TCDS G3IN

Page No. 1 2 Rev. No. - - DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION G3IN ELLIOTTS EON 460 Series 1 April 1, 1963 TYPE CERTIFICATE DATA SHEET NO. G3IN This data sheet which is a part of type certificate No. G3IN prescribes conditi ons and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder Elliotts of Newbury Ltd. Newbury, Berkshire, England I - Model EON 460 Series 1, approved February 25, 1963 Airspeed limits Glide or dive 118 knots (136 m.p.h.) (indicated airspeed) Airpla ne tow 82 knots (94 m.p.h.) Auto-winch tow 65 knots (75 m.p.h.) Maximum speed in rough air 74 knots (85 m.p.h.) Airbrakes extended 118 knots (136 m.p.h.) C.G. range (-1.5) to (+2.8) Datum Centre line of wing main spar Leveling means Straight e dge across mainplane joint pins at main and rear spar joints Maximum weight 630 lb. No. of seats 1 (-22.5) Baggage None Control surface movements Elevator Up 22° Down 22° Elevator trim tab Up 10° Down 30° Rudder Right 25° Left 25° Aileron Up 28° Down 12 1/2° Airbrakes 5.75" above and below wing surfaces Serial Nos. eligible The United Kingdom Certificate of Airworthiness for export endorsed as noted below under "Certification basis" must be s ubmitted for each individual glider for which application for certification is made. G31N 2 Certification basis CAR 10. Type Certif icate No. G3IN, issued February 25, 1963 Application for Type Cer tificate dated November 14, 1961. Each glider and any replacement parts manufactured in the United Kingdom must be clearly labeled as imported. A U.S. Airworthiness Certificate may be issued on the basis of a United Kingdom Certificate of Airworthiness signed by a representative of the Ministry of Aviation, containing the following statement: "The glider covered by this certificate has been examined and found to comply with British Civil Airworthiness Requirements for gliders current on 1st January 1960 and confor ms to T.C. G3IN." This certification is equivalent to CAR 5 effective February 15, 1956. Equipment: The basic required equipment as prescr ibed in the applicable airworthiness regulations (see Certification basis) must be in stalled in the glider for certification. NOTE 1: Current weight and balance re port including list of equipment included in certificated empty weight, must be in each glider at the time of original certification. NOTE 2: The following placards must be in stalled in full view of the pilot: (a) "Flight in cloud perm issible only when altimeter and turn and bank indicators of an approved type are installed." (b) "Maneuvers permitted - Tight turn s, stall turns, inside loops, spins." (c) "Night flyi ng is prohibited." (d) "When flying in rough air the speed is not to exceed 74 knots IAS." ...END...