BGA glider data sheet - ASW 20 B & BL Data source Schleicher Manual Date of issue: 7/4/1983 Manufacturer: Schleicher Web site: Phone: Fax: UK Agent: Peter Wells Link to mandatory mods: E Mail: zuluglasstek@clara.net Phone:01844 208 157 Fax: 01844 201 028 URL : http://www.as-segelflugzeuge.de/englisch/e_main.htm Weighing Data: Control deflections in mm Kg Pounds Max weight with water ASW 20 B 525 1158 ASW 20 BL 430 948 Up Down Distance - Max hinge to measuring point free play Max weight of non lifting 245 540 components (everything except wings) Ailerons See separate sheet 79 1,75 total BGA concession non-aerobatic max weight of non lifting components [+5%] Max pilot weight (seat load) 257 567 115 254 Elevator Rudder 64± 10 Left 160 ±15 53 ±5 Right 160 ±15 154 310 3 total 4,5 total Flaps See separate 148 sheet 2,75 total Weight Kg Balance cm kg Rudder 2,25 - 2,65 6,57 - 9,13 mm Inches Elevator (half) 0,70 - 0,90 1,70 - 2,20 Forward C of G limit (aft of datum) 240 9,45 Elevator actuator 0,21 - 0,27 1,00 - 1,20 Aft C of G limit (aft of datum) 360 14,17 Aileron 1,76 - 2,1 1,88 - 2,53 Light pilot position (forward) 625 24.6 Flap 3,64 - 4,46 7,07 - 9,23 Heavy pilot position (forward) 550 21.65 Aileron extensions 0,23 - 0,29 0,56 - 0,66 Longitudinal datum: Wing root LE (not the fairing). Horizontal datum: Rear fuselage top 1000: 45 tail down Maximum speeds Kts Kph BB VNE Rough air Manoeuvre U/C down Aerotow 151 280 103 190 103 190 103 190 103 190 Kts Kph BL BL 143 265 92 170 92 170 92 170 92 170 Kts Kph Winch / auto tow Flaps pos 2 & 3 Flaps position 4 Landing flaps 70 119 92 70 130 220 170 130 Height feet 10 000 + 16 400 + 23 000 + 29 500 + 36 000 to 42 600 VNE kts B 130 116 105 92 78 VNE Kph B 240 215 195 170 145 VNE kts BL VNE Kph BL Max winch weak link: 600 Kg (Blue) Tyre pressure: 2,3 - 2,6 Bar Main and tail wheel Semi aerobatic in 15 meter form without water. Cloud flying is permitted The Hydraulic brake fluid is Aeroshell Fluid 4 or Esso Univis J-13. Theses fluids are mineral based and are very corrosive. The 1 kg trim disks in the nose each reduce the min cockpit load by 2,5 Kg (5 ½ lb) This sheet compiled by Tim Macfadyen Last up-date 2 Jan 08 (Speed data for 15 Meter version added) Page 27 of 224