# TCDS P13EA: McCauley Propeller Systems

- Type: Type certificate data sheet
- Status: Current
- Holder: McCauley Propeller Systems
- Revision: 4
- Revised: February 26, 2009
- Product: Propeller
- Certification basis: Part 14, CAR 14
- Data sheet PDF: https://openairdocs.org/files/sha256/e4/23/e42329c45115bb0cb13f2fc71d8c343d3a691ab38e3fe34a8cf6915d287187e1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BD89F037779B736486257576004944A1.0001
- Page: https://openairdocs.org/tcds/P13EA

## Models (1)

As the data sheet lists them.

- 1A180/SEM

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
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...
```

## ADs (1, in force first)

- [AD 2005-14-11](https://openairdocs.org/ad/2005-14-11): Failed propeller blade · Hartzell Propeller BHC-92W, BHC-92ZF-1, BHC-92ZF-3 and 391 more. Effective Aug 17, 2005

## STCs approved under this data sheet (2)

- [STC SP01222WI](https://openairdocs.org/stc/SP01222WI): Installation of Aircraft Development propeller vortelators.. Aircraft Development Co
- [STC SP00582NY](https://openairdocs.org/stc/SP00582NY): Installation of Prop-Guard Polyurethane Protective Tape on the leading edge of metal propellers.. McFarlane Aviation, Inc.

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