RWD-14 Czapla
RWD-14b Czapla | |
---|---|
Role | reconnaissance and liaison aircraft |
Manufacturer | LWS
|
First flight | 1936 |
Introduction | 1939 |
Primary users | Polish Air Force Romanian Air Force |
Produced | 1938–1939 |
Number built | 65 (+4 prototypes) |
The RWD-14 Czapla (LWS Czapla) was a Polish
Design and development
The aircraft was designed in response to a
The first prototype was flown in early
The LWS built a series of 65 RWD-14b Czapla by February 1939. They were also known under a military designation LWS Czapla.[4]
Operational history
The Czapla entered service in the Polish Air Force in the spring of 1939, equipping some observation squadrons (eskadra obserwacyjna). Due to its long development, it was not a modern aircraft, only a little better than the Lublin R-XIII. Its advantage was its short take-off (140 m) and landing (120 m), enabling it to operate from fields and meadows.[1] Its modern successor, the LWS-3 Mewa, did not manage to enter operational units due to the war.[5]
By the
Most – 35 RWD-14b were destroyed during the campaign.[4] At least 14 were withdrawn to Romania (the sources quote numbers from 14 to 17).[4] They were taken over by the Romanian Air Force and used for training and auxiliary duties. Several aircraft were captured in Poland by the Germans or the Soviets, but were not used by them. No RWD-14b has survived.[4]
Technical description
Mixed construction braced
Operators
Specifications (RWD-14b)
Data from Polish Aircraft 1893–1939[6]
General characteristics
- Crew: 2
- Capacity: 475 kg (1,047.2 lb) useful load
- Length: 9 m (29 ft 6 in)
- Wingspan: 11.9 m (39 ft 1 in)
- Height: 3 m (9 ft 10 in)
- Wing area: 22 m2 (240 sq ft)
- Empty weight: 1,225 kg (2,701 lb)
- Gross weight: 1,700 kg (3,748 lb)
- Powerplant: 1 × PZL G-1620B Mors-II 9-cylinder air-cooled radial piston engine, 350 kW (470 hp) at 2,375 rpm for take-off
- 430 hp (321 kW) at 2,150 rpm at sea level
- Propellers: 2-bladed Szomański fixed-pitch propeller
Performance
- Maximum speed: 247 km/h (153 mph, 133 kn)
- Cruise speed: 232 km/h (144 mph, 125 kn)
- Stall speed: 80 km/h (50 mph, 43 kn) ca
- Range: 675 km (419 mi, 364 nmi)
- Service ceiling: 5,100 m (16,700 ft)
- Rate of climb: 6.1 m/s (1,200 ft/min)
- Wing loading: 77 kg/m2 (16 lb/sq ft)
Armament
- 1 × fixed, forward-firing wz.33 machine gun
- 1 × flexible, rearward-firing Vickers Kmachine gun for observer
See also
Aircraft of comparable role, configuration, and era
- Heinkel He 46
- Henschel Hs 126
- Breguet 270
- Potez 390
References
- Andrzej Glass (1977): "Polskie konstrukcje lotnicze 1893–1939" (Polish aviation constructions 1893–1939), WKiŁ, Warsaw (in Polish)
- Andrzej Morgała (2003): "Samoloty wojskowe w Polsce 1924–1939" (Military aircraft in Poland 1924–1939), Bellona, Warsaw, ISBN 83-11-09319-9(in Polish)
- Wojciech Mazur (2014): "Samoloty RWD.14 i LWS.3", series Wielki Leksykon Uzbrojenia Wrzesień 1939 no.39, Edipresse, Warsaw, ISBN 978-83-7769-587-6(in Polish)