# TCDS P-874: McCauley Propeller Systems

- Type: Type certificate data sheet
- Status: Current
- Holder: McCauley Propeller Systems
- Revision: 20
- Revised: April 21, 2011
- Product: Propeller
- Certification basis: Part 14, Part 21, Part 35, CAR 14
- Data sheet PDF: https://openairdocs.org/files/sha256/d1/2f/d12f7ac2041d72b8961bfea293045b430e204654f62a188e29892565bb38c486
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/95170E7EB56254A68625787A0069BB3B.0001
- Page: https://openairdocs.org/tcds/P-874

## Models (4)

As the data sheet lists them.

- 1C200
- 1A200
- 1D200
- 1B200

## 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 3 4 
Rev. No. 20 20 17 19 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL  AVIATION  ADMINISTRATION 
 
 P-874  
 Revision 20  
 McCauley  
 1A200 
 1B200 
 1C200 
 1D200 
April 21, 2011  
 
TYPE CERTIFICATE DATA SHEET NO. P-874 
 
Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 874) and other 
approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in 
accordance with the pertinent aircraft data sheets and applicable portions 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 McCauley Propeller Systems 
7751 East Pawnee 
Wichita, Kansas  67207 
 
Type Fixed pitch metal 
Material Aluminum Alloy 
No. of Blades Two 
 
Model Standard No. Dia. Bolt Dia. Pilot Hub Dim. Wt. (lb.)
(See Note 2) HP RPM Dia. Pitch Holes Holes Circle Hole Dia. Thick. (Max. Dia.)
1A200/FM 225 2650 90"-78" 100"-40" 8 29/64" 6" 2-1/4" 7" 3-9/16" 43
1B200/HM 225 2650 90"-78" 100"-40" 8 29/64" 6" 3-1/2" 7" 3-9/16" 43
1C200/FC 225 2650 90"-78" 100"-40" 6 1/2" 4" 2-1/4" 7" 3-9/16" 43
1A200/FA 300 2700 90"-78" 100"-40" 6 33/64" 4.75" 2-1/4" 6" 3-9/16" 42
1A200/FAM 180 2700 84"-78" 100"-40" 6 25/64" 4.75" 2-1/4" 6" 3-9/16" 42
1D200/OM 185 2500 90"-84"  64"-34" 6 33/64" 4" 2-1/4" 5-1/4" 3-7/16" 35
1A200/DFA 300 2700 90"-78" 100"-40" 6 33/64" 4.75" 2-1/4" 6" 4-13/16" 45*
1A200/AOM 230 2600 90"-78" 100"-40" 6 33/64" 4" 2-1/4" 5-1/4" 3-7/16" 40
1A200/HFA 290 2700 90"-78" 100"-40" 6 33/64" 4.75" 2-1/4" 6" 5-9/16" 46*
1A200/WFA 290 2700 90"-74" 100"-40" 6 33/64" 4.75" 2-1/4" 6" 3-9/16" 48*
* Weight includes integral doweled spacer
Takeoff Hub Drilling Hub Dimensions
Max. Cont.
 
Certification Basis: 
 
Propeller Certification Basis  Method of Approval  Application Date  Approval Date  
           
1A200/FM 
CAR Part 14 eff Nov 1, 1949 
Amdt 14-1  July 27, 1950 September 8, 1950 
           
1B200/HM 
CAR Part 14 eff Nov 1, 1949 
Amdt 14-1  July 27, 1950 September 8, 1950

P-874 2 Rev. 20 
 
1C200/FC 
CAR Part 14 eff Nov 1, 1949 
Amdt 14-1  September 23, 1953 September 23, 1953 
           
 
 
 
Propeller Certification Basis  Method of Approval  Application Date  Approval Date  
1A200/FA 
CAR Part 14 eff Nov 1, 1949 
Amdt 14-1 
DOA Part 410 of the Regs 
of the Admin May 16, 1962 May 16, 1962 
     
 
1A200/FAM 
CAR Part 14 eff Nov 1, 1949 
Amdt 14-1  February 10, 1961 February 10, 1961 
     
 
 
1D200/OM 
CAR Part 14 eff Nov 1, 1949 
Amdt 14-1  July 9, 1959 July 9, 1959 
     
 
1A200/DFA 
CAR Part 14 eff Dec 15, 1956 
Amdt 14-1 
DOA Part 410 of the Regs 
of the Admin July 16, 1964 July 16, 1964 
     
 
1A200/AOM 
14 CFR Part 35, Amdt 35-1 
(February 1, 1965) 
DOA under 14 CFR Part 
21, Subpart J November 2, 1965 November 2, 1965 
     
1A200/HFA 
14 CFR Part 35, Amdt 35-1 to 
35-2 (April 3, 1967) 
DOA under 14 CFR Part 
21, Subpart J April 1, 1974 April 1, 1974 
     
 
 
 
1A200/WFA 
14 CFR Part 35, Amdt 35-1 to 
35-6 (August 18, 1990) 
DOA under 14 CFR Part 
21, Subpart J April 27, 1998 April 27, 1998 
     
 
 
 
 
 Date of Application for Type Certificate July 27, 1950 
 
Production Basis: Production Certificate No. 3 
 
NOTE 1. Installation .   
Propeller model 1A200/FM is for use on SAE #4 flanged propeller shaft and must be installed in accordance with 
McCauley C-1175. 
 
