TCDS P-879

Page No. 1 2 Rev. No. 10 5 DEPARTMENT OF TRANSPORATION FEDERAL AVIATION ADMINISTRATION P-879 Revision 10 Textron Aviation 272 October 12, 2016 TYPE CERTIFICATE DATA SHEET NO. P-879 Propellers of models described herein conforming with this specification and approved data on file with the Civil Aeronautics Administration are rated as airworthy for use in certificated aircraft in accordance with pertinent aircraft specifications a nd applicable portions of the Civil Air Regulations provided they are installed, operated, and maintai ned 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 16, 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 Constant speed; hydro-mechanical (see NOTES 3 and 4) Engine shaft SAE # 20 spline shaft Hub material Steel Blade material Aluminum alloy Number of blades 2 Hub model eligible 272-100 series (see NOTE 1) Blades Eligible Maximum Continuous Takeoff Diameter Approx. Max. Wt. Complete (for reference only) (See Note 2) HP RPM HP RPM Limits (See Notes 3, 4 & 7) 272-234-101 to 325 2000 375 2180 101" - 88" 95 lbs. 272-234-88 P-879 2 Rev. 10 Certification Basis Type Certificate No. 879 Production Basis Production Certificate No. 501 NOTE 1. Hub Model Designation Basic model Minor change not affecting eligibility Basic drawing identity 272 - 1 05 NOTE 2. Blade Model Designation Basic blade model Minor change (when used) not affecting eligibility Propeller diameter in inches 272 - 234 96 1 Basic blade design - - NOTE 3. Pitch Control Eligible. Eligible only with Beech control unit 272-200 and Beech governor B200-250. Additional weight of governor 3-1/2 lbs. (Weight of transmission is included in approximate weight of propeller listed above. NOTE 4. Feathering. Eligible only with Beech full feathering control. NOTE 5. Left-Hand Models. Not applicable. NOTE 6. Interchangeable Blades. Not applicable. NOTE 7. Accessories. (a) Propeller Deicing (1) Eligible with Beech fluid deicer slinger ring included in Item (b)(1). (2) Eligible with Beech No. 279-404 (Goodrich No. 37572) propeller deicer fluid feed strips when installed in accordance with instructions issued by Beech. (b) Propeller Spinner Eligible with: (1) Beech spinner 272-102 (additional weight 6 lbs.) (2) Beech spinner 268-203 (additional weight 7 lbs.) NOTE 8. Not applicable. NOTE 9. Table of Propeller-Engine Combinations Approved Vibrationwise for Use on Single-Engine Tractor Aircraft The maximum and minimum propeller diameters that can be used from a vibration standpoint are shown, and do not necessarily represent the diameter of the propeller actually used in any particular installation. Blade Model Engine Model Max. Dia. (inches) Min. Dia. (inches) Placards 272-234-98 Lycoming GO-435-C2 98-1/2 97-1/2 Avoid continuous operation between 2875 and 3075 rpm. Lycoming GO-435-C2-6 98-1/2 94-1/2 97-1/2 92 Avoid continuous operation between 2200 and 2550 rpm. ....END....