TCDS P-900

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P-900 P-900 REVISION: 6 de HAVILLAND MODEL/S: PD-/4N6/- March 12, 2007 Propellers of models described herein conforming with this data sheet (which is a part of type certificate No. P-900) 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 Hawker Siddeley Dynamics Limited Manor Road Hatfield, Hertfordshire, England Type Constant Speed; hydraulic. (See NOTES 3 and 4) Engine Shaft No. 6. S.B.A.C. Hub Material Steel Blade Material Steel (with internal rubber filler) Number of blades 4 Propeller Types eligible PD202/4N6/ (See NOTE 1) Blade Assemblies Maximum Eligible Continuous Takeoff Nominal Hub and (See NOTES 1 & 2) HP RPM HP RPM Diameter Blade Weight PP16N1062A-X 3420 920 3840 1000 16'0" 759 lb. Certification basis CAR 10. Type Certificate No. P-900 The FAA validated this product under U.S. Type Certificate Number P-900. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the United Kingdom of Great Britain and Northern Ireland. TC (Import) No: None TC Application Date: August 23, 1955 TC Issued : September 10, 1957 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 UKCAA on behalf of the European Community which contains the following language: (1) This propeller conforms to its United States type design (TC No. P-900) and is in a condition for safe operation. (2) This propeller has been subjected by the manufacturer to a final operational check and is in a proper state of airworthiness. 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, Airworthiness Certification of Civil Aircraft, Engines, Propellers and Related Products, Imported into the United States. Each individually imported propeller and replacement parts must be accompanied by the pertinent Inspection Certificate and Approved Certificate and be clearly identified as imported. Page No. 1 2 3 Rev. No. 6 6 6 P-900 Page 2 of 3 NOTE 1. Propeller Type Designation. Propeller type designation PD 202/ 4 N 6/ 1 Minor change not affecting eligibility S.B.A.C. Propeller Shaft Size Blade Shank Size Number of Blades Major Model Type Civil Type of Propeller Propeller Blade Assembly Cuff Plating Type Numbers Standard Standard PD202/4N6/1 PP16N1062A-8 Hard Rubber Zinc PD202/4N6/1 PP16N1062A-11 Hard Rubber Zinc PD202/4N6/1 PP16N1062A-14 Soft Rubber Zinc PD202/4N6/2 PP16N1062A-12 Hard Rubber Nickel PD202/4N6/2 PP16N1062A-15 Soft Rubber Nickel NOTE 2. Blade Assembly Designation Blade Model Designation PP 16 N 10 62 A-15 Blade Assembly Model Designation Direction of Rotation and Reduction from Basic Diameter.* Major Aerodynamic Characteristics Blade Shank Size Blade Root Model Designation Civil Type of Propeller Blade *Numbers 00 indicate a right hand rotation. Numbers 50 indicate a left hand rotation. The reduction from basic diameter in inches is added to the above numbers, so that 62 corresponds to 12 ins. reduction from the basic blade diameter with a left hand rotation. NOTE 3. Pitch Control. Eligible with de Havilland Constant Speed Unit Governor only. NOTE 4. (a) Feathering. Eligible with full feathering control installed in accordance with the propeller manufacturer's instructions. (b) Reversing. Eligible with reversing controls installed in accordance with the manufacturer's instructions. NOTE 5. Not applicable. NOTE 6. Interchangeable Blades. None. Page 3 of 3 P-900 NOTE 7. Accessories. (1) Propeller Deicing. Eligible only with de Havilland electrical deicing equipment installed in accordance with the manufacturer's instructions. Weight per propeller, 44 lb. (2) Propeller Spinner. Eligible with spinner supplied by de Havilland Propellers. Weight, 25-1/2 lb. NOTE 8. Not applicable. NOTE 9. Approved Installations. Propellers listed in this data sheet are approved only for use in the engine-aircraft combinations shown below: Propeller Aircraft Engine FAA Data Sheet Model Model Model Aircraft Engine *PD202/4N6/1 & 2 Britannia 305 Proteus 756 7A2 E-296 *This approval is conditioned upon the following r.p.m. limitations being observed: Ground running: Continuous operation prohibited between 590 and 750 propeller r.p.m. Flight: Continuous operation prohibited between 530 and 680 propeller r.p.m. 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 UKCAA. 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...