Propeller model 1B200/HM is eligible with McCauley hub P/N C-1225 on SAE #20 splined propeller shaft.  
When hub C-1225 is used, propeller is to be installed in accordance with McCauley Drawing C-1174. 
 
Propeller model 1C200/FC is for use on the special Continental Motors Corp. propeller flange and must be 
installed in accordance with McCauley Drawing C-1530. 
 
Propeller model 1A200/FA is for use on SAE #2 modified flange and must be installed in accordance with 
McCauley Drawing C-2337. 
 
Propeller model 1A200/FAM is for use on SAE #2 modified flange and must be installed in accordance with 
McCauley Drawing C-2720. 
 
Propeller models 1A200/AOM and 1D200/OM are for use on the special Continental Motors Corp.  
propeller flange and must be installed in accordance with McCauley Drawing C-2359. 
 
Propeller model 1A200/DFA is for use on SAE #2 modified flange with McCauley P/N B-3434 spacer and must 
be installed in accordance with McCauley Drawing C-3433. 
 
Propeller model 1A200/HFA is for use on SAE #2 modified flange with McCauley P/N B-4585 spacer and must 
be installed in accordance with McCauley Drawing C-4586. 
 
Propeller model 1A200/WFA is for use on SAE #2 modified flange with McCauley P/N B-3637 spacer and must 
be installed in accordance with McCauley Drawing C-7565.

P-874 3  Rev. 20 
 
NOTE 2. Propeller Model Designation .   
 
                 Basic Model Designation 
            
              Suffix  
                
1A200/ FM  90  47     
               Inches pitch at .75 radius 
              
                Propeller diameter in inches 
             
            FM Denotes SAE No. 4 Flange 
            FC Denotes Special Flange 4" B.C. 
            HM Denotes Special Flange 6" B.C. 
            FA Denotes SAE No. 2 Flange Modified (6-1/2" bolts) 
                 DFA Denotes SAE No . 2 Flange Modified (6-1/2" bolts) and B-3434 spacer 
           FAM Denotes SAE No. 2 Flange Modified (6-3/8" bolts) 
           OM Denotes Special Flange 4" B.C.; square tips 
           AOM Denotes Special Flange 4" B.C.; square tips 
           HFA Denotes SAE No. 2 Flange Modified (6-1/2" bolts) and B-4585 spacer 
           WFA Denotes SAE No. 2 Flange Modified (6-1/2" bolts) and B-3637 spacer 
            
                  Basic Design No. 
 
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 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. 
 
Propeller Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards 
 
1A200/FM 
 
 
Continental O-470-11 
 
 
90 
 
 
80 
 
 
None 
 
1B200/HM 
 
Continental E-225 
 
90 
 
86 
 
None 
 
1C200/FC 
 
Continental O-470-A 
 
90 
 
86 
 
None 
 
1C200/FC 
 
Continental O-470-E 
 
90 
 
86 
 
None 
 
1C200/FC 
 
Continental O-470-J 
 
90 
 
86 
 
None 
 
1A200/FM 
 
 
Continental E-185 with SAE No. 4 
flange and dampered shaft 
 
90 
 
 
80 
 
 
None 
 
 
1A200/FA or 
1A200/DFA 
 
Lycoming O-360 series  
(Up to 180 hp and 2700 rpm) 
 
82 
 
 
78 
 
 
None 
 
 
1A200/HFA 
 
 
Lycoming O-360 series  
(Up to 180 hp and 2700 rpm) 
 
80 
 
 
79 
 
 
“Avoid continuous 
operation while 
descending 
between 1700 to 
2100 rpm”

P-874 4 Rev. 20 
 
 
Propeller Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards 
 
1A200/FA or 
1A200/DFA 
 
 
 
Lycoming O-540 & IO-540 with one 5th order 
and one 6th order crankshaft damper 
configuration  (Up to 260 hp and 2700 rpm) 
 
 
90 
 
 
 
 
80 
 
 
 
 
None 
 
 
 
1A200/FA or 
1A200/DFA 
 
 
Lycoming IO-540 series with one 5th order 
and one 6th order crankshaft damper 
configuration  (Up to 300 hp and 2575 rpm) 
 
90 
 
 
 
86 
 
 
 
None 
 
 
 
1A200/FAM 
 
 
Lycoming O-320 series  
(Up to 160 hp and 2700 rpm) 
 
82 
 
 
78 
 
 
None 
 
 
1D200/OM 
 
 
Continental GO-300 series  
(175 hp and 2400 rpm) 
 
90 
 
 
86 
 
 
None 
 
 
1A200/AOM 
 
 
 
Continental O-470 series with one 5th order 
and one 6th order crankshaft damper 
configuration  (Up to 230 hp and 2600 rpm 
 
90 
 
 
 
86 
 
 
 
None 
 
 
 
 
NOTE 10. The word “eligible” as used herein does not signify  approval.  For approval, compliance with the applicable 
aircraft airworthiness requirements is necessary. 
 
 
…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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