Summary
The CAMS 58 was a transport flying boat built in France in the early 1930s intended as a successor to the highly successful CAMS 53. Compared to the earlier design, the CAMS 58 featured a newly designed Biplane wing cellule and an all-metal hull in place of its predecessor's wooden hull. Work was slow, with three years passing from the start of design work to the prototype's first flight. When the newly formed Air France showed no interest in purchasing the type, CAMS redesigned it to be powered by two pairs of engines in tractor-pusher installations. Again, no interest was forthcoming. The final iteration of the design, reverting to a single pair of more powerful engines and a wooden hull, met with only slightly more success. Air France bought two machines and operated them briefly before declaring them uneconomical and removing them from service.
| 58 | |
|---|---|
| |
| CAMS 58/2 | |
| Role | Flying boat airliner |
| Manufacturer | CAMS |
| First flight | 1933 |
| Primary user | Air France |
| Number built | 4 |
Variants edit
- 58/0 - prototype with Hispano-Suiza 12Fa engines (one built)
- 58/2 - four-engine version with Lorraine 9Na Algol engines (one built)
- 58/3 - version with Hispano-Suiza 12Nbr engines (two built)
Specifications (58/3) edit
General characteristics
- Crew: three
- Capacity: four passengers
- Length: 14.91 m (48 ft 11 in)
- Wingspan: 24.30 m (79 ft 9 in)
- Height: 6.14 m (20 ft 2 in)
- Wing area: 129.7 m2 (1,396 sq ft)
- Empty weight: 5,428 kg (11,967 lb)
- Gross weight: 8,450 kg (18,629 lb)
- Powerplant: 2 × Hispano-Suiza 12Nbr , 485 kW (650 hp) each
Performance
- Maximum speed: 200 km/h (125 mph, 109 kn)
- Range: 950 km (590 mi, 510 nmi)
- Service ceiling: 4,500 m (14,765 ft)
References edit
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 226.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 891 Sheets 03.