

Fuel Capacity

5,366 L

Cargo Volume

14 m³

Production & History

Total Produced

4

Production Status

Out of production

Manufacturing Period

1995–1996

First Flight

November 1, 1995

Entered Service

January 1, 1996

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