TCDS 7G10

Page No. 1 2 Rev. No. 1 - FEDERAL AVIATION AGENCY 7G10 Revision 1 SLINGSBY Swallow Type T.45 May 22, 1964 TYPE CERTIFICATE DATA SHEET NO. 7G10 This data sheet which is a part of type certificate No. 7G10 prescribes conditions 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 Slingsby Sailplanes Ltd. Kirbymoorside York, England I Model Swallow Type T.45, Approved September 19, 1961 Airspeed limits Glide or dive 118 knots Airplane tow 69 knots Auto-winch tow 64 knots Maximum speed in rough air 69 knots Dive brakes extended 118 knots C.G. range (+19.2) to (+23.2) Datum Wing leading edge at root Leveling means The fuselage horizontal datum is level when the top of the rear fuselage slopes tail down at 3°5’. Maximum weight 700 lb. No. of seats 1 Baggage None Control surface Movements Elevator Up 14°42’ Down 22°30’ Rudder Right 25°20’ Left 25°20’ Aileron Up 25°18’ Down 12°26’ Dive brakes 5.90" above and 5.70" below wing surfaces Serial Nos. eligible The United Kingdom Certificate of Airworthiness for Export endorsed as noted under "Certification basis" must be submitted for each individual glider for which application for certification is made. Certification basis CAR 10. Type Certificate No. 7G10 issued September 19, 1961. Date of Application for Type Certificate August 22, 1961. Each glider and any replacement parts manufactured in the United Kingdom must be designated as "import" and clearly labeled as such in accordance with CAR 10.30. A U.S. Airworthiness Certificate may be issued on the basis of a United Kingdom Certificate of Airworthiness for Export signed by a representative of the Ministry of Transport and Civil Aviation containing the following notation: "The glider covered by this certificate has been examined and found to comply with the British Glider Airworthiness Requirements and conforms to T.C. 7G10." 7G10 2 Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification basis) must be installed in the aircraft for certification. NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary, must be provided for 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 the following instruments of an approved type are installed: Altimeter and Turn and Bank." (b) "The following aerobatic maneuvers are permitted: loops, stall turns, tight turns (3 1/2g), spins." (c) "When flying in rough air the speed is not to exceed 69 knots." (d) "Night flying is prohibited." ...END...