# TCDS P00015CH: Hartzell Propeller LLC - Type: Type certificate data sheet - Status: Current - Holder: Hartzell Propeller LLC - Revision: 11 - Revised: November 15, 2024 - Product: Propeller - Certification basis: Part 35 - Data sheet PDF: https://openairdocs.org/files/sha256/56/ba/56baf64ae2734189c9d89776763fa8dbc62e8a917f0ea24b252b2d859b62e47e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128786819120250912160443.0001 - Page: https://openairdocs.org/tcds/P00015CH ## Models (2) As the data sheet lists them. - 5D3 - 5D5 ## 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 P00015CH FEDERAL AVIATION ADMINISTRATION Revision 11 Hartzell 5D3, 5D5 TYPE CERTIFICATE DATA SHEET NO. P00015CH September 12, 2025 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P00015CH) and other approved data on file with the Federal Aviation Administration me et 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 Holde r Hartzell Propeller LLC Pi qua, OH 45356 T ype Certificate Holder Record Hartzell Pro peller Inc. Piqua, OH 45356 T ype Constant s peed; hydraulic (see Notes 3 and 4) Engine shaft Special flange (see Note 1) Hub material Aluminum Allo y Blade material See “Notes” column in table below Number of blades Five Hub models 5D3-N338( ), 5D3-NK366( ), 5D31-N K366( ), 5D5-NK( ) Maximu m Diamete r A pprox. Max. Wt. Complete Blades Continuous Takeoff Limi ts (For Reference Only) Notes (see Note 2) HP RPM HP RPM (see Note 2) (See Notes 3 and 7) (See Note 10) 5D3-N338( ) 78D01-0 850 2000 850 2000 82.5” to 76.5” 132 lb. Carbon Com posite to 78D01-6 (-0 to -6) 5D3-N K366( ), 5D31-NK366( ) 86DB01 950 2000 950 2000 91” to 81” 134 lb Carbon Com posite to 86DB01-10 (-0 to -10) 5D3-N K366( ) 91D15-0 850 2000 850 2000 96” to 89” 119 lb. Carbon Com posite to 91D15-7 (-0 to -7) 91D17-0 750 2200 750 2200 96” to 89” 136 lb. Carbon Composite to 91D17-7 (-0 to -7) 5D5-NK( ) 100DB45 800 1591 800 1591 105” to 95” 139 lb. Carbon Composite to 100DB45-10 (-0 to -10) Certification Basis: Pro peller models are approved in accordance with Organization Designation Authorization procedures of 14 CFR Part 183 Subpart D. The certification basis for this Type Certificate is in accordance with 14 CFR Part 35 with amendments 35-1 through 35-9 effective March 19, 2013. Propellers model(s) include: 5D3-N338 The following models were added, updated or revised in accordance with 14 CFR Part 35 with amendments 35-1 through 35-10 effective August 30, 2017: 5D3-N338( ), 5D3-NK366( ), 5D31-NK366( ), 5D5-NK( ) Production Basis: Production Certificate no. 10 P00015CH, Revision 11 Page 2 of 4 Note 1: Hub Model Designation (See Notes 4 and 5) 5 D 3 1 - N 338 B2 YL Y when used with 5D3 or 5D31 models indicates o ptional start locks L when used denotes left-hand rotation One or more alphanumeric hub descriptor (first character must be an alpha betical letter) “A” in the first character indicates a small diameter c ylinder “B” in the first character indicates a large diameter cylinde r “C” in the first character indicates a 5” diameter bolt-on c ylinder Any other alphabetical character liste d here denotes a minor change not affecting eligibility A n y numeric character indicates minor configuration change not affecting eligibility E x t e n s i o n : Distance in inches between en gine flange and blade centerline (implied decimal after first digit) E x a m ple: 338 = 3.38 inches M o u n t i n g flange : N denotes flan ge with eight 9/16” bolts and two ½” dowels on a 4.25” bolt circle NK denotes flange with eight through bolts and two ½” dowels on a 4.25” bolt circle O p e r a t i n g M o d e : 1 - w h e n p r e s e n t , designates engine electronic control system 3 – Constant speed, feathering, reversing, external beta ring 5 - Constant speed, feathering, reversing, internal beta feedback mechanism, start locks Preload t ype : Basic hub series (D) Number of blades Note 2: Blade Model Designation (See Notes 5 and 6) H 78 D 01 A B - 2 Number of inches cut off from (or added to if +) basic diamete r B or K denotes deicing boots A n y other character identifies a minor design change or unique application Basic blade model (two character numeric) First Character: Basic blade series for hub model (must match hub series) Second character when used: Major blade characteristic Basic diameter rounde d to the nearest inch. Add four inch correction for all blade models.