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PZL SZD-30 Pirat
Polish single-seat glider, 1966 From Wikipedia, the free encyclopedia
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The SZD-30 Pirat is a single-seat multipurpose glider aircraft from the Polish firm PZL Bielsko which first flew in 1966,[1] and began production in 1967.[2]
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Development
The SZD-30 is largely constructed out of wood.[1] The high-mounted wing incorporates air brakes on both the upper and lower surfaces. The inner section of the wing is constant-chord and the outer section is tapered.[3]
The forward section of the otherwise all-wood fuselage is made of fiberglass.[1] The single-wheel main landing gear is fixed, the formed one-piece canopy is side-mounted,[4] the fuselage can be equipped with radios and an oxygen system. There are also two baggage compartments.[4]
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Variants
Operational limitations
In 2011, following a number of cases of glue failure in the wooden joints, leading to structural failure, the type certificate holder issued a bulletin which reduced a number of the limiting speeds of the aircraft. Specifically, the maximum speed (VNE) was reduced to 195 km/h (121 mph, 105 knots) and aerobatic flight was prohibited.
Specifications
Data from Australian Gliding Museum [7]
General characteristics
- Crew: 1
- Length: 6.86 m (22 ft 6 in)
- Wingspan: 15.00 m (49 ft 3 in)
- Height: 0.96 m (3 ft 2 in)
- Wing area: 13.8 m2 (148.5 sq ft)
- Aspect ratio: 16.3
- Airfoil: FX-61-168/60-1261
- Empty weight: 260 kg (573 lb)
- Gross weight: 370 kg (816 lb)
Performance
- Maximum speed: 250 km/h (155 mph, 135 kn)
- Stall speed: 60.2 km/h (37.4 mph, 32.5 kn)
- Maximum glide ratio: 33
- Rate of sink: 0.70 m/s (138 ft/min)
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See also
References
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