# STC SA360CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: McCauley Propeller Systems, United States
- Description: Installation of McCauley propeller Model B3D36C424/74SA-0.
- Applied: March 28, 1995
- Status date: July 19, 2006
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 1A15](https://openairdocs.org/tcds/1A15)
- Certificate PDF: https://openairdocs.org/files/sha256/43/9f/439f963b97ed6ae81db727e9c944c84167cf1c0a507747fffe4c95b0902cf7f5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/95B2C76D997525DE862571CD005B5CEA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA360CH

## ADs that name it (0)

None.

## Approved models (1)

- The New Piper Aircraft Inc. PA-24 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA FORM 8110-2(10-68) PAGE 3 of 2 PAGES Number SA360CH This certificate issued to McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207

Part 3 of the Civil Air Regulations.

See Type Certificate Data Sheet 1A15 for complete certification basis.

Original Product-Type Certificate Number : 1A15 Make : The New Piper Aircraft, Inc.

Model : PA-24

Installation of McCauley Propeller Systems propeller model B3D36C424/74SA-0 in accordance with McCauley Technical Report No. 836, no revision, dated March 24, 1995 and McCauley Drawing No. D-60155, no revision, dated May 19, 1995, or later FAA approved revision.

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

2. FAA Approved Airplane Flight Manual Supplement Technical Report No. 835, dated June 8, 1995, or later FAA approved revision, is required.

3. Lycoming Engine models O-360-A1A or -A1D are eligible with McCauley propeller model B3D36C424/74SA-0 with maximum continuous and takeoff rating of 180 HP and 2700 RPM and with propeller operating limits/placard as listed in McCauley Technical Report Number 836.

4. 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.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date reissued : July 19, 2006

( Signature) Thaddeus D. Krolicki, Jr.

Manager, Propulsion Branch Chicago Aircraft Certification Office

(Title)

Date of application: March 28, 1995

Date of issuance : June 8, 1995

## Every issue (1)

- July 19, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/43/9f/439f963b97ed6ae81db727e9c944c84167cf1c0a507747fffe4c95b0902cf7f5)

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