STC SA02192CH
FAA DRS lists SA02192CH as Current · Reissued, held by D'Shannon Products Ltd., for Hawker Beechcraft 36, Hawker Beechcraft A36, and Hawker Beechcraft A36TC. Recorded change: Increase of maximum gross weight from 3600/3650 lb. to 4010 lb. for normal category operation. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA02192CH 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: Hawker Beechcraft 36, Hawker Beechcraft A36, and Hawker Beechcraft A36TC. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related aircraft performance STCs
Incorporation of change in aircraft weight and balance by supplementing the current aircraft weight and balance manual with Newport Aeronautical Development Report No. NAD 2004-101, Revsion A, dated June 16, 2004, or later FAA approved revision.
FAA holder: Newport Aeronautical Development
Installation of side-facing divan certified for take-off and landing use.
FAA holder: Gulfstream Aerospace Corporation
Approval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY).
FAA holder: Structural Integrity Engineering
FAA record reference
- STC number
- SA02192CH
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- August 26, 2004
- Revision date
- June 17, 2011
- CFR references
- Part 3, Part 21