STC SA281SW

Supplemental type certificate · Steve Noyes

Holder
Steve Noyes · United States
Status
Current · Amended
Status date
January 10, 2011
Applied
May 1, 1963
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheets
TCDS3A14TCDS5A5

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of gravity flow fuel system, carburetor heater system, and fuel selector valve in accordance with Ector Aircraft Company Drawing No. 271000 dated 9/16/1963; 72000 Rev. 2/18/1964, Ector Aircraft Drawings dated 10/16/1963 and 7/1/1963, or later FAA approved revisions and seven photographs. Or Installation of gravity flow fuel system, carburetor heater system, and fuel selector valve in accordance with Air Repair, Inc. Engineering Report AR063 dated May 12, 2009, or later FAA approved revision.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Part 3 of the Civil Air Regulations.

Installation of gravity flow fuel system, carburetor heater system, and fuel selector valve in accordance with Ector Aircraft Company Drawing No. 271000 dated 9/16/1963; 72000 Rev. 2/18/1964, Ector Aircraft Drawings dated 10/16/1963 and 7/1/1963, or later FAA approved revisions and seven photographs.

Or Installation of gravity flow fuel system, carburetor heater system, and fuel selector valve in accordance with Air Repair, Inc.

Engineering Report AR063 dated May 12, 2009, or later FAA approved revision.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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.

Stephen Noyes 4924 Onondaga Rd Onondaga, MI 49264 See attached FAA Approved Model List (AML) for the list of approved airplane models, applicable installation data requirements and specific limitations. Make: Model:

Date of application: May 1, 1963

Date of issuance : November 14, 1963

Date reissued : March 22, 2002; May 6, 2010

Date amended : March 10, 1964; November 18, 1980;

January 10, 2011 By direction of the Administrator

Original Signed By:

John M. Tallarovic

( Signature) Michael Downs Acting Manager, Propulsion Branch Chicago Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) Page 2 of 2 PAGES

Number SA281SW Date of Issuance: November 14, 1963 Date Amended: January 10, 2011

1. Required Placard: Each fuel quantity gage 20 Gallons Total; 18 Gallons Usable.

2. When gravity flow fuel system is installed the fuel pressure gage is to be deleted.

3. FAA Approved Airplane Flight Manual Supplement dated 11/6/1963, or later FAA approved revision, is required.

4. Enlarged oil cooler per drawing dated 7/1/1963, or later FAA approved revision, is optional.

- END -

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 · 6

MakeModelData sheet
Regal Air Inc.305A5A5
Regal Air Inc.305B3A14
Regal Air Inc.305C5A5
Regal Air Inc.305D5A5
Regal Air Inc.305E3A14
Regal Air Inc.305F5A5

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
January 10, 2011Amended, currentCertificateApproved model list
May 6, 2010Reissued, earlier issueCertificate