STC SA02407AK

FAA DRS lists SA02407AK as Current · Issued, held by Kenneth MacDonald, for Piper Aircraft PA-18-105 (Special), Piper Aircraft PA-18-125 (Army L-21A), and Piper Aircraft PA-18-135, and 15 more aircraft configurations. Recorded change: Installation of lowered baggage floor. Snapshot dated June 30, 2026.

FAA-listed holder

Kenneth MacDonald

Aircraft configurations

FAA revision date

March 13, 2013

FAA status

Current · Issued

Recorded modification

What the FAA record covers

SA02407AK 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: Piper Aircraft PA-18-105 (Special), Piper Aircraft PA-18-125 (Army L-21A), and Piper Aircraft PA-18-135, and 15 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Buyer checks

Confirm before sourcing

SA900CEAircraft structuresRevised Jan 26, 2012

Replace round wingtips with constant-chord, square tips and wing splates per Flanagan Aircraft Drawing List No. 1 dated February 1, 1975, or later Federal Aviation Administration approved revision.

FAA holder: Cub Crafters Inc

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SA00009SEAircraft structuresRevised Dec 23, 2011

Fiberglass wing tips and wing tip landing lights.

FAA holder: Aircraft Lighting & Components

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ST03042NYAircraft structuresRevised Dec 21, 2011

Installation of Fuselage Side Fairings.

FAA holder: Northrop Grumman Systems Corporation

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SR09257RCAircraft structuresRevised Dec 8, 2011

Fabrication, modification, and installation of a new vertical fin spar in accordance with Global Helicopter Technology, Inc., Drawing number VTF-030-800, Revision D, dated March 26, 2001, or later FAA approved revision.

FAA holder: Global Spar LLC

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What the FAA record covers

Aircraft named in FAA DRS

Confirm before sourcing

Related aircraft structures STCs

Replace round wingtips with constant-chord, square tips and wing splates per Flanagan Aircraft Drawing List No. 1 dated February 1, 1975, or later Federal Aviation Administration approved revision.

Fiberglass wing tips and wing tip landing lights.

Installation of Fuselage Side Fairings.

Fabrication, modification, and installation of a new vertical fin spar in accordance with Global Helicopter Technology, Inc., Drawing number VTF-030-800, Revision D, dated March 26, 2001, or later FAA approved revision.