Robin HR100

Last updated
Robin HR.100
D-EKRF Robin HR.100 250TR Tiara (EHLE 1993-05-22).jpg
Robin HR.100/250TR Tiara aircraft D-EKRF, at Lelystad Airport (EHLE), 22 May 1993
RoleFour-seat light monoplane
National origin France
Manufacturer Avions Pierre Robin
Designer Chris Heintz
First flight 1969
Produced1969-1976
Number built178
Developed from Robin DR.200

The Robin HR100 is a French four-seat light monoplane, designed by Chris Heintz [1] and built by Avions Pierre Robin as metal-winged version of the Robin DR253 Regent.

Contents

Development

The prototype of the Robin HR100 was the prototype DR253 Regent which was rebuilt with metal wings and powered by a 180 hp (134 kW) Lycoming O-360 engine. It first flew on 3 April 1969 as the Robin HR100/180. The HR100 is a low-wing cantilever monoplane with a conventional cantilever tail unit and a fixed tricycle landing gear. A number of different variants were produced in the 1970s. From 1972 a high-powered improved version was produced as the HR100/285 with a 285 hp (213 kW) Continental Tiara 6-285B engine and retractable landing gear and airframe modifications.

French Air Force HR.100/250 communications aircraft at Nancy Essey airfield in 1977 Robin HR.100.250 531 EJ Nancy Essey 09.06.77 edited-2.jpg
French Air Force HR.100/250 communications aircraft at Nancy Essey airfield in 1977

The French Air Force ordered a number of HR.100/250 aircraft in the mid 1970s and these were used for communications and other duties.

A two-seat trainer version was developed as the HR200, and a modified version with a lighter airframe and new fin and rudder was developed as the R1180 Aiglon in 1977.

Variants

HR.100 Royal
1969 Prototype with a 180hp (134kW) Lycoming O-360 engine, one built.
HR.100/180
1976 Prototype with a 180hp (134kW) Lycoming O-360 engine, one built.
HR.100/200B Royal
Initial production version with a 200hp (149kW) Lycoming IO-360 engine.
HR.100/210 Safari
Production version with a 210hp (157kW) engine, 113 built of both 200B Royal and 210 Safari variants.
HR.100/235TR
Experimental HR.100 with an enlarged tail and retractable landing gear and a 235hp Lycoming O-540-B engine, one built.
HR.100/250TR
HR.100/235 with a 250hp (186kW) Lycoming IO-540-C4B5 engine, 24 built.
HR.100/285TR Tiara
HR.100/235 with a 285hp (213kW) Continental Tiara 6-285 engine, 37 built
HR.100/320 4+2
Experimental version with two extra children's seats, one built

Operators

Military operators

Flag of France.svg  France

Specifications (HR.100/285)

Data from Jane's All the World's Aircraft 1976–77 [2]

General characteristics

Performance

See also

Related development

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References

  1. Calderwood, Dave (3 May 2021). "Zenair's Chris Heintz RIP". Flyer. Archived from the original on 3 May 2021. Retrieved 5 May 2021.Cite has empty unknown parameter: |1= (help)
  2. Taylor 1976, pp. 62–63