BGA glider data sheet - Nimbus 3DT (two seat “turbo” 25.6 meter span) Data source: Flight Manual (Nov 1987) & Maintenance Manual Rev 12 (Dec 1999) Manufacturer: Schempp Hirth, Flugzeugbau GmbH, Postfach 1443, D-73222 Kirchheim/Teck, Germany Phone: 00 49 7021 7298-0 Fax: 00 49 7021 7298-199 www.schempp-hirth.com UK Agent: Southern Sailplanes Phone: 0148 871774 Weighing Data: Control deflections in mm Max weight (with water) Kg Pounds 800 1764 Up Down Distance - Max hinge to free measuring point play Max landing weight Max pilot weight (seat load) 800 1764 110 242 Ailerons 28 Flaps +2 ±5 14 ±3 141 3 mm total Max weight of non lifting 450 992 components (everything except wings) Elevator 51 ±5 51 ±5 167 3 mm total mm Inches Forward C of G limit (aft of datum) 20 0.79 Aft C of G limit (aft of datum) 200 7.87 Front pilot (forward of datum) 1468 57.8 Rear pilot (forward of datum) 339 13.35 Each standard nose weight reduces min front pilot weight by 5 Kg. Rudder Flaps -2 0 L L & brakes Left Right 190 190 ±20 ±20 32 ± 5 Up 0 42 ± 5 down 110±12 down 410 185 3 mm total Spoileron 75±10 up 53 Measure spoileron with flaps L and full aileron Longitudinal datum: Wing root LE root rib. Horizontal datum: Rear fuselage top 1000:45 tail down The main wheel is on datum (a = 0). Main wheel to tail skid (b) 5290mm. Main wheel to tail wheel is 5252mm. The fuel is 291mm aft. Upper tank 16 litres (15 useable, lower tank 14 litres (13.5 useable). The fin tank is 5290mm aft, max capacity 5 Kg. Engine is 1110mm aft of datum. Max fore & aft play of wing tip 30mm Maximum speeds Controls Weights and balance Knots Kph VNE at altitude see Maintenance Manual page 2.2.1 VNE 148 275 Height in feet Knots Kph Rough air 103 190 10 000 142 263 Aerotow 97 180 13 000 134 249 U/C down 97 180 16 500 127 236 Winch / auto tow 81 150 20 000 23 000 121 224 114 212 Flaps +2, +1 & 0 Flaps “L” 86 76 160 140 26 000 29 500 108 200 102 188 Engine out 73 135 33 000 96 177 39 500 83 154 Max winch weak link: 1040 daN (black) Tyre pressures: Main 57 psi (4 Bar) Tail 43 psi (3 bar) Non aerobatic, intentional spinning prohibited. Cloud flying is not permitted. Fuel is 2 stroke min RON 96. Fuel oil mixture 30:1. Oil is Castrol Super TT two stroke oil. Brake fluid SAE - J 1703 or US specification FMVVS 116, DOT 3 resp. DOT 4 This sheet compiled by: Tim Macfadyen Date: 14 May 2002 Latest update 14 April 2015 Cloud flying not permitted, previously allowed in error. Ref BGA Technical Committee meeting 11/4/2015