TCDS P-873

Page No. 1 2 3 Rev. No. 10 6 10 DEPARTMENT OF TRANSPORATION FEDERAL AVIATION ADMINISTRATION P-873 Revision 10 Textron Aviation 215 October 12, 2016 TYPE CERTIFICATE DATA SHEET NO. P-873 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 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, 1007 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 and constant speed; electric (see NOTE 3) Engine shaft SAE # 20 Hub material Steel Blade material Aluminum alloy Number of blades 2 Hub model eligible 215-100 series Blades Eligible Maximum Continuous Takeoff Diameter Approx. Max. Wt. Complete (for reference only) (See Note 2) HP RPM HP RPM Limits (See Notes 3 and 7) 215-207-88 to 275 2600 285 2800 88" - 82" 68 lbs. 215-207-82 215-213-84 to 275 2600 285 2800 84" - 82" 68 lbs. 215-213-82 P-873 2 Rev. 10 Certification Basis Type Certificate No. 873 Production Basis Production Certificate No. 501 NOTE 1. Hub Model Designation Basic model Minor change not affecting eligibility Basic drawing identity 215 - 1 07 NOTE 2. Blade Model Designation Basic blade model Minor change (when used) not affecting eligibility Propeller diameter in inches 215 - 207 88 1 Basic blade design - - NOTE 3. Pitch Control Eligible. Additional Weights (a) Propeller Assembly 215-106, manual electric; Motor Part No. B900-104 5 lbs. (b) Propeller Assembly 215-110, manual electric; Motor Part No. 215-110 3 lbs. (c) Propeller Assembly 215-108, constant speed; Motor Part No. 215-210 3 lbs. Flight Research Engineering Corp. Governor, Model 31A 7 lbs. (d) Propeller Assembly 215-113, constant speed; B200-241 or B200-239 governor, B200-236 motor 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 blades listed in the same group of the following listed groups are sufficiently similar aerodynamically and vibrationwise to permit interchangeability in the same diameter without a flight test. Group (a) 215-207, 215-213 (blades are identical when cut to same length). NOTE 7. Accessories. Eligible with Beech Model 35-960026 spinner (weight 3 lbs.). NOTE 8. Not applicable. Rev. 10 3 P-873 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 below. No reduction below the minimum diameter listed is permissible since this figure includes the diameter reduction allowable for repair purposes. Blade Model Engine Model Max. Dia. (inches) Min. Dia. (inches) Placards 215-207-88 Continental E-165 Continental E185-1, -8, -11; serial nos. below 22183 88 88 86 86 None None Continental E185-1, -8, -11; serial nos. 22183 and above 88 82 None Continental E225-8; serial nos. below 30087 88 86 None Continental E225-8; serial nos. 30087 and above 88 82 None 215-213-84 Continental E185-1, -8, -11; serial nos. 22183 and above 84 82 None Continental E225-8; serial nos. 30087 and above 84 82 None ....END....