TCDS P-867

Page No. 1 2 3 Rev. No. 17 13 17 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-867 Revision 17 Textron Aviation B200 October 12, 2016 TYPE CERTIFICATE DATA SHEET NO. P-867 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 Constant speed or manually controllable; electric or hydraulic (see NOTE 3). Engine shaft SAE #20 spline shaft Hub material Steel Blade material Laminated birch veneer, with cellulose nitrate covering all over, and with brass, Everdue, or stainless steel tipping. Number of blades 2 Hub model eligible B200-100 series (see NOTE 1) P-867 2 Rev. 17 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) B200-220-88 to 250 2550 275 2805 88" - 85" 56 lbs. B200-220-85 B200-234-88 to 250 2550 275 2805 88" - 85" 56 lbs. B200-234-85 B200-244-88 to 250 2550 275 2805 88" - 85" 56 lbs. B200-244-85 B200-264-88 to 250 2550 275 2805 88" - 85" 56 lbs. B200-264-85 B200-247-96 to 240 1925 260 2200 96" - 93" 59 lbs. B200-247-93 *FA200-244-88 to 250 2550 275 2805 88" - 85" 56 lbs. FA200-244-85 *FA200-245-88 to 250 2550 275 2805 88" - 85" 56 lbs. FA200-245-85 *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. 867. (Except Universal and Flottorp blades) Production Basis Production Certificate No. 501. (Except Universal and Flottorp blades) NOTE 1. Hub Model Designation Basic model Minor change not affecting eligibility Basic drawing identity B 20 - 1 02 Design series SAE No. 20 spline 0 - NOTE 2. Blade Model Designation Basic blade model Propeller diameter in inches B200 -220 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. Rev. 17 3 P-867 NOTE 3. Pitch Controls Eligible (a) Beech Aircraft Corp. controls Manual - 2 lbs. Electrical - 5 lbs. (b) Beech Aircraft Corp. hydraulic constant speed control components. Adapter Beech B200-238 4 lbs. Governor Beech B200-237 3 lbs. Governor Beech B200-250 3 lbs. Motor Beech B200-236 2 lbs. (c) Flight Research Engineering electric constant speed controls Governor Model 31A - 7 lbs. Motor - 5 lbs. 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: (a) B200-220 B200-234 B200-244 B200-264 FA200-244 FA200-245 Blade models B200-220-88, B200-234-88 and B200-244-88 may be used in mixed pairs in the same propeller hub provided the blades are in the same weight category. NOTE 7. Accessories. Eligible with Beech Model 35-960026 spinner. Weight 3 lbs. ....END....