TCDS P8EA

Page No. 1 2 Rev. No. 8 8 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P8EA Revision 8 GRUMMAN J-5404/MA96K SR-5404/MA96K SR-5404R/MA96K April 30, 1982 TYPE CERTIFICATE DATA SHEET NO. P8EA This data sheet, which is part of Type Certificate No. P8EA, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Schweizer Aircraft Corporation P O Box 147 Elmira, New York 14902 Type Ground adjustable Engine shaft SAE #20 spline Hub material Alloy steel Blade material Aluminum alloy Number of blades Two Hub models eligible J-5404, SR-5404, SR-5404R Blade Eligible Maximum Continuous Takeoff Diameter Limits Approx. Max. Wt. Complete (See Note 2) HP RPM HP RPM Max. Min. (for reference only) MA-96K-0 to MA-96K-2 300 2200 350 2200 96" 94" 81 lbs. Certification basis CAR 14 effective December 15, 1956. Type Certificate No. P8EA issued November 27, 1962. Date of Application for Type Certificate November 19, 1962 T.C. reissued: September 25, 1969 April 19, 1973 September 1, 1978 May 14, 1980 May 11, 1981 Production basis None. Prior to the certification of each propeller manufactured after January 2, 1973, an FAA representative must perform a detailed inspection for workmanship materials and conformity with the approved technical data. NOTE 1. (a) Hub Model Designation Hub model designation SR - 5404R Navy hub design Ground adjustable No. of blades (2) SAE No. 20 J - Jacobs (Manufacturer) SR - Inspected and found acceptable by Sensenich P8EA 2 (b) Installation These models are for installation on a splined shaft (see Note 1(a) above). Installation is to be made in accordance with instructions furnished by the manufacturer (Drawings No. E-4012 and E-4013). NOTE 2. Blade Model Designation Blade model designation MA - 96 K - N Number of inches cut off from basic diameter Basic model or template Basic diameter in inches Denotes metal adjustable NOTE 3. Pitch control. Not applicable. NOTE 4. Feathering. Not applicable. NOTE 5. Left-Hand Models. Not applicable. NOTE 6. Interchangeable Blades. Not applicable. NOTE 7. Accessories. Not applicable. NOTE 8. Shank Fairings. Not applicable. NOTE 9. Special Limits Table of Propeller-Engine Combinations Approved Vibrationwise for use of Normal Category 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 MA96K-O Continental R-670-4 (MIL W670-6N) 96" 96" None MA96K-0 Jacobs R755 Series - Direct Drive; 300 hp @2200 rpm or less 96" 94" None MA96K-0 Jacobs R755S Series - Direct Drive 300 hp @2200 max. continuous and 350 hp @2200 rpm takeoff 96" 94" None NOTE 10. Special Notes. The word "eligible" as used herein does not signify approval. For approval, compliance with the applicable aircraft airworthiness requirements is necessary. NOTE 11. The type designs included in this data sheet are controlled by the FAA, New England Region. .....END.....