TCDS P13EA

Page No. 1 2 Rev. No. 4 3 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P13EA Revision 4 McCauley 1A180 February 26, 2009 TYPE CERTIFICATE DATA SHEET NO. P13EA Propellers of models described herein conforming with this data sheet (which is a part of propeller Type Certificate No. P13EA) and other approved data on file with the Federal Aviation Administration, 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 McCauley Propeller Systems 7751 E. Pawnee Wichita, Kansas 67207 Type Fixed Pitch Metal Material Aluminum Alloy Number of Blades Two Takeoff & Hub Drilling Diameter Weight Model Max. Cont. Standard No. Dia. Dia. Bolt Pilot Hub Dimensions (lb.) (See Note 2) HP RPM Diameter Pitch Holes Ho les Circle Hole Dia. Thickness (Max.Dia.) 1A180/SEM 200 2700 78"-68" 75"-40" 6 33/64" 4" 2-1/4" 4-7/8" 3-7/16" 30.5 Certification basis Civil Air Regulations Part 14, effective December 15, 1956. Type Certificate No. P13EA issued August 30, 1963 under Delegation Option Authorization provisions of the Regula tions of the Administrator, Part 410. Date of Application for Type Certificate, June 21, 1963. Production basis Production Certificate No. 3. NOTE 1. Installation. Propeller Model 1A180/SEM is for use on special Continental Motors Corp. flanged propeller shaft and must be installed in accordance with McCauley Drawing P/N C-3295. For installation on flanged propeller shaft ends. Any front plate supplied by engine manufacturer is not to be used. Install with special alloy steel bolts specified or furnished by McCauley. NOTE 2. Propeller Model Designation. The propeller model designation consists of a series of numbers suffixed to the basic design number to indicate propeller diam eter and geometric pitch at the .75 radius. Basic Model Designation S u f f i x 1A180 / SEM 78 56 Pitch at .75R in inches Diameter in inches SEM denotes Special Flange 4" B.C. Basic design number P13EA 2 Rev 4 NOTES 3, 4, 5, 6, 7, and 8. Not applicable. NOTE 9. Table of Propeller-Engine Combinations Approved Vibrationwise for Use on Normal Category Single-Engine Tractor Aircraft The maximum and minimum propelle r 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. Propeller Engine Damper Max. Dia. Min. Dia. Model Engine Model Configuration (Inches) (Inches) Placards 1A180/SEM Continental IO-360 Two-6th Order 78 74 None series (up to 180 hp. @ 2700 r.p.m.) NOTE 10. The word "eligible" as used herein does not signify approval as part of this type certificate. "Eligible" accessories must be approved as part of the aircraft type certificate upon compliance with the applicable airworthiness requirements. ...END...