BGA glider data sheet - Mosquito A & B Data source Manufacturers’ Handbook Date of issue: Manufacturer: Glasflügel Web site: Phone: Fax: Agent: H G Streifeneder, Glasfaser-Flügzeug-Service, Brühlstrasse 12, 7318-Lenningen 2, Germany Link to mandatory mods: Weighing Data: Control deflections in mm Max weight (dry) Kg Pounds 380 838 Up Down Distance - Max hinge to free measuring point play BGA concession non-aerobatic max weight (dry) [+3%] Max weight with water 391 863 450 992 Ailerons 33 ±3 14 ±2 81 (tip) Flaps neutral ±3 At root Max landing weight 380 Max weight of non lifting 240 components (everything except wings) 838 529 Elevator 41±5 41±5 138 ±2 at centre BGA concession non-aerobatic max weight of non lifting components [+5%] Max pilot weight (seat load) 252 556 110 242 C of G limits (aft of datum) mm Forward C of G limit Mosquito A 235 Aft C of G limit Mosquito A 360 Forward C of G limit Mosquito B 200 Aft C of G limit Mosquito B 325 Pilot position (forward of datum) 440 inches 9.25 14.17 7.87 12.80 17.32 Airbrakes 60° ±3° Rudder Flaps 117 ± 9 Left & Right 28 42 ±3,5 ±3,5 120±5 270 220 ±2 fully open ±5 at bottom ±3 at 141 rad Longitudinal datum: Wing root LE (425mm from fuselage centre). Horizontal datum: Rear fuselage top 1000:52 tail down Minimum gap between flaps and ailerons 4,5mm Maximum speeds Knots Kph Knots Kph VNE 135 250 Aerotow 81 150 Rough air 108 200 Winch / auto tow 81 150 Manoeuvre Flaps +1 & +2 108 200 Max winch weak link: 650 Kg [Blue] Tyre pressure:Main wheel 36/50 psi [2,5/3,5 bar] without water ballast/with water ballast Tail wheel 22 psi [1,5 bar] Semi aerobatic. Cloud flying permitted. Brake/flap gas strut - With the flaps set to -2 the torque to move the flap down is 23-26 Nm [17-19 ft-lb]. Rig the glider with the flaps set to -2, the brake handle in the middle and the flaps lifted. CAIR Aviation “Ottfur” hook(s) may be fitted in place of the original hooks. This sheet compiled by: Tim Macfadyen Last update: 27 April 2009 (CAIR Aviation hooks added) Page 156 of 226