# STC SA803SO - Type: Supplemental type certificate - Status: Current, Amended - Holder: Swift Museum Foundation Inc - Description: Installation of a Lycoming O-360-A1A engine, equipped with either a McCauley Model 2D34C53-A/74E-0 propeller or a Hartzell Model HC-C2YK-1BF/F7666A-2 propeller - Status date: September 5, 2018 - Data sheets: A-766 - Certificate PDF: https://openairdocs.org/files/sha256/28/bd/28bd41d99db92fd6036308ddc45609e81c869f5c4c73ec3f266cb4ec715c4731 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F4EAAB2AAF3D89F68625830800488B23.0001 - Page: https://openairdocs.org/stc/SA803SO ## ADs that name it None. ## Approved models (1) - Swift Museum Foundation Inc. GC-1B (TCDS A-766) ## 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. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to th e design data nor to alter an aircraft, aircraft engine, or propeller. FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA803SO This certificate issued to: Swift Museum Foundation, Inc. 223 County Road 552 Athens, Tennessee 37303 Certifies, that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of Part * of the Civil Air Regulations *CAR 4a, alteration in accordance with CAR3 as amended to May 15, 1956, and amendments 3-1 through 3-8 thereto Original Product – Type Certificate Number: A-766 Make: Globe Model: GC-1B Description of Type Design Change: Installation of a Lycoming O-360-A1A engine, equipped with either a McCauley Model 2D34C53-A/74E-0 propeller, installed in accordance with Aeronautical Engineering, Inc. Drawing List Report Number R -274, dated August 12, 1974, or a Hartzell Model HC -C2YK- 1BF/F7666A-2 propeller, installed in accordance with Aeronautical Eng ineering, Inc. Report Number FA 1009 H, dated January 3, 1983. Limitations and Conditions: Aircraft operation is limited to 125 horsepower maximum, maximum propeller governor setting 2500 RPM. Wing tip tanks, if installed, are not eligible for use. This approval should not be extended to other aircraft of the same model on which other approved modifications have been made unless it has first been determined that the interrelationships between these various modifications will have no adverse effect on the airworthiness of the aircraft. 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. See Continuation Sheet 3. Date of Application: October 25, 1967 Date Reissued: December 20, 1999 Date of Issuance: August 30, 1974 Date Amended: September 5, 2018 By Direction of the Administrator Signature Title: Christina M. Underwood Manager, Atlanta ACO Branch FAA Form 8110-2 (5/14) Page 2 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA803SO To (Name and address of transferee) From (Name and address of grantor) FAA Form 8110-2 (5/14) Page 3 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA787WE Hartzell hub models HC-C2YK-1BF and HC-C2YR-1BF can be used interchangeably with Hartzell blade model F7666A-2 per TC P-920 and the Hartzell Standard Practices Manual 202A Volume 3 Section 12 Subsection A (Rev 35, dated July 2015). --------------------------------------------------------------------------------END-------------------------------------------------------------------------- ## Every issue (1) - September 5, 2018: Amended, Current. [certificate](https://openairdocs.org/files/sha256/28/bd/28bd41d99db92fd6036308ddc45609e81c869f5c4c73ec3f266cb4ec715c4731) --- 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.