TCDS P-894

Page No. 1 2 Rev. No. 2 2 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-894 Revision 2 AEROPRODUCTS A6341FN December 15, 1963 TYPE CERTIFICATE DATA SHEET NO. P-894 Propellers of models described herein conforming with this data sheet (which is a part of type certificate no. 894) and other approved data on file with the Federal Aviation Agency meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Civil Air Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Detroit Diesel Allison Division General Motors Corporation Indianapolis, Indiana Type Turbine propeller; constant speed; hydraulic (see NOTES 1, 3 and 4) Engine shaft SAE No. 60A spline Hub material Steel Blade material Hollow steel No. of blades Three Design series eligible A6341FN-196A (see NOTE 1) Blades Eligible Maximum Continuous Takeoff Nominal Approx Maximum Weight Complete (See NOTE 2) Shaft HP RPM Shaft HP RPM Dis. (For reference only) E-33482 2880 1105 3017 1105 15' - 0" 890 lbs. Certification basis CAR 14 as amended to May 18, 1954. Type Certificate No. 894 issued September 7, 1955. Date of Application for Type Certificate January 20, 1955. Production basis None. Prior to the certification of each propeller manufactured after June 20, 1961, an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data. NOTE 1. Propeller Model Designation. The propeller model designation covers the complete propeller assembly, including the spinner and integral hydraulic governor. Basic model designation Design specification Design revision Specific design Negative thrust (reversing) Feathering Blade shank size Number of blades SAE No. 60A spline shaft Aeroproducts A 6 3 41 F N 196 A- P-894 2 NOTE 2. Blade Model Designation. The blade model number has no special significance. NOTE 3. Pitch Control. Eligible with Aeroproducts hydraulic governor and electronic governor and synchronizer. NOTE 4. (a) Feathering. Eligible with feathering under control of the aircraft operating condition lever, installed in accordance with the propeller manufacturer's instructions. (b) Reversing. Eligible with reversing under the control of the aircraft power lever, installed in accordance with the propeller manufacturer's instructions. NOTE 5. Left-Hand Model. 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. Not applicable. NOTE 7. Accessories. (a) Propeller deicing. Eligible with only Aeroproducts electrical deicing provisions. (b) Spinners. Eligible with only Aeroproducts spinners. ....END....