Sopwith Triplane Typhoon

Cierva C.17

For a description of the format and data included in Production Tables, see here.

Contents

Type Description
Production Details

Type Description

  • C.17 Mk.I
  • (Avro Type 612) Two seat autogyro using a fuselage of the Avro 594 Avian IIIA, with cable braced paddle-type four blade rotor mounted on a tripod above the front cockpit, and featuring stub wings and a wide track undercarriage. One 95 h.p. ADC Cirrus III powerplant.

C.17 Mk.I Specification
Rotor Dia Length Span * Empty Wt Max AUW Minimum Speed Maximum Speed Range Service Ceiling
33 ft 3.5 in 28 ft 9 in 970 lb 1455 lb 25 mph/ 22 kn 90 mph/ 78 kn 210 mi
10.15 m 8.76 m 440 kg 660 kg 40 kph 145 kph 338 km

Span * = span of stub wing

  • C.17 Mk.II
  • (Avro Type 620) As C.17 Mk.I but featuring stub wings with upturned tips and no fixed fin. One 100 h.p. Avro Alpha powerplant.

Production Details

C/n Initial
Registration
Type Notes
1 aircraft built by A.V. Roe & Co. Ltd., Hamble, as their Type 612. First flew October 1928.
5110 G-AABP C.17 Mk.I To the Cierva Autogiro Co. Ltd., Hamble.
1 aircraft built by A.V. Roe & Co. Ltd., Hamble, as their Type 620. First flew in April or May 1929. 3 further aircraft were completed as C.19.
5129 G-AAGJ C.17 Mk.II To the Cierva Autogiro Co. Ltd., Hamble. Converted into the C.17 Hydrogiro floatplane using twin Avro Avian floats in 1929/30, but reverted to C.17 Mk.II after unsuccessful trials. Rebuilt as Avro Avian G-AEDO in 1935.
G-AAGK Not built. Registration reallocated to C.19.
G-AAGL Not built. Registration reallocated to C.19.
G-AAHM Not built. Registration reallocated to C.19.
Total Production  2
Total Production (Not Completed)  3

Production Summary

All Aircraft By Type
Type Built New Conv Canc'd Total
C.17 Mk.I 1 1
C.17 Mk.II 1 3 4
C.17 Hydrogiro (1) 1
2 (1) 3

Production References

  1. Cierva Autogiros - The Development of Rotary-Wing Flight, Peter W. Brooks (Airlife, 1988)