Main Menu

PZL Bielsko SZD-10 Czapla

PZL-Bielsko SZD-10bis Czapla
The Czapla (Heron) was a tandem two-seat training glider, with a strut- supported, forward-swept, high-set wing and a welded steel tube fuselage with fabric covering. Design of the Czapla commenced in 1952 to the order of the Soldier's Friends' League paramilitary organization, to enable aeroclubs to train glider pilots in a two-seat trainee/instructor system. Main designers were Roman Zatwarnicki, Irena Kaniewska and Marian Gracz. The Czapla was designed to be launched by bungee, winch or aero-tow, and the prototype first flew on 23 November 1953, demonstrating the need for several improvements, which were introduced in the second prototype (flown on 26 March 1954) and the production model SZD-10bis Czapla.
PZL-Bielsko SZD-10bis Czapla OH-204 / OH-KCC
Production was carried out from 1955 at ZSLS (ZSLS - sport aviation equipment workshops) in Krosno, Wrocław, Bielsko and Poznań and the Military Repair workshop at Łódź, with Czapla being used for everyday club flying up to the early 1980s, and exported to Finland and Turkey. A total of 157 were built.
SZD-10-2 Czapla
two prototypes
SZD-10bis Czapla
19 production aircraft
Wingspan: 16 m (52 ft 6 in)
Wing area: 24 m2 (258 ft2)
Wing profile: Göttingen 549
Aspect ratio: 10.67
Length: 8.7 m (28 ft 7 in)
Height: 1.98 m (6 ft 6 in)
Empty weight: 280 kg (617 lb)
Gross weight: 435 kg (959 lb)
Maximum speed: 160 km/h (99 mph)
Stall speed: 48 km/h (30 mph)
Maximum glide ratio: 17 @ 64 km/h (40 mph/35 kts)
Rate of sink: 0.96 m/s (189 ft/min)
Crew: 1 pilot
Capacity: 1 passenger
SZD-10bis A Czapla
136 production aircraft, first flew in June 1958

Copyright © 2021 all-aero. All Rights Reserved.
Joomla! is Free Software released under the GNU General Public License.