# STC SA505SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Stephen Noyes
- Description: Installation of McCauley 1A200FM propeller.
- Status date: December 1, 2014
- Data sheets: 5A5
- Certificate PDF: https://openairdocs.org/files/sha256/c8/61/c861ed8031cae5698a793918f2ea31979813fe7bf621ca813849e2c0343881d2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/60788FBD7651DD9A86257DA100512D5F.0001
- Page: https://openairdocs.org/stc/SA505SW

## ADs that name it

None.

## Approved models (1)

- Regal Air Inc. 305A (TCDS 5A5)

## 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.

Number SA505SW

FAA Form 8110-2 (8/13) Page 1 of 3 This certificate issued to:

Stephen Noyes 4924 Onondaga Road Onondaga, MI 49264 CAR 3 of the Civil Air Regulations.

Original Product - Type Certificate Number: 5A5 Make: Cessna Model: 305A

Installation of McCauley Model 1A200FM Propeller.

1. Operation must be in accordance with Noyes Enterprises Aircraft Flight Manual Supplement (AFMS), FAA approved on November 21, 2014, or later FAA approved revision.

The AFMS must be carried in the aircraft during all flights.

(continued on Page 3 of 3)

Date of Application: January 12, 1965 Date reissued: March 22, 2002; September 20, 2007; December 01, 2014

Date of Issuance: April 13, 1965 Date amended: December 16, 1980

Signature Robert G. Mann

Manager, Boston Aircraft Certification Office Title

**SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)**

FAA Form 8110-2 (8/13) Page 2 of 3

**TRANSFER**

**ENDORSEMENT**

To (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and ZIP Code)

From (Name of grantor)

(Address of grantor)

(Number and street)

(City, State, and ZIP Code)

Number SA505SW December 01, 2014

FAA Form 8110-2 (8/13) Page 3 of 3

Limitations and Conditions: (continued from Page 1 of 3)

2. Static RPM at maximum permissible throttle setting not less than 1950 RPM; not more than 2050 RPM. Diameter 80 inches +1.5 inches, -0.

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

------------------------------------------------------------END-------------------------------------------------------

## Every issue (2)

- December 1, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c8/61/c861ed8031cae5698a793918f2ea31979813fe7bf621ca813849e2c0343881d2)
- September 20, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/26/70/2670b706dac01de71d0406abd657942351d81559b8a62dedc28c57767bcfd85a)

---
From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.