BGA glider data sheet - Pirat (SZD 30) Data source: BGA data sheet & Manufacturer’s manuals Date of issue: 1973 Manufacturer: PZL Poland Type approval holder: Zaklad Szybowcowy “Jezow” Henryk Mynarski, Ul.Dlugu 93, 58-521 Jezow, Sudelki, Poland. szd_jezow@szdjezow.pl Weighing Data: Kg Pounds Control deflections in mm Up Down Measuring point Max all up weight 370 815 BGA concession non-aerobatic max all up weight [+3%] 381 839 Max pilot weight (seat load) 115 253 (Pilot + Parachute + Disposable Load) mm Inches Forward C of G limit (aft of datum) 270 10.63 Aft C of G limit (aft of datum) 416 16.38 Pilot position (forward) 277 10.9 Ailerons 124-140 65 - 73 Root TE Elevator Trim Tab Small rudder Large rudder 67-75 8 - 10 Left & right Left & right 64-72 Centre TE 18 - 22 Centre TE 340 - Rear TE 370 (Chord~620) 440 - Rear TE 470 (Chord 770) Airbrakes 155-165 165-175 Top of blade to Top Bottom wing surface Longitudinal datum: Wing root LE Horizontal datum: Rear fuselage datum mark 250mm higher than front one. Front mark is approximately 300mm forward of the canopy’s front edge. The rear mark is near the rear carrying handle. Maximum speeds Knots Kph Knots Kph VNE 105 195 Winch / auto tow 65 120 Rough air* Manoeuvre 72 72 135 135 Airbrake extension or retraction 81 150 Aerotow 75 140 Airbrake extension or retraction in rough air 73 135 *Note, Rough air is defined as maximum gusts of up to ± 10 m/s Turbulent conditions are defined as gusts of > ± 10 m/s. Flight in turbulent conditions is prohibited. Non aerobatic, cloud flying not permitted. Max load factors +4 & -1.5 Max winch weak link BGA figure: 600 kg (Blue) Tyre pressure:Main Wheel 26 psi (1.8 Bar) EASA approval AP143 TCDS BG-32/2 (25 March 2002) This sheet compiled by: Tim Macfadyen & James Hunneman (James_Hunneman@msn.com) : 4 Oct 2005 Updated 26 July 2011:- Speeds & limitations reduced as EASA AD 2011-0089 & BE-035/30/2010, Type approval holder changed. Last update 5 July 2012:- Rudder deflections corrected as per BE-032/92