STC ST00925AT
FAA DRS lists ST00925AT as Current · Reissued, held by Structural Integrity Engineering, for Boeing 727-200 Series. Recorded change: Approval of increased operating weights as substantiated by the design data listed in Structural Integrity Engineering (SIE) Master Report List No. SIE-28-707, no revision, dated August 28, 1995, and modified. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
ST00925AT 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: Boeing 727-200 Series. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related other aircraft modifications STCs
Installation of a dual TAWS system in accordance with Pyka MDL 1B07-DL-001-501 Rev. D dated October 29, 2004, or later FAA approved revision. Airplane Flight Manual Supplement 1B07-FM-001 Rev. IR dated November 05, 2004, or later FAA approved revision, is required.
FAA holder: Pyka Aerospace Corp
Installation of high temperature, semi-rigid, coaxial fire/overheat detection wire harness cable assemblies.
FAA holder: Meggitt Safety Systems, Inc.
Installation of an Internal Load Attaching Means.
FAA holder: Van Horn Aviation LLC
FAA record reference
- STC number
- ST00925AT
- Product
- Aircraft · Large Multi-Engine
- Country
- United States
- Application date
- May 12, 1995
- Revision date
- March 28, 2007
- CFR references
- Part 21