Fieseler Fi 167
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The Fieseler Fi 167 biplane was designed as the prime torpedo and reconnaissance bomber for the new German aircraft carriers then in planning. With the beginning of the construction of the first carrier Graf Zeppelin in 1937, two aircraft producers, Fieseler and Arado, were ordered to produce prototypes for a carrier based torpedo bomber. By summer of 1938 the Fiesler design proved to be superior to the Arado design, the Ar 195.
After two prototypes (Fi 167 V1 & Fi 167 V2), twelve pre-production models (Fi 167 A-0) were built. These had only slight modifications from the prototypes. The aircraft exceeded by far all requirements, had excellent handling capabilities and could carry about twice the required weapons payload. Like the famous Fieseler Fi 156 Storch, the Fi 167 had surprising slow-speed capabilities; the plane would be able to land almost vertically on a moving aircraft carrier.
For emergency landings at sea, the Fi 167 could jetison its landing gear, airtight compartments in the lower wing would help the aircraft stay afloat at least long enough for the two-man crew to evacuate.
Since the Graf Zeppelin was not expected to be completed before the end of 1940, the construction of the Fi 167 had a low priority. When the construction of the Graf Zeppelin was stopped in 1940, the completion of further aircraft was stopped and the completed examples were taken into Luftwaffe service in the "Erprobungsgruppe 167".
When the construction of the Graf Zeppelin was resumed in 1942 the Ju 87C took over the role as a reconnaissance bomber, and torpedo bombers were no longer seen to be needed. Nine of the existing Fi 167 were sent to a coastal naval squadron in the Netherlands and then returned to Germany in summer of 1943. After that they were sold to Croatia. The remaining planes were used in the "Deutsche Versuchsanstalt für Luftfahrt" (German Aircraft Experimental Institute) in Budweis, Czechia for testing different landing gear configurations. The large wing area and resulting low landing speeds made the Fi 167 'too good' for this task, so in order to test landings with higher wing loads, the two test aircraft had their lower wings removed just outboard of the landing gear
No examples of this aircraft exist today
[edit] Specifications (Fieseler Fi 167)
General characteristics
- Crew: 2
- Length: 11.4 m (37 ft 4 in)
- Wingspan: 15.5 m (44 ft 4 in)
- Height: 4.7 m (15 ft 9 in)
- Wing area: 45.5 m² (488 ft²)
- Empty weight: 2,800 kg (6,173 lb)
- Loaded weight: 4,850 kg (9,920 lb)
- Max takeoff weight: 4,850 kg (10,690 lb)
- Powerplant: 1× Daimler-Benz DB 601B 12-Cylinder liquid cooled inverted V, 809 kW (1,100 PS)
Performance
- Maximum speed: 325 km/h (203 mph)
- Cruise speed: 250 km/h (155 mph)
- Range: 1,500 km (808 mi)
- Service ceiling: 8200 m (24,606 ft)
- Wing loading: 107 kg/m² (21.9 lb/ft²)
- Power/mass: 0.169 kW/kg (0.112 hp/lb)
Armament
- 2x 7.92 MG 17 machine guns
- 1x 1000 kg bomb
- 1x 765 kg torpedo
[edit] External links
| Related content | ||
|---|---|---|
| Related development | Fieseler Fi 156 | |
| Similar aircraft | ||
| Designation series |
FK 166 - Fi 166 - Fi 167 - Fi 168 - Fi 158 - He 170 |
|
| Related lists | ||
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