Jodel D.11. Specifications. A photo.
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Jodel D.11. Specifications. A photo.

Jodel D.11. Specifications. A photo.

 

Jodel D.11 - of small-French monoplane produced since 1950, the company «Jodel».

 

Photo Jodel D.11

 

Developments light multipurpose aircraft Jodel D.11 begun by French engineers in the postwar period, with the main reason was the need to create a suitable aircraft for private use and for the training of future pilots, in which, at the end of 40-ies in France tested obvious deficiency.

Designing aircraft Jodel D.11 conducted on the basis of other, earlier model Jodel D.9, however, French experts largely improved the structure of the aircraft, increasing its flight performance and operational use, in particular, the plane could be used as individuals for their own goals and objectives, and the flying school for the above identified problems of pilot training.

 

Jodel D.11 photo

 

The Jodel D.11 aircraft has a fairly compact size, which in turn allows it to take on board no more than two people or an equivalent amount of cargo, however, due to its compact design, the aircraft has high maneuverability properties, which in some situations allows it to be used and as a sports aircraft. One of the main improvements of the aircraft from the French aviation engineers was the increased maximum flight distance, which is about 900 kilometers for the basic version of the aircraft, and about 1300 kilometers for subsequent modifications.

The Jodel D.11 aircraft uses a piston power plant represented, depending on the modification, by the Continental O-200 aircraft engine, the working cylinders of which are capable of developing 100 hp of thrust. The aircraft is capable of developing a maximum flight speed of 210 km / h. (depending on the modification), and is very reliable in terms of its operation.

 

Aircraft Jodel D.11

 

During the production period of the French aircraft manufacturers of the company «Jodel» was built a few dozen very different modified versions of the aircraft, including:

  • Jodel D.11 - The original version of the aircraft, powerplant equipped 45 Salmson 9Adb;
  • Jodel D.111 - an improved version of the aircraft, equipped with a Minié 4.DC with a capacity of 75 hp;
  • Jodel D.112 - A modified version of the aircraft Jodel D.11, equipped with engine capacity of 65 hp to 120 hp that affects the flight performance of the aircraft;
    • Jodel D.112A - An improved version of the aircraft;
    • Jodel D.112D - Modified version with minor technical improvements;
    • Jodel D.112V - Technically improved version of the aircraft;
  • Jodel D.113 - an improved version of the aircraft, equipped with a Continental O-200-A piston engine with a capacity of 100 hp;
  • Jodel D.114 - A modified version of the engine equipped Minié 4.DA.28 (70 hp);
  • Jodel D.115 - a variant with an installed Mathis 4G-F-60 engine with a capacity of 75 hp;
  • Jodel D.116 - version with a Salmson 9ADr engine with a capacity of 60 hp;
  • Jodel D.117 - an improved version of the aircraft with an updated electrical system and a Continental C90 engine;
    • Jodel D.117A - The version marketed by «Alpavia»;
  • Jodel D.118 - Upgraded version with Walter Mikron II engine (60 HP);
  • Jodel D.119 - An updated version version Jodel D.117;
    • Jodel D.119A - An improved version of the aircraft;
    • Jodel D.119V - An improved version;
    • Jodel D.119D - An upgraded version;
  • Jodel D.120 - An option available from «Wassmer»;
    • Jodel D.120A - Version with air brakes;
    • Jodel D.120R - A special version for the acceleration of gliders;
    • Jodel D.120RA - An option that combines features of version Jodel D.120A and Jodel D.120R;
  • Jodel D.121 - Version with an engine capacity of Continental A75 75 hp .;
  • Jodel D.122 - Version equipped engine Praga;
  • Jodel D.123 - modified version with Salmson 5Ap.01 engine;
  • Jodel D.124 - an improved version with a Salmson 5Ap.01 engine with a traction power of 80 hp;
  • Jodel D.125 - Modified version with an improved control panel and a new engine capacity of Kaiser 90 hp .;
  • Jodel D.126 - Version with used motor Continental C85 (85 hp);
  • EAC Jodel D.127 - A special version with an improved version of the passenger compartment;
  • EAC Jodel D.128 - A modified version of EAC Jodel D.127;
  • Jodel D.11 Special - A special version equipped with a powerful piston engine. The production does not start;
  • Falconar F.11 - A modified version of the Canadian production;
  • Uetz U2V - The Swiss version of the aircraft with a reinforced fuselage;
  • Aero Difusion D-11 Compostela - An improved version of the aircraft;
  • Aero Difusion D-112 Popuplane - A modified version;
  • Aero Difusion D-119 Popuplane - An updated version of the aircraft;
  • Aero Difusion D-1190S Compostela - Improved modification of the aircraft;
  • Blenet RB.01 Joze - A special version equipped engine Continental A65-8F.

 

Specifications Jodel D.11.

 

  • Crew: 1 people;
  • Passenger: 1 people;
  • aircraft Length: 6,2 m (depending on version).
  • Wingspan: 8,2 m (depending on version).
  • Plane Height: 2,1 m .;
  • Weight of empty aircraft: 340 kg. (Depending on version);
  • Payload: 280 kg. (Depending on version);
  • Maximum takeoff weight: 620 kg. (Depending on version);
  • Cruising speed: 195 km \ h. (Depending on version);
  • Maximum flight speed: 210 km \ h. (Depending on version);
  • Maximum flight distance: 900 km. (Depending on version);
  • Maximum flight height: 4200 m .;
  • aircraft engine type: a piston;
  • Powerplant: Continental O-200 (depending on version);
  • Power: 100 hp (Depending on version).

 

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