BGA glider data sheet - Ventus 2c 15 & 18 meter Turbo Data source: Flight Manuals Date of issue: Nov 2003, updated to 1 Jan 2015 Manufacturer: Schempp Hirth, Flugzeugbau GmbH, Postfach 1443, D-73222 Kirchheim/Teck, Germany Phone: 00 49 7021 7298-0 www.schempp-hirth.com UK Agent: Southern Sailplanes Phone: 0148 871774 Weighing Data: Control deflections in mm Kg Pounds Up Down Distance - hinge to measuring point Max weight with water 15 M 525 1157 Elevator 54±2 50±4 161 Max weight with water 18 M 600 1323 Ailerons 34±3 26±3 131 Max weight of non-lifting components (everything except wings) Max mass baggage compartment 310 2 Max water capacity (approximately) 174 Max pilot weight (seat load) 110 682 4.4 383 242 Free-play - inboard ailerons ±2, between inboard and mid ailerons ±2, between mid and outboard ±1. Rudder Flaps S1 0° L Left & Right 160±20 31 ± 2 up 0±2 24 ± 2 down 340 131 Weight kg Moment kg cm Elevator half 0.72 - 0.88 2. 5 - 3.5 Rudder 4.0 - 5.0 -2.0 - 2.1 mm inches Flap/inner aileron Mid aileron 1.4 - 1.85 2.0 - 2.5 6.5 - 8.5 2.7 - 3.5 Forward C of G limit (aft of datum) 260 10.24 Outer ailerons 15m 0.54 - 0.66 1.5 - 1.9 Aft C of G limit (aft of datum) 380 14.96 Outer ailerons 18m 0.7 - 0.9 2.1 - 2.7 Pilot position (forward of datum) 520 20.47 Tip ailerons 18m 0.18 - 0.23 0.45 - 0.55 Longitudinal datum: Wing root LE Horizontal datum: Rear fuselage top tail down 1000:44 Max fore & aft play at the wing tip 30mm. The water in the wings is 179mm aft of datum. Distance datum to wheel (a) 100mm. Distance wheel to tail skid/wheel (b) 4145mm. Fin water & battery are 4275mm aft, nose weights are 1740mm forward, battery at panel is 1095mm fwd. The three nose weights each weigh 2.1 kg (4.6 lb). Each reduces minimum cockpit load by 5 kg (11 lb). Maximum speeds VNE at altitude Knots Kph Height (Meters) Height (feet) Knots Kph VNE 154 285 3000 10 000 144 266 Rough air 108 200 4 000 13 000 136 253 Manoeuvre 108 200 5 000 6 500 129 240 Aerotow 97 180 6 000 20 000 122 227 Winch / auto tow` 81 150 7 000 23 000 116 215 Flaps 0, +1, +2 & L 108 200 8 000 26 000 109 203 U/C operating Engine extended ignition on 97 81 180 150 9 000 10 000 30 000 33 000 103 191 97 180 Engine extended ignition off 97 180 Extending/retracting engine 65 120 Max winch weak link: 750 daN (Tost Red) Early models may be different, check flight manuals. Tyre pressure: 4 bar (58 psi). Tail wheel 2 bar (29 psi) Category “Utility” Aerobatic manoeuvres and cloud flying not approved. LBA Type certificate number 349 The hydraulic wheel brake takes Dot 3/Dot 5 brake fluid. This sheet compiled by: Tim Macfadyen 29 April 2015