What it approves
Fabrication of engine mount and fiberglass cowling
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.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate 14 CFR 21.120) FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 3 Number: SA302NW This certificate issued to:
Fabrication of engine mount and fiberglass cowling in accordance with Descriptive Data List No.
DDL-SA302NW, Revision C, dated July 16, 2007, or later FAA approved revision, and installation of a Lycoming Model 0-360 180-hp engine and a Hartzell Model HC-C2YK-1BF/7666A propeller, or a McCauley Model 1A-200-DFA-82 propeller with that engine mount and that fiberglass cowling in accordance with Burl’s Aircraft Rebuild, LLC, Installation and Drawing Instructions, No. RW1000-1, Revision C, dated June 6, 2007, or later FAA approved revision.
Compatibility of this design change with previously approved modifications must be determined by the installer.
Burl’s Aircraft, LLC P.O. Box 671487 Chugiak, AK 99567-1487 Original Product Type Certificate Number: A-802 Make: AeroSedan, LLC Model: 15AC and S15AC Date of application: January 30, 1976 Date of issuance: June 21, 1976 Date reissued: See Continuation Sheet Page 3 of 3 Date amended: November 22, 1976; December 15, 1976 December 05, 1980; August 04, 2000;
November 09, 2001; July 30, 2007 By direction of the Administrator Signature:
August A. Asay Title: Manager, Anchorage ACO Branch Part 3 of the Civil Air Regulations.
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 3
Number: SA302NW
Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA302NW
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 3
(Continuation Sheet) Number: SA302NW
Date of application: January 30, 1976 Date of issuance: June 21, 1976 to Richard Welsh, Jr.
Date reissued: April 27, 1978, to Monahan Aircraft, Inc.
November 23, 1988, to Mr. Herman Cantrell April 28, 1992, to Mr. William Brad Mitchell August 04, 2000, to Mr. Burl A. Rogers March 22, 2022 to Burl’s Aircraft, LLC Date amended: November 22, 1976; December 15, 1976;
December 05, 1980; August 04, 2000;
November 09, 2001; July 30, 2007
Limitations and Conditions: (Continued):
Landplanes incorporating this design change must be equipped with one of the following wheel and brake installations:
Supplemental Type Certificate Number and Holder Cleveland Wheels and Brakes Kit Number Brake Type Wheel Size Tire Sizes Eligible SA1113NW Burl’s Aircraft Rebuild 199-04600 Single Piston 6.00 – 6 Type III 6.00 – 6 SA1114NW Burl’s Aircraft Rebuild 199-06200 Dual Piston 6.00 – 6 Type III 8.00 – 6 8.50 – 6
This approval is valid for only the engine models, propeller models and engine/propeller combinations specified in Burl’s aircraft Rebuild, LLC, Installation Drawings and Instructions No. RW1000-1, Revision C, dated June 06, 2007, or later FAA approved revision.
FAA approved Airplane Flight Manual Supplement amended April 20, 1979, or later FAA approved revision, is a required part of this installation.
14 CFR Part 43 is adequate to insure continued airworthiness of this modification.
-END-
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