BGA glider data sheet - AC-5t - Not a BGA certified type This glider has a self sustaining SOLO 210cc (15 HP) engine Data source: Manufacturer’s data Date of issue: Manufacturer: Avia Stroitel ltd UK Agent: Web site: Phone: Link to mandatory mods: Fax: Weighing Data: Kg Pounds Max weight (dry) 300 662 Max pilot weight (seat load) Forward C of G limit (aft of datum) Aft C of G limit (aft of datum) Tall pilot position (forward)* Short pilot position (forward)* mm 127 267 380 440 Inches 5.00 10.51 15.0 17.3 Control deflections in mm Up Down Distance - hinge to measuring point Ailerons Elevator Max free play Rudder *It is strongly recommended that the glider is weighed with the pilot in due to the large effect that the pilot size and weight has on the C of G position of this small and light glider. Longitudinal datum: Wing root LE Horizontal datum: Rear fuselage top 1000:90 tail down The 2 nose weights weigh 3.6 kg (8 lb) each and are 1200 mm forward of datum. Maximum speeds Knots Kph Knots Kph Altitude feet VNE** Rough air Manoeuvre Aerotow **119 87 87 87 220 161 161 161 Winch / auto tow Airbrakes open U/C operation Engine operation 60 97 87 45 - 55 111 180 161 83 - 102 6500 - 9800 9800 - 13100 13100 - 16400 16400 - 19600 VNE knots 112** 106** 100** 95** **VNE is presently limited to 87 Knots by BGA Mod 035/02/2003 Max winch weak link: 500 Kg (White) Tyre pressure: Main 29 psi (2 Bar), rear 22 psi (1.5 bar) Aerobatics and cloud flying are prohibited Span 12.6 meters Fuel tank capacity 10 litres, mixture 50:1 Unleaded fuel, min 91 octane, synthetic 2 stroke oil Max RPM 5500 for 5 minutes, 5000 continuous. Max cylinder head temp 500°F This sheet compiled by: Tim Macfadyen Date: 7 Feb 2003 Page 6 of 218