# TCDS P00014WI: McCauley Propeller Systems

- Type: Type certificate data sheet
- Status: Current
- Holder: McCauley Propeller Systems
- Revision: 1
- Revised: March 31, 2015
- Product: Propeller
- Certification basis: Part 35
- Data sheet PDF: https://openairdocs.org/files/sha256/45/c3/45c3b3a5b6661797a8a572b2aac9ddc0fa7ed8a19d12dacc3b66ed08c4867620
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/23CD36A3A52F163B86257E19005BDD09.0001
- Page: https://openairdocs.org/tcds/P00014WI

## Models (1)

As the data sheet lists them.

- D3A37C3401

## 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 
Rev. No. 1 0 0 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
 
P00014WI 
Revision 1 
McCauley 
[X]3A37C(34--) 
March 31, 2015  
 
 
 
 
 
 
 
TYPE CERTIFICATE DATA SHEET NO. P00014WI 
 
Propellers of models described herein conforming with this data sheet, which is part of Type Certificate No. 
P00014WI 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 
One Cessna Boulevard 
PO Box 7704 
Wichita, KS 67277 
 
Type Constant speed, hydraulic (See NOTE 3) 
Engine Shaft S.A.E. ARP 502 Type 1 Flange (six 1/2" mounting bolts in 4” dia bolt circle) 
Hub Material Aluminum Alloy 
Blade Material Composite Laminate 
No. of Blades Three 
Hubs Eligible D3A37C3401 
  
 
 
Blades 
Eligible 
 
Maximum 
Continuous 
 
 
Take-Off 
 
Diameter 
Limits 
 
Approx. Max. 
Weight Complete 
(See NOTE 2) 
 
HP RPM HP RPM (See NOTE 2) (Max. Dia.) 
 
Hub Model D3A37C3401 
C80MNF-1 
to 
C80MNF-4 
 
 
350 
 
2700 
 
350 
 
2700 
 
79" - 76" 
(-1 to -4) 
 
47 Lbs.

P00014WI 2 Revision 1 
 
Certification Basis: 
 
Propeller Certification Basis Application Date Approval Date 
D3A37C3401 
14 CFR Part 35, effective 
February 1, 1965, 
including Amendments 
35-1 through 35-8 
February 3, 2009 April 11, 2014 
    
    
 
 
Production Basis: Production Certificate No. 3 
 
NOTE 1: Hub Model Designation 
 
 [X]  3  A  37  C  3401  - [X] 
 
 Minor change not affecting interchangeability or eligibility. 
 Numerals defining specific design and major change affecting eligibility or interchangeability. 
 
 Type of propeller - C, constant speed model. 
      
 McCauley Design Reference Information. 
      
 Denotes S.A.E. ARP 502 Type 1 Flange - 4.00” B.C. 
  
 Denotes number of blades 
 
 Indicates dowel location with respect to centerline through blade sockets, viewing hub from  
 mounting face. 
 D - 90° and 270° clockwise with No.1 blade vertical and up. 
 
 
 
NOTE 2:  Blade Model Designation 
 
 [X] – C   80   MN[X] -  2 
 
 
 
 Reduction in inches from basic diameter. 
 (As -2, diameter reduced 2 inches to 78 inches) 
 Characteristics of blade design (planform, etc.). 
 Suffix [X] indicates blade butt staking dimensions for actuating pin attachment. 
 Basic design diameter in inches.  (Diameter limits are nominal diameters of the assembled 
propeller. They do not include the + or - 1/8-inch 
manufacturing tolerance the FAA allows for propellers 
with basic diameter less than 14 feet. They also do not 
include the + or - 1/4-inch the FAA allows for propellers 
with a basic diameter of 14 feet or larger.) 
 Denotes type of blade; 
 “C” indicates composite blade construction. 
 Minor change not affecting interchangeability or eligibility.

P00014WI 3 Revision 1 
 
NOTE 3: Substantiated pitch control components not included in propeller type design. 
Hub Model Blade Model Component Description Component Model Reference Estimated Weight (pounds) 
D3A37C3401 C80MNF-[X] McCauley Hydro-mechanical Governor C290D[X]/T[X] 2.8 
     
 
NOTE 4: Feathering and Reversing  Not applicable 
 
NOTE 5: Left Hand Models  Not applicable 
 
NOTE 6: Interchangeable Blades  Not applicable 
 
NOTE 7: Accessories  Substantiated accessories not included in propeller type design: 
 Propeller Deice 
Hub Model Blade Model Component Description Part Number Installation Drawing (reference) 
D3A37C3401 C80MNF-[X] McCauley Deicer B-40746-30 E-7898 
D3A37C3401 C80MNF-[X] McCauley Anti-ice feed shoe C-40323-81 E-7898 
 Propeller Spinner 
Hub Model Blade Model Component Description Part Number 
D3A37C3401 C80MNF-[X] McCauley Spinner Assembly E-8049 
    
 
NOTE 8: Shank Fairings  Not applicable 
 
NOTE 9: Special Limits  Not applicable 
 
NOTE 10: The propeller installation must be approved as part of the aircraft type certificate to demonstrate  
 compliance with the applicable aircraft airworthiness standards. 
 
NOTE 11: Special Limits  Airworthiness limitations, if any, are specified in McCauley Manual MPC-27( ). 
 
NOTE 12: Special Notes  Not applicable 
 
 
 
.......... END ……
```

## ADs

None name its models.

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