Netherlands' Fokker T.VIII-W bomber1,2

Fokker T.VIII-W:
Netherland's Fokker T.VIII-W bomber

Fokker T.VIII-Wm used by Germans in the Aegean Sea:
Netherland's Fokker T.VIII-Wm used by Germans in the Aegean Sea

Design

In 1937 the Dutch navy issued a specification for a twin engine seaplane capable of carrying a torpedo internally and optionally bombs.1,2 In 1938 Fokker created a twin engined sea plane that would be used by the Dutch navy.1

Engine

The engines powered two bladed metal propellers.1

Wing

The Fokker T.VIII-W had a mid wing with the two engines.1 Two large duralumin floats were located underneath.1

Nose

The observer for the T.VIII-W was located in a glazed nose.1

Armament

The radio operator was located in the compartment behind the pilot and controlled a flexible machine gun.1 The pilot controlled a machine gun that was installed in a half wing.1

Prototype

The prototype first flew in 1938.2

The T.VIII-W/C first flew in late 1939.2

Production

In 1938 an order for five T.VIII-Ws was placed.1 These were delivered by June of 1939.1 Then the Dutch Navy ordered 26 more for the East Indies.1
Nineteen were initially ordered.2 In early 1940 twelve were ordered for the Netherlands Naval Air Force.2 None made it to the Netherlands East Indies.2

Finland

In 1939 Finland ordered the Fokker T.VIII-Wc.1 Five were constructed, and the last one converted to a land plane.2 All were confiscated by the Germans.2

Variants

Usage

Britain, Germany, and the Netherlands used the Fokker T.VIII-W.2

Germany

28 of T.VIII-Ws were used by the Germans as naval reconnaissance in the Mediterranean and the North Sea.1
Germany took over or received delivery of:

United Kingdom

On May 14, 1940, eight T.VIII-Ws flew to the United Kingdom.1,2 These were used by the No. 320 Squadron (Dutch personnel) in the North Sea as convoy escorts.1,2 Eventually the lack of spare parts caused the T.VIII-Ws from being used.1,2

  Fokker T.VIII-W1 Fokker T.VIII-W/G2 Fokker T.VIII-W/M2 Fokker T.VIII-Wc1
Fokker T.VIII-W/C2
Type Bomber1
Torpedo bomber2
Reconnaissance2
     
Crew 31,2
Pilot, observer, radio operator
     
Engine (Type) 2: Wright Whirlwind1 2: Wright R-975-E3 Whirlwind2 2: Wright R-975-E3 Whirlwind2 2: Bristol Mercury XI1,2
Cylinders Radial 91 Radial 92 Radial 92 Radial 92
Cooling Air1      
Net HP 450 each1 450 each2 450 each2 902 each1
Propeller blades 2 each1      
Dimensions        
Span 59'1
17.98 m1
59' 1"2
18 m2
59' 1"2
18 m2
65' 6"1, 65' 7"2
19.98 m1, 20 m2
Length 42' 8"1
13 m1
42' 8"2
13 m2
42' 8"2
13 m2
48' 7"1, 49' 3"2
14.8 m1, 15.01 m2
Height 16' 5"1
5 m1
16' 5"2
5 m2
16' 5"2
5 m2
 
Wing area        
Weight        
Empty   7,055 lb2
2,150 kg2
  9,700 lb2
4,400 kg2
Loaded 11,030 lb1
5,000 kg1
11,023 lb2
5,000 kg2
  14,550 lb2
6,600 kg2
Performance        
Speed 177 mph1
285 kph1
    224 mph2
360 kph2
Speed @ 9,840' /
3,000 m
  177 mph2
285 kph2
   
Cruising speed   137 mph2
220 kph2
   
Endurance        
Climb        
Service ceiling 22,300'1
6,800 m1
22,310'2
6,800 m2
  19,030'2
5,800 m2
Range 1,710 miles1
2,750 km1
1,305 miles2
2,100 km2
  1,056 miles2
1,700 km2
Armament 2 - 3: MG1      
Nose   2: 7.9 mm MG2    
Dorsal   2: 7.9 mm MG2    
Ventral   2: 7.9 mm MG2    
Bombs or torpedo 1,330 lb1
603 kg1
1,323 lb2
600 kg2
   

Sources:

  1. Complete Book of World War II Combat Aircraft, Enzo Angelucci, Paolo Matricardi, Pierluigi Pinto, 1988
  2. Aircraft of WWII, Stewart Wilson, 1998
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