BGA glider data sheet - DG 202-17C (Carbon fibre version) See separate sheet for Glass fibre versions (DG 200/202-15 & 17) Data source: Manufacturer’s flight & maintenance manuals updated with TN 323-15 Manufacturer: Glaser-Dirks Flugzeugbau GmbH Web site dgflugzeugbau.de UK Agent: Bob McLean Phone: 01904 738653 Fax: 01904 738146 Link to mandatory mods: http://www.dg-flugzeugbau.de/tech-mitteilungen-e.html Weighing Data: Control deflections in mm Max weight with water Kg Pounds 15M 480 1058 17M 450 992 Up Down Distance - hinge to measuring point Max weight of non lifting 15M 240 529 components 17M 236 520 Ailerons 42±3 21±3 123 BGA concession non- 15M aerobatic max weight of non lifting components [+5%] 17M 252 248 555 546 Elevator 57±1 48±1 150 Max pilot weight (seat load) 110 242 Flap±12° 30±3 30±3 145 Max weight in baggage 15 compartment 33 Rudder Left & right 243±10 460 Controls max free play (controls central) mm Inches Aileron 2mm total with other aileron fixed. Forward C of G limit (aft of datum) 230 9.06 Flap 3mm total with other flap fixed. Aft C of G limit (aft of datum) 385 15.16 With one aileron fixed 3mm total at top of stick. Pilot position (forward of datum) 560- 22-23 580 With elevator fixed 3mm total at top of stick. Rudder vertical play 0,5mm. Longitudinal datum: Wing root LE Horizontal datum: Top of rear fuselage 1000:36.7 rear down The maximum dry weight limit was effectively removed by TN 323-15 which redefined the max dry weight as the max weight of the non lifting components (including pilot) + the weight of the wings. Knots Kph Maximum speeds Knots Kph VNE at altitude Knots Kph VNE 146 270 Winch / auto tow 70 130 0-6600 feet 146 270 Rough air 103 190 U/C down 103 190 6600–10 000 138 256 Manoeuvre 103 190 Flaps +4 & +8 103 190 10 000–13 000 131 243 Aerotow 103 190 Landing flap 80 150 13 000–16 000 124 230 16 000-20 000 117 218 Max winch weak link: 600 Kg (Tost blue) Tyre pressure:Main 42 psi (3 bar), rear 28 psi (2 bar) Semi aerobatic only in 15 meter span without water only. Cloud flying permitted. With a standard 2.2 Kg weight on the right of the panel, min cockpit weight is reduced 3.6 Kg (8 lb). Span 15 or 17 meters This sheet compiled by: Tim Macfadyen Date: 11 Feb 2008 Page 54 of 226