TCDS P00014WI

Page No. 1 2 3 Rev. No. 1 0 0 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P00014WI Revision 1 McCauley [X]3A37C(34--) March 31, 2015 TYPE CERTIFICATE DATA SHEET NO. P00014WI Propellers of models described herein conforming with this data sheet, which is part of Type Certificate No. P00014WI and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with the 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: McCauley Propeller Systems One Cessna Boulevard PO Box 7704 Wichita, KS 67277 Type Constant speed, hydraulic (See NOTE 3) Engine Shaft S.A.E. ARP 502 Type 1 Flange (six 1/2" mounting bolts in 4” dia bolt circle) Hub Material Aluminum Alloy Blade Material Composite Laminate No. of Blades Three Hubs Eligible D3A37C3401 Blades Eligible Maximum Continuous Take-Off Diameter Limits Approx. Max. Weight Complete (See NOTE 2) HP RPM HP RPM (See NOTE 2) (Max. Dia.) Hub Model D3A37C3401 C80MNF-1 to C80MNF-4 350 2700 350 2700 79" - 76" (-1 to -4) 47 Lbs. P00014WI 2 Revision 1 Certification Basis: Propeller Certification Basis Application Date Approval Date D3A37C3401 14 CFR Part 35, effective February 1, 1965, including Amendments 35-1 through 35-8 February 3, 2009 April 11, 2014 Production Basis: Production Certificate No. 3 NOTE 1: Hub Model Designation [X] 3 A 37 C 3401 - [X] Minor change not affecting interchangeability or eligibility. Numerals defining specific design and major change affecting eligibility or interchangeability. Type of propeller - C, constant speed model. McCauley Design Reference Information. Denotes S.A.E. ARP 502 Type 1 Flange - 4.00” B.C. Denotes number of blades Indicates dowel location with respect to centerline through blade sockets, viewing hub from mounting face. D - 90° and 270° clockwise with No.1 blade vertical and up. NOTE 2: Blade Model Designation [X] – C 80 MN[X] - 2 Reduction in inches from basic diameter. (As -2, diameter reduced 2 inches to 78 inches) Characteristics of blade design (planform, etc.). Suffix [X] indicates blade butt staking dimensions for actuating pin attachment. Basic design diameter in inches. (Diameter limits are nominal diameters of the assembled propeller. They do not include the + or - 1/8-inch manufacturing tolerance the FAA allows for propellers with basic diameter less than 14 feet. They also do not include the + or - 1/4-inch the FAA allows for propellers with a basic diameter of 14 feet or larger.) Denotes type of blade; “C” indicates composite blade construction. Minor change not affecting interchangeability or eligibility. P00014WI 3 Revision 1 NOTE 3: Substantiated pitch control components not included in propeller type design. Hub Model Blade Model Component Description Component Model Reference Estimated Weight (pounds) D3A37C3401 C80MNF-[X] McCauley Hydro-mechanical Governor C290D[X]/T[X] 2.8 NOTE 4: Feathering and Reversing Not applicable NOTE 5: Left Hand Models Not applicable NOTE 6: Interchangeable Blades Not applicable NOTE 7: Accessories Substantiated accessories not included in propeller type design: Propeller Deice Hub Model Blade Model Component Description Part Number Installation Drawing (reference) D3A37C3401 C80MNF-[X] McCauley Deicer B-40746-30 E-7898 D3A37C3401 C80MNF-[X] McCauley Anti-ice feed shoe C-40323-81 E-7898 Propeller Spinner Hub Model Blade Model Component Description Part Number D3A37C3401 C80MNF-[X] McCauley Spinner Assembly E-8049 NOTE 8: Shank Fairings Not applicable NOTE 9: Special Limits Not applicable NOTE 10: The propeller installation must be approved as part of the aircraft type certificate to demonstrate compliance with the applicable aircraft airworthiness standards. NOTE 11: Special Limits Airworthiness limitations, if any, are specified in McCauley Manual MPC-27( ). NOTE 12: Special Notes Not applicable .......... END ……