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Engine and powerplant

STC SA2628WE

FAA DRS lists SA2628WE as Current · Amended, held by Alpha Aviation Inc, for Univair Aircraft 415D. Recorded change: Installation of Continental O-200-A engine, McCauley 1A101/DCM 6948 propeller, electric fuel transfer pump and associated changes. Snapshot dated June 30, 2026.

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FAA-listed holder
Alpha Aviation Inc
Aircraft configurations
1
FAA revision date
FAA status
Current · Amended

Recorded modification

What the FAA record covers

SA2628WE identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.

Applicability

Aircraft named in FAA DRS

Named aircraft: Univair Aircraft 415D. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Univair Aircraft 415DA-787

Related engine and powerplant STCs

SA01801ATEngine and powerplant

For the Cessna 172 airplane models incorporating Lycoming O-320 engines: Modification of the standard exhaust system as documented in Laminar Flow Systems Installation Instructions Document, "Laminar Flow System Extractor Exhaust System" Revision A, dated, November 20, 1998 and Technical Drawing List, Book No. PFS-B-800, dated, November 16, 1998 or per Power Flow Systems, Inc. Installation Instructions Document PFS-0058-00, Rev. A, dated October 5, 2001 and Master Drawing List, Report No. PFS-0032-00, Rev. IR, dated August 10, 2000, or later FAA approved revisions. For the Cessna 172 airplane models incorporating Lycoming O-320 ,O-360 0r IO-360 engines: Modify the standard exhaust system as document in Power Flow Systems, Inc. Installation Instructions Document PFS-13250-00, Rev B, dated, December 9, 2002 and Master Drawing list PFS-13240-00, Rev, IR, dated October 3, 2002.

FAA holder: Power Flow Systems Inc

View record

FAA record reference

STC number
SA2628WE
Product
Aircraft · Single-Engine
Country
United States
Application date
May 1, 1972
Revision date
January 16, 2020
CFR references
Part 21