# TCDS P-832: R. Hunt Propeller - Type: Type certificate data sheet - Status: Current - Holder: R. Hunt Propeller - Revision: 14 - Revised: September 17, 2007 - Product: Propeller - Certification basis: Part 14, CAR 14 - Data sheet PDF: https://openairdocs.org/files/sha256/8e/6c/8e6c12de19dcd1c0ef6b282b74b7071e2a0fef4aeb07a128b52cfc538d1cef75 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/167495499A4E25A6862575380050E697.0001 - Page: https://openairdocs.org/tcds/P-832 ## Models (1) As the data sheet lists them. - R100 ## 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 FEDERAL AVIATION ADMINISTRATION Page No. 1 2 Rev. No. 14 11 P-832 Revision No. 14 R. HUNT PROPELLER (TARVER) (BROWN PROPELLER) (SOUTH 80) (UNIVAIR) (FLOTTORP) R100 SEPTEMBER 17, 2007 TYPE CERTIFICATE DATA SHEET NO. P-832 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 832) 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 R. Hunt Propeller 6400 Tripp Road China, Michigan 48054 Tarver Propellers, LLC 1500 Rio Vista Drive, Hangar C4 Fallon, Nevada 89406 Type Manually controllable; mechanical or electrical (See NOTE 3). Engine Shaft SAE No. 10 spline Hub Material Steel Blade Material See below No. of Blades Two Hub Models R100-101 (See NOTE 1). *Varnished Laminated birch veneer with fabric; and brass, Everdure, or stainless steel tipping. **Plastic covered laminated birch veneer with brass, Everdure, or stainless steel tipping. Blades Eligible Maximum Continuous Takeoff Diameter Approx. Maximum Weight Complete (For reference only) Blade Construction (See Note 2) HP RPM HP RPM Limits (See Note 3) R100-207-80 To R100-207-77 125 2550 125 2550 80” – 77” 40 lbs. * R100-217-80 To R100-217-73 160 2600 175 2800 80” - 73” 40 lbs. * R100-221-88 To R100-221-85 188 2400 205 2640 88” – 85” 47 lbs. * R100-238-73T 160 2600 175 2800 73” 40 lbs. ** 2 P-832 Certification Basis Civil Air Regulati ons Part 14 effective July 15, 1942. Date of issuance of Type Certificate No. 832, November 27, 1945. Date of application for Type Certificate unavailable. Production Basis None NOTE 1. Hub Model Designation . Hub model designation denotes basis model, shaft size, design series, hub assembly and design changes. For example: Basic model designation Assembly R 10 0 = 1 01 Minor change not affecting eligibility Major change Design series SAE No. 10 spline shaft NOTE 2. Blade Model Designation . The dash and number added to the basic model number indicates the propeller diameter in inches. This number suffixed by the letter “T” indicates that the basic diameter has been reduced by telescoping. Telescoped blades are eligible at the same rating and diameter limitations as cut-off blades. For example: Basic model R100 = 207 = 80 T Reduction of blade diameter by telescoping Propeller diameter in inches Design features NOTE 3. Pitch Control . Eligibility with manual and electric controls only. Weight of Controls: Type Weight R100-400-A (Manual) 3 lbs. R100-400-D (Manual Electric) 5 lbs. NOTE 4. (a) Feathering . Not applicable. (b) Reversing . Not applicable. NOTE 5. Left Hand Models . The left hand version of an approved model propeller is eligible at the same rating and diameter limitations as liste d for the right hand model. NOTE 6. Interchangeable Blades . Only blades in the same group of the following listed groups are sufficiently similar aerodynamically to be considered interchangeable in the same diameter without flight tests. Blades with different model numbers, however, should not be incorporated in the same propeller, and reference should always be made to the ratings of the blades. (a) R100-217, R100-238 The manufacturer is authorized to strip the varnish from propeller blades, and apply plastic covering as a service rework. The varnished blades and the corresponding blades with plastic covering are aerodynamically interchangeable in pairs. The letter “Y” or “Z” following the propeller serial number indicates that rework has been accomplished on the blades in this manner. NOTES 7, 8 and 9. Not applicable. .....END...... ``` ## ADs None name its models. ## STCs approved under this data sheet (1) - [STC SP01222WI](https://openairdocs.org/stc/SP01222WI): Installation of Aircraft Development propeller vortelators.. Aircraft Development Co --- 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.