STC ST01468SE
FAA DRS lists ST01468SE as Current · Amended, held by Raisbeck Engineering, for Learjet 35, Learjet 35A (C-21A), and Learjet 36, and 1 more aircraft configuration. Recorded change: Installation of a drag reduction system (including outboard trailing edge extension, leading edge vortilons, and contoured flap) in accordance with Raisbeck Engineering Drawing Number 202L-5700, Revision A, dated August 29, 2004, or later FAA approved revisions. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
ST01468SE 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: Learjet 35, Learjet 35A (C-21A), and Learjet 36, and 1 more aircraft configuration. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
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