# TCDS P00017CH: Hartzell Propeller Inc. - Type: Type certificate data sheet - Status: Current - Holder: Hartzell Propeller Inc. - Revision: 0 - Revised: July 1, 2016 - Product: Propeller - Certification basis: Part 35, Part 183 - Data sheet PDF: https://openairdocs.org/files/sha256/cc/81/cc811bb38e2b432da98e68d5b0637bbe8ba56c2d68e14267aa2268671ad3e4c1 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D5F435F6A0BB5C4586257FED006FFF50.0001 - Page: https://openairdocs.org/tcds/P00017CH ## Models (1) As the data sheet lists them. - H01 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION P00017CH FEDERAL AVIATION ADMINISTRATION Revision - Hartzell H01 TYPE CERTIFICATE DATA SHEET NO. P00017CH July 1, 2016 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P00017CH) 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, OH 45356 Type Fixed Pitch Metal Material Aluminum Alloy Number of blades Two Basic Takeoff & Diameter Hub Drilling Dia. Hub Weight @ max dia. Model Max.Cont. Limits Standard No. Dia. Dia. Bolt Pilot Dimensions (Ref Only) (see Note 2) HP RPM (see Note 2) Pitch Holes Holes Circle Hole Dia. Thk (See Note 7) H01-77( )R 180 2700 77” to 67” 49”-60” 6 17/32” 4 3/4” 2.25 6” 3.44 34.7 lb. (-0 to -10) Certification Basis: Models added after August 31, 2009 are approved in accordance with Organization Designation Authorization procedures of 14 CFR Part 183 Subpart D. Models listed below are in accordance with 14 CFR Part 35 with amendments 35-1 through 35-9A effective July 26, 2013: H01 Production Basis: Production Certificate no. 10 Note 1: Installation These models are for installation on flanged propeller shaft ends (see note 2). Installation is to be made with special steel bolts which are furnished or specified by the propeller manufacturer in accordance wi th the appropriate propeller assembly drawing. See Note 7 for spacer designations and Note 9 for approved spacer lengths. Note 2: Model Designation H01 - 77 49 R A 32 -2 ( ) Denotes a minor configuration change not affecting eligibility Diameter cutoff (inches) Spacer length (in 1/8” increments) (see Note 7) Spacer Clocking Letter: Indicates mounting flange angular index with respect to blade centerline, viewed clockwise facing propeller flange Letter Angular Index Clocking Feature Non counter bored hole of “R” flange A 0 and 180 degrees Denotes interface between the engine flange and the propeller (or propeller‘s spacer): R: SAE # 2 flange with six ½” bolts and five ¾” drive bushings on a 4-3/4” bolt circle Blade pitch in inches Basic diameter in inches Propeller Model P00017CH, Revision - Page 2 of 2 Note 3, 4, 5, 6. Not applicable. Note 7: Accessories (a) Propeller spinner. (weight of spinner extra) (1) Approved with Hartzell and other manufacturers’ spinners when listed on Hartzell type design data. (2) All propeller spinners must be approved as part of the aircraft installation regardless of manufacturer. (See NOTE 10) (b) Spacers (weight of spacer extra) (1) Spacers are identified by flange letters and by length/thickness (see note 2) Note 8: Not applicable Note 9: Special Limits Table of Propeller-Engine Combinations Approved Vibrationwise for Use on Normal Category Single-Engine Tractor Aircraft The maximum and minimum propeller diameters that can be used from a vibration standpoint are shown below. No reduction below the minimum diameter listed is permissible, since this figure includes the diameter reduction allowable for repair purposes. The engine models listed below are the configurations on the engine type certificate unless specifically stated otherwise. Modifications to the engine or airframe that alter the power of the engine models listed below during any phase of operation have the potential to increase propeller stresses and are not approved by t his list. Such modifications include, but are not limited to, the addition of a turbocharger or turbonormalizer, increased boost pressure, increased compression ratio, increased RPM, altered ignition timing, electronic ignition, full authority digital engine controls (FADEC), or tuned induction or exhaust. Also, any change to the mass or stiffness of the crankshaft/counterweight assembly is not approved by this list. Propeller Model Engine Model Max Dia. (Inches) Min. Dia. (Inches) Placards Note 10: Propeller installation must be approved as part of the aircraft Type Certificate and demonstrate compliance with the applicable aircraft airworthiness requirements. Propeller models included herein contain additional characters to denote minor changes and specific features as explained in Note 2. Refer to the aircraft Type Certificate Data Sheet for the specific propeller model applicable to the installation. Note 11: Retirement Time (a) Life Limits and Mandatory Inspections (1) Airworthiness limitations, if any, are specified in Hartzell Manual 500. Note 12: Special Notes (a) Refer to Hartzell Manual no. 202( ) for overspeed and overtorque limits. (b) Refer to Hartzell Service Letter HC-SL-61-61( ) for overhaul periods. END ``` ## ADs None name its models. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.