* Denotes blade configuration: Blank – Right-hand tractor H - Right-Hand pushe r J - Left hand tractor L - Left-hand pusher * 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 a basic diameter of less than 14 feet. Page 3 of 4 P00015CH, Revision 11 Note 3: Pitch Control (weight of pitc h control extra) (See Notes 4 and 10) (a) Maximum output pressure: 5D3( )-N( )A, and 5D5 models 5D3( )-N( )B models 500 psig 700 psig (b) All propeller models have counterweighted blades and use governor oil to decrease pitch. (c) All governors and propeller control systems must be approved as part of the aircraft installation regardless of manufacturer. (d) Hartzell propeller model 5D31-( ) is controlled by an in tegrated electronic system which is part of the engine type design. Propeller model 5D31-( ) comp lies with the propeller airworthiness requirements when used with the engine(s) listed in Hartzell Type Design Data (Manual 159). Any change to the engine, including its control system, which affects or may affect the propeller approval must be substantiated to demonstrate that the propeller as integrated with the changed engine, including its control syst em, still complies with the propeller certification basis. Also, any change to the engine resulting from a change to the propeller must be substantiated to demonstrate that the changed engine still complies with the engine certification basis. Note 4: Featherin g (a) The 5D3 and 5D31, and 5D5 models incorporate feathering and unfeathering features. Reversing (a) The 5D3, 5D31, and 5D5 models are approved for installation as reversing propellers with appropriate reversing controls. Note 5: Left-Hand Models (see Notes 1 and 2) The left-hand version of an approv ed propeller model is approved at the same rating and diameter as listed for the ri ght-hand model. Note 6: Interchan geability (a) Refer to Hartzell service Letter HC-SL-30-260 for ice protection system component interchangeability. Note 7: Accessories (a) Pro peller 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) Pro peller deicing (weight of deicing equipment extra) (1) Propeller models listed in this data sheet are a pproved for use with propeller ice protection equipment listed in Hartzell Manual 159( ) or in other Hartzell type design data. (2) All propeller ice protection equipment must be approve d as part of the aircraft installation regardless of manufacturer. (See NOTE 10) Note 8: Shank Fairings Not applicable. Note 9: Special Limits Not applicable. Note 10: Propeller installation must be ap proved as part of the aircraft Type Certificate and demonstrate compliance with the applicable aircraft airworthiness standards. Propeller models listed herein consist of basic hub and blade models. Most propeller models include additional characters to denote minor changes and specific features as explained in Notes 1 and 2. Refer to the aircraft Type Certificate Data Sheet for the specific propeller model applicable to the installation. Propellers with composite blades must be evaluated for bird impact resistance prior to approval on any type aircraft. Hartzell Propeller must perform tests a nd/or analyses based on aircraft conf iguration and operating conditions to determine the potential hazard as a result of a bird strike. P00015CH, Revision 11 Page 4 of 4 Note 11: Retirement Time (a) Life Limits and Mandatory Inspections (1) Airworthiness limitations, if an y, are specified in Hartzell Manual 486. (2) The propeller Certificate Management Certification Branch must evaluate the propeller installation for each new aircraft installation to assess possible changes in the airworthiness limitations. Note 12: S pecial Notes (a) Refer to Hartzell Manual no. 202( ) for overspeed and overtorque limits. (b) Refer to Hartzell Service Lett er 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.