TCDS P1IN

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P1IN P1IN REVISION: 3 RATIER-FIGEAC FH-76 Series February 28, 2007 Propellers of models described herein conforming with this data sheet (which is a part of Propeller Type Certificate No. P1IN), and other approved data on file with the Federal Aviation Agency, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft Data Sheets and applicable portions of the Civil Air Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder RATIER-FIGEAC B .P. N°2 46101 FIGEAC Cedex F RANCE Type Turbine propeller, electrically controllable - feathering and reversing Engine shaft Integral with propeller hub barrel Hub material Steel Blade material Aluminum alloy No. of blades 3 Design series eligible FH 76-1-05, FH 76-1-06, FH 76-1-07, FH 76-1-09, FH 76-2-07 Blades Eligible Maximum Continuous Takeoff Diameter Max. Weight (See Note 2) HP RPM HP RPM Limits complete, lb. FH 76-205 473 2200 523 2200 83.5" - 82.5" 142.5 FH 76-206 473 2200 523 2200 75.6" - 74.6" 150.2 FH 76-207 473 2080 523 2080 98.4" - 97.4" 157.0 FH 76-209 473 2200 523 2200 81.1" - 80.1" 142.5 FH 76-2-260 630 2066 670 2066 98.51" - 98.43" 163.8 Certification basis FAR Section 21.29 and French Standard AIR 2051 Chapter 9. (AIR 2051 Chapter 9 certified by Secretariat Generale a l'Aviation Civile as equivalent to CAR Part 14 as amended to December 15, 1956, and Amendment 14-1). The FAA validated this product under U.S. Type Certificate Number P1IN. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the Government of France. TC (Import) No: None TC Application Date: September 19, 1960 TC Issued : November 9, 1962 Import requirements: To be considered eligible for installation on U.S. registered aircraft, each propeller to be exported to the United States shall be accompanied by a Certificate of Airworthiness for export endorsed by the Direction Générale de l’Aviation Civile (DGAC) on behalf of the European Community which contains the following language: (1) This propeller conforms to its United States type design (TC No. P1IN) and is Page No. 1 2 3 Rev. No. 3 3 3 P1IN 2 in a condition for safe operation. (2) This propeller has been subjected by th e manufacturer to a final operational check and is in a proper state of airworthine ss. Reference FAR Section 21.500 which provides for the airworthiness acceptance of aircraft engines or propellers manufactured outside the U.S. for which a U.S. type certificate has been issued. Additional guidance is contained in FAA Advisory Circular 21-23, Ai rworthiness Certification of Civil Aircraft, Engines, Propellers and Related Produc ts, Imported into the United States. NOTE 1. Propeller Model Designation. The propeller model designation consists of a series of numbers suffixed to the basic model designation (as shown below) to indicate Modifications and specifications. Basic model designation F H 76 - 2 - 07 A 1 2 3 4 Cuff Electrical pitch repeating instrument Deicing Removable hub Non de-iced propellers Specific design Basic modification Design series Propeller division Manufacturer NOTE 2. Blade Model Designation FH 76 2 2 60 Specific design Reference of corresponding subassembly drawing Basic propeller modification Basic model designation NOTE 3. Pitch Control. 76-1 Series eligible with Ratier-Figeac mechanical-electrical pitch control and indicator system No. FH 76.1.500 or in addition electrical pitch repeater No. FH 138.550.76-2-07 eligible with No. FH 76-2-500. NOTE 4. (a) Feathering Electrical feathering is accomplished with control in cockpit which also shuts off fuel to engine and is installed in accordance with the propeller manufacturer's instructions. Emergency hydraulic feathering is also available with special pilot control provided by aircraft manufacturer. (b) Reversing Reversing is accomplished with the propeller pitch changing control designed to prevent inadvertent operation. NOTE 5. Not applicable. NOTE 6. Interchangeable Blades Only blades that can be fitted without requiring re-balance or any other testing are eligible as interchangeable blades, provided they are installed as a set of 3 to the propeller. NOTE 7. Accessories (a) Propeller Deicing Eligible with only Ratier-Figeac electrical deicing provisions. 3 P1IN (b) Spinners Eligible with only Ratier-Figeac spinner. (c) Relay Box Not applicable (76-1; all types). Eligible only with Ratier-Forest electric Relay Box Model FH 170-1. (76-2-07) NOTE 8. Not applicable. NOTE 9. Approved installations. Propellers listed in this data sheet are approved vibrationwise only for use in the engine-aircraft combinations shown below: Propeller Aircraft Engine Data Sheet Model Model Model Aircraft Engine FH 76-1-06 Beech-Sferma 60 Turbomeca Astazou II D, II-J A9IN E2IN FH 76-1-07 Pilatus PC-6/A Series Turbomeca Astazou II E, IIG 7A15 E2IN FH 76-2-07 Short Bros. & Harland SC-7 Skyvan Turbomeca Astazou XIIH-1 A15EU E6EU NOTE 10. Service Information. Each of the documents listed below must state that it is approved by the European Aviation Safety Agency (EASA) or – for approvals made before September 28, 2003 – by the DGAC. Any such documents are accepted by the FAA and are considered FAA approved. • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. .....END.....