Allstar SZD-54 Perkoz

The Allstar SZD-54 Perkoz (English: Grebe) is a Polish two-seat, glider, designed and produced by Allstar PZL Glider of Bielsko-Biała.[1]

SZD-54 Perkoz
SZD-54 Perkoz in front of the Tatra Mountains
Role Glider
National origin Poland
Manufacturer Allstar PZL Glider
Status In production (2011)
Produced 2011-present
Unit cost
€74,950 (2011)[1]

Design and development

The SZD-54 was designed in 1991, but company and political upheaval in Poland resulted in the glider not being put into production until 2011.[1]

The aircraft is type certified to European Aviation Safety Agency CS22 standards. It features a cantilever mid-wing, a two-seats-in-tandem enclosed cockpit under a large bubble canopy and fixed monowheel gear with a small nosewheel and a tail caster.[1]

The aircraft is made predominantly from fibreglass. Its 20 m (65.6 ft) span wing has an area of 17.82 m2 (191.8 sq ft) and mounts air brakes, as well as winglets. Optional wing tips are available for 17.5 m (57.4 ft) with winglets in the utility category and without winglets for aerobatics. All controls are automatically connected upon assembly. Despite its fixed landing gear, the SZD-54 has a best glide ratio of 42:1 with the 20 m (65.6 ft) span wing.[1]

The SZD-54 has a design airframe life of 15,000 flight hours, but is approved for 3,000 hours and comes from the factory with a two-year warranty.[2]

Operational history

By November 2012 two examples had been registered in the United States with the Federal Aviation Administration.[3]

In December 2017, the Colombian Air Force had received two SZD-54-2 gliders for training purposes.[4]

Specifications (SZD-54-2, 20 m configuration)
SZD-54 Perkoz

Data from Bayerl and Allstar[1][5]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 8.25 m (27 ft 1 in)
  • Wingspan: 20 m (65 ft 7 in)
  • Height: 2.05 m (6 ft 9 in)
  • Wing area: 17.82 m2 (191.8 sq ft)
  • Aspect ratio: 24.75:1
  • Empty weight: 379 kg (836 lb)
  • Gross weight: 600 kg (1,323 lb)

Performance

  • Stall speed: 62 km/h (39 mph, 33 kn)
  • Never exceed speed: 240 km/h (150 mph, 130 kn)
  • g limits: +5.3/-2.65
  • Maximum glide ratio: 42:1 at 102 km/h (63 mph)
  • Rate of sink: 0.58 m/s (114 ft/min) at 78 km/h (48 mph)
  • Wing loading: 33.7 kg/m2 (6.9 lb/sq ft)

See also

Related lists

References
  1. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 150. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. Allstar PZL Glider Sp. z o.o. (n.d.). "SZD-54 Perkoz". Retrieved 13 December 2012.
  3. Federal Aviation Administration (13 December 2012). "Make / Model Inquiry Results". Retrieved 13 December 2012.
  4. Sanchez, Alejandro (20 December 2017). "Colombian Air Force receives new training aircraft". IHS Jane's 360. Archived from the original on 26 December 2017. Retrieved 26 December 2017.
  5. Allstar PZL Glider Sp. z o.o. (n.d.). "Allstar SZD-54 Perkoz" (PDF). Retrieved 13 December 2012.
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