# TCDS P00023AT: Sensenich Propeller Company - Type: Type certificate data sheet - Status: Current - Holder: Sensenich Propeller Company - Revision: 4 - Revised: September 17, 2026 - Product: Propeller - Certification basis: Part 35 - Data sheet PDF: https://openairdocs.org/files/sha256/3d/67/3d67755b90efe365061857b9b6b948c20445876e3684276c2d4a6e50ba821bcd - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167170238420260924151802.0001 - Page: https://openairdocs.org/tcds/P00023AT ## Models (3) As the data sheet lists them. - 2G0M6 - 2G0M7 - 2G0M8 ## 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. 4 4 4 4 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. P00023AT Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P00023AT ) 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 t hey are installed, operated and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Sensenich Propeller Company 2008 Wood Court Plant City, Florida 33563 Type Ground Adjustable Engine Mounting SAE No. 2, 5, 6 ( see NOTE 1 ) Hub Material Aluminum Alloy Blade Material Composite Number of Blades Two Hub Models 2G0M6, 2G0M7, 2G0M8 (see NOTE 1) Maximum Diameter Approximate Blades Continuous Takeoff Limits Weight (see N OTE 2) HP RPM HP RPM (see N OTE 2) (lb) C76PGF 180 2700 180 2700 76” to 72” 19 to C76PGF -4 C76PGF to C76PGF -4 C82BGF 180 2700 180 2700 82” to 78” 20 to C82BGF -4 C82BGF to C82BGF -4 Certification Basis: 14 CFR Part 35 as amended through amendment 10 , effective August 30, 201 7. Date of application for Type Certificate P00023 AT : June 22, 2021 Issuance of Type Certificate: April 22, 2022 Production Basis: Production Certificate No. 335CE P00023AT Revision 4 SENSENICH 2G0M6, 2G0M7, 2G0M8 September 17, 2026 P00023AT Revision 4 2 NOTE 1. Hub Model Designation . 2 G 0 M8 S4 Spacer designation in 1/4 inch increments. S4 designates 4/4 inch spacer or 1 inch. S16 designates 16/4 inch spacer or 4 inch. If left blank no spacer is utilized. Flange interface: M6 for SAE Type No. 2 propeller flange. M7 for SAE Type No. 5 propeller flange. M8 for SAE Type No. 6 propeller flange. Distance to center of rotation change from nominal in inches. Sensenich blade shank size. Number of blades. NOTE 2. Blade Model Designation . C 82 B G F __ - __ Denotes tip cutoff diameter reduction in inches. L denotes left-hand rotation. Blank denotes right-hand rotation. Denotes minor change. Does not affect eligibility. Sensenich blade shank size and structure. Sensenich blade aero design (Airfoils, Chords, Twist, etc). Maximum nominal diameter in inches. C denotes composite ground adjustable. NOTE 3. Not applicable. NOTE 4. Not applicable. NOTE 5. Left -Hand Models . The left -hand version of an approved propeller model is eligible at the same rating and diameter limitations as listed for the right -hand model. NOTE 6. Not applicable. P00023AT Revision 4 3 NOTE 7. (a) Extensions . Propeller is approved for extensions up to and including 4. 00 ”. (b) Spinners . Approved with Sensenich spinners when listed on approved type design data . NOTE 8. Not applicable. NOTE 9 . Special Limits . Table of Propeller -Engine Combinations Approved Vibrationwise for Use on Normal Category Single -Engine Tractor Aircraft Hub Model Blade Model Engine Model Max. Dia. (inches) Min. Dia. (inches) Placard s 2G0M6 C76PGF Lycoming (I)O-320 Series 160hp @ 2700 RPM or less 76 72 None 2G0M6 C82BGF Lycoming (I)O -320 Series 160hp @ 2700 RPM or less 82 78 None 2G0M7 C76PGF Lycoming (I)O -320 Series 160hp @ 2700 RPM or less 76 72 None 2G0M7 C82BGF Lycoming (I)O -320 Series 160hp @ 2700 RPM or less 82 78 None 2G0M 8 C76PGF *Non -Counterweighted Lycoming (I)O -360 Series 180hp @ 2700 RPM or less 76 72 None 2G0M 8 C82BGF *Non -Counterweighted Lycoming (I)O -360 Series 180hp @ 2700 RPM or less 82 78 None *Counterweighted Lycoming O -360 series engines are denoted by a number as the fourth (4th) character after engine displacement. P00023AT Revision 4 4 NOTE 10. Sensenich Propeller must perform tests and/or analyses based on aircraft configuration and operating conditions to determine the potential hazard as a result of a lightning strike prior to approval on any type aircraft. NOTE 11. Special Limits . Propeller life limits and airworthiness limitations are specified in Sensenich manual SICA -G_20220214 NOTE 12. Not applicable. ... END ... ``` ## ADs None name its models. --- 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.