STC ST02841AT
FAA DRS lists ST02841AT as Current · Issued, held by Kruse Aerospace Corporation, for Learjet 35A (C-21A). Recorded change: Installation of a lower pressure bulkhead penetration at FS 346.6 (Frame 15) and structural reinforcement in accordance with Kruse Aerospace Corporation (KAC) Drawing No. 200402, dated April 7, 2004, and DCN A1, dated April 17, 2004, or later FAA approved revision. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
ST02841AT 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 35A (C-21A). Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related aircraft structures STCs
Provisions for an H.F. coupler mounted in aft fuselage.
FAA holder: Page AvJet Corp
Assembly and installation of three place variable steel couch frame.
FAA holder: Page AvJet Corp
Installation of side facing coat closet between fuselage stations(FS) 230 and FS 280.
FAA holder: Aircraft Modular Products Inc.
FAA record reference
- STC number
- ST02841AT
- Product
- Aircraft · Large Multi-Engine
- Country
- United States
- Application date
- April 1, 2004
- Revision date
- April 19, 2004
- CFR references
- Part 21, Part 25