STC ST00795AT
FAA DRS lists ST00795AT as Current · Reissued, held by Structural Integrity Engineering, for Boeing 727-200 Series. Recorded change: Approval of maximum zero fuel weight increase (155,000 lbs.) and maximum landing weight increase(164,000 lbs.). Data pertaining to this modification are considered inadequate for duplication in other aircraft.This approval is limited to the installation in the Boeing 727-200, (Serial Number 20938 only). Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
ST00795AT 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 fuel systems STCs
Installation of 18 gallon nylon auxiliary fuel tanks on airplanes equipped with standard range 64 gallon capacity bladder tank or 62 gallon fiberglass fuel tanks. (A185F thru S/N 18503683 and later airplanes originally equipped w/bladder fuel tanks).
FAA holder: Hartwig Aircraft Fuel Cell Repair
FAA record reference
- STC number
- ST00795AT
- Product
- Aircraft · Large Multi-Engine
- Country
- United States
- Application date
- May 10, 1995
- Revision date
- January 20, 2005
- CFR references
- Part 21