# TCDS P-875: R. Hunt Propeller - Type: Type certificate data sheet - Status: Current - Holder: R. Hunt Propeller - Revision: 11 - Revised: September 27, 2007 - Product: Propeller - Certification basis: Part 14, CAR 14 - Data sheet PDF: https://openairdocs.org/files/sha256/71/e0/71e0326d0a40bdbf602e68bbe51ac934f21d1b23382a3d601aa4d44f87972a4b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/701B5AD4214AF192862573610066CC25.0001 - Page: https://openairdocs.org/tcds/P-875 ## Models (2) As the data sheet lists them. - FA-203 - FA-200 ## 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. 11 8 8 8 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-875 Revision 11 R. HUNT PROPELLER TARVER (BROWN PROPELLER) (SOUTH 80) (UNIVAIR) (FLOTTORP) FA-200 FA-203 Replacement Blades SEPTEMBER 17, 2007 TYPE CERTIFICATE DATA SHEET NO. P-875 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 875) 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 Chinca, Michigan 48054 Tarver Propellers, LLC 1500 Rio Vista Drive, Hangar C4 Fallon, Nevada 89406 Type Constant speed or manually controllable (See NOTE 3). The propellers consist of Beech Aircraft Corporation hubs and controls, and South 80, Univair, Flottorp Manufacturing Co., or Tarver replacement blades. The Beech identification shall be retained on the hub, whereas South 80, Univair, Flottorp or Tarver identification shall be confined to the blades only. Engine Shaft SAE No. 20 spline Hub Material Steel Blade Material These replacement blades incorporat e used metal parts from similar Beech blades, but are fabri cated from a new laminated birch or maple veneer blank, using new cellulose acetate plastic covering all over, with new brass, Everdure, or stainless steel tipping. No. of Blades 2 Hub Models Beech hub models R201-100, R202-100, R203-100 series. See Propeller Data Sheet P-807. In addition to the Beech blades listed on P-807, South 80, Univair, Flottorp, or Tarver FA203-218, FA203-219, and FA203-220 blades are eligible for use in these hubs. Beech hub models B200-100 series. See Propelle r Data Sheet P-867. In addition to the Beech blades listed on P-867, South 80, Univair, Flottorp, or Tarver FA-200-244 and FA-200-245 blades are eligible for use in these hubs. 2 P-875 Blades Eligible Maximum Continuous Takeoff Diameter Approx. Maximum Weight Complete (For reference only) (See Note 2) HP RPM HP RPM Limits (See Note 3) Hub Model B200-100 FA200-244-88 to 250 2550 275 2805 88” - 85” 67 lbs. FA200-244-85 FA200-245-88 to 250 2550 275 2805 88” - 85” 56 lbs. FA200-245-85 Hub Models R201-100, R202-100, R203-100 FA203-218-88 to 185 2300 185 2300 88” - 85” 67 lbs. FA203-218-85 FA203-219-88 to 185 2300 185 2300 88” - 85” 67 lbs. FA203-219-85 FA203-220-90 to 245 1990 260 2180 90” - 88” 67 lbs. FA203-220-88 Certification Basis Civil Air Regulations Part 14 effective November 1, 1949. Type Certificate No. 875 issued May 24, 1950 Date of application for Type Certificate unavailable. Production Basis None NOTE 1. Hub Model Designation . B a s i c m o d e l B 20 0 - 1 02 Minor change not affecting eligibility Basic drawing identity Design series SAE No. 20 spline 3 P-875 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 th e same rating and diameter limitations as cutoff blades. The suffix "X" indicates a minor change in driving the lag screws. The suffix "A" indicates revised pitch change slot. For example: B a s i c m o d e l FA 20 0 - 244 - 85 T Minor change. T denotes reduction of blade. diameter by telescoping Diameter in inches Indicates applicable blade drawing Change in model SAE No. 20 spline shaft NOTE 3. Pitch Controls Eligible . (a) Beech Model B200-100 hubs (1) Beech controls Manual - 2 lbs. Electric - 3 lbs. (2) Beech electric constant speed control components. Adapter Beech B200-238 - 4 lbs. Governor Beech B200-237 - 3 lbs. Governor Beech B200-250 - 3 lbs. Motor Beech B300-236 - 2 lbs. (3) Flight Research Engineeri ng electric constant speed components Governor Model 31A - 7 lbs. Motor - 5 lbs. (b) Beech Model R201-100, R202-100 hubs (1) Beech R203-400-A (Manual) - 4 lbs. (2) Beech R203-400-D (Manual electric) - 5 lbs. (3) Beech R203-400-E (Manual electric) - 5 lbs. (4) Beech R203-400-F (Manual electric) - 5 lbs. (5) Flight Research Engineering governor M odel 31A - 4-1/8 lbs. (including replacement of Beech electric pitch control motor with Fli ght Research Engineering electric pitch control motor without weight increase.) 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 permit interchangeability in the same diameter without a flight test: (a) FA203-218 FA203-219 *R201-217 *R203-218 (b) FA200-244 FA200-245 *B200-220 #B200-234 #B200-244 #B200-264 * Beech Aircraft Corp. blades. See P-807. # Beech Aircraft Corp. blades. See P-867. 4 P-875 NOTES 7, 8 and 9. Not applicable. NOTE 10. Special Notes . The word "eligible" as used herein does not signify approval as part of this type certificate. "Eligible" accessories and pitch controls must be a pproved as part of the aircraft type certificate upon compliance with the applicable aircraft airworthiness requirements. .....END..... ``` ## ADs (1, in force first) - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. 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