The Robin DR200 Series

The Robin DR200 Series


G-AYDZ Jodel DR 200 at the LAA Rally, Sywell in 09/17
G-AYDZ Jodel DR 200 at the LAA Rally, Sywell in 09/17


By 1965, it was time to replace the DR 1050. The DR 250 was introduced. The 250 was no longer called a Jodel, but received the name Robin. It was merely a modified and improved DR 1050. The major changes being:

DR250 in Iceland

DR220 F-BOKF

After winning the Sicile races with the DR1051, Robin wanted something even faster. In an era where improvements in General Aviation were following up very quickly, the 6 year old design of the DR1050M was becoming obsolete. Robin fitted a larger engine to the DR1050, made it more roomy, streamlined it even more and thus created the DR250 Capitaine.

The 250 proved very competative in the Sicile racings, securing the first seven positions in the rankings, Robin as always firmly on the number one spot.

DR221 in flight TF-ROB, a DR221 in flight

Robin experimented with a 180 hp engine in his personal DR250, with which he obtained an avarage speed of 317 kph during one of the Sicile air races. Such was his lead, that the race organizers asked Robin not to enter the next race, since this would render the rest of the field without chances of winning!

DR221 in flight
TF-ROB, a DR221 in flight

The succes of the races had its impact on sales, which boomed. There was however an increasing demand for a more affordable aircraft that was suited for training purposes. Recognising the potential of the DR250, Robin created a spin off, the DR220. The 220 received a slightly enlarged vertical tailplane, to make it more stable, lacked the wing tanks, was given dual throttle controls for flying school duties, and was fitted with a 100 hp Continental or Rolls Royce O-200 engine, the same that had been used on the DR1050. The 125 hp fuel injected engine that Potez had promised never made it into production, and was therefore never fitted.

Like the DR250, the DR220 proved successful, and a total of 83 were built. In 1967, the DR221 was introduced. The DR221 Dauphin was a more luxurious version of the 220, fitted with a 115 hp Lycoming O-235 L2C engine and extensive sound proofing. Of the Dauphin, 62 were built.


Exploded view of DR250
Exploded view of the DR250.
Click on the picture to get a large version (400 kB).

Specifications

Model: DR220 DR221 DR250
Number produced 84 62 101
Production years 1966-1970 1967-1970 1965-1969
Overall dimensions:      
Length 6.90 m 6.90 m 6.90 m
Wing span 8.72 m 8.72 m 8.72 m
Wing area 13.6 m2 14.15 m2 14.15 m2
Weights and loadings:      
Empty weight 440 kg 480 kg 500 kg
Max Take off weight 780 kg 830 kg 960 kg
Useful load 340 kg 350 kg 460 kg
Fuel capacity (wings) none 2 x 40 l 2 x 40 l
Fuel capacity (rear) 110 l 110 l 110 l
Other specs:      
Gear Tailwheel Tailwheel Tailwheel
Seats 2+2 4 4
Controls Stick and rudder Stick and rudder Stick and rudder
Material Wood and fabric Wood and fabric Wood and fabric

TF-ROB being refitted with new engine
Icelandic DR221 TF-ROB being refitted with overhauled engine.
Note the curious detail: A DR221 without wing tanks.

Engine:      
Make Continental Lycoming Lycoming
Model O-200 O-235 O-320
Power 100 hp 108/115 hp 150/160 hp
Fuel 80/87 80/87 or 100/130 100/130
Fuel burn 20 l/hr 22 l/hr 32 l/hr
Performance:      
Max speed, sea level 230 km/h 245 km/h 282 km/h
Cruise speed, 75% sea 205 km/h 230 km/h 250 km/h
Cruise speed, 75% 3000 m 215 km/h 230 km/h 265 km/h
Service ceiling 4600 m ? 5200 m
Range, no reserves 1050 km 1000 km 1150 km

Click for large picture of DR220 panel
Pictures of F-BOKF, a DR 220 owned by M. Jaques le Coguiec.
Click on any one of them for a larger size

The end of the sixties was an era where every self respecting aircraft manufacturer switched from taildragger to trigear configuration. In this light, the DR 250 was given a nosewheel undercarriage. Along with it, the engineers at Robin decided to enlarge the fuselage, in order to seat the back seat passengers more comfortably. To propell these passengers at an ever greater pace, an even larger 180 hp Lycoming O-360-D2A engine was fitted. The resulting aircraft was given the name DR 253 Regent.

G-AVOC us a DR221
 
G-CPCD is a DR221

The regent was farther developed into the DR 300 series.

Author Hans Teijgeler
The photos in this web site are from the excellent book by Xavier Massé,
sent in by happy Jodel owners, lifted from the web or taken by myself.