TCDS P00114CH

Pa ge No. 1 2 3 Rev. No. 0 0 0 DEPARTMENT OF TRANSPORTATION P00114CH FEDERAL AVIATION ADMINISTRATION Revision 0 Hartzell 5FB TYPE CERTIFICATE DATA SHEET NO. P00114CH July 18, 2025 Propellers of models described herein c onforming with this data sheet (which is part of Type Certificate No. P00114CH) and other approved data on file with the Fede ral Aviation Administration meet the minimum standards for use in certificated aircraf t 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 Type Certificate Holder Recor d Hartzell Propeller LLC Pi qua, OH 45356 Type G round adjustable pitch En gine shaft S pecial flange (See Note 1) Hub material Aluminum Alloy Blade material Com posite Number of blades Five Hub Models 5FB-F ( ) Maximum Diameter 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) Hub Models: 5FB-F(375 through 919) (see Note 1) 73FB01 373 2550 373 2550 76.5” to 69.5” 36 lb.* Carbon Com posite (-0 to -7) * Weight based on 3.750” hub extension length Certification Basis: 14 CFR Part 35 with ame ndments 35-1 through 35-10 effective August 30, 2017. Type Certificate No. P00114CH issued July 18, 2025. Date of application for Type Certificate: January 10, 2024 Propeller Models listed below are approved under the original certification basis: 5FB-F( ) Production Basis: Production Certificate no. 10 P00114CH, Revision 0 Page 2 of 3 Note 1: Hub Model Designation 5 F B - F 375 A 1 H Denotes configuration: Blank – Right-hand tractor H – Right-hand pusher J – Left-hand tractor L – Left-hand pusher Any numeric character indicates mi nor configuration change not affecting eligibility Any alphabetical character listed here denotes a minor change not affecting eligibility Extension: Distance in inches from engine mounting flange to blade centerline (implied decimal after first digit) Example: 375 = 3.75 inches Flange Designation: F denotes flange with six 1/2” bolts and two 1/2” dowels on a 4” bolt circle circle Shank Size Fixed Angle (ground adjustable) Blade count Note 2: Blade Model Designation (See Notes 5 and 6) L 73 F B 01 B – 2R Number of inches cut off from (or added to if +) basic diamete r R when used denotes s pecifically rounded tip for cutoff diameter A n y other character in this location denotes tip shape B or K denotes deicing or anti-ice boots Any other alpha character listed he re denotes a minor change not affecting eligibility Basic blade model (two character numeric) Second al phabetical character when used: Major blade characteristic First alphabetical character - Shank diameter: (must match hub series) Basic diameter rounded to the nearest inch (when installed in a two-bladed hub) * Denotes blade confi guration: L - L e f t - h a n d pusher * Diameter limits are nominal di ameters 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. Note 3: Pitch Control Not Applicable Note 4: Feathering and Reversing Not A pplicable 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. Page 3 of 3 P00114CH, Revision 0 Note 6: Interchangeability (a) Pro pellers Not applicable (b) Governors Not a pplicable (c) Blades Not applicable (d) Ice Protection S ystems Refer to Hartzell service Letter HC-SL-30-260 for ice protection system component interchangeability. Note 7: Accessories (a) Propeller spinner. (weight of spinner extra) (1) A pproved 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) Propeller ice protection system (wei ght of ice protection equipment extra) (1) Propeller models listed in this data sheet are approved 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 approved 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 and blade a ngle(s) 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. Propellers with composite blades must be evaluated for bird impact resistance prior to approval on any type aircraft. Hartzell Propeller must perform tests and/or analyses based on aircraft configuration and operating conditions to determine the potential hazard as a result of a bird impact. Note 11: Retirement Time (a) Life Limits and Mandatory Inspections (1) Airworthiness limitations, if an y, are specified in Hartzell Manual 505. (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: Special 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