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Landing gear and brakes

STC SA01598AT

FAA DRS lists SA01598AT as Current · Amended, held by Lowe Aviation Aircraft Maintenance, for Textron Aviation 150, Textron Aviation 150A, and Textron Aviation 150B, and 3 more aircraft configurations. Recorded change: Conversion from tricycle landing gear arrangement to convertional landing gear arrangement. Snapshot dated June 30, 2026.

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FAA-listed holder
Lowe Aviation Aircraft Maintenance
Aircraft configurations
6
FAA revision date
FAA status
Current · Amended

Recorded modification

What the FAA record covers

SA01598AT 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: Textron Aviation 150, Textron Aviation 150A, and Textron Aviation 150B, and 3 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Textron Aviation 1503A19Textron Aviation 150A3A19Textron Aviation 150B3A19Textron Aviation 150C3A19Textron Aviation 150D3A19Textron Aviation 150E3A19

Related landing gear and brakes STCs

SA00918SELanding gear and brakes

Precise Flight Inc. speed brake system. Manufactured in accordance with Precise Flight Engineering Drawing List 010S0000, Revision W, or later FAA approved revision. Installed in accordance with Precise Flight Engineering Drawing List 300S0000, Revision J, or later FAA approved revision. Maintained in accordance with Precise Flight Instructions for Continued Airworthiness, contained in Airplane Flight Manual Supplement Document 300SMAN0001, latest FAA approved revision. NOTE: This approval is limited to airplanes which have had speed brake provisions installed in the wing at the Lancair factory during the manufacture of the airplane.

FAA holder: Precise Flight Inc

View record

FAA record reference

STC number
SA01598AT
Product
Aircraft · Small Airplane
Country
United States
Application date
October 27, 1997
Revision date
August 19, 2016
CFR references
Part 21