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Friedrichshafen FF.33

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FF.33
Type Fighter
Manufacturer Flugzeugbau Friedrichshafen GmbH
Maiden flight 1914
Introduced 1914
Primary user Kaiserliche Marine
Number built FF.33E: 180
FF.33L: 135

Friedrichshafen FF.33 was a German single-engined amphibious reconnaissance biplane designed by Flugzeugbau Friedrichshafen in 1914.

Versions

FF.33
Initial production version powered by a Mercedes D.II engine, six built
FF.33b
FF.33 with pilot and observers postions reversed, additional obervers-operated machine-gun and powered by 160 hp (119 kW) Maybach inline piston engine, five built.
FF.33e
Main production reconnaissance variant powered by a Benz B.III inline engine, longer twin floats, under tail central float removed, and radio transmitter instead of armament, about 180 built.
FF.33f
Scout/Fighter version based on FF.33e with reduced span wings and reduced length but fitted with a machine-gun on a pivoted mount, five built.
FF.33h
FF.33f with aerodynamic refinements, and duplication of wing-bay bracing cables as a safeguard if the observer has to fire his machine-gun forward through the wings, about 50 built.
FF.33j
FF.33e with aerodynamic refinements and the provision of a radio transmitter and receiver.
FF.33l
Main production scout/fighter version, with further aerodynamic improvements, about 130 built
FF.33s
dual-control trainer version
FF.39
Refined version of the FF.33e with a 200 hp (149 kw) Benz Bz.IV engine, 14 built.
FF.49c
Further improved FF.39 with strengthened structures, balanced controls, a radio receiver and transmitter, machine-gun for observer, over 200 built.
FF.49b
Bomber variant of the FF.49c, crew positions reversed, deletion of observers machine-gun and provision to carry a light bombload, 15 built.
FF.59a
Development aircraft based on FF.39 with different tail, one built.
FF.59b
Development aircraft based on FF.39 with different tail, one built.
FF.59c
FF.39 with modified tail unit, wing interplane struts moved outwards and inner-bay bracing wires removed.
C.I
A landplane version of the FF.33l with wheeled landing gear, one built.

Operators

Specifications (FF.33E)

Data from Thulinista Hornetiin

General characteristics

  • Crew: 2
  • Length: 10.22 m (33 ft 6 in)
  • Wingspan: 16.60 m (54 ft 6 in)
  • Height: 3.75 m (12 ft 4 in)
  • Max takeoff weight: 1,550 kg (3,412 lb)
  • Powerplant:Benz Bz.III inline engine, 112 kW (150 hp)

Performance

Armament

  • 8 × 12 kg (26.4 lb) bombs

  • References

    • Friedrichshafen FF.33s history
    • Timo Heinonen (1992). Thulinista Hornetiin - 75 vuotta Suomen ilmavoimien lentokoneita. Tikkakoski: Keski-Suomen ilmailumuseo. ISBN 9519568824. 

    Template:Idflieg C-class designations

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    This article is licensed under the GNU Free Documentation License.
    It uses material from the Wikipedia article "Friedrichshafen FF.33".