TCDS P14NE

Page No. 1 2 Rev. No. 1 1 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P14NE HARTZELL HC-A6A Revision 1 August 10, 1990 TYPE CERTIFICATE DATA SHEET NO. P14NE Propellers of models described herein conforming with this data sheet, (which is part of Type Certificate No. P14NE) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations provided they are installed, operated and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Hartzell Propeller Inc. Piqua, Ohio 45356 Type Constant speed; hydraulic (See NOTES 3 and 4) Engine flange Special flange 5-1/8" bolt circle with twelve 9/16" bolts Hub material Aluminum alloy Blade material See below Number of blades Six Hubs eligible HC-A6A-3 Blades Maximum Approx. Max. Wt. Complete Eligible Continuous Takeoff Diameter (For Reference Only) Blade (See NOTE 2) HP RPM HP RPM Limits (See NOTES 3 and 7) Construction A10460 1492 1700 1492 1700 108" 184 lb. Aramid Composite Certification Basis Federal Aviation Regulations Part 35 effective October 14, 1980, with Amendments 1 through 5 Type Certificate No. P14NE issued February 27, 1987 Date of Application for Type Certificate October 31, 1985 Production Basis Production Certificate No. 10 NOTE 1. Hub Model Designation. Hub model designation HC - A 6 A - 3 A Denotes minor change not affecting eligibility Denotes specific design features (See NOTE 4) A denotes Special Flange 5-1/8" bolt circle with twelve 9/16" bolts and two 5/8" dowel holes Number of blades Identifies basic design Hartzell controllable P14NE 2 NOTE 2. Blade Model Designation. Blade model designation A 104 60 E K An external de-ice element is installed An internal de-ice element is installed Basic model or template Basic diameter in inches Blade shank configuration NOTE 3. Pitch Control. Eligible with the following governors: Woodward Model x210xxx or x210x-xxx series Maximum Out-Put Pressure 800 PSI NOTE 4. (1) Feathering. The -3 model incorporates feathering and unfeathering features. (2) Reversing. The -3 model is approved for installation as a reversing propeller with appropriate reversing controls. NOTE 5. Left-Hand Models. The left-hand version of an approved model propeller is approved at the same rating and diameter as listed for right-hand model. (See NOTES 1 and 2.) NOTE 6. Interchangeability: Not applicable. NOTE 7. Accessories. (a) Propeller Spinner (1) With Hartzell spinners (weight of spinner extra). (b) Propeller Deicing. (1) With Goodrich 77-xxx or 65-xxx or 67-xxx deicing kit when installed in accordance with manufacturer's instructions (Goodrich Report 59-728) ( ); or Goodrich Drawing No. 7E-1633 NOTE 8. Shank Fairings. Not applicable NOTE 9. Special Limits. Not applicable NOTE 10. Special Notes. Aircraft installation must be approved as part of the aircraft type certificate upon compliance with the applicable aircraft airworthiness requirements. ...END...