TCDS G-20

Page No. 1 2 Rev. No. 1 1 FEDERAL AVIATION AGENCY G-20 Revision 1 SLINGSBY Type 41 Series 2 April 1, 1964 GLIDER SPECIFICATION G-20 Manufacturer Slingsby Sailplanes Ltd. Kirbymoorside, York, England I Model Skylark Type 41 Series 2, 1 PCLM, Approved July 28, 1955 Airspeed limits Glide or dive 120 mph True Ind. Airplane tow 75 mph True Ind. Auto-winch tow 65 mph True Ind. Drive brakes extended 120 mph True Ind. C.G. range (+13.5) to (+19.0) Maximum weight 680 lbs. No. seats 1 (+15.5) Baggage None Control surface Movements Elevator Up 25° 8' Down 28° 8' Rudder Right 25°20' Left 25°20' Aileron Up 24°44' Down 12°24' Dive brakes 5.1 in. above and below wing surfaces Serial Nos. eligible Each provided glider accompanied by United Kingdom certificate of airworthiness as indicated under "Certification basis" Required equipment Item 401 Specifications Pertinent to All Models Datum Wing leading edge at root Leveling means Glider level when top of rear fuselage slopes 1° tail down Certification basis Type Certificate No. G-20 issued under CAR 10. Airworthiness certificate may be issued on basis of a United Kingdom certificate of airworthiness signed by a representative of the Ministry of Transport and Civil Aviation. Equipment: Interior Equipment 401. Airspeed Indicator 402. Altimeter 403. Compass 404. Turn and Bank G20 2 NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, must be in each glider at the time of original certification and at all times thereafter. NOTE 2. The following placards must be installed in full view of the pilot: (a) "Flight in cloud is permitted provided that the following instruments of an approved type are installed: Altimeter and Turn and Bank indicator." (b) "The following acrobatic maneuvers are permitted: Loops, stall turns, tight turns and spins." (c) "Night flight is prohibited." ...END...