# TCDS P-807: Textron Aviation Inc. - Type: Type certificate data sheet - Status: Current - Holder: Textron Aviation Inc. - Revision: 13 - Revised: October 12, 2016 - Product: Propeller - Data sheet PDF: https://openairdocs.org/files/sha256/59/e9/59e95241b8c27065822c01e3d8f34398e0bc104a4b4c97817ccea6528999d436 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/73A742F6BB087780862580FE00587483.0001 - Page: https://openairdocs.org/tcds/P-807 ## Models (3) As the data sheet lists them. - R203 - R202 - R201 ## 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 Rev. No. 13 9 9 DEPARTMENT OF TRANSPORATION FEDERAL AVIATION ADMINISTRATION P-807 Revision 13 Textron Aviation R201 R202 R203 October 12, 2016 TYPE CERTIFICATE DATA SHEET NO. P-807 Propellers of models described herein conforming with these specifications and approved data on file with the Civil Aeronautics Administration are rated as airworthy for use in certificated aircraft as indicated herein in accordance with pertinent aircraft specifications and applicable portions of the Civil Air Regulations provided they are installed, operated and maintained as prescribed by the manufacturer. Type Certificate Holder Textron Aviation Inc. One Cessna Boulevard Wichita, KS 67215 Type Certificate Holder Record Beech Aircraft Company transferred to Raytheon Aircraft Company on April 15, 1996 Raytheon Aircraft Company transferred to Hawker Beechcraft Corporation on March 26, 2007 Hawker Beechcraft Corporation transferred to Beechcraft Corporation on April 12, 2013 Beechcraft Corporation transferred to Textron Aviation Inc. on October 12, 2016 Type Manually controllable; electric (see NOTES 3 and 4). Engine shaft SAE #20 Hub material Steel Blade material See below Number of blades 2 Hub model eligible R201-100, R202-100, R203-100 series (see NOTE 1) P-807 2 Rev. 13 Blades Eligible Maximum Continuous Takeoff Diameter Approx. Max. Wt. Complete (for reference only) (See NOTE 2) HP RPM HP RPM Limits (See Note 3) Blade Construction R201-200-85 to R201-200-82 200 2550 200 2550 85" - 82" 60 lbs. Laminated birch veneer with fabric from 29" sta. to tip with brass, Everdur, or stainless steel tipping. R201-209-96 to R201-209-93 210 1925 210 1925 96" - 93" 63 lbs. Laminated birch veneer with fabric from 29" sta. to tip with brass, Everdur, or stainless steel tipping. R201-211-88 to R201-211-85 200 or 240 2550 or 2200 200 or 246 2550 or 2420 88" - 85" 61 lbs. Laminated birch veneer with fabric from 29" sta. to tip with brass, Everdur, or stainless steel tipping. R201-217-88 to R201-217-85 185 2300 185 2300 88" - 85" 67 lbs. Laminated birch veneer with fabric from 29" sta. to tip with brass, Everdur, or stainless steel tipping. R203-218-88 to R203-218-85 185 2300 185 2300 88" - 85" 67 lbs. Laminated birch veneer with cellulose nitrate covering all over, with brass, Everdur, or stainless steel tipping. R201-237-88 to R201-237-85 200 or 240 2550 or 2200 200 or 246 2550 or 2420 88" - 85" 61 lbs. Laminated birch veneer with cellulose nitrate covering all over, with brass, Everdur or stainless steel tipping. *FA203-218-88 to FA203-218-85 185 2300 185 2300 88" - 85" 67 lbs. Laminated birch veneer with cellulose nitrate covering all over, with brass, Everdur or stainless steel tipping. Blades Eligible Maximum Continuous Takeoff Diameter Approx. Max. Wt. Complete (for reference only) (See Note 2) HP RPM HP RPM Limits (See Note 3) Blade Construction *FA203-219-88 to FA203-219-85 185 2300 185 2300 88" - 85" 67 lbs. Laminated birch veneer with cellulose nitrate covering all over, with brass, Everdur or stainless steel tipping. *FA203-220-90 to FA203-220-88 245 1990 260 2180 90" - 88" 67 lbs. Laminated birch veneer with cellulose nitrate covering all over, with brass, Everdur, or stainless steel tipping. *Blades remanufactured by Flottorp Manufacturing Company under TC 875 and PC 4, or by Universal Aircraft Industries under TC 875 (see P-875). Certification Basis: Type Certificate No. 807. (Except Universal and Flottorp blades) Production Basis: Production Certificate No. 501. (Except Universal and Flottorp blades) Rev. 13 3 P-807 NOTE 1. Hub Model Designation Basic model Minor change not affecting eligibility Basic drawing identity R 20 - 1 03 Design series SAE No. 20 spline 1 NOTE 2. Blade Model Designation Basic blade model Propeller diameter in inches R201 -211 85 T Basic blade design - - T denotes telescoped blade X denotes minor change in driving lag screws A denotes revised pitch change slot Telescoped blades are eligible at the same rating and diameter limitations as cutoff blades. NOTE 3. Pitch Controls. Eligible with: (a) Beech Aircraft Corp. R203-400-A Manual Weight - 4 lbs. . R203-400-D (Manual electric) Weight - 5 lbs. R203-400-E (Manual electric) Weight - 5 lbs. R203-400-F (Manual electric) Weight - 5 lbs. (b) Flight Engineerng Research Corp. Governor, Model 31A, Weight 4-1/8 lbs. (including replacement of Beech electric pitch control motor by Flight Engineering Research Corp. electric pitch control rotor 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 listed for the right-hand model. NOTE 6. Interchangeable Blades. Only bladed listed in the following group are sufficiently similar aerodynamically to permit interchangeability in the same diameter without a flight test. 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) R201-217 R203-218 FA203-218 FA203-219 (b) R201-211 R201-237 NOTE 7. Accessories. Not applicable. NOTE 8. Shank Fairing. Not applicable. NOTE 9. Special Limits. Not applicable. NOTE 10. The manufacturer is authorized to apply plastic covering to certain propeller blades during manufacture, or as a service rework. Blades eligible for rework and corresponding designations are: Varnished blades Plastic covered blades (a) R201-217 R202-218 (b) R201-211 R202-237 ....END.... ``` ## ADs (1, in force first) - [AD 76-10-12](https://openairdocs.org/ad/76-10-12): Textron 214, B200 (propeller), R201 and 2 more. Effective Jun 2, 1976 ## STCs approved under this data sheet (2) - [STC SP01222WI](https://openairdocs.org/stc/SP01222WI): Installation of Aircraft Development propeller vortelators.. Aircraft Development Co - [STC SP00582NY](https://openairdocs.org/stc/SP00582NY): Installation of Prop-Guard Polyurethane Protective Tape on the leading edge of metal propellers.. McFarlane Aviation, Inc. --- 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.