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Aircraft structures

STC SA02174AK-D

FAA DRS lists SA02174AK-D as Current · Issued, held by Aero Twin, Inc, for Cessna Aircraft 208 and Cessna Aircraft 208B. Recorded change: Fabrication and installation of antifog window liner kit no. ATSW8 in Model 208, or Kit No. ATSW8-B in Model 208B. Snapshot dated June 30, 2026.

FAA-listed holder
Aero Twin, Inc
Aircraft configurations
2
FAA revision date
FAA status
Current · Issued

Recorded modification

What the FAA record covers

Fabrication and installation of antifog window liner kit no. ATSW8 in Model 208, or Kit No. ATSW8-B in Model 208B.

SA02174AK-D 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 208 and Cessna Aircraft 208B. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Cessna Aircraft 208A37CECessna Aircraft 208BA37CE

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Cessna Aircraft 208 and Cessna Aircraft 208B model, serial range, and configuration?
  2. 02Which configuration, loads, materials, inspections, and damage limits apply?
  3. 03Who can legally supply the design data, kit, instructions, and ICAs?
  4. 04What parts, labor, conformity, and return-to-service work are excluded?

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Installation of a cockpit door and modification of the forward bulkhead in accordance with U. S. Technical Master Drawing List Document No. 4099-25-000, revision G, dated March 4, 2004, or later FAA approved revision. FAA Approved Airplane Flight Manual Supplement (AFMS), U.S. Technical Document No. U10-0127, dated March 8, 2004, or later FAA approved revision, is a required part of this modification. Instructions for Continued Airworthiness can be found in U. S. Technical Document No. U10-0129, release 1, dated March 4, 2004, U. S. Technical Document U10-0128, release 1, dated March 4, 2004, and U. S. Technical Document U10-0130, release 1, dated March 4, 2004.

FAA holder: U.S. Technical

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Installation of Lompoc Aero Specialties inner Plexiglass pane in swing out window frames presently employing a single window in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacture of the windows is controlled by Lompoc Aero Specialties Drawing LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.

FAA holder: G & D Aero Products Inc.

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