| Letov Š-16 | |
|---|---|
![]()  | |
| Letov Š-116 | |
| Role | Bomber | 
| Manufacturer | Letov Kbely | 
| Designer | Šmolík | 
| First flight | 1926 | 
| Primary user | Czechoslovakian Air Force | 
| Number built | 89 | 
The Letov Š-16 was a Czechoslovak single-engined, two-seat biplane bomber. It was designed by Alois Šmolík at Letov Kbely. The Š-16 first flew in 1926.[1]
Variants
- Š-16
 - Two-seat bomber, reconnaissance biplane.
 - Š-16J
 - Seaplane version for Yugoslavia. One built.
 - Š-16L
 - Export version for Latvia.
 - Š-16T
 - Export version for Turkey.
 - Š-116
 - version with Skoda L engine
 - Š-216
 - version with Walter-built Bristol Jupiter engine
 - Š-316
 - version with Hispano-Suiza 12N engine
 - Š-416
 - version with Breitfeld-Danek BD-500 engine
 - Š-516
 - version with Isotta-Fraschini Asso 750 engine
 - Š-616
 - version with Hispano-Suiza 12Nbr engine
 - Š-716
 - version with Skoda L engine
 - Š-816
 - version with Praga ESV engine
 - Š-916
 - version with Lorraine-Dietrich engine
 - Š-17
 - third prototype Š-16 with a V-12 Breitfeld-Danek (Praga) BD-500 engine[2]
 
Operators
- Czechoslovakian Air Force (115 aircraft)
 
- Aviation Regiment (21 aircraft)
 
- Turkish Air Force (16 aircraft)
 
- Yugoslav Royal Navy (one aircraft)
 
Specifications (Š-316)

Data from Jane's all the World's Aircraft 1928[3]
General characteristics
- Crew: 2
 - Length: 10.22 m (33 ft 6 in)
 - Wingspan: 15.3 m (50 ft 2 in)
 - Height: 3.23 m (10 ft 7 in)
 - Wing area: 46.4 m2 (499 sq ft)
 - Empty weight: 1,400 kg (3,086 lb)
 - Gross weight: 2,450 kg (5,401 lb)
 - Powerplant: 1 × Hispano-Suiza 12N V-12 water-cooled piston engine, 340 kW (450 hp)
 
Performancemaximum
- 228 km/h (142 mph; 123 kn) at 1,800 m (5,900 ft)
 
- Stall speed: 90 km/h (56 mph, 49 kn)
 - Service ceiling: 6,000 m (20,000 ft)
 - Rate of climb: 3 m/s (590 ft/min)
 - Time to altitude: 5,000 m (16,000 ft) in 23 minutes 30 seconds
 - Wing loading: 52.7 kg/m2 (10.8 lb/sq ft)
 - Power/mass: 0.138 kW/kg (0.084 hp/lb)
 
Armament
- Guns: 1x fixed, forward-firing, 7.7 mm (0.303 in) ZB vz.09 machine-gun in the forward fuselage; 2x 7.7 mm (0.303 in) Lewis guns on a flexible mount in the rear cockpit.
 
See also
Wikimedia Commons has media related to Letov Š-16.
Related lists
References
- ↑ Taylor, John W. R.; Alexander, Jean; et al. (1969). Combat aircraft of the world. London: Ebury P.; Michael Joseph. pp. 62–63. ISBN 0-71810-564-8.
 - ↑ "Letov Designations".
 - ↑ Grey, C.G., ed. (1928). Jane's all the World's Aircraft 1928. London: Sampson Low, Marston & company, ltd. p. 78c.
 
Bibliography
- Passingham, Malcolm (February 1997). "Le Letov S-16 (première partie)". Avions: Toute l'aéronautique et son histoire (in French) (47): 19–27. ISSN 1243-8650.
 - Passingham, Malcolm (April 1997). "Le Letov S-16 (3ème et dernière partie)". Avions: Toute l'aéronautique et son histoire (in French) (49): 14–16. ISSN 1243-8650.
 
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