# TCDS P-804: R. Hunt Propeller - Type: Type certificate data sheet - Status: Current - Holder: R. Hunt Propeller - Revision: 17 - Revised: September 17, 2007 - Product: Propeller - Certification basis: Part 14, CAR 14 - Data sheet PDF: https://openairdocs.org/files/sha256/a7/27/a727672db043ea8eee23d095351178a3df07a72693733ce81ac2b44c7e49f3e4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/94E7FCC2A95DA5638625736100677F80.0001 - Page: https://openairdocs.org/tcds/P-804 ## Models (2) As the data sheet lists them. - R003 - R002 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 Rev. No. 17 16 14 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-804 Revision 17 R. HUNT PROPELLER TARVER (BROWN PROPELLER) (SOUTH 80) (UNIVAIR) (FLOTTORP) R002 R003 SEPTEMBER 17, 2007 TYPE CERTIFICATE DATA SHEET NO. P-804 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 804) 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 Co. 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. 0 taper, SAE Nos. 1 and 2 flange (See NOTE 7). Hub Material Steel. Blade Material See below. No. of Blades Two Hub Models R002-100 and R003-100 Series (See NOTE 1). 2 P-804 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 and 7) (See Note 2) R002-205-72 to R002-205-68 * R002-217-72 to R002-217-68 80 2700 80 2700 〉 〈 or 〉 72” - 68” 30 lbs. R002-218-72 to 85 2575 85 2575 R002-218-68 R003-230-72 to R003-230-68 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 and 7) (See Note 2) R003-233-72 to ** R003-233-68 R003-234-72 to 80 〉 〈 2700 or 80 2700 〉 72”-68” 30 lbs. R003-234-68 85 2575 85 2575 R003-235-72 to R003-235-68 R003-201-75 to * R003-201-72 〉 〈 85 2575 93 2824 75”-72” 29 lbs. ** R003-231-75 to R003-231-72 R003-225-75 to * R003-225-63 R003-232-75 to 〉 〈 103 2700 113 2970 75”-63” 29 lbs. R003-232-63 ** R003-237-75 To 〉 〈 75 2650 75 2650 75”-63” 29 lbs. * R003-237-63 ** *Varnished laminated birch or m aple veneer with fabric; and brass, Everdure, or stainless steel tipping. **Plastic covered laminated birch or maple veneer with or without brass, Everdure, or stainless steel tipping. Certification Basis Civil Air Regulati ons Part 14 effective July 15, 1942. Date of issuance of Type Certificate No. 804 September 5, 1944. Date of application for Type Certificate unavailable. 3 P-804 Production Basis None NOTE 1. Hub Model Designation . The last two digits of the number following the dash in the hub model designation indicates a minor change which does not affect the eligibility. Basic model designation A s s e m b l y R 0 02 - 1 01 Minor change not affecting eligibility Major change Design series SAE No. 0 taper shaft NOTE 2. Blade Model Designation . The dash and number added to the blade drawing number indicates the propeller diameter in inches. This number su ffixed 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 Diameter suffix F R003 - 201 - 72 T Reduction of blade diameter by telescoping Diameter in inches Design features Reinforced plastic leading edge - no metal. NOTE 3. Pitch Control . Eligible with manual and electric controls only Weight of Controls: Type W e i g h t R003-403-A (Manual) 3 lb. R003-403-B (Manual) 3 lb. R003-403-C (Manual) 5 lb. R003-403-D (Manual, Electric) 5 lb. 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 lis ted 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 th e 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) R002-205, R002-217, R002-218, R 003-230, R003-233, R003-234, R003-235. (b) R003-201, R003-225, R003-231, R003-232, R003-237. 4 P-804 The manufacturer is authorized to strip the varn ish from certain propeller blades, and apply plastic covering as a service rework. The eligible varn ished blades and their corresponding blade designations with plastic covering, which are aerodynamica lly interchangeable in pairs are as follows: Varnished Blades Plastic Covered Blades R002-205 R003-235 R002-217 R003-233 R002-218 R003-234 R003-201 R003-231 R003-225 R003-232 NOTE 7. Accessories . (1) Adapters . These propellers are eligible for installation on engines with integral flange on crankshaft when used with adapters; R003-349 adapter for No. 1 flange, and R003-342 adapter for No. 2 flange. Add 4 lbs. to weight of propeller when adapters are used. NOTES 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.