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Engine and powerplant

STC SA785GL

FAA DRS lists SA785GL as Current · Reissued, held by McFarlane Aviation Inc, for Cessna Aircraft 210, Cessna Aircraft 210M, and Cessna Aircraft 210N, and 7 more aircraft configurations. Recorded change: Installation of a cooling shroud on engine driven dry air pumps. Snapshot dated June 30, 2026.

FAA-listed holder
McFarlane Aviation Inc
Aircraft configurations
10
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

SA785GL 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: Cessna Aircraft 210, Cessna Aircraft 210M, and Cessna Aircraft 210N, and 7 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Cessna Aircraft 2103A21Cessna Aircraft 210M3A21Cessna Aircraft 210N3A21Cessna Aircraft 210R3A21Cessna Aircraft P210N3A21Cessna Aircraft P210R3A21Cessna Aircraft T210L3A21Cessna Aircraft T210M3A21Cessna Aircraft T210N3A21Cessna Aircraft T210R3A21

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Related engine and powerplant STCs

SA10339SCEngine and powerplant

Installation of CenTex Inc. proprietary engine torque indicating system including engine transducer and cockpit indicator in accordance with CenTex Aerospace, Inc. drawing no 008-0000-1000, Rev. A, dated September 2, 2004, or later FAA approved revision. Type design data is contained in CenTex Aerospace, Inc. Master Drawing List 008-0000-0000, Rev. A, dated September 2, 2004 or later FAA approved version. Required instructions for continued airworthiness are contained in CenTex Aerospace, Inc. drawing no 008-0000-1000, Rev. A, dated September 2, 2004, or later FAA approved revision.

FAA holder: CenTex Aerospace Inc.

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