PZL SZD-30 Pirat
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| SZD-30 Pirat | |
|---|---|
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| SZD-30 Pirat at EPSU, August 2007 | |
| Role | Club-class, formerly Standard-class sailplane |
| National origin | Poland |
| Manufacturer | PZL Bielsko |
| Designer | Jerzy Smielkiewicz |
| First flight | 19 May 1966 |
| Introduction | 1967 |
| Number built | 776 (1967-1980) |
The SZD-30 Pirat is a single-seat multi-purpose glider aircraft from the Polish firm PZL Bielsko, which first flew in 1966 and began to be produced in 1967.
Development
The SZD-30 is of wooden construction. The high-mounted wing incorporates air brakes on both upper and lower surfaces. The inner section of the wing is constant-chord and the outer section is tapered.
The forward section of the otherwise all-wood fuselage is made of fiberglass. The single-wheel main landing gear is fixed. The formed one-piece canopy is side-mounted. The fuselage can be equipped with radios and oxygen system. There are two baggage compartments.
Variants
- SZD-30 - Initial production version
- SZD-30B - A single prototype
- SZD-30C - Later production version, with smaller partially balanced ailerons of fiberglass, and larger cockpit. The first -30C flew on 10 January 1978.
Specifications
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)
Operational Limitations
In 2011, following a number of cases of glue failure in wooden joints leading to structural failure, the type certificate holder issued a bulletin which reduces a number of the limiting speeds of the aircraft. Specifically, the maximum speed (VNE) is reduced to 195 km/h (121 mph, 105 knots) and aerobatic flight is prohibited.
References
