TCDS P-882

Page No. 1 2 3 4 Rev. No. 16 12 12 16 DEPARTMENT OF TRANSPORATION FEDERAL AVIATION ADMINISTRATION P-882 Revision 16 Textron Aviation 278 October 12, 2016 TYPE CERTIFICATE DATA SHEET NO. P-882 Propellers of models described herein conforming with these specifications and approved data on file with the Federal Aviation 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, operate d, 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 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; hydraulic (see NOTE 3) Engine shaft Special flange shaft, 4" diameter bolt circle Hub material Steel Blade material Aluminum alloy Number of blades 2 Hub model eligible 278-100, 278-107 (see NOTE 1) P-882 2 Rev. 16 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) 277-207-91 240 2600 240 2600 91" 69 lbs. 278-207-88 to 240 2600 240 2600 88" - 82" 69 lbs. 278-207-82 278-208-82 to 250 2600 250 2600 82" - 81½ 69 lbs. 278-208 81½ 278-208-84 to 260 2625 260 2625 84" - 82" 69 lbs. 278-208-82 278-209-84 to 250 2600 250 2600 84" - 82" 73 lbs. 278-209-82 278-213-82 250 2600 250 2600 82" 73 lbs. 278-214-82 260 2625 260 2625 82" 69 lbs. Certification Basis Type Certificate No. 882 Production Basis Production Certificate No. 501 NOTE 1. Hub Model Designation Basic model Minor change not affecting eligibility Basic drawing identity 278 -100 1 NOTE 2. Blade Model Designation Basic blade model Minor change (when used) not affecting eligibility Propeller diameter in inches 278 - 207 96 1 Basic blade design - - Rev. 16 3 P-882 NOTE 3. Pitch Control. Applicable Blades Governor Governor Pressure* Applicable Airplane 278-207-88 Woodward 210060 500 p.s.i. Beech 45 (T-34) or or 278-208-84 Beech 278-220 278-208-84 Woodward 210175 450 p.s.i. Beech H-35 (thru "G" revision) or Woodward 210235 278-209-84 Woodward 210175 320 p.s.i. Beech H-35 ("H" revision and later) 278-213-82 Woodward 210235 450 p.s.i. Beech J-35 or 278-214-82 *Includes 50 p.s.i. inlet pressure. Additional weight of governor 3-1/2 lbs. NOTE 4. Feathering. Not applicable NOTE 5. Left-Hand Models. Not applicable. NOTE 6. Interchangeable Blades. Not applicable. NOTE 7. Accessories. Propeller is equipped with Model 278-205 spinner. Weight of spinner is included in approximate weight of propeller listed above. (Approximately 4 lbs. less if spinner is not used.) NOTE 8. Not applicable. P-882 4 Rev. 16 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 Continental 0-470-13 278-207-88 0-470-13A 88 82 None Continental 278-208-82 IO-470-C 82 81½ None 278-214-82 IO-470-N 82 82 None Blade Model Engine Model Max. Dia. (inches) Min. Dia. (inches) Placards Continental 0-470-13 278-208-84  0-470-13A 84 82 None 0-470-4 *278-208-84 Continental 0-470-G 84 83 None *278-209-84 Continental 0-470-G 84 83 None *Eligible only on Beech Model H35 airplane which was certificated under Part 410 of the Regulations of the Administrator. ....END....