Netherlands' Fokker T.VIII-W bomber1,2
Fokker T.VIII-W:
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
- Fokker T.VIII-Wc: 51,2
- Fokker T.VIII-Wg: 191,2
- Fokker T.VIII-Wm: 121,2
- Total: 361,2
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
- Fokker T.VIII-Wg: Mixed wood and metal structure.1,2 Fabric cover.2
- Fokker T.VIII-Wm: All metal.1,2
- Fokker T.VIII-Wc: Larger mixed wood and metal structure.1
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:
- T.VIII-W/G: 82
- T.VIII-W/M: 122
- T.VIII-W/C: 52
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:
- Complete Book of World War II Combat Aircraft, Enzo Angelucci, Paolo Matricardi, Pierluigi Pinto, 1988
- Aircraft of WWII, Stewart Wilson, 1998

