BGA glider data sheet - Nimbus 4T (single seat “turbo” 26.4 meter span) Data source: BGA data sheet Date of issue: 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 Fax: Weighing Data: Control deflections in mm Max weight (with water) Kg Pounds 800 1764 Up Down Distance - Max hinge to measuring point free play Max landing weight Max pilot weight (seat load) 750 1654 110 242 Ailerons Flaps +2 mm total Max weight of non lifting components (everything except wings) Elevator mm total Forward C of G limit (aft of datum) Aft C of G limit (aft) Pilot (forward of datum) mm Inches Each standard nose weight reduced min pilot weight by Kg. Rudder Left Right Flaps -2 0 L L & brakes Up down down mm total Spoileron up Measure spoileron with flaps L and full aileron Longitudinal datum: Wing root LE root rib. Horizontal datum: Rear fuselage top 1000: tail down The main wheel is mm aft of datum (a). Main wheel to tail skid (b) mm. Main wheel to tail wheel is mm. The fuel is mm aft. Upper tank litres (useable, lower tank litres (useable). The fin tank is mm aft, max capacity Kg. Engine is mm aft of datum. Max fore & aft play of wing tip mm Maximum speeds Controls Weights VNE Knots 154 Kph 285 VNE at altitude Height in feet Knots Kph Rudder Weight Kg Balance cm Kg Rough air 97 180 10 000 Elevator without fitting Aerotow 97 180 13 000 Flap U/C down 97 180 16 500 Inboard aileron Winch / 81 150 20 000 auto tow 23 000 Middle aileron Outboard aileron Flaps +2, +1 & 0 26 000 Tip aileron Flaps “L” 29 500 Engine limitations Engine out 33 000 Max cylinder head temp °C 39 500 Max engine speed RPM 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 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: 19 Feb 2003 Page 163 of 218