STC SA8728SW-D
FAA DRS lists SA8728SW-D as Current · Reissued, held by RAM Aircraft Limited Partnership, for Cessna Aircraft 414A. Recorded change: Increase maximum ramp weight to 7140 pounds, increase takeoff weight to 7105 pounds and the addition of optional McCauley model 3AF32C515/82NLA-4.0 or Hartzell model PHC-C3YF-2UF/FC7663D-2Q or PHC-C3YF-2UF/FC7663DB-2Q propellers.. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA8728SW-D 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: Cessna Aircraft 414A. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related aircraft performance STCs
Installation of dual IS&S Digital Air Data Computers, electronic altimeters and airspeed indicators.
FAA holder: United States Navy Naval Air Systems Command Commercial Derivative Aircraft Program
Utilization of reduced thrust takeoff procedures.
FAA holder: Honeywell International Inc
Fabrication and installation of AeroAcoustics Aircraft Systems (AASI) Aircraft Payload Extender XL gross weight increase system.
FAA holder: AeroAcoustics Aircraft Systems Inc.
FAA record reference
- STC number
- SA8728SW-D
- Product
- Aircraft · Small Multi-Engine
- Country
- United States
- Application date
- May 20, 1993
- Revision date
- September 11, 2008
- CFR references
- Part 21