STC SA00915CH

Supplemental type certificate · McCauley Propeller Systems

Holder
McCauley Propeller Systems · United States
Status
Current · Reissued
Status date
September 23, 2005
Applied
April 17, 1998
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS2A13

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of McCauley Propeller Model D3A36C436/74SA-0, and spinner assembly.

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00915CH This certificate issued to: McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207 Certifies that the change in the type design for the following product with the limitations and conditions therefor as spooified hereon meets the airvorthiness requirement's of Part 3 of the Civil Air Poegulations.

Original Product - Type Certificate Number: 2A13 Make: The New Piper Aircraft, Inc.

Model: PA-28R-201T, PA-28RT-201T and PA-28-201T Description of Type Design Change:

Installation of McCauley Propeller Model D3A36C436/74SA-0, and spinner assembly in accordance with McCauley Technical Report No. 911, No Revision, dated April 17, 1998, and McCauley Drawing No. D-60248, no revision, dated July 16, 1998, or later FAA Approved revisions.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

2. This modification did not increase the noise level and was not considered an acoustical change as defined in paragraph 21.93(b) of the Federal Aviation Regulations.

3. PAA Approved Airplane Flight Manual Supplement for the Piper Aircraft Models PA-28R-201T, PA-28RT-201T, and PA-28-201T Technical Report Number 912, dated July 22, 1998, or later FAA Approved revisions, is required.

4. Teledyne Continental Motors engine models TSIO-360-F, and -FB are eligible with the McCauley propeller model D3A36C436/74SA-0 with maximum continuous and takeoff rating of 200 HP and 2575 RPM.

5. Aircraft specification limits are the same as listed on Type Certificate Data Sheet No. 2A13 except as listed in McCauley Technical Report Number 912

6. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: April 17, 1998 Date Reissued: September September 2005 Date of Issuance: July 22, 1998 Date Amended:

FEDERAL AVIATION dire tratos (Signature) Thaddeus D. Krolicki, Jr.

TOMINISTRATO Manager, Propulsion Branch Chicago Aircraft Certification Office (Title)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 3

MakeModelData sheet
The New Piper Aircraft Inc.PA-28-201T2A13
The New Piper Aircraft Inc.PA-28R-201T2A13
The New Piper Aircraft Inc.PA-28RT-201T2